CN214648976U - Bimodal green unmanned aerial vehicle - Google Patents
Bimodal green unmanned aerial vehicle Download PDFInfo
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- CN214648976U CN214648976U CN202120814607.9U CN202120814607U CN214648976U CN 214648976 U CN214648976 U CN 214648976U CN 202120814607 U CN202120814607 U CN 202120814607U CN 214648976 U CN214648976 U CN 214648976U
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- 230000002902 bimodal effect Effects 0.000 title claims abstract description 33
- 238000003780 insertion Methods 0.000 claims description 27
- 230000037431 insertion Effects 0.000 claims description 27
- 238000009434 installation Methods 0.000 claims description 24
- 210000002445 nipple Anatomy 0.000 claims description 9
- 239000010409 thin film Substances 0.000 claims description 9
- 239000000306 component Substances 0.000 description 25
- 230000000712 assembly Effects 0.000 description 5
- 238000000429 assembly Methods 0.000 description 5
- 238000005516 engineering process Methods 0.000 description 4
- 239000007789 gas Substances 0.000 description 4
- 239000001307 helium Substances 0.000 description 4
- 229910052734 helium Inorganic materials 0.000 description 4
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 4
- 230000009977 dual effect Effects 0.000 description 2
- 238000005265 energy consumption Methods 0.000 description 2
- 239000005431 greenhouse gas Substances 0.000 description 2
- 239000002699 waste material Substances 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 239000008358 core component Substances 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000010408 film Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
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Abstract
The utility model relates to a bimodal green unmanned aerial vehicle, which comprises an ellipsoidal main body air bag, a plurality of groups of mounting platform components arranged inside the main body air bag, side rotors arranged at the two sides of the middle part of the main body air bag, a tail rotor arranged at the tail part of the main body air bag and an undercarriage arranged at the bottom of the main body air bag, wherein a plurality of groups of empennage brackets are fixedly arranged on the main body air bag in the circumferential direction of the tail rotor, the empennage brackets are in annular array by taking the axial lead of the main body air bag as the center of circle, the number of the empennage brackets is preferably four, the side rotors are symmetrically arranged along the axial lead of the main body air bag, the number of the undercarriage is preferably four, the empennages are respectively arranged at the four corners of the main body air bag, the mounting platform components are used for fixedly connecting the propellers, the side rotors, the tail rotors and the undercarriage with the main body air bag, thereby solving the current aeronautical technical field, most of the existing unmanned aerial vehicles can only be applied to one working scene, and the problem that the current general aviation application scene is changeable cannot be solved.
Description
Technical Field
The utility model belongs to the technical field of the aviation, a bimodal green unmanned aerial vehicle is specifically disclosed.
Background
In current aviation technical field, traditional unmanned aerial vehicle product is more, can satisfy most market demands in quantity, but current unmanned aerial vehicle product most can only be applied to a job scene, can not satisfy the changeable requirement of current general aviation application scene, can't satisfy different crowds' different demands, lead to relevant unmanned aerial vehicle and derived product property ability to fall behind the market demand, greatly reduced unmanned aerial vehicle's practicality, not only caused the idle waste of resource, and can't adapt to the real-time in aviation field, for a long time, abroad always seeks new development thinking in this field lackly, seek more advanced novel aircraft is used for solving this type of problem, in recent years, the research in this aspect is also being actively carried out domestically.
Therefore, technical personnel in the field are dedicated to developing a bimodal green unmanned aerial vehicle, namely, the bimodal green unmanned aerial vehicle is combined with different unmanned aerial vehicle components on the basis of a main body air bag, the flight mode of the unmanned aerial vehicle is adjusted according to the characteristics of an application scene, so that one unmanned aerial vehicle can be applied to various working scenes, the changeable requirement of the current general aviation application scene is met, the practicability of the unmanned aerial vehicle is improved, the real-time performance of the aviation field is adapted, and the working efficiency is improved.
