KR910007246A - Dynamic generation and buoyancy, thrust, power generation, power generation, and buoyancy devices using fluids and electric motors - Google Patents

Abstract

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Description

Power generation and buoyancy, thrust, power generation using fluid and power generation, power generation and buoyancy device using cooling and electric motor

As this is a public information case, the full text was not included.

1 is a side cross-sectional view of a structure in which the blade length of the centrifugal compressor (compressor) is gradually lengthened toward the rear end portion (3 fluid outlets),

FIG. 2 is a schematic top view of FIG. 1 of FIG.

3 is a 2 (wing) cross section and a structure diagram of the soil of FIG.

4 is a side cross-sectional view of a structure without a wing side plate (7 cover) and the casing 10 serves as a cover,

5 is a partial perspective view of FIG.

6 is an explanatory diagram of a method of calculating the blade length expansion ratio.

Claims (1)

(See FIGS. 1-18.) The lengths 18 and 19 of the rotor blades 1 of the rotor and the compressor having the lid 7 of the rotor blades 1 are gradually lengthened toward the outlet 4, and between the blades 15 16) The distance is gradually increased and the flow path area in the memory (1) is gradually enlarged. 18. The flow path cross-sectional area of the part 18) is at least about 1. Centrifugal type of structure expanded at the ratio becoming more than 5 times,  Ceremonial,  Eating,  Side Flow,  Compressors and flowers such as screw type,  (See also FIGS. 19-35) A flow path tube 7 in which the flow path cross section is gradually enlarged at a constant rate to the discharge port 3 of the blower and the compressor 2, 9), but the distance between the flow path cross section where the flow path cross section is enlarged about 4 times in the blade end portion 14 is calculated as the circular cross section (24 in Fig. 6) having the same area. Centrifugal type having a structure enlarged at a rate that is at least about twice as long as the diameter 11,  Ceremonial,  Eating,  Axial Flow,  Screw Type,  Reciprocating,  Eccentric Blade Type,  Swash Plate,  Rotary blowers and compressors,  (See also paragraphs 36-43) Blowers, pumps and compressors (1, 2, a flow path tube 8 which gradually reduces or expands at a constant ratio to the inlet 5 and the outlet 10 of the inlet 5; 10), but the distance between the end face of the inlet port (18) and the inlet port (7) of the inlet port (7) and the inlet port (10) of the outlet port side pipe tube (10) is enlarged by about four times. 4) The flow path cross-sectional area of 4) is enlarged at a rate that is at least about twice as large as the length of the diameter calculated as the circular section of the same area (centrifugal equation,  Ceremonial,  Axial Flow,  Screw Type,  Liquid jet nozzle 18 is mounted in a narrow flow path of a pump and (see FIG. 44) a suction port (7).  Devices capable of injecting or spraying mixed liquids or using mixed fluids (see also 45-55) and the inner blades (3, 3) for the inlet and outlet of the axial turbine (2); 4) and a flow path tube 7 in which a flow path section gradually expands to the discharge port 5 of the exit guide blade 4;  8) and connecting the flow path of the flow pipe outlet 6 and the compressor 10 to the suction inlet, and installing the guide blade 11 at the compressor outlet, and installing the cross-sectional enlarged flow path pipe 32 at the guide blade outlet 12, (17) A ring-type reduction suction device 14 having a streamlined cross section which connects the suction port 16 to reduce the flow path cross section and separates the flow path into the flow path reduction part 13 to smoothly reduce the cross section. The heat exchanger outlet 24 and the turbine inlet shaft 26 are connected to each other, and the flow path section of the connection portion is reduced, and the reduction section suction device 25 is mounted on the reduction portion, and the motor 15 is connected to the rotary shaft 33 of the compressor 10. ) And the generator (1) on the turbine (2) axis of rotation to mount the device in the inlet (23) and the outlet and the flower (20) in the box (22) to allow fluid to flow inside. When an external current is supplied to the electric motor 15, it is caused by the rotation of the compressor 10. The sieve is sucked in and the fluid intake of the turbine inlet 26 is rotated so that the turbine rotor blade 2 is rotated, and the turbine guide vane 4 causes the flow direction of the fluid at the outlet of the turbine 2 to go straight in the axial direction. Sectional enlargement (7,  8) the flow rate is reduced and sucked into the compressor (10) and the fluid at the compressor outlet to direct flow (11) is a direct flow, the cross-sectional path is reduced and sucked into the heat exchanger (16) through the suction device (14) for suction When a part of the output current of the generator 15 is supplied to the electric motor 1 by a circulation device that absorbs external heat from the heat exchanger 17 and re-absorbs it to the turbine inlet side 26, the compressor is operated by the self-generated current. It uses spontaneous operation even when the external current is cut off, and uses a part of the generated electric current. Since the cooled fluid absorbs the heat of the external fluid in the heat exchanger 17, the external circulating fluid can be cooled and used. The automatic power generation and cooling generating device that can be powered by installing a power transmission device such as a pulley on the rotating shaft (see also 56-61), and the centrifugal compressor (19) having a large rotating radius instead of the side flow turbine and the axial compressor. Flow path pipe 45 whose flow path cross-sectional area is gradually reduced in the centripetal direction on the inlet 6 side,  46) and centrifugal turbine guide vanes (4), rotary vanes (2) and guide vanes (3) by connecting with the inlet pipe (5), and the generator (1) on the turbine (2) rotary shaft and the compressor (10). The motor 15 is mounted on the rotating shaft, and the guide blade 1 is mounted on the compressor outlet side, and is connected to the guide blade 11 to mount a diffuser 47 having a cylindrical structure in which the flow path area is gradually enlarged. The diffuser 47 and the heat exchanger The flow path section of the connecting portion 13 of (17) is reduced, and the circulator that connects the heat exchanger (17) outlet (24) with the turbine inlet (26) is mounted on the reduction section, and the inlet ( 23) the compressor 10 is rotated when the electric motor 15 is operated by an external current by the structure in which the flower 20 is installed in the box 22 to allow fluid to pass through. Suction into turbine 2, rotate turbine 2, direct current by guide vane 4, suck into compressor blade 10, And automatically power and cooling apparatus for ripening by changing the swirl flow (11) sucked into the diffuser 47, and circulated to the heat exchanger 17 via the cross-sectional reduction 14,  (See also 62-63) Compressor (10) The structure in which the device is placed in a cylinder with a thin metal plate or metal thread so that the heat conduction is good inside and outside of a metal cylinder with high thermal conductivity without connecting the outlet shaft to a heat exchanger with a long thin tube. Compressor 10 outlet side flow path cross-sectional enlarged portion 49 is thickened to be smooth curvature, the inner surface 55 of the metal cylinder 53 and the outer surface of the device is a flow path (51,  52 so that the flow path cross-sectional area is gradually enlarged in the turbine (2) inlet direction (52), and the cross-sectional area of the flow path is reduced on the turbine inlet (26) side;  Exit (21,  23) Automatic power generation and cooling arrangements in which the device is placed in a box 22 through which fluid flows (see also 64-65) and the side turbo turbine blades 2 and the guide blades 3, 4) the radius of rotation is increased and the channel expansion pipe (7, 8) By connecting the axial compressor blade 10 as a whole and the motor and generator 56 mounted on the common rotary shaft 59, the motor 56 is initially rotated with an external current and the external speed is reached. Chinese character as a circulation device by stopping the supply of current and connecting the heat exchanger to the channel expansion end 13 and the turbine inlet side 26 at the outlet side of the compressor 10 at the outlet side of the compressor 10, and putting it in a box through which the fluid passes. Dynamic power generation and cooling systems (see Figure 66), side turbine turbines (2) and guide vanes (3,  4) and the radius is larger and the channel enlargement pipe (7,  8) and turbine guide vanes (3,  4) and the compressor guide blades 11 are connected and fixed, and the rotary shaft 59 of the turbine rotor blade 2 and the rotary shaft 60 of the compressor blade 10 are integrally connected to each other, and the generator / motor 56 is connected to the common shaft. An automatic power generation and cooling system which connects the mounted structure, the end of the compressor shaft flow path expansion tube, and the turbine guide vane inlet port 26 with a heat exchanger, and puts the device in a box through which the fluid passes (see FIG. 67). A flow path tube 7 whose cross section is gradually reduced in the centripetal direction of the centrifugal compressor 10 having a large turning radius and the guide vane 11 at the discharge port,  8) and guide day (3, to inlet and outlet)  (2) Turbine rotor blades (4) are connected to each other and the generator and motor 56 are mounted on the pain rotating shaft 59 to rotate the generator and the motor 56 with an external current at first. The automatic power generation and cooling system connected to the circulation device by stopping the supply of electricity and using the generated electric current, connecting the heat exchanger to the end of the flow path expansion part 61 of the compressor outlet and the turbine inlet, and putting it in a box through which the fluid passes. 