CN103101632B - Unmanned aerial vehicle body modularization folding tool platform and usage of the same - Google Patents
Unmanned aerial vehicle body modularization folding tool platform and usage of the same Download PDFInfo
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- CN103101632B CN103101632B CN201210588222.0A CN201210588222A CN103101632B CN 103101632 B CN103101632 B CN 103101632B CN 201210588222 A CN201210588222 A CN 201210588222A CN 103101632 B CN103101632 B CN 103101632B
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Abstract
The invention provides an unmanned aerial vehicle body modularization folding tool platform and a usage method of the unmanned aerial vehicle body modularization folding tool platform, wherein the unmanned aerial vehicle body modularization folding tool platform and the usage method of the unmanned aerial vehicle body modularization folding tool platform are used for composite plates. The unmanned aerial vehicle body modularization folding tool platform and the usage method of the unmanned aerial vehicle body modularization folding tool platform comprise a base platform, a main body structural part, a lower plate folding part and an upper plate folding part. The main body structural part constitutes a main boy frame of a tool, and is fast jointed, repeatedly constructed and used. The main body structural part comprises several kinds of supporting rods, pressing plates and base positioning plates, connecting plates and lower plate supporting frames which are all with different heights. The lower plate folding part comprises a lower plate limiting plate, a lower wing mounting assembly, a front launching supporting point mounting assembly, a rear supporting point mounting assembly, a vertical-type frame plate positioning seat, an air inlet duct front end positioning assembly and an air inlet duct rear end positioning assembly. The upper plate folding part comprises a nose mounting assembly, an upper plate limiting plate, an empennage mounting assembly, an upper plate mounting frame assembly and a wing mounting sliding platform. A matrix-type trapezoid-shaped groove is formed on the base platform, and the base platform is used for vehicle body folding tool platforms with different vehicle types.
Description
Technical field
What unmanned plane body modularization of the present invention closed up that tooling platform and using method thereof relate to is that a kind of unmanned plane body modularization for composite panels closes up tooling platform and using method thereof.
Background technology
At present, all kinds of novel unmanned plane R&D cycle is short, speed fast, and Fixture Design thinking is closed up in traditional integration and the process-cycle is difficult to meet actual requirement, and the large cost of the difficulty of processing of integrated tooling is high, store and transport extremely inconvenient, the production of the modernization unmanned plane be unsuitable for.The housing construction of unmanned plane adopts glass and carbon-fiber composite material usually, need to carry out 2 times or repeatedly close up step by step, also there is a large amount of Improvement requirements in novel unmanned plane development, integrated structure was not suitable with the needs of type conversion and upgrading improvement in the past, local can not adjust, and in use uses inconvenient operation.
Summary of the invention
The object of the invention is to close up tool structure for above-mentioned integration and improve difficulty, the deficiencies such as the cycle is long, a kind of unmanned plane body modularization is provided to close up tooling platform and using method thereof, that a kind of modular body closes up tooling platform, it is characterized in that carrying out modular combination, lower plate closes up part, upper plate closes up the substep that part meets body respectively and closes up requirement, tooling platform synchronously can be upgraded according to the improvement conversion of type, what meet variety classes type closes up requirement, save production site, be very suitable for the production of modernization research and development class unmanned plane.
Unmanned plane body modularization of the present invention closes up tooling platform and using method takes following technical scheme to realize:
Unmanned plane body modularization closes up that tooling platform tooling platform comprises basic platform 1, body junction component, lower plate closes up part and upper plate closes up part, 4 elements.
The material of described basic platform 1 is cast iron, and good stability distortion is little, and table-surface level and flatness is high has matrix form dovetail groove, may be used for the various body without different type of machines and close up tooling platform.