SUMMERY OF THE UTILITY MODEL
In view of this, the utility model discloses a solve current aviation technical field, current unmanned aerial vehicle majority can only be applied to a job scene, can not satisfy the changeable requirement of current general aviation application scene, lead to relevant unmanned aerial vehicle and derived product property ability to lag behind the market demand, greatly reduced unmanned aerial vehicle's practicality, not only caused the idle waste of resource, can not adapt the problem of aviation field real-time nature moreover, provide a bimodal green unmanned aerial vehicle.
In order to achieve the above purpose, the utility model provides a following technical scheme: the utility model provides a bimodal green unmanned aerial vehicle, when for rotation rotor formula flight mode, including the main part gasbag of ellipsoid type, set up a plurality of groups mounting platform subassemblies in main part gasbag inside, the side rotor of setting in main part gasbag middle part both sides, the afterbody rotor of setting at main part gasbag afterbody and the undercarriage of setting in the main part gasbag bottom, fixed mounting has a plurality of groups of fin support on the main part gasbag of afterbody rotor circumference, fin support uses the axial lead of main part gasbag to be the annular array as the centre of a circle, fin support quantity is four, the side rotor sets up along the axis symmetry of main part gasbag, undercarriage quantity is four, install the four corners department at the main part gasbag respectively, the top of main part gasbag is provided with the screw, the mounting platform subassembly is used for the screw, the side rotor, the fixed connection of afterbody and undercarriage and main part gasbag.
Further, the main airbag comprises an ellipsoidal airbag skin and an airbag framework arranged inside the airbag skin.
The utility model provides a bimodal green unmanned aerial vehicle, when four rotor formula flight mode for long duration, including the main part gasbag of ellipsoid type, a plurality of groups of mounting platform subassemblies of setting inside the main part gasbag, the side rotor of setting in main part gasbag middle part both sides, main part gasbag afterbody circumference fixed mounting has a plurality of groups of fin support, the fin support uses the axial lead of main part gasbag to be the annular array as the centre of a circle, fin support quantity is four, the side rotor sets up along the axis symmetry of main part gasbag, main part gasbag front portion and rear portion both sides are fixed mounting respectively have main rotor, the quantity of main rotor is four, and four main rotors use the main part gasbag to be the rectangular array as the center, the mounting platform subassembly is used for the side rotor, the fixed connection of main rotor and main part gasbag.
Furthermore, the four corners of the bottom of the main air bag are respectively and fixedly provided with a horn-shaped air cushion, and the air cushions are fixedly connected with the main air bag through a mounting platform assembly.
Further, all cup jointed the installation component on the installation platform subassembly, the installation platform subassembly includes screw thread post and plug handle, the installation component all includes the plug sleeve, supporting spring, a bearing, connector and the nipple of threading, the plug sleeve cup joints the surface at the plug handle, and the position department that the inside top of plug sleeve corresponds the plug handle is provided with supporting spring, the bearing has been cup jointed on the surface of plug handle, the bearing joint is in the connector that threads that the nipple top was seted up, the nipple cup joints in the plug sleeve, and the plug sleeve is kept away from the one end of plug handle and the main part gasbag fixed connection that corresponds.
Furthermore, a main power supply and a control element are arranged in the main body air bag, and a camera is arranged below the empennage bracket.
Further, a thin film solar cell electrically connected with the control element is attached to the top of the main air bag.
Furthermore, the overlooking section shape of the insertion handle is a regular polygon structure.
The beneficial effect of this scheme lies in:
1. the utility model discloses a bimodal green unmanned aerial vehicle, rotation rotor formula flight mode is including the main part gasbag, the inside helium that is filled with of main part gasbag, support through the gasbag skeleton, and connect different unmanned aerial vehicle parts in gasbag skeleton mounted position department, the gasbag skeleton is connected with afterbody rotor and two side rotors, the screw is connected to gasbag skeleton central point top of putting, the support mounting undercarriage system of gasbag skeleton below, contain preceding gliding wheel and back gliding wheel, the gasbag skeleton still is connected with the connection fin, a balance for controlling the main part gasbag, be provided with the main power supply in the main part gasbag, a control element, the camera, the main power supply provides power for afterbody rotor and side rotor, and control element realizes opening of control afterbody rotor and side rotor, functions such as rotational speed.