68.) Cross-sectional enlarged flow path tube (7) between the outlet side guide blade (4) of the axial flow turbine (2) with the inlet side guide blade (3) and the axial compressor blade (10) with the guide blade (11) at the outlet port.  8) bent to a curvature to connect the turbine rotary shaft 59 and the compressor rotary shaft 60 so that the generator and motor 56 are mounted on the common rotary shaft, and the compressor outlet side diffuser end 13 and the turbine guide vane inlet 26. Is connected to a heat exchanger and the device is placed in a box through which fluid flows, and the automatic power generation and cooling system (see also 69-70) and the guide vane (3,  4) a cross-sectional enlarged flow path tube 7 for connecting the compressor inlet 6 and the turbine outlet 5 by integrally connecting the centrifugal turbine 2 with the centrifugal compressor 10 with  8,  65,  66 to form a compressor blade 10 suction inlet flow path toward the turbine blades 2 to prevent uneven pressure distribution at the cross section of the compressor inlet 6 due to the centrifugal force caused by curvature induction. (2) the common axis of rotation (59,  60) the generator and the electric motor 56 is mounted, the guide vane 11 and the flow path cross-section tube or diffuser 68 at the compressor 10 outlet and the compressor outlet side flow-tube expansion tube end or diffuser 68 end And turbine intake shaft 26 connected to a heat exchanger, and the apparatus is placed in a box through which fluid flows, and the automatic power generation and cooling system (see also 71-73) and the outlet of the axial compressor blade 10 A flow path with a spherical curvature connecting the turbine outlet (5) and the compressor inlet (6) by mounting the axial turbine gear (2) with guide vanes (4) and the generator and motor (56) on the common rotary shaft (59). Sectional enlarged tube (7,  8) guide vanes (11,  3) and the automatic power generation and cooling system connected to the compressor outlet diffuser 68 and the turbine inlet diffuser 67 by a heat exchanger, and the apparatus is put in a box through which the fluid is passed and the circulation device is installed. (See also 74-75)) A flow path cross-section pipe (7), which is equipped with a diffuser (27) at the outlet of the axial turbine (2) with a guide vane (3) at the inlet, and connects the diffuser outlet (5) and the inlet of the axial compressor (10). ,  8) and the flow path expansion pipe outlet (6) and the axial compressor (10) suction inlet, and the guide vane 11 and the flow path section expansion pipe (32) attached to the compressor outlet and the flow path section reduction suction device (14) To the heat exchanger and to the heat exchanger and to the automatic induction and cooling system (see also 76-78) of the circulator connected to the turbine inlet (26) and the inlet (3). To the outlet side guide vane (4) outlet port (5) and the axial compressor (10) inlet port (6).  8) and a structure in which the guide vane 11 and the flow path cross-sectional expansion pipe 32 are connected to the outlet of the compressor 10, and the flow path expansion pipe 32 end 61 and the turbine 2 suction port side of the compressor 10 side. Automatic power generation and cooling system of a structure in which a circulation device connecting the guide vane 3 to a heat exchanger in a box through which fluid passes (see FIG. 79), and various known compressors (eccentric blade type,  Screw Type,  Eating,  Reciprocating,  Swash Plate,  To the inlet 6 of a rotary type, etc.)  8) and the turbine (meat type,  Centrifugal,  Ceremonial,  Convection type, etc.) A structure in which a flow path cross-sectional expansion pipe 32 is connected to the outlet 74 of the compressor 10 and a flow path expansion pipe end 61 of the compressor 10 side and a turbine-side diffuser are connected. 27) Automatic generation and cooling of the structure in which the circulator connecting the suction port 26 to the heat exchanger in a box through which the fluid passes (see FIG. 80-82) and a flow path expansion pipe at the center of the centrifugal compressor 10 7,  8) and a centrifugal turbine (2) equipped with a turbine guide vane (4) so as to have no guide vane at the inlet side of the centrifugal turbine (2) and a guide vane at the compressor outlet (74). The direction of the direction of rotation and the straight line connecting the north end and the end of the compressor blades are close, and the compressor outlet port 74 gradually reduces (76) the flow path section and then expands (77) the turbine rotor blades (2). An automatic power generation and cooling device having a structure in which a circulating device connecting the structure and the compressor shaft passage expansion end 61 and the turbine inlet 26 to a heat exchanger is placed in a box through which the fluid passes;  (See Figs. 83-85) A diffuser 27 is attached to the inlet port of the axial turbine blade 2 and a guide blade 4 is attached to the outlet port so as to be connected to the flow path inlet tube 5 and the flow channel outlet tube 6 And the axial compressor blade 10 are connected to the compressor blade outlet 74 so that there is no guide blade, and the compressor outlet 74 gradually reduces (76) the flow path of the compressor outlet (74) and gradually expands (77) the rotation of the compressor blade (10). The direction and the angle formed by the straight line connecting the compressor blade rear end and the end are small so that the direction of the fluid in the compressor blade 10 is closer to the straight stream, and the end of the compressor shaft flow path expansion tube end 61 and the turbine 2 suction port. Automatic generation and cooling of the structure in which the circulator connected to the diffuser 27 is placed in a box through which the fluid passes (see FIG. 86), and guide vanes (3,  4) Axial flow turbine (2) equipped with a rotary shaft (59,  60 to slave gear (78,  79) and the generator and motor 56 are mounted on the compressor shaft 60 and the heat exchanger is connected to the turbine inlet side 26 and the compressor outlet side 13 and put in a box through which the fluid passes. Automatic power generation and cooling systems (see Figure 87) and guide vanes at the inlet and outlet (3,  4) Centrifugal turbine () equipped with and flow path pipe (7,  8) and the rotary shaft 59 and the compressor rotary shaft 60 of the apparatus of the apparatus consisting of a centrifugal compressor 10 equipped with a guide vane 11 at the outlet of the slave gear 78,  79) is equipped with a motor and generator 56 to the rotary shaft 60 of the compressor 10, and the cross section enlarged flow path tube 32 is installed at the outlet of the guide blade 11 of the compressor 10 and the inlet and outlet (26,  13) Axial turbine (2) rotary shaft with a heat exchanger connected to it, automatic power generation and cooling system (see Fig. 88) and a diffuser (27) at the inlet and a guide vane (4) at the outlet. (59) and the enlarged cross-section flow path is a curvature of the rotating shaft 60 of the axial compressor (10) equipped with a guide blade (11) in the wheel structure and the discharge port in curvature (78,  79) and the generator to the compressor shaft 60,  A structure in which an electric motor 56 is mounted and a flow path enlarged pipe () is connected to the outlet of the compressor guide vane (11), and the flow path enlarged pipe (32) and a heat exchanger are connected to the compressor side. In the turbine (2) inlet-side diffuser (27) and the automatic power generation and cooling system (see Fig. 89) of the structure in which the device is placed in a box through which the fluid passes (see Fig. 89).  