Described body junction component constitutes the main body frame of frock, can splice fast and repeat to build Reusability.Body junction component comprises the support bar of several differing heights, pressing plate, base positioning plate, connecting plate and lower plate holding frame; Support bar comprises support bar one, support bar two, and all there is the locating hole of 4 standards at the two ends of support bar one, support bar two, are located by connecting very convenient; Pressing plate is for being separately fixed at basic platform by support bar one, support bar two; Base positioning plate comprises base positioning plate one, base positioning plate two and base positioning plate three, have employed matrix form locating hole, while reduction own wt, keeps enough rigidity, can layering combine, also freely can connect according to body different length; Connecting plate is respectively used to the connection of base positioning plate one, base positioning plate two and base positioning plate three; Lower plate holding frame comprises lower plate holding frame one, lower plate holding frame two, lower plate holding frame three, lower plate holding frame four, lower plate holding frame five, lower plate holding frame one is arranged on below base positioning plate one, lower plate holding frame two is arranged on above base positioning plate two, lower plate holding frame three, lower plate holding frame four and lower plate holding frame five are arranged on base positioning plate three respectively, and left and right connects; The location adopting strand drilling screw to carry out body junction component be connected.
Described lower plate close up part comprise lower plate limiting plate, bottom wing installation component, front transmitting fulcrum installation component, after penetrate fulcrum installation component, vertical deckle board positioning seat, air intake duct front end positioning component and air intake duct rear end positioning component; Lower plate limiting plate (symmetrical) is arranged on the below of base positioning plate one, base positioning plate three both sides respectively; Bottom wing installation component is arranged on basic platform and utilizes T-slot to locate; Front transmitting fulcrum installation component (each 2 of left and right) is arranged on below base positioning plate one, after penetrate below fulcrum installation component (each 2 of left and right) installation foundation location-plate three; Vertical deckle board positioning seat is arranged on base positioning plate three, air intake duct front end positioning component is arranged on base positioning plate two, air intake duct rear end positioning component is arranged on base positioning plate three.
Described upper plate closes up part and comprises head installation component, upper plate limiting plate, empennage installation component, upper plate installing frame assembly and wing installation slide unit.The head that head installation component is arranged on tooling platform utilizes the base positioning plate one of the left and right sides to fix; Upper plate limiting plate (symmetrical) is arranged on the top of base positioning plate one and base positioning plate three both sides respectively, uses handle type alignment pin quick position; Empennage installation component is arranged on base positioning plate three, and upper plate installing frame assembly comprises upper plate press box one, upper plate press box two is arranged on base positioning plate three respectively and on base positioning plate one, wing is installed slide unit assembly and is arranged on base positioning plate three.
Described unmanned plane body modularization closes up the using method of tooling platform, it is characterized in that:
First, assembled body junction component on basic platform, select support bar one and the support bar two of differing heights, wherein support bar one is higher than support bar two, pressing plate is used to be fixed on basic platform by support bar one, support bar two, pressing plate adopts screw rod to be arranged in the matrix form dovetail groove of basic platform, and the two ends of support bar one and support bar two have the locating hole of 4 standards; Base positioning plate one and base positioning plate two have matrix form locating hole, strand drilling screw is utilized to be connected with support bar one by base positioning plate one respectively, base positioning plate two is connected with support bar two, combine, and then utilize connecting plate head and the tail to connect to form left side frame, same assembling method composition right side frame; The use lower plate holding frame one of the framework of arranged on left and right sides, lower plate holding frame two, lower plate holding frame three, lower plate holding frame four, lower plate holding frame five connect respectively, lower plate holding frame one, lower plate holding frame two, lower plate holding frame three, lower plate holding frame four, lower plate holding frame five have the installing hole of uniform sizes and centre-to-centre spacing, the correspondence position of strand drilling screw below base positioning plate one is utilized to be connected and fixed, the installation of body junction component.
Carry out the installation that lower plate closes up part after the installation of body junction component, first, lower plate limiting plate is arranged on respectively the below of base positioning plate one both sides, lower plate limiting plate plays the position-limiting action of the unmanned plane body lower plate left and right sides; Front transmitting fulcrum installation component comprises fixed mounted seat one, plate perforate drill bushing, fulcrum position fixing handle one, rear transmitting fulcrum installation component comprises fixed mounted seat two, plate perforate drill bushing, fulcrum position fixing handle two, and front transmitting fulcrum installation component and rear transmitting fulcrum installation component are arranged on correspondence position below base positioning plate one respectively; Plate super hole cutter cover is used for the perforate location of composite machine body lower plate in frock, unmanned plane lower plate is put into tooling platform, carry out the perforate of lower plate, extraction drill bushing after perforate completes, insert fulcrum position fixing handle one, fulcrum position fixing handle two respectively, launch the location of fulcrum and body lower plate before and after fulcrum position fixing handle one, fulcrum position fixing handle two are respectively used to, quick locking is located.