2. The utility model discloses a bimodal green unmanned aerial vehicle, the long-endurance four-rotor type flight mode is covered with flexible film solar cells on the air bag skin besides the main body air bag, the installation platform components on the air bag framework are connected with different unmanned aerial vehicle components, four main rotor wings are connected at the four main rotor wing installation platform components, two side rotor wings are connected at the two side rotor wing installation platform components, the tail part of the main air bag is provided with an empennage bracket, the lower part of the main air bag is provided with a camera, the lower end of the main air bag is connected with four air cushions, the main air bag is internally provided with a main power supply and a control element, the main power supply and the flexible thin-film solar cell supply power to the main rotor motor and the side rotor motor together, and the control element is connected with and controls the main motor, the side motor and the camera.
3. The utility model discloses a bimodal green unmanned aerial vehicle, through combining core part main part gasbag and different unmanned aerial vehicle subassemblies, can adjust unmanned aerial vehicle's flight mode according to the characteristics of application scene, when being in autorotation rotor wing formula flight mode, because of the buoyancy advantage of itself, the lift that provides is great, the dead time is long, take-off and flight speed are faster, the load-carrying capacity is good, under the same load condition, the volume is smaller, the carrying capacity of the existing unmanned aerial vehicle is greatly improved, the unmanned aerial vehicle characteristics of small size, fast speed, low energy consumption, low cost and large load are satisfied, through the rapid assembly of unmanned aerial vehicle parts, when being converted into the long-endurance four-rotor wing formula flight mode, the bimodal green unmanned aerial vehicle has the dual advantages of fixed wing aircraft and airship, the flight speed is fast, the load capacity is big, the flight is stable, the manipulation performance is superior, hover in the air, and the like, still combines the existing advanced solar energy technology and the air buoyancy technology, helium contained in the product is green pollution-free gas, the flexible thin-film solar cell covered on the surface of the bag body also utilizes green and environment-friendly solar energy, and pollution gas or greenhouse gas cannot be generated in the service life cycle of the product.
Additional advantages, objects, and features of the invention will be set forth in part in the description which follows and in part will become apparent to those having ordinary skill in the art upon examination of the following or may be learned from practice of the invention. The objectives and other advantages of the invention may be realized and attained by the means of the instrumentalities and/or combinations particularly pointed out in the appended claims.
Drawings
Fig. 1 is a schematic perspective view of a bimodal green unmanned aerial vehicle according to an embodiment of the present invention;
fig. 2 is a schematic perspective view of a bimodal green unmanned aerial vehicle in a second embodiment of the present invention;
fig. 3 is an exploded view of a first mounting assembly of a bimodal green drone according to the present invention;
fig. 4 is a schematic view of a three-dimensional structure of an insertion sleeve in a bimodal green unmanned aerial vehicle;
fig. 5 is a schematic view of the three-dimensional structure of the airbag frame in the bimodal green unmanned aerial vehicle;
figure 6 is the utility model relates to a composite structure schematic diagram of undercarriage and third installation component among bimodal green unmanned aerial vehicle.
The drawings are numbered as follows: 1. a main body airbag; 101. covering the air bag with skin; 102. an air bag framework; 2. mounting a platform assembly; 201. a threaded post 202, an insertion handle; 3. an empennage bracket; 4. a tail rotor; 5. a first mounting assembly; 501. a plug bush; 502. a support spring; 503. a bearing; 504. a traversing connection port; 505. a threaded connecting sleeve; 6. a landing gear; 7. a second mounting assembly; 8. a propeller; 9. a third mounting assembly; 10. a side rotor; 11. a fourth mounting assembly; 12. an air cushion; 13. a thin film solar cell; 14. a main rotor; 15. and a fifth mounting assembly.