8) flow path cross-section tube 7 of the centrifugal compressor 10 equipped with the guide vane 11,  8) and guide vanes on inlet and outlet (3,  4) The cylindrical outer surface 54 of the metal having good thermal conductivity in a structure in which a centrifugal turbine (2) equipped with a double row top and bottom blades and a generator and an electric motor (56) are mounted on a common rotating shaft (59). And the inner surface of the cylinder is attached to the metal plate or metal thin yarn with good thermal conductivity, but the flow path formed between the cylindrical inner surface 55 and the device outer surface 82 is gradually enlarged in cross section toward the turbine inlet 26 compressor 10 The wall surface of the outlet side end-side enlargement tube end 49 is thickened to have a smooth curvature, to form a smooth flow path with the cylindrical surface 55, and the end face reduction suction device 25 is mounted on the turbine inlet 26. Automatic power generation and cooling apparatus having a structure in which the apparatus for reducing and suctioning the turbine guide vane 3 is placed in the box 22 having the inlet port 23 and the inlet port 20 is mounted (90 degrees) Guide vanes on the inlet and outlet (3,  4) Turbine rotary shaft (59) and compressor rotary shaft (60) of the device connected to the axial flow turbine (2) equipped with an axial flow compressor (10) equipped with a guide blade (11) in the structure and the exhaust port is curved in curvature A thick curvature tube with a thin metal plate or metal thread attached to the inner surface 55 and the outer surface 54 of the metal cylindrical tube having high thermal conductivity so as to have a good conductivity. (53), but the flow path between the inner surface of the cylindrical tube and the outer surface (82) of the device is configured so that the flow path cross-sectional area from the compressor side guide blade (11) outlet (12) to the vicinity of the turbine inlet port (52) gradually expands. (26) to reduce the suction, but the flow path wall surface is uniformly smooth, and the cylinder 53, the inner surface 55 has a low friction with the fluid attached to the fine yarn or not attached to the inner surface only attached to the outer surface, smooth flow path Let the outlet structure 21, the automatic power generation and cooling system equipped with a flower 20 and mounted in a box 22 having an inlet 23 (see also 91-95) and an entrance 6,  The cylindrical wall surface 13 opposite the inlet 6 of the cylinder through which the hole 14 is drilled has a radius of curvature larger than that of the cylindrical wall 10 between the inlet 6 and the outlet 14 by the inlet flow path width 6, but the outlet ( 14, the inner wall surface of the outlet port 14 and the inner wall surface 19 of the outlet port 14, The line member cylinder 7 having a structure in which the portion 20 where the cylindrical wall surface 10 meets is sharpened so that the outlet passage width 16 is narrower than the inlet passage width 15.  8,  9) by connecting several short circuits, the compressor 2 is mounted on the inlet 6 side, and the turbine 23 connected to the same rotation shaft 29 as the compressor 2 on the outlet 21 side, and the turbine outlet 25 ) And the compressor inlet (5) to the heat exchanger (26), but gradually expanding the heat exchanger (26) internal flow path from the turbine outlet (25) toward the compressor inlet (5), the first common rotation axis by the structure of smooth curvature When the external current is supplied to the generator and the motor (1) mounted on (29), vortex occurs in the fluid flowing into the cylinder (7) by the rotation of the compressor (2), and the flow velocity is increased in the cylinder speed. Cylinder of (7,  8,  9) as the flow rate increases, it flows into the turbine 23 through the diffuser 22 of the turbine inlet 21, rotates, enters the heat exchanger 26, and enters the compressor 2 through the heat exchanger outlet 28. Automatic power generation and cooling system (refer to Figure 96) that uses regenerated circulation and uses current generated by self-operation even if the external current is cut off, and puts the device into a box through which fluid flows to obtain cooling fluid. Guide vanes (37, 38. The centrifugal compressor (2) equipped with a centrifugal turbine (23) equipped with a guide vane (3) is integrally connected to the outlet port, and the flow path cross-sectional expansion pipe (44) is connected between the compressor inlet port (40) and the turbine outlet port (39). To the turbine inlet-side diffuser (41) having a structure in which a generator and an electric motor (1) are mounted on a common rotating shaft (29).  8,  Automatic power generation and cooling device that connects the outlet 21 of 9) and connects the heat exchanger 26 to the diffuser 4 of the compressor 2 outlet in a box through which the fluid passes. And automatic power generation and cooling system (see also 100-101) with a structure in which holes are made in the upper and lower portions of the cylindrical core 42 of the cylinder so that external fluid can be sucked during operation. The secondary wire (1) of (13) is wound separately from the primary winding (2), and the iron core (3), which can be moved in between, can be mounted in close contact with the core of the electromagnet 15 Mounting the moving core (6) of the same structure between the connection to the moving core (3) and the common shaft 17, but fixed with a bearing or bushing (16) to move smoothly and the spring (4,  5) and a part of the secondary winding (1) is connected to the inductance coil (9), but the output side 18 is connected in series with the light bulb (10) so that the current flows weakly at the rated voltage and the electromagnet winding (7) When the voltage on the output side 18 changes, the current flowing through the inductance condition 9 changes and the current flowing through the light bulb 10 changes in series with the photoelectric tube 12 or the photo transistor in series. When the magnetic force of the electromagnet 15 is changed by the change of the current flowing through the electromagnet winding 7 by the change of the current of the phototube 12 or the photo transistor, the moving core 6 is changed. When the pulling force is changed and the moving core 6 is moved, the contact surface of the iron core is changed so that the voltage of the secondary winding 1 is changed, and the voltage automatic regulator (see also 102-103) and the structure without the moving core Separate the secondary winding 24 side of the transformer 21 Connect (parallel) and connect the inductance wire 26 and the bulb 27 in series, and a little current flows at the rated voltage, and connect the Hall element 31 in series with the secondary winding 24, 31) stimulation of the electromagnet 33 (35,  36, a photoelectric tube in which the resistance of the Hall element 31 changes according to the strength of the electromagnet 33 so that the current amount of the secondary winding 24 changes, and the electromagnet winding 30 is mounted on the light bulb 27. (28) or a voltage automatic regulator having a structure connected to a battery 29 in series with a photo transistor (see also 104-124) and a thick conductor (1, 2) Connect the AC power source 35, mount the diode 4, and gradually reduce the cross-sectional area of the plus (5) side conductor to make the end (8) sharper, make the cross section of the minus (3) side thicker, The plate-shaped conductor 7 is fixed and assembled with the plus (5) side, and the pointed end portion (8) on the plus (5) side is brought closer to the center portion 33 of the disc-shaped conductor 7 so as to be a counter electrode. And the disk-shaped conductor (7) and the pointed end (8) part using a part of the secondary winding (10) of the transformer (34), which is connected to the transformer (34) by a bus bar, and lowered the voltage, and a part of the generator (17). Is connected to the electric motor (15) equipped with the generator 17 output as the power supply 35 of the power transmission device, the rollers shaft (5) and the negative shaft (3) and the disk-shaped conductor (7) with an electrical insulator, The generator 17 rotates by operating the vibrator 15 with the external power source 14 first by increasing the voltage of the power source 35 side or increasing the frequency. When raw power (1,  2) Since it becomes the side current, a large current is supplied to the motor 15 by the boosted current from the power supply device, operates by its own current, and continues to use part of the generated current even when the external current 14 is stopped. The automatic power generator (see also Figure 113) and the positive side lead 38 of the DC power supply 29 are gradually reduced in cross section so that the end is pointed (8) and the negative side lead 31 is gradually thickened. The disk-shaped conductor (7) is attached to the portion, and the positive () side pointed portion (8) is charged close to the center portion (33) of the disk-shaped conductor (7), and the disk-shaped conductor (7) and the pointed end The part 8 is connected to the electric motor 15 by a conductor, the part is connected to the current-using device 12 in parallel, and the direct current generator 39 is mounted on the motor shaft 16 to output the output 27,  28, the power supply side lead 31 connected to the storage battery 29  38) and a multi-pole alternator (17) mounted on the rotary shaft (16) of the high speed motor (15) and the automatic power generator (see FIG. 114) for winding and using a separate winding. With the side as the power source, the conductor cross-section becomes thinner and the sharp end (42,  43) with each other and pointed ends (42,  43, the lead wire 23 is connected to the primary winding 9 of the transformer 34, using part 11 of the secondary winding 10 (12) and using part 13 as the motor 15 power source. The generator 17 is mounted on the automatic power generating device having the structure of FIG. 1 and the rotating shaft 16 of the motor 15, and the generator output 1,  2) A diode (4) is mounted on the positive lead (5) of the boosting device using the power supply, and the insulating wire containing the coolant (4) is separated from the lead (7) side of the large power supply conductor (7) which gradually reduces the flow path area. The secondary winding (8) mounted in the cylinder (46) and connected to the primary winding (9) of the transformer (34) by connecting the positive counter electrode (8) and the negative side power supply plate (7) to the transformer (34) with a conductive wire. 10) a magnetoelectric multi-pole generator (73) and an automatic power generation device (see also 125-127) which uses part 11 in connection with the current-operating device 12 and inputs part 13 to the motor 15. Electric winding (57,  61) Wind the number of turns (Tarn number) less (1-2 times) and gradually thicken to make one pole 60 thicker, one pole 58 thinner, and