Air intake duct front end positioning component comprises sliding panel and 2, left and right air inlet keeper, sliding panel can on the base positioning plate two of the left and right sides slide anteroposterior and location, air inlet keeper is arranged on sliding panel, keeper profile coordinates with the air intake duct front end internal orifice of composite, air intake duct rear end positioning component is arranged on base positioning plate one, comprise positioning table and rear end positioning sleeve and positioning spigot circle, positioning table is connected with base positioning plate one across on body junction component, rear end positioning sleeve is vertically fixed on positioning table, positioning spigot circle coordinates with rear end positioning sleeve, seam circle seam part coordinates with UAV Inlet rear end inwall, realize the space orientation in UAV Inlet and body plate frock, vertical deckle board positioning seat is divided into left and right two pieces and is arranged on both sides base positioning plate one respectively, ensures the at right angle setting of unmanned plane body deckle board and body lower plate.Bottom wing installation component is combined by centralized positioning plate and bottom wing locating piece, and centralized positioning plate is arranged on basic platform, and to locate about platform chute, bottom wing locating piece 16-2 is arranged on centralized positioning plate, realizes coordinating with bottom wing aerofoil profile locating; Completing above peace enters after body closes up dress, knocks off in assembling platform by unmanned plane lower plate, can carry out body lower plate and each deckle board, front and back launch fulcrum, air intake duct, bottom wing location and once close up solidification.
Once close up after solidification completes, carry out closing up of body upper plate and lower plate.Extract the positioning spigot cover of air intake duct aft-end assembly first out, take off air intake duct rear end positioning component, take off vertical deckle board positioning seat, unmanned plane body upper plate is combined on lower plate; Head installation component is arranged on the front portion of tooling platform, and utilize the base positioning plate one of the left and right sides to fix, head installation component is made up of supporting ring in circular seam and circumferential alignment pin, for the body head metal frame of positioning round; Body junction component is installed plate press box one, upper plate press box two, and upper plate press box one, upper plate press box two match with fuselage upper plate profile for semi-circular; Wing is installed slide unit assembly and is made up of the backup block of the left and right sides, crossbeam, vertical beam, can realize the space orientation of the parts such as unmanned plane wing slide unit respectively; Empennage installation component is made up of the backup block of the left and right sides, crossbeam, crossbeam has 4 empennage locating holes can locate empennage connector; Finally utilize handle type latch to locate body upper plate limiting plate, upper plate limiting plate is arranged on the top of base positioning plate one both sides respectively, and when upper plate limiting plate can prevent from closing up, upper plate is outwards out of shape; The secondary carrying out body after completing closes up solidification, secondary takes off head installation component, wing slide unit assembly, empennage installation component respectively after closing up solidification, to heading slip air intake duct front end positioning component, seam part is thrown off, forward and backward generation fulcrum positioning sleeve is extracted out, take out the upper plate limiting plate that latch takes off both sides, finally the unmanned plane body closed up is taken out in tooling platform.
Unmanned plane body modularization of the present invention closes up the advantage of tooling platform and using method thereof:
1, modular combination design, can according to different housing construction feature rapid build, and versatility is good, has met the feature of modernization unmanned plane product;
2, seam problem on deformation when the plate solving composite closes up, meets the needs that body substep closes up;
3, tooling platform cost is low, and easy to operate efficiency is high, and detachable storage is suitable for the needs of modern production;
4, have employed the component positioning precisions such as high-precision base positioning plate high, the body closed up by this tooling platform has higher precision and reliability.
Accompanying drawing explanation
Below with reference to accompanying drawing, the invention will be further described:
Fig. 1 is that unmanned plane body modularization of the present invention closes up tooling platform structural representation.