Detailed Description
The following is further detailed by way of specific embodiments:
example one
As shown in figures 1, 3-6, a bimodal green unmanned aerial vehicle comprises an ellipsoidal main air bag 1, a plurality of groups of mounting platform assemblies 2 arranged inside the main air bag, and side rotary wings arranged on two sides of the middle part of the main air bag, the setting is at the afterbody rotor 4 of main part gasbag afterbody and sets up the undercarriage in the main part gasbag bottom, fixed mounting has a plurality of groups of empennage support 3 on the main part gasbag of afterbody rotor circumference, empennage support 3 uses the axial lead of main part gasbag to be the annular array as the centre of a circle, empennage support quantity is preferred four, the side rotor sets up along the axis symmetry of main part gasbag, 6 quantity of undercarriage are preferred four, install the four corners department at the main part gasbag respectively, the top of main part gasbag is provided with screw 8, the mounting platform subassembly is used for the screw, side rotor 10, the fixed connection of afterbody rotor 4 and undercarriage and main part gasbag.
The main body air bag comprises an ellipsoidal air bag skin 101 and an air bag framework 102 arranged inside the air bag skin, wherein the air bag framework 102 is annular frameworks arranged at the front part, the middle part and the rear part of the main body air bag respectively and is marked as a first annular framework, a second annular framework and a third annular framework from front to back respectively.
The mounting platform assembly at the tail of the main air bag is sleeved with a first mounting assembly 5 for fixedly mounting a tail rotor, the mounting platform assembly at the top of the main air bag is sleeved with a second mounting assembly 7 for fixedly mounting a propeller, the mounting platform assembly at the bottom of the main air bag is sleeved with a third mounting assembly 9 for fixedly mounting an undercarriage, and the mounting platform assemblies at the two sides of the middle of the main air bag are sleeved with a sixth mounting assembly for fixedly mounting a side rotor.
The mounting platform assembly comprises a threaded column 201, one end of the threaded column 201 is arranged on the air bag framework 102, the other end of the threaded column 201 is fixedly connected with an insertion handle 202, and the overlooking section of the insertion handle 202 is of a regular polygon structure. The mounting platform subassembly fixed mounting of main part gasbag afterbody is on the third annular skeleton of gasbag skeleton 102, and the mounting platform subassembly fixed mounting at main part gasbag top is on the second annular skeleton of gasbag skeleton 102, and the mounting platform subassembly fixed mounting of main part gasbag bottom is on the first annular skeleton and the third annular skeleton of gasbag skeleton 102, and the mounting platform subassembly fixed mounting of main part gasbag middle part both sides is on the second annular skeleton of gasbag skeleton 102.
The first installation component 5, the second installation component 7, the third installation component 9 and the sixth installation component have the same structure and respectively comprise an insertion sleeve 501, a support spring 502, a bearing 503, a passing connection port 504 and a threaded connection sleeve 505, the insertion sleeve 501 is sleeved on the surface of the insertion handle 202, the support spring 502 is arranged at the position, corresponding to the insertion handle 202, of the top of the inner side of the insertion sleeve 501, the bearing 503 is sleeved on the surface of the insertion handle 202, the bearing 503 is clamped in the passing connection port 504 formed in the top of the threaded connection sleeve 505, the threaded connection sleeve 505 is sleeved in the insertion sleeve 501, and one end, far away from the insertion handle 202, of the insertion sleeve 501 is fixedly connected with the corresponding main body airbag 1.
A main power supply, a control element and a camera are arranged in the main air bag 1, the main power supply provides power for the tail rotor 4 and the side rotor 10, and the control element controls the start, stop, rotation speed and other functions of the tail rotor 4 and the side rotor 10.