a diode 59 mounted on one conductor The positive and the thick winding is negative, and the electric motor 63 is mounted on the rotation shaft 65 of the generator 73, and the power winding connects a part 72 to the motor 63 and uses a part 70 as a current. With the structure connected to the device 71, the motor 63 is initially operated by the external power source 67, and the motor 63 is generated by the self-generated current using a part 70 of the generator 73 output current 68. Inserts an electrical insulator or dielectric 93 between the automatic power generator in operation and the thin conductor 77-84 whose cross-sectional area is gradually reduced (see also 128-130) or forms an oxide film on the conductor surface to insulate and By stacking them in layers, the conductors (77-84) are connected in parallel with each other to form side plates. An automatic power generator using a portion of the boosted current by connecting the current using device 89 to one end 88 and rotating the electric motor mounted with the generator to use the generated current toward the power source 74;  (See also 131-132) A circular conductor 95 having a gradual cross-sectional area is inserted into a central portion of a cylindrical conductor 94 whose diameter and thickness gradually decrease, and an insulator or dielectric 96 is inserted therebetween, and a thick portion ( 94,  95) to the AC power source (74), the pointed end (97) to connect the current-using device (89) and input the part (90) to the electric motor equipped with a generator to use the generated current as the power source (74) With automatic power generator,  (133-134 degrees) A cylindrical cone cylinder made of an insulator (105,  Ionic liquid (107,  108) Insert the conductor disc 102 for the wide cross section and connect the high frequency or high voltage power supply 100 and the pointed ends 111,  112 is connected to the electric wire to use a part of the current connected to the current using device 115, and part 113 is an automatic power generation device to re-enter the generated current to the power supply 100 by operating the motor equipped with a generator And (see also 135-138), a high-frequency or high-voltage power supply 121 is installed by mounting an iron core 116 wound with a winding 117 at the center of a cylindrical tube 127 made of an electromagnetic insulator bent at a point C at both ends. Fill the ionic liquid 118 in the cylindrical tube and connect the AC power 121 to the winding 117 wound on the iron core 116 to generate an induction current in the ionic liquid 118.  123 is connected to the electric wire 124 to connect a part to the current using device 126 to use the current, and part 125 is an automatic power generation using the generated current as a power source 121 by operating an electric motor equipped with a generator Mount the reduction gear (7) on the device and the rotation side (4) of the motor (1) (see also 139-165) and the reduction gear side (6) and the reduction motor body (1,  7) The generator 8 and the high speed electric motor 22 are mounted on the rotary shaft 24 mounted on the rotary shaft 24.  7) The input current 21 of the internal vibrator 1 and the high speed motor 22 side so that the body and the reduction shaft 6 rotate together and the voltage of the output current 10 of the generator 8 is kept constant. Automatic voltage regulator 12 for controlling the voltage of  14,  19,  20) When the external current is first supplied to the motor input shaft 21, the reduction motor 1 and the high speed motor 22 rotate, and the rotor of the generator 8 mounted on the reduction rotation shaft 6 rotates to generate electric current. Part of two electric motors (1,  22) When supplied to the input lead 21, even if the external power supply is stopped by spontaneous operation, it continues to operate and may be used by using a part of the generator output 10 or by a pulley 9 mounted on the rotation shaft 6. Automatic power generation and power generator that can obtain power and automatically regulate the voltage;  (See also 139-141) A part of the output current 27 of the generator 8 is connected to the inductance winding 11 and the bulb 14 in series so that the current changes according to the brightness of the bulb. The phototransistor is mounted adjacent to the bulb 14 and the phototube 15 and the electromagnet winding 18 are connected in series to the cell 17 to stimulate the iron core 25 of the electromagnet 19.  The Hall element 20 is installed in the gap between the two generators.  22) The resistance of the Hall element 20 connected in series with the input wire of the side is changed and the motor 1,  22) The automatic voltage adjusting device in which the output voltage is adjusted by the change of the rotational speed and the rotational force due to the change of the input voltage (see also 142-144) and the inductance winding 11 of the part 27 of the output current of the generator 8 side. ) And the current changes according to the brightness of the light bulb 14 by connecting it in series with the light bulb 14. The photoelectric tube 15 or the phototransistor is adjacent to the light bulb 14 and the variable resistor or input voltage in series with the photoelectric tube 15. When the current amount of the same electromagnet winding 33 is changed to the electromagnet core 29 equipped with the rotary iron core 32 so as to rotate the rotation side 37 to adjust the resistance 36, the spring mounted on the rotary iron core 32 ( 31) When the rotating iron core 32 rotates due to the difference in the force between the magnetic force of the electromagnet 29 and the variable resistance or inductance (slidax) resistance 36 changes, and the generator output 10 voltage changes, the motor input ( 21) the variable resistor or inductance resistor 36 connected in series to the An automatic voltage regulator (see also 145-147) and a deceleration gear 45 mounted on the rotating shaft 4 of the electric motor 1 and the output power of the generator 8 and the output 10 according to the change of the speed and the rotational power thereof. The reduction motor (1, 1) is mounted on the rotating shaft (6) so that a large diameter generator field (42) can be mounted and the generator armature (40) can be integrally rotated with the internal motor (1).  45 is mounted on the body of the reduction gear shaft (6) and the reduction motor (1,  The generator 8 and the high-speed electric motor 22 are mounted on the rotating shaft 24 mounted on the body of 45. When the motor rotor 2 rotates inside, the generator field magnet 41 mounted on the deceleration rotating shaft 6 is mounted. ) Rotates so that the electric current is generated in the electric current 40, and thus the deceleration motor 1,  The generator armature 40 integrated with the 45 generates a rotational force in the same direction as the deceleration rotation side 6 and the internal generator 40,  42 is used by connecting the current generated through the slip ring 43 and the brush 44, and a part of the current of the external generator 8 is transferred to the electric motor 1,  22) Automatic power generation and power generators (see Figure 148) and motors (1) supplied to the input lead (21) and used in part or powered by a pulley (9) mounted on the generator rotating side (6). Reduction gear (48, 49) and the generator armature 51 is mounted on the reduction shaft 6 to be integrally connected with the reduction motor 47 to mount the generator field 50, and the power winding 51 is connected with aluminum die-cast or enclosed rod. The ridge winding is made with a rough ring to have the same structure as the rotor of the induction motor. The rotary shaft 53 is integrally mounted to the central portion of the reduction motor body 47 and the generator 8 and the high speed motor 22 are mounted on the rotary shaft. And the pulley (9) is mounted on the generator rotary shaft (52) to supply current to the motor input side (21) busbar first, and when the normal speed is reached, a part of the output current of the generator (8) side is input to the motor input lead (21). Rotational power 4 in the direction of the rotational axis of the automatic power generation and power generator and the rotational cylinder 54 (see FIG. 149). Reducer on rotating shaft of two motors (1) mounted facing (56,  57) two motor shafts 4 rotate one reduction gear 58 together, and a shaft 61 is mounted on the body of the reduction shaft 6 and the cylinder 54, and the shafts 6, 61 holds the generator 8, the high speed motor 22 and the pulley 9, with the output of the generator 6 supplying some to two motor input leads 21 and using some or powering the pulley 9 And a reversing gear on the rotating shaft 4 of the electric motor 1 and the revolving shaft 62 integrally with the reversing rotating shaft 63 and the power generator body 64. The generator 8 and the high speed motor 22 to supply a part of the generator 8 output 10 to the internal motor 1 and the high speed motor 22, and use a part or pulley to the rotary shaft 63. (9) Equipped with two automatic motors (1) with a rotational axis in the radial direction at the center of the automatic power generation and power generating device (see also 151-152) and the rotating cylinder (70). Gear (67,  65) and connects the reduction gear 66 with a diameter of two reduction gear shaft 65 and the centripetal shaft of the cylinder 28 as the rotation shaft, and double-deceleration and the generator to the reduction gear shaft 6 and the cylindrical shaft shaft 69. (8) and the high speed motor 22, the internal motor (1) and the high speed motor 22 to supply a part of the generator (8) output (10) current to the input side 21 and to use a part of the rotating shaft (6) Deceleration shaft 6 and motor body 71 of a deceleration motor 72 with a built-in pulley 9 for automatic power generation and power generation (see FIG. 153) and a known reduction gear 71. ,  When the oscillator 8 and the high-speed motor 22 are mounted on the rotating shaft 73 attached to the motor 72 to supply current to the motor input 21 side, the deceleration motor 71  72 shaft and electric motor body (71,  As the 72 rotates, a large power is generated in the generator shaft 6 and a part of the output of the generator 8 is reduced.  