Fig. 2 is that unmanned plane body modularization of the present invention closes up tooling platform stereogram.
In figure: 1, basic platform, 2, pressing plate, 3, support bar one, 4, base positioning plate one, 5, front transmitting fulcrum installation component, 6, connecting plate, 7, lower plate holding frame one, 8, lower plate limiting plate, 9, lower plate holding frame two, 10, air intake duct front end positioning component, 11, support bar two, 12, rear transmitting fulcrum installation component, 13, attaching nut, 14, lower plate holding frame three, 15, lower plate holding frame four, 16, bottom wing installation component, 17, lower plate holding frame five, 18, handle type alignment pin, 19, empennage installation component, 20, upper plate press box one, 21, positioning component after air intake duct, 22, vertical deckle board positioning seat, 23, wing installs slide unit assembly, 24, strand drilling screw, 25, upper plate press box two, 26, upper plate limiting plate, 27, head installation component, 28, base positioning plate two, 29, base positioning plate three.
5-1, fixed mounted seat one, 5-2, fulcrum position fixing handle one, 12-1, fixed mounted seat two, 12-2, fulcrum position fixing handle two, 16-1, centralized positioning plate, 16-2, bottom wing locating piece.
Detailed description of the invention
With reference to accompanying drawing 1,2, unmanned plane body modularization closes up that tooling platform comprises basic platform 1, body junction component, lower plate closes up part and upper plate closes up part, 4 elements.
The material of described basic platform 1 is cast iron, and good stability distortion is little, and table-surface level and flatness is high has matrix form dovetail groove, may be used for the various body without different type of machines and close up tooling platform.
Described body junction component constitutes the main body frame of frock, can splice fast and repeat to build Reusability.Body junction component comprises the support bar of several differing heights, pressing plate 2, base positioning plate, connecting plate 6 and lower plate holding frame; Support bar comprises support bar 1, support bar 2 11, and all there is the locating hole of 4 standards at the two ends of support bar 1, support bar 2 11, are located by connecting very convenient; Pressing plate 2 is for being separately fixed at basic platform 1 by support bar 1, support bar 2 11; Base positioning plate comprises base positioning plate 1, base positioning plate 2 28 and base positioning plate 3 29, have employed matrix form locating hole, while reduction own wt, keep enough rigidity, layering can combine, also freely can connect according to body different length; Connecting plate 6 is respectively used to the connection of base positioning plate 1, base positioning plate 2 28 and base positioning plate 3 29; Lower plate holding frame comprises lower plate holding frame 1, lower plate holding frame 29, lower plate holding frame 3 14, lower plate holding frame 4 15, lower plate holding frame 5 17, lower plate holding frame 1 is arranged on below base positioning plate 1, lower plate holding frame 29 is arranged on above base positioning plate 2 28, lower plate holding frame 3 14, lower plate holding frame 4 15 and lower plate holding frame 5 17 are arranged on base positioning plate 3 29 respectively, and left and right connects; The location adopting strand drilling screw 24 to carry out body junction component be connected.
Described lower plate close up part comprise lower plate limiting plate 8, bottom wing installation component 16, front transmitting fulcrum installation component 5, after penetrate fulcrum installation component 12, vertical deckle board positioning seat 22, air intake duct front end positioning component 10 and air intake duct rear end positioning component 21; Front transmitting fulcrum installation component 5 described in lower plate limiting plate 8 comprises fixed mounted seat one 5-1, plate perforate drill bushing, fulcrum position fixing handle one 5-2; Rear transmitting fulcrum installation component 12 comprises fixed mounted seat two 12-1, plate perforate drill bushing, fulcrum position fixing handle two 12-2, and front transmitting fulcrum installation component 5 and rear transmitting fulcrum installation component 12 are arranged on correspondence position below base positioning plate 1 respectively.Plate super hole cutter cover is used for the perforate location of composite machine body lower plate in frock, unmanned plane lower plate is put into tooling platform, carry out the perforate of lower plate, extraction drill bushing after perforate completes, insert fulcrum position fixing handle one 5-1, fulcrum position fixing handle two 12-1 respectively, the location of fulcrum and body lower plate is launched before and after fulcrum position fixing handle one 5-1, fulcrum position fixing handle two 12-1 are respectively used to, can quick locking location.