When this bimodal green unmanned aerial vehicle uses, earlier with 1 inside helium of main part gasbag, gasbag covering 101 passes through gasbag skeleton 102 and supports in main part gasbag 1, and connect different unmanned aerial vehicle parts in gasbag skeleton 102 mounted position department, connect afterbody rotor 4 and two side rotors 10 on the gasbag skeleton 102, the screw 8 is connected to gasbag skeleton 102 central point puts the top, the support mounting undercarriage 6 of gasbag skeleton 102 below, install preceding gliding wheel and back gliding wheel on undercarriage 6, be convenient for slide of main part gasbag 1. The air bag framework 102 is further connected with a connecting tail wing 3 and used for controlling the balance of the main air bag 1, a main power supply in the main air bag 1 provides power for the tail rotor 4 and the side rotor 10, and the control element realizes the functions of controlling the start and stop, the rotating speed and the like of the tail rotor 4 and the side rotor 10.
Example two
As shown in fig. 2-6, bimodal green unmanned aerial vehicle, main part gasbag 1 including the ellipsoid type, a plurality of groups of mounting platform subassembly 2 of setting inside the main part gasbag, the side rotor of setting in main part gasbag middle part both sides, the fixed mounting of main part gasbag afterbody circumference has a plurality of groups of fin support 3, fin support 3 uses the axial lead of main part gasbag as the centre of a circle to be annular array, fin support quantity is preferred four, the side rotor sets up along the axis symmetry of main part gasbag, the mounting platform subassembly is used for the fixed connection of side rotor 10 and main part gasbag.
The main body air bag comprises an ellipsoidal air bag skin 101 and an air bag framework 102 arranged inside the air bag skin, wherein the air bag framework 102 is annular frameworks arranged at the front part, the middle part and the rear part of the main body air bag respectively and is marked as a first annular framework, a second annular framework and a third annular framework from front to back respectively.
And the mounting platform components on the two sides of the middle part of the main air bag are sleeved with sixth mounting components for fixedly mounting the side rotors.
The mounting platform assembly comprises a threaded column 201, one end of the threaded column 201 is arranged on the air bag framework 102, the other end of the threaded column 201 is fixedly connected with an insertion handle 202, and the overlooking section of the insertion handle 202 is of a regular polygon structure. The mounting platform assemblies on both sides of the middle of the main body airbag are fixedly mounted on the second annular frame of the airbag frame 102.
The anterior main rotor wing of having respectively fixed mounting in main part gasbag and rear portion both sides, main rotor wing 14's quantity is four, and four main rotor wings 14 use main part gasbag 1 to be the rectangular array as the center. The main rotor wings on the front part and the rear part of the main air bag are symmetrically arranged along the axis of the main air bag. The main rotor 14 is connected with the main air bag 1 through a mounting platform assembly. The four corners of the bottom of the main air bag 1 are respectively and fixedly provided with a horn-shaped air cushion 12, and the air cushion 12 is connected with the main air bag through a mounting platform assembly.
A layer of thin-film solar cells 13 is attached to the top of the main body air bag, and the solar cells 13 convert solar energy into power for operation of the unmanned aerial vehicle, so that energy is saved. And fifth mounting assemblies 15 for fixedly mounting the main rotor wing are sleeved on the mounting platform assemblies at the front part and the rear part of the main air bag. And a fourth mounting component 11 for fixedly mounting an air cushion is sleeved on the mounting platform component at the bottom of the main air bag.
The fourth installation component 11, the fifth installation component 15 and the sixth installation component have the same structure, and each of the fourth installation component 11, the fifth installation component 15 and the sixth installation component includes an insertion sleeve 501, a support spring 502, a bearing 503, a through connection port 504 and a threaded connection sleeve 505, the insertion sleeve 501 is sleeved on the surface of the insertion handle 202, the support spring 502 is arranged at the position of the top of the inner side of the insertion sleeve 501 corresponding to the insertion handle 202, the bearing 503 is sleeved on the surface of the insertion handle 202, the bearing 503 is clamped in the through connection port 504 formed at the top of the threaded connection sleeve 505, the threaded connection sleeve 505 is sleeved in the insertion sleeve 501, and one end of the insertion sleeve 501, which is far away from the insertion handle 202, is fixedly connected with the corresponding main airbag 1.