72) and the high-speed electric motor 22, the automatic power generation and power generating device that automatically rotates with its own generated current to use a part of the generator output 10 or to mount the Raleigh 9 on the rotating shaft 6 to obtain power. (See also 154-156) Two motors 1 are mounted inside the rotating cylinder 76 so that the rotating shaft is in the axial direction, and the generator field 74 is mounted on the rotating shaft 4 of the motor. A generator armature 75 of a large closed circuit squirrel winding is mounted so that two generator field magnets 74 are adjacent to each other in the armature 75, and the rotating shaft 79 and the generator armature 75 of the rotating cylinder 76 are mounted. When the generator 8 and the high speed electric motor 22 are mounted on the rotary shaft 6 of the motor and the external current is first supplied to the internal motor 1 and the high speed motor 22, the rotary shaft 4 of the internal motor 1 and the high speed motor are supplied. A part of the current generated in the external generator output side 10 by the rotation of the motor 22 is transferred to the motor input side 2 1) an automatic power generation and power generating device which is powered by using part of it or by mounting a pulley 9 on the rotating side 6 (see FIG. 157) and two reduction gears on the rotating shaft 4 of the motor 1. Mount the gear 80, but the generator field 81 is mounted on the reduction shaft 84, and the closed circuit squirrel winding of the large rotation radius is mounted on the outside of the field magnet 81, the generator armature 82, generator armature 82 And deceleration motors (1,  The body of the 83 is integrally connected so that the separate rotation shaft (85,  86) and the generator 8 and the mother motor 22 are mounted so that an external current is initially supplied to the internal motor 1 and the high speed motor 22 so that a part of the output current of the generator 8 is supplied to the motor input side 21. Deceleration to the rotary shaft (4) of the electric motor (1) and to the generator and the generator (see also 158-162), powered by a pulley (9) which is supplied to and used in part or mounted on the rotary shaft (86). The gear 94 is mounted so that the reduction shaft 93 matches the shaft center of the motor 4 so that the axial compressor blade 97 having a large rotation radius is mounted so that the inner diameter 102 of the blade 87 and the outer diameter of the reduction motor are mounted. The flow path of the double cylindrical closed circuit between the (103) (89.  90.  92 and form an axial turbine blade 88 opposite the compressor blade 87, and gradually enlarge the cross-sectional area of the flow path in the turbine blade 88 to pass through the inside of the compressor blade 87 inner diameter 102 to form a swirl flow passage wall. By turning (101) to enter the compressor blade (87) and gradually expanding the cross section of the flow path at the compressor blade outlet (92), the cylindrical flow path to the turning flow path wall 101 outside the turbine blade (88) By turning to the turbine blades 88, the guide blade 91 is mounted so that the swirling fluid does not swirl, and the rotary shaft 95,  100), but the generator 8 and the high-speed motor 22 is mounted in accordance with the motor (1) rotary shaft (4) and the deceleration shaft (93), so that the internal motor (1) and the high-speed motor ( 22) When the external current is supplied to the normal speed, a part of the output current 10 of the generator 8 is supplied to the motor input side 21, and even when the external supply is stopped, the motor rotates with the self-generated current to output the current of the output 10. The automatic power generation and power generating device which uses a part or defines a pulley 9 on the rotating shaft 100 (see also 163-164) and the rotating shaft 112 and the body (field axis) of the electric motor 1. Axial Compressor Blade (104,  105) but with the vane (104,  Between the inner diameter 116 and the cylindrical outer diameter 114 of the double-cylinder closed circuit;  110,  111, but the outer flow path (109,  Compressor blades 104 equipped with an axial turbine gear 106 and rotating opposite to each other.  105, the flow path cross-sectional area is gradually enlarged from the outlet 110 to the turbine blade inlet 117 and reduced at the turbine inlet 117 so that the passage cross section is gradually enlarged at the outlet 111 of the turbine 106 (111,  109) The rotor blade 107 is not swirled to adjust the angle of the blade 105 so that the direction of the fluid at the compressor outlet 110 flows into the turbine inlet 117 flow path efficiently, and the rotational direction of the high speed motor 22 is controlled. And turbine blades (104,  The axis of rotation of the cylinder 114 to be rotated by 105 coincides with the axis of rotation 113,  115), but in line with the rotating shaft (4) of the motor 91, the generator (8) and the high-speed motor (22) is mounted to supply an external current to the motor input side (21) at first, and the generator output current at normal speed The automatic power generation and power generating device which supplies a part of the to the motor input side 21, stops the external current supply, and uses the part of the output 10 or is powered by the pulley 9 mounted on the rotating shaft 113 and ( (See FIG. 165) Two motors 1 are mounted so that the rotary shaft 4 is directed radially to the central portion of the large diameter cylinder 113, and the meat compressor blade has a large radius of rotation in the central portion of the cylinder 133. (119) is equipped with a gear 120 is connected to the small gear of the motor rotating shaft (4) to be a deceleration rotating shaft 134, and the flow path (122,  123,  125 to form the axial turbine gear 126 in the cylinder flow path 127 inside the compressor blade 119, the turbine blade 126 rotates in the rotational direction of the compressor blade 110, and the cylinder 133 The core body is equipped with a rotating shaft 134 rotating in accordance with the reduction shaft, and the generator 8 and the high-speed motor 22 are mounted to supply external current to the high-speed motor 22 and the internal motor 1 at first. A part of the output 10 is connected to the motor 1,  22) an automatic power generation and power generating device which is powered by using part of the output (10) or by mounting a pulley (9) on the rotating shaft (131) and the passage section inside the passage (see also 166-203). Rotary shaft of post-wing vane axial multistage compressor (6-10) gradually shrinking (2,  25 is equipped with a multi-stage axial flow turbine blade (15-17) in which the flow path inside thereof is gradually enlarged toward the outlet 14, and the flow path inside the turbine is slightly enlarged, and the compressor inlet (11) at the turbine outlet (14). Narrow flow path having a tendency formed inside the compressor blade inner diameter 29 by turning by the turning flow path wall 4 having a groove formed at the bottom of the compressor discharge port 5 and gradually decreasing in the compressor blade. 30), which is equipped with a ring-shaped cross-sectional reduction suction device 24 (Nos. 53-55 degrees) of a streamlined cross-section which inhales, but separates the flow path into several parts in the flow-path reduction part, and reduces the cross-section. The cross-section gradually expands slightly from the inside of the turbine blade-type buoyancy device 12-13 toward the outlet 22 so as to be constant from the outlet 22 to the turbine blade inlet 18, and that of the turbine blade-type buoyancy device 12-13. Forming a groove in the inner bottom The inlet of the groove is round (Fig. 172), elongated rectangle (Fig. 179) or rectangular (Fig. 188) so that the inner space of the groove is hemispherical (173), spherical (Fig. 174) or cylindrical ( (175 degrees) or twisted hemispherical (176 degrees) or cylindrical (177 degrees) or twisted circular shapes (178 degrees) or grooves (188-189) and elongated grooves (179-180 degrees) respectively. The internal space structure of the semicircular (181 degrees) or cylindrical (FIG. 182) or V-shaped groove (FIG. 183) or twisted V-shaped groove (FIG. 184) or one wall of the groove is semi-circular and circular groove ( 185) or twisted semi-circular grooves (186 degrees) or twisted U-shaped grooves (187 degrees) or internal spaces are hemispherical and the inlet is rectangular (190 degrees), but the long rectangular grooves and the rectangular grooves are The guide wall is shaped so that the direction is perpendicular to the direction of the fluid so that flow paths such as flow paths between axial impulse turbine turbines are connected in multiple stages. A structure in which the grooves 45 are formed on the bottom side of the vertical surface and the turbine 15-17 is downwardly sucked by the turning wall 19 from the discharge port 22, but the flow path section is constant. The buoyancy force that generates the buoyancy upward of the stationary body 28 due to the structure in which buoyancy is generated in the compressor blade 6-10 and fluid flows in the groove portion of the turbine blade-type flow path, thereby reducing the pressure of the groove and generating buoyancy. A groove is formed in the rear surface 58 of the thrust generator and the axial impulse turbine turbine blades (191 degrees) and a portion (bottom surface) of the north surface 56 and the rebound turbine blades (192 degrees) A buoyancy and / or thrust generating device in which a groove is formed on the rear surface 63, a groove is formed on the rear surface 69 of the axial compressor blade, and upward buoyancy is generated by the fluid passing through the flow path between the rotary blades. 