Described air intake duct front end positioning component 10 comprises sliding panel and 2, left and right air inlet keeper, sliding panel can on the base positioning plate 2 28 of the left and right sides (lower one deck) slide anteroposterior and location, air inlet keeper is arranged on sliding panel, and keeper profile coordinates with the air intake duct front end internal orifice of composite.
Described air intake duct rear end positioning component 21 is arranged on (higher one deck) on base positioning plate 1, comprise positioning table and rear end positioning sleeve and positioning spigot circle, positioning table is connected with base positioning plate 1 across on body junction component, rear end positioning sleeve is vertically fixed on positioning table, positioning spigot circle coordinates with rear end positioning sleeve, seam circle seam part coordinates with UAV Inlet rear end inwall, realizes the space orientation in UAV Inlet and body plate frock.
Described vertical deckle board positioning seat 22 is divided into left and right two pieces and is arranged on both sides base positioning plate 1 respectively, ensures the at right angle setting of unmanned plane body deckle board and body lower plate.
Described bottom wing installation component 16 is combined by centralized positioning plate 16-1 and bottom wing locating piece 16-2, centralized positioning plate 16-1 is arranged on basic platform 1, to locate about platform chute, bottom wing locating piece 16-2 is arranged on centralized positioning plate 16-1, realizes coordinating with bottom wing aerofoil profile locating.
Described head installation component 26 is made up of supporting ring in circular seam and circumferential alignment pin, for the body head metal frame of positioning round.
Main frame is installed plate press box 1, upper plate press box 2 25, and upper plate press box 1, upper plate press box 2 25 match with fuselage upper plate profile for semi-circular; Wing is installed slide unit assembly 23 and is made up of the backup block of the left and right sides, crossbeam, vertical beam, can realize the space orientation of the parts such as unmanned plane wing slide unit respectively; Empennage installation component 19 is made up of the backup block of the left and right sides, crossbeam, crossbeam has 4 empennage locating holes can locate empennage connector.
26(is symmetrical for upper plate limiting plate) be arranged on the below of base positioning plate 1, base positioning plate 3 29 both sides respectively; Bottom wing installation component 16 is arranged on basic platform 1 and utilizes T-slot to locate; Front transmitting fulcrum installation component (each 2 of left and right) is arranged on below base positioning plate 1, after penetrate below fulcrum installation component (each 2 of left and right) installation foundation location-plate 3 29; Vertical deckle board positioning seat 22 is arranged on base positioning plate 3 29, air intake duct front end positioning component 10 is arranged on base positioning plate 2 28, air intake duct rear end positioning component 21 is arranged on base positioning plate 3 29.
Described upper plate closes up part and comprises head installation component 27, upper plate limiting plate 26, empennage installation component 19, upper plate installing frame assembly and wing installation slide unit.The head that head installation component 27 is arranged on tooling platform utilizes the base positioning plate 1 of the left and right sides to fix; 26(is symmetrical for upper plate limiting plate) be arranged on the top of base positioning plate 1 and base positioning plate 3 29 both sides respectively, use handle type alignment pin 18 quick position; Empennage installation component 19 is arranged on base positioning plate 3 29, upper plate installing frame assembly comprises upper plate press box 1, upper plate press box 2 25 is arranged on base positioning plate 3 29 respectively and on base positioning plate 1, wing is installed slide unit assembly 23 and is arranged on base positioning plate 3 29.