The long-endurance four-rotor type flight mode is characterized in that flexible thin-film solar cells 13 are covered on an air bag skin besides a main air bag 1, a mounting platform assembly 2 on an air bag framework 102 is connected with different unmanned aerial vehicle components, four main rotors 14 are connected with the mounting platform assembly 2 of the four main rotors 14, two side rotors 10 are connected with two side rotors 10 at the mounting platform assembly 2, a tail wing support is mounted at the tail part of the main air bag 1, a camera is mounted below the tail wing support, an air cushion 12 is connected to the lower end of the main air bag 1, four air cushions 12 are provided, the four air cushions can be adsorbed on the ground when landing and parking on the ground at any place, strong wind is avoided, a main power supply and a control element are mounted inside the main air bag 1, the main power supply and the flexible thin-film solar cells 13 supply power to a main rotor 14 motor and a side rotor 10 motor together, and the control element is connected with and controls the main rotor, the main rotor 14 motor, the side rotor 10, and the control element controls the main rotor 10, Side motor and camera.
The implementation mode of the bimodal green unmanned aerial vehicle is specifically as follows: by combining the core component main body airbag 1 with different unmanned aerial vehicle components, the flight mode of the unmanned aerial vehicle can be adjusted according to the characteristics of an application scene, when the unmanned aerial vehicle is in a self-rotation rotor wing type flight mode, the provided lift force is larger, the dead time is long, the taking-off and flight speeds are faster, the load-bearing performance is good, and the size is smaller under the condition of equal load, so that the carrying capacity of the existing unmanned aerial vehicle is greatly improved, the characteristics of the unmanned aerial vehicle with small size, high speed, low energy consumption, low cost and large load are met, the dual advantages of a fixed wing aircraft and an airship are realized when the unmanned aerial vehicle is converted into a long-endurance four-rotor wing type flight mode through the rapid assembly of the unmanned aerial vehicle components, the unmanned aerial vehicle has the advantages of high flight speed, large load weight, stable flight, superior operating performance, hovering and the like, and the existing advanced solar technology and the floating power technology are combined, helium contained in the product is green pollution-free gas, the flexible thin-film solar cell 13 covered on the surface of the bag body also utilizes green and environment-friendly solar energy, and pollution gas or greenhouse gas cannot be generated in the service life cycle of the product.
The above description is only an example of the present invention, and the common general knowledge of the known specific structures and characteristics of the embodiments is not described herein. It should be pointed out that to those skilled in the art, without departing from the structure of the present invention, a plurality of modifications and improvements can be made, which should also be regarded as the protection scope of the present invention, and these will not affect the effect of the implementation of the present invention and the utility of the present invention.
Claims (10)
1. The utility model provides a bimodal green unmanned aerial vehicle which characterized in that: including the main part gasbag of ellipsoid type, a plurality of groups of mounting platform subassembly of setting inside the main part gasbag, the side rotor of setting in main part gasbag middle part both sides, the afterbody rotor of setting at main part gasbag afterbody and the undercarriage of setting in main part gasbag bottom, fixed mounting has a plurality of groups of fin support on the main part gasbag of afterbody rotor circumference, fin support uses the axial lead of main part gasbag to be the annular array as the centre of a circle, fin support quantity is four, the side rotor sets up along the axis symmetry of main part gasbag, undercarriage quantity is four, install respectively in the four corners department of main part gasbag, the top of main part gasbag is provided with the screw, the mounting platform subassembly is used for the screw, the side rotor, the fixed connection of afterbody rotor and undercarriage and main part gasbag.