209) turbine rotor blades by the inner flow path wall 84 and the outer flow path wall 85 of the cylindrical flow path 74-76. The turning portion of the turbine blade-type buoyancy device 74-76 and the flow path upper portion 76 in which a flow path structure of the flow path 74-76 is formed into a corrugated cylindrical shape and a groove 75 is formed in the inner bottom thereof. A linear guide vane (77 in FIG. 206) is radially mounted on (19) so that the fluid flowing into the centripetal section is not swirled and the multistage turbine blade (15-17) is connected to the rotation axis of the multistage compressor (6-6) at the centripetal section. The flow path cross-sectional area inside the post-wing multi-stage compressor blade (6-6) is gradually enlarged by gradually increasing the flow path cross section from the turbine outlet (14) to the compressor inlet (11). The turbine blade-type buoyancy is gradually reduced and the turbine blade-type flow path inlet 73 is fitted with a section reduction suction device 24 so as to be sucked into the turbine blade-type buoyancy device 74-76 having a narrow cross section. To the apparatus 74-76 and compressor blades 6-8 and turbine blades 15-17. A buoyancy and thrust generating device (if the groove is formed in the turbine gear) where upward buoyancy occurs (see also 210-212) and a post-stationary vane type axial multistage compressor blade (6). -10) is mounted on the same rotary shaft, and an upward cross-sectional enlarged flow path tube 97-98 is formed in the inner center of the blade inner diameter 99, and the compressor blade 6-10 is lowered by the upper turning flow path wall 19. Flow path cross section inside the multi-stage compressor blades 6-10 gradually decreases, and slightly expands from the compressor outlet 95 to the turbine blade inlet 94. And the cross section is reduced to flow into the turbine blade (87-91) and gradually increase the turbine blade internal induction and upward from the turbine outlet (86), the passage section gradually enlarges and the flow passage bottom of the turbine outlet (86) Buoyancy and main force generating device having a groove (4) in the structure and (see Figure 213) An upstream turbine blade-type buoyancy device (103-104) is mounted on the outer periphery of the post-wing rotor axial multistage compressor blade (6-10), and the flow path tube whose upward cross-section is gradually enlarged at the outlet 105 of the turbine blade-type buoyancy device ( 105-110, a cross-sectional reduction suction device 112 is mounted on the upper circulating flow path 110, and suctions into the axial multistage turbine blades 106-109 through a suction port 11 having a reduced cross section, and a turbine blade exit. At 114, the flow passage section is gradually enlarged and connected to the compressor inlet 115, and is gradually reduced inside the compressor blade 6-10 to form a groove 4 at the bottom of the compressor discharge port 102. A buoyancy and thrust generator having a structure in which the flow path section is reduced in the buoyancy device suction port 101 and the section reduction suction device 24 is fixed to the reduced portion and the axial flow multi-stage compressor 119-121 (see FIG. 214) are guided. With no structure, but between the corneas as far as the width of the The blade length is gradually shortened toward the outlet 116, the flow path cross-sectional area is gradually enlarged (117), and the axial multi-stage turbine (15-17) blade is mounted on the compressor (119-121) with the same axis of rotation (2). Turning in 116, the flow path cross section is gradually enlarged and upward, the turbine inlet 129 is enlarged and the flow path cross section is reduced. ) Grooves 4 on the bottom of the compressor blades 119-121 by a structure in which the grooves 4 are formed on the bottom of the compressor outlet 116 and grooves are formed in the compressor blades and the turbine blades. Buoyancy and thrust generating device that generates upward buoyancy by) and the axial multi-stage turbine turbine blades (139-143) are installed on the same side on the upper part of the post-swing rotor axial multi-stage compressor (6-10). Outside the compressor blades (6-10) and turbine blades (139-143) Forming an upward flow passage 131-132 whose surface is gradually enlarged, forming a groove 4 at the bottom of the flow passage bottom of the compressor discharge port 130, and gradually turning upward and expanding a cross section of the flow passage and reducing at the turbine inlet 134. Suction unit, but the flow path section reduction suction device 133 is attached to the reduction portion, the internal flow path of the turbine blades (139-143) is slightly enlarged, and gradually expands from the turbine outlet (135) to the compressor inlet (136) and the compressor (6-10). ) Buoyancy and thrust generating device for generating buoyancy by the compressor blades 6-10, turbine blades 139-143, and grooves 4 on the bottom by a structure that gradually shrinks inside (see FIG. 216). Compressor rotor blades (158,  160,  Compressor guide vane 157, having the same number of paragraphs as 162,  159,  161 and turbine rotorcraft (152,  Buoyancy and thrust generating device which eliminates turning components of the fuselage due to rotational recoil by a structure that rotates in the opposite direction by a separate electric motor 149 equipped with a guide blade of the number of paragraphs such as (154). Reference) A multi-stage axial turbine blade (166-168) is settled inside the inner diameter (177) of the post-stage multi-stage axial compressor blade (174-176), and the multi-stage turbine blade-type buoyancy device (169-170) is located above the turbine blade. It is connected to the outlet (171-173) pressure accumulator inlet (173) that the downward passage is gradually expanded by the flow of the outlet port 171 in the upper portion is gradually enlarged and the cross section of the flow path gradually inside the compressor blades and the compressor outlet (165) Turbine inlet 163 is pivoted upward to form a groove 4 on the front of the flow path, the flow path is reduced, the flow path section reduction suction device 164 is installed in the reduction portion and gradually enlarges slightly inside the turbine blades turbine outlet 178 On the same euro cross section A buoyancy and thrust generating device which sucks up to the wing type buoyancy device (169-170) and generates upward buoyancy due to a structure in which the passage section is gradually enlarged inside (see FIG. 220) and a device having a structure as shown in FIG. Compressor Rotary Wings (182,  184,  Compressor guide vane 183, having the same number of paragraphs as 186,  185,  187) and turbine rotorcraft (196,  198,  Turbine guide vane (195,  197,  The buoyancy and thrust generating device (refer to Nos. 221-222) which has no rotating component of the fuselage due to the rotational reaction due to the structure rotating in the opposite direction by a separate electric motor 193 equipped with 199) Two centrifugal compressors 202 rotating opposite to each other,  203, the axis of rotation (219,  A dual cylindrical turbine blade buoyancy device 214 having a single short or multi-stage axial turbine blade 206-211 mounted on 220, and upwardly and downwardly on top thereof.  215 to the compressor outlet 212,  The fluid of 222 is reduced by the flow path section reduction device 213 attached to the turbine blade-type buoyancy device 214, the inlet 217 of the upward direction, and the flow path section is slightly enlarged, and the flow path section is slightly enlarged inside and pivoted from the top. It is sucked into the turbine blade-type buoyancy device 215 downwards, and the passage cross section is slightly enlarged therein, turning at the outlet 218 to be sucked into the turbines 206-211, and gradually enlarged slightly inside the turbine, so that the turbine outlet 204,  In 205, the passage cross section is gradually enlarged so that the compressor 202,  203) buoyancy and thrust generating device free of swing components of the body by the suction structure (see also 223-224) and multi-stage axial flow on the same axis of rotation on the top of post-wing type axial flow multi-stage compressor 226-228. A multi-stage axial turbine blade (235-236) having a structure in which a turbine (231-233) is mounted and grooves are formed on the rear surface (237) and the rear surface (240) in the turbine and the compressor blades is provided with a buoyancy force. When the inner flow path of the blade tentacle and the groove (4) is formed in the bottom of the flow path of the discharge port 233, the turbine blade-type buoyancy device 236, the suction inlet flow path is reduced, but the reduction section suction device 224 is mounted on the reduction portion. The