Described front transmitting fulcrum installation component 5 comprises fixed mounted seat one 5-1, plate perforate drill bushing, fulcrum position fixing handle one 5-2; Rear transmitting fulcrum installation component 12 comprises fixed mounted seat two 12-1, plate perforate drill bushing, fulcrum position fixing handle two 12-2, and front transmitting fulcrum installation component 5 and rear transmitting fulcrum installation component 12 are arranged on correspondence position below base positioning plate 1 respectively.Plate super hole cutter cover is used for the perforate location of composite machine body lower plate in frock, unmanned plane lower plate is put into tooling platform, carry out the perforate of lower plate, extraction drill bushing after perforate completes, insert fulcrum position fixing handle one 5-1, fulcrum position fixing handle two 12-1 respectively, the location of fulcrum and body lower plate is launched before and after fulcrum position fixing handle one 5-1, fulcrum position fixing handle two 12-1 are respectively used to, can quick locking location.
Described air intake duct front end positioning component 10 comprises sliding panel and 2, left and right air inlet keeper, sliding panel can on the base positioning plate 2 28 of the left and right sides (lower one deck) slide anteroposterior and location, air inlet keeper is arranged on sliding panel, and keeper profile coordinates with the air intake duct front end internal orifice of composite;
Described air intake duct rear end positioning component 21 is arranged on (higher one deck) on base positioning plate 1, comprise positioning table and rear end positioning sleeve and positioning spigot circle, positioning table is connected with base positioning plate 1 across on body junction component, rear end positioning sleeve is vertically fixed on positioning table, positioning spigot circle coordinates with rear end positioning sleeve, seam circle seam part coordinates with UAV Inlet rear end inwall, realizes the space orientation in UAV Inlet and body plate frock.
Described vertical deckle board positioning seat 22 is divided into left and right two pieces and is arranged on both sides base positioning plate 1 respectively, ensures the at right angle setting of unmanned plane body deckle board and body lower plate.
Described bottom wing installation component 16 is combined by centralized positioning plate 16-1 and bottom wing locating piece 16-2, centralized positioning plate 16-1 is arranged on basic platform 1, to locate about platform chute, bottom wing locating piece 16-2 is arranged on centralized positioning plate 16-1, realizes coordinating with bottom wing aerofoil profile locating;
Described head installation component 26 is made up of supporting ring in circular seam and circumferential alignment pin, for the body head metal frame of positioning round;
Main frame is installed plate press box 1, upper plate press box 2 25, and upper plate press box 1, upper plate press box 2 25 match with fuselage upper plate profile for semi-circular; Wing is installed slide unit assembly 23 and is made up of the backup block of the left and right sides, crossbeam, vertical beam, can realize the space orientation of the parts such as unmanned plane wing slide unit respectively; Empennage installation component 19 is made up of the backup block of the left and right sides, crossbeam, crossbeam has 4 empennage locating holes can locate empennage connector.
The using method that unmanned plane body modularization closes up tooling platform is as follows:
First, assembled body junction component on basic platform, select support bar 1 and the support bar 2 11 of differing heights, wherein support bar 1 is higher than support bar 2 11, pressing plate is used to be fixed on basic platform 1 by support bar 1, support bar 2 11, pressing plate 2 adopts screw rod to be arranged in the matrix form dovetail groove of basic platform 1, and the two ends of support bar 1 and support bar 2 11 have the locating hole of 4 standards; Base positioning plate 1 and base positioning plate 2 28 have matrix form locating hole, strand drilling screw 24 is utilized to be connected with support bar 1 by base positioning plate 1 respectively, base positioning plate 2 28 is connected with support bar 2 11, combine, and then utilize connecting plate 6 head and the tail to connect to form left side frame, same assembling method composition right side frame; The use lower plate holding frame 1 of the framework of arranged on left and right sides, lower plate holding frame 29, lower plate holding frame 3 14, lower plate holding frame 4 15, lower plate holding frame 5 17 connect respectively, lower plate holding frame 1, lower plate holding frame 29, lower plate holding frame 3 14, lower plate holding frame 4 15, lower plate holding frame 5 17 have the installing hole of uniform sizes and centre-to-centre spacing, the correspondence position of strand drilling screw 24 below base positioning plate 1 is utilized to be connected and fixed, the installation of body junction component.