2. The bimodal green drone of claim 1, wherein: the main airbag comprises an ellipsoidal airbag skin and an airbag framework arranged inside the airbag skin.
3. The bimodal green drone of claim 1 or 2, characterized in that: all cup jointed the installation component on the mounting platform subassembly, the installation platform subassembly includes screw thread post and plug handle, the installation component all includes the plug sleeve, supporting spring, a bearing, connector and the nipple of going through, the plug sleeve cup joints the surface at the plug handle, and the position department that plug sleeve inboard top corresponds the plug handle is provided with supporting spring, the bearing has been cup jointed on the surface of plug handle, the bearing joint is in the connector that goes through that the nipple top was seted up, the nipple cup joints in the plug sleeve, and the plug sleeve is kept away from the one end of plug handle and the main part gasbag fixed connection who corresponds.
4. The bimodal green drone of claim 3, wherein: the overlooking section of the insertion handle is in a regular polygon structure.
5. The utility model provides a bimodal green unmanned aerial vehicle which characterized in that: including the main part gasbag of ellipsoid type, a plurality of groups of mounting platform subassembly of setting inside the main part gasbag, the side rotor of setting in main part gasbag middle part both sides, main part gasbag afterbody circumference fixed mounting has a plurality of groups of fin support, the fin support uses the axial lead of main part gasbag to be the annular array as the centre of a circle, fin support quantity is four, the side rotor sets up along the axis symmetry of main part gasbag, main part gasbag front portion and rear portion both sides fixed mounting respectively have main rotor, the quantity of main rotor is four, and four main rotors use the main part gasbag to be the rectangle array as the center, the mounting platform subassembly is used for the side rotor, the fixed connection of main rotor and main part gasbag.
6. The bimodal green drone of claim 5, wherein: the four corners of the bottom of the main air bag are respectively and fixedly provided with a horn-shaped air cushion, and the air cushions are fixedly connected with the main air bag through a mounting platform assembly.
7. The bimodal green drone of claim 5 or 6, characterized in that: all cup jointed the installation component on the mounting platform subassembly, the installation platform subassembly includes screw thread post and plug handle, the installation component all includes the plug sleeve, supporting spring, a bearing, connector and the nipple of going through, the plug sleeve cup joints the surface at the plug handle, and the position department that plug sleeve inboard top corresponds the plug handle is provided with supporting spring, the bearing has been cup jointed on the surface of plug handle, the bearing joint is in the connector that goes through that the nipple top was seted up, the nipple cup joints in the plug sleeve, and the plug sleeve is kept away from the one end of plug handle and the main part gasbag fixed connection who corresponds.
8. The bimodal green drone of claim 1 or 5, characterized in that: a main power supply and a control element are arranged in the main body air bag, and a camera is arranged below the empennage bracket.
9. The bimodal green drone of claim 1 or 5, characterized in that: a thin film solar cell electrically connected with the control element is attached to the top of the main air bag.
10. The bimodal green drone of claim 7, wherein: the overlooking section of the insertion handle is in a regular polygon structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120814607.9U CN214648976U (en) | 2021-04-20 | 2021-04-20 | Bimodal green unmanned aerial vehicle |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120814607.9U CN214648976U (en) | 2021-04-20 | 2021-04-20 | Bimodal green unmanned aerial vehicle |
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| CN214648976U true CN214648976U (en) | 2021-11-09 |
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| CN202120814607.9U Expired - Fee Related CN214648976U (en) | 2021-04-20 | 2021-04-20 | Bimodal green unmanned aerial vehicle |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115324828A (en) * | 2022-09-20 | 2022-11-11 | 重庆交通大学 | Flight high altitude power generation system |
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2021
- 2021-04-20 CN CN202120814607.9U patent/CN214648976U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115324828A (en) * | 2022-09-20 | 2022-11-11 | 重庆交通大学 | Flight high altitude power generation system |
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