flow path cross section of the turbine blade type buoyancy device (236-235) gradually expands slightly, turns upward from the top, and downwards, and the flow path section remains constant, flows into the turbine blade 233, and the flow path cross section inside the turbine blades 231-233 Slightly zoomed in to compressor inlet 220 at turbine outlet 230. Buoyancy and thrust generating device having a structure in which the flow path section gradually expands to (see Fig. 225) and multi-stage turbine wing type buoyancy device (11,  2 centripetal compressors (3, under 12)  4) the rotating shaft (18,  19) becomes horizontal and the inlet (5,  6) are mounted facing each other to rotate opposite to each other, connecting the turbine blade-type buoyancy device inlet and the compressor outlet, the turbine blade-type buoyancy device (11,  In the outer periphery of 12), a flow path 13-10 is formed in which a downward cross section gradually expands, and the downward fluid is sucked into the compressor inlet port 8 and sucked into the turbine blade-type buoyancy device inlet port 7 upward from the center. A buoyancy and thrust generator having a structure in which the flow path cross-section is reduced in size than the compressor inlet port 8, and the cross-sectional reduction suction device 9 is attached to the downward flow path cross-section expansion tube end 10 to reduce the flow path cross section; (See also 226-229.) The tip 30 is wide and the tip is 26. 12) The flow path 27 of the multi-paragraph structure in which the flow path 27 is upwardly inclined in the axial direction gradually moves away from the vanes, the flow path section is enlarged and is upwardly upward 29, and the structure inclined in the opposite axial direction is repeated. The turbine blade 25 is mounted inside the inner diameter of the compressor blade 24 below the cylinder 16 on which the blade flow path is mounted, and the flow path of the compressor blade outlet 23 is pivoted to be mounted on the turbine inlet 3 upward. Flow path section reduction The flow path section is reduced and sucked by the suction device 22 to be sucked into the memory flow path 11-12 at the turbine outlet, and the flow path area is gradually enlarged slightly inside the gear path, and flows downward from the discharge port 14. The blade-shaped flow path 11, due to the structure that the cross section is gradually enlarged and re-sucked into the compressor blade 24,  12) and the buoyancy and thrust generator that generates buoyancy by the compressor blades 24 and the bottom surface 21 in which the grooves are formed (see also 230-214) and the upper surface of the disk-shaped rotating body 34 which rotates horizontally. Guide grooves 36 of a structure in which a groove 35 is formed on the same rotary shaft 33 in the axial direction in multiple stages, and a three-sided radially connected straight line having a lateral curved surface (40 in FIG. 233) between each paragraph. But the guide blade 36 and the disc (the gap) is narrow, the bottom 38 of the disc 34 is uniform and smooth, and the inlet of the groove 35 is round (234 degrees) or square (235 degrees) Since the inside of the long rectangle (Fig. 237) or the rectangular groove (42 of Fig. 239) circular groove 35 or the groove formed inside the rectangular groove or the long rectangular groove in a double structure (239-241 degrees) The groove inner space structure is a groove having various structures such as 173-190 degrees so that the motor 20 mounted on the rotating shaft 33 of the disc 34 is rotated at a high speed. When the fluid input of the groove part is lowered, the buoyancy and thrust generator which generates upward buoyancy and the guide vane of the device having the structure as shown in Fig. 230 and without the guide vane, 34) Rotational disk with buoyancy and thrust generator having strong structure by connecting (44) to each other in the vicinity of circumference with a large radius of rotation, and grooves (various grooves such as 230) Four inlets (50-53) are used to allow fluid to pass through the center of the cylinder, while the upper section has a larger inlet cross-section and gradually decreases, connecting each paragraph (57-61) to each other at the outer diameter area (48). Radially inside the outer facing (49) of the guide (52, 54) and the upper portion of the casing 49 to the curved surface 56, the fluid is rotated and sucked into the centripetal suction port 53, and circulated in the centrifugal direction again, and the motor 20 is rotated at high speed to obtain upward buoyancy. A cylindrically shaped rotary plate 66-70, which is about 45 degrees from the buoyancy and thrust generator and the horizontal plane (see also 248-250), is fixed to the same rotation axis 33 as a short circuit, and the grooves of the music grains on the side in the space between each short circuit (FIG. 233) When the guide blades 71-74 formed with the radial direction are rotated to rotate the disc, the pressure inside the groove 64 formed on the disc lowers and the buoyancy and thrust generating device generates upward buoyancy; (See FIG. 251.) Each paragraph has a structure in which grooves 64 (various grooves as shown in FIG. 230) are formed on the upper surface of each paragraph of the multi-stage conical rotating plate 66-71 having an angle with the horizontal plane of about 45 degrees. With no guide vane structure in between, each inlet plate (85-89) However, the suction port of the first paragraph (66) is larger and gradually smaller, and the cross section of the passage 91 formed by the kising section 77 and the disc of the outer valley is gradually enlarged and formed with a groove in the passage bottom portion 90. When the motor 20 mounted on the rotating shaft 33 rotates at a high speed, the buoyancy and thrust generator which generates upward buoyancy due to the pressure drop inside the upper groove 64 and the multi-paragraph (see also 252-255) The groove 64 is formed in the upper surface of each paragraph of the rotary disk plate 66-69, and the suction port 102-105 is formed in the center and the groove 64 is enlarged and gradually released from the upper surface of the first paragraph. Bend the conical plate inlet (102-105) of each paragraph with curvature toward the inlet to facilitate the suction of the fluid, and install the linear blade (98-101) radially of each paragraph, and the downward direction formed by the disc outlet and the inner surface of the kissing (75) Multistage turbine blades (94-96) on the rotating shaft (33) below the disk, gradually increasing the flow path cross-sectional area Buoyancy and thrust generator having a structure in which the turbine inlet (93) flow path section is measured and the flow path section reduction suction device (92) is mounted on the reduction part and the turbine inlet (97) is gradually enlarged from the disc outlet port (97) to the disc inlet port (102). (See also 256-257) A buoyancy and thrust generating device having a multi-stage turbine blade (94-96) mounted on the upper end of the durable rotary shaft 33 above the suction port 102 of the structure shown in FIG. Top and bottom of the rectangular flow conduit (see also 256-271).  11) the angle with the horizontal plane is about 45 degrees and the side (12,  13) to be vertical and to form a groove (4) on the inner bottom surface of the inner space of the groove with the opening of the groove (circle (263-264 degrees) or square (266 degrees) or long square (268 degrees) structure) The structure is similar to that of 173-190 degrees, and the tube is wound into a spiral cylinder, and each layer 83-86 of the spiral cylinder is attached to each other to form an integrated cylinder, and the compressor 7 is mounted in the center space. The guide vane 17 and the diffuser 2 are installed at the outlet to connect the diffuser outlet 3 and the spiral square tube inlet 6 of the spiral and connect the outlet 10 of the upper flow tube to the central core interstitial 9. A buoyancy and thrust generating device that generates a buoyancy due to the pressure in the groove 4 of the bottom face of the flow path being lowered by a circulation device which gradually enlarges the cross section of the flow path and re-suctions the compressor 7 through the compressor inlet 8. And (see Fig. 272) the inner cross section of the rectangular flow conduit is upper (32,  35 is horizontal with sides 34  38) so that the inclination angle with the horizontal surface of the side is about 45 degrees and the length of the side is upper (32,  35) buoyancy and thrust generators having a structure that is more than twice its length (see also 273-275) and the side surfaces (52,  53) is tilted and top and bottom (48,  50) the flow pipe of the horizontal structure is wound horizontally in a concentric spiral (51) the outlet 46 of the spiral pipe gradually enlarged the cross-sectional area of the flow path through the center portion and connects to the suction port 43 of the centrifugal compressor (42) A buoyancy and thrust generator having a structure circulating through the diffuser 44 to the suction port 45 of the spiral and the outer diameter and the upper and lower surfaces of the rectangular flow channel (see FIG. 276).  78) and the side (77,  79) to be inclined (about 45 degrees) but up and down (76,  78) the length of the side (77,  At least twice as long as the bottom of the inner channel wall (65,  66, a groove formed in the center and connected to the compressor suction port 58 by a flow path tube whose downward flow path section is gradually enlarged.  