The installation that lower plate closes up part is carried out after the installation of body junction component.First, lower plate limiting plate 8 is arranged on respectively the below of base positioning plate 1 both sides, lower plate limiting plate 8 plays the position-limiting action of the unmanned plane body lower plate left and right sides; Front transmitting fulcrum installation component 5 comprises fixed mounted seat one 5-1, plate perforate drill bushing, fulcrum position fixing handle one 5-2, rear transmitting fulcrum installation component 12 comprises fixed mounted seat two 12-1, plate perforate drill bushing, fulcrum position fixing handle two 12-2, and front transmitting fulcrum installation component 5 and rear transmitting fulcrum installation component 12 are arranged on correspondence position below base positioning plate 1 respectively.Plate super hole cutter cover is used for the perforate location of composite machine body lower plate in frock, unmanned plane lower plate is put into tooling platform, carry out the perforate of lower plate, extraction drill bushing after perforate completes, insert fulcrum position fixing handle one 5-1, fulcrum position fixing handle two 12-1 respectively, the location of fulcrum and body lower plate is launched before and after fulcrum position fixing handle one 5-1, fulcrum position fixing handle two 12-1 are respectively used to, can quick locking location.
Air intake duct front end positioning component 10 comprises sliding panel and 2, left and right air inlet keeper, sliding panel can on the base positioning plate 2 28 of the left and right sides (lower one deck) slide anteroposterior and location, air inlet keeper is arranged on sliding panel, keeper profile coordinates with the air intake duct front end internal orifice of composite, air intake duct rear end positioning component 21 is arranged on (higher one deck) on base positioning plate 1, comprise positioning table and rear end positioning sleeve and positioning spigot circle, positioning table is connected with base positioning plate 1 across on body junction component, rear end positioning sleeve is vertically fixed on positioning table, positioning spigot circle coordinates with rear end positioning sleeve, seam circle seam part coordinates with UAV Inlet rear end inwall, realize the space orientation in UAV Inlet and body plate frock, vertical deckle board positioning seat 22 is divided into left and right two pieces and is arranged on both sides base positioning plate 1 respectively, ensures the at right angle setting of unmanned plane body deckle board and body lower plate.Bottom wing installation component 16 is combined by centralized positioning plate 16-1 and bottom wing locating piece 16-2, centralized positioning plate 16-1 is arranged on basic platform 1, to locate about platform chute, bottom wing locating piece 16-2 is arranged on centralized positioning plate 16-1, realizes coordinating with bottom wing aerofoil profile locating; Completing above peace enters after body closes up dress, knocks off in assembling platform by unmanned plane lower plate, can carry out body lower plate and each deckle board, front and back launch fulcrum, air intake duct, bottom wing location and once close up solidification.
Once close up after solidification completes, carry out closing up of body upper plate and lower plate.Extract the positioning spigot cover of air intake duct aft-end assembly 21 first out, take off air intake duct rear end positioning component 21, take off vertical deckle board positioning seat 22, unmanned plane body upper plate is combined on lower plate; Head installation component 26 is arranged on the front portion of tooling platform, and utilize the base positioning plate 1 of the left and right sides to fix, head installation component 26 is made up of supporting ring in circular seam and circumferential alignment pin, for the body head metal frame of positioning round; Body junction component is installed plate press box 1, upper plate press box 2 25, and upper plate press box 1, upper plate press box 2 25 match with fuselage upper plate profile for semi-circular; Wing is installed slide unit assembly 23 and is made up of the backup block of the left and right sides, crossbeam, vertical beam, can realize the space orientation of the parts such as unmanned plane wing slide unit respectively; Empennage installation component 19 is made up of the backup block of the left and right sides, crossbeam, crossbeam has 4 empennage locating holes can locate empennage connector; Handle type latch 18 is finally utilized to locate body upper plate limiting plate 26, upper plate limiting plate 26(symmetrical member) be arranged on the top of base positioning plate 1 both sides respectively, when upper plate limiting plate 26 can prevent from closing up, upper plate is outwards out of shape; The secondary carrying out body after completing closes up solidification, secondary takes off head installation component 26, wing slide unit assembly 23, empennage installation component 19 respectively after closing up solidification, to heading slip air intake duct front end positioning component 10, seam part is thrown off, forward and backward generation fulcrum positioning sleeve is extracted out, take out the upper plate limiting plate that latch takes off both sides, finally the unmanned plane body closed up is taken out in tooling platform.