59) the rotating shaft (87,  88 is horizontal and the suction inlet 58 is opposed to each other to be mounted so as to rotate opposite to each other and connect the suction port 58 and the flow channel expansion tube 62 of the central portion and the fluid at the compressor outlet 57 is a square flow path suction ( 61) A buoyant thrust generator that generates upward buoyancy due to the structure of inflow to the inlet by reducing the cross section of the flow path (see FIG. 277) and the upper and lower surfaces (73,  80) is horizontal,  Side (81,  82) the structure in which the inclined structure is wound in a concentric spiral manner (Fig. 273) is also stacked up and down, so that the flow path becomes longer and the compressor 56,  59) The buoyancy and thrust generating device (see 278-280) and the conical flow path tube 26 having the rotating shaft mounted horizontally are upward and downward on the inclined plane of about 45 degrees (14,  18 flows into the centripet 28 and flows back to the centrifugal section 14, but is provided with a turning guide vane 12 and a straight guide vane 17 in the central section in a large diameter portion.  Equipped with a turning guide blade (19) in the center of the downward flow path, and equipped with a straight guide blade (17) in the centrifugal portion, equipped with a turning guide blade (19) in the centrifugal portion of the downward flow path and a straight guide blade (12) in the centrifugal portion. The bottom of the flow path (22,  23,  Two compressors (2, 2) having a groove formed in the groove (24) and having a downward flow path (12) connected to the suction port (5) of the central portion and the rotating shaft mounted in a horizontal direction  3) The flow path cross section is reduced in the suction port 9, and the flow path is gradually enlarged to the centripet 28, and the flow path cross section is gradually enlarged at the exit 10 of the straight guide vane 12 by keeping the downward flow path cross section constant. Compressor (2,  3) The upward flow path 8 of the buoyancy and thrust generator having the structure expanded to the suction port 6 and the conical guide tube having the groove 22 formed on the bottom (see FIG. 281).  9) flows into the centripet 15 on the inclined surface of about 45 trillion, and descends by the turning flow path 15 through the straight guide vane 14 to be sucked into the axial multi-stage turbine blade 16-16-18 and the turbine outlet 12 ), The flow path cross-sectional area is gradually enlarged and sucked into the axial multistage compressor (3-5) mounted on the turbine blade (16-18) and the same shaft (19). ), The flow path section is reduced and sucked by the flow path section reduction suction device 21 at the entrance of the turning guide blade 7 upward, and the upflow path 8,  The cross section of 9) is gradually enlarged slightly, slightly reduced at the turbine inlet 15, gradually enlarged slightly at the inside of the turbine blade 16-18, and upwardly by a structure in which a groove 20 is formed at the bottom of the flow path of the compressor outlet 2. Euro (8,  9) A buoyancy and thrust generator that generates buoyancy by grooves 22 at the bottom face, grooves 20 at the bottom of the compressor blades 3-5 and compressor outlet 2, and a conical flow path (see FIG. 282). Various compressors known in the center of the (eccentric blade type,  Screw Type,  Gear Type,  Reciprocating,  Rotary,  The inlet 9 of the swash plate, etc., upwards to allow the fluid to be sucked in, and the fluid of the lower outlet 4 flows upwardly.  In the turning guide vane 6 mounted on the suction port 5 of 11), the flow path section is reduced and sucked by the flow path section reduction suction device 16, and the upward flow path 7,  11) the buoyancy and thrust generating device for generating upward buoyancy by the structure in which the flow path area of 11) is made constant or slightly enlarged, the inclination of the upward flow path is about 45 degrees, and the groove 8 is formed on the bottom of the flow path. 283) The inlet 9 and the outlet 4 of the compressor 2 of the apparatus having the structure shown in FIG. 282 are reversed and the inlet 18,  9) Buoyancy of the structure in which the inclination angle of the flow path is large (about 30 degrees) and the turning guide vane 17 is mounted in the place where the downward fluid turns upward 18 and the fluid upwardly swirling to the inlet 9 is swirled. And the thrust generator (see also 284-287) and the long flow path tube 11 of circular or rectangular cross section is wound with spirals, and the spiral pipes are in close contact with each other to form a cylindrical structure, and the direction of the centripetal axis of the spiral pipe cylinder is horizontal. Bottom part of the flow path which turns up and down (8,  12) the centrifugal compressor (36) is mounted on the spiral centripetal shaft with the same rotation axis as the centripetal shaft, and the diffuser (5) is mounted at the compressor outlet so that the fluid at the outlet of the compressor (3) spirals through the diffuser (5). The flow pipe inlet 5 is mounted so that the fluid at the outlet of the compressor 3 flows into the spiral flow pipe inlet 6 through the diffuser 5 and gradually enlarges the cross-sectional area of the flow pipe 7 (9,  2) the buoyancy and thrust generator having a structure that is sucked into the compressor (3) (see also 288-291) and the groove (28) on the bottom of the conical channel (9,  20) is connected to the multi-paragraph inflow into the centripet (35) in the outer direction to be a flow path that is repeatedly distributed in the outer direction (36) and turning guide blades (8,  12,  15,  19) so that the fluid flows upward while swirling and the compressor suction port 24, through the cross-sectional enlarged flow path tube (22-23) formed in the center portion in the upper portion 22  25 is sucked into the compressor outlet (3,  6) the structure in which the fluid is sucked into the swing guide vane 8 mounted on the upwardly conical curved guide groove inlet 9 whose cross section is constructed, and the flow path cross-sectional area in the curved guide 9-9-20 is gradually enlarged and the two On the contrary, the suction shaft 24 of the compressor rotating in the horizontal direction  25) buoyancy and thrust generators that generate upward buoyancy due to centrifugal force and bottom groove while the upstream fluid swirls in conical induction due to its structure facing each other. (See also 292-300) Install the heating device (8) in the internal flow path of the device, but the case (7,  15) buoyancy and thrust generators of a structure that supplies heat to the fluid by a structure (Fig. 293) that allows the fluid to pass through in a large number of holes, Combustion buoyancy thrust generator of the structure formed by the inlet port () in the rear part and the external fluid is sucked in and the combustor (FIG. (See also 304-305.) The outer wall 6 of the buoyancy device is made of metal with high thermal conductivity, and the outside is wrapped in a cylinder 9 insulated, and a suction blower 1 and a combustor 4 are mounted on the bottom of the Upward combustion chamber flow path 5 surrounding the outside  7) A buoyancy and thrust generator having a structure that supplies heat to the inner fluid by attaching a thin metal plate or fine thread or a pipe having high thermal conductivity to each other (see also 306-308) and the anode of two electromagnets or permanent magnets Closely close the gap between the magnetic poles and insert a winding in which a DC current flows between them, while winding to become a concentric spiral rectangular surface, while the core (6) is closely wound between the windings to be a straight line between the magnetic poles (9). And a device that obtains buoyancy and thrust by deflection force in the direction perpendicular to the direction of current by the direct current in the windings between the poles and the multiple gaps between several permanent magnets or electromagnets (see also 309-312). Connect each other to form a donut shape, make the gaps (gaps) of two rows of donut magnets coincide, and insert a current winding into the gap (9) The buoyancy and thrust generator is supplied by the coolant 22 by the buoyancy and thrust generator which obtains the upward buoyancy or thrust by rectifying and supplying the rod, and the donut-shaped magnet and the current winding of two rows. Insulation bucket (23,  24) A buoyancy and thrust generator that is mounted inside and obtains strong buoyancy and thrust (see also 314-319), and the current (armature) winding (1) is made of superconductor or copper wire, and the electromagnet winding (3) is made of superconductor tightly. Winding device (23-31) and coolant (14) inside are connected by narrowing the gap (gap) with the current winding (1) and inserting a strong electromagnetic insulator cylinder (2) instead of an iron core into a two-row donut structure. Insulated canister (21, 22, the secondary winding 9 of the transformer 10 to which an external AC power supply 33 is connected,  11) is connected to the electromagnet winding 19 and the armature winding (1), the anode 35 of the electromagnet winding (3) and the conductor 19 side of the armature winding (1)  36) is connected to each other on both sides with the diode 17 in between, and closed, and strong by the structure in which the conductors connecting the diode 18 in series to the transformer secondary winding 11 on both sides of the diode 17 are connected. Buoyancy and thrust generator to obtain buoyancy and thrust. ※ Note: It is to be disclosed by the contents of the original application.