Claims (10)
1. unmanned plane body modularization closes up a tooling platform, it is characterized in that: comprise basic platform, body junction component, lower plate closes up part and upper plate closes up part;
Described body junction component constitutes the main body frame of tooling platform, and can splice fast and repeat to build Reusability, body junction component comprises the support bar of several differing heights, pressing plate, base positioning plate, connecting plate and lower plate holding frame; Support bar comprises support bar one, support bar two, and all there is the locating hole of standard at the two ends of support bar one, support bar two, are located by connecting very convenient; Pressing plate is for being separately fixed at basic platform by support bar one, support bar two; Base positioning plate comprises base positioning plate one, base positioning plate two and base positioning plate three, have employed matrix form locating hole, can layering combine, and also freely can connect according to body different length; Connecting plate is respectively used to the connection of base positioning plate one, base positioning plate two and base positioning plate three; Lower plate holding frame comprises lower plate holding frame one, lower plate holding frame two, lower plate holding frame three, lower plate holding frame four, lower plate holding frame five, lower plate holding frame one is arranged on below base positioning plate one, lower plate holding frame two is arranged on above base positioning plate two, lower plate holding frame three, lower plate holding frame four and lower plate holding frame five are arranged on base positioning plate three respectively, and left and right connects; The location adopting strand drilling screw to carry out body junction component be connected;
Described lower plate closes up part and comprises lower plate limiting plate, bottom wing installation component, front transmitting fulcrum installation component, rear transmitting fulcrum installation component, vertical deckle board positioning seat, air intake duct front end positioning component and air intake duct rear end positioning component; Lower plate limiting plate is arranged on the below of base positioning plate one, base positioning plate three both sides; Bottom wing installation component is arranged on basic platform and utilizes T-slot to locate; Front transmitting fulcrum installation component is arranged on below base positioning plate one, below rear transmitting fulcrum installation component installation foundation location-plate three; Vertical deckle board positioning seat is arranged on base positioning plate three, air intake duct front end positioning component is arranged on base positioning plate two, and air intake duct rear end positioning component is arranged on base positioning plate three;
Described upper plate closes up part and comprises head installation component, upper plate limiting plate, empennage installation component, upper plate installing frame assembly and wing installation slide unit assembly; The head that head installation component is arranged on tooling platform utilizes the base positioning plate one of the left and right sides to fix; Upper plate limiting plate is arranged on the top of base positioning plate one and base positioning plate three both sides respectively, uses handle type alignment pin quick position; Empennage installation component is arranged on base positioning plate three, and upper plate installing frame assembly comprises upper plate press box one, upper plate press box two is arranged on base positioning plate three respectively and on base positioning plate one, wing is installed slide unit assembly and is arranged on base positioning plate three.
2. unmanned plane body modularization according to claim 1 closes up tooling platform, it is characterized in that: the material of described basic platform is cast iron, table-surface level and flatness is high, have matrix form dovetail groove, the body for various different type of machines closes up tooling platform.
3. unmanned plane body modularization according to claim 1 closes up tooling platform, it is characterized in that: described front transmitting fulcrum installation component comprises fixed mounted seat one, plate perforate drill bushing, fulcrum position fixing handle one; Rear transmitting fulcrum installation component comprises fixed mounted seat two, plate perforate drill bushing, fulcrum position fixing handle two, and front transmitting fulcrum installation component and rear transmitting fulcrum installation component are arranged on correspondence position below base positioning plate one respectively; Plate super hole cutter cover is used for the perforate location of composite machine body lower plate in tooling platform, unmanned plane lower plate is put into tooling platform, carry out the perforate of lower plate, extraction drill bushing after perforate completes, insert fulcrum position fixing handle one, fulcrum position fixing handle two respectively, the location of fulcrum and body lower plate is launched before and after fulcrum position fixing handle one, fulcrum position fixing handle two are respectively used to, can quick locking location.
4. unmanned plane body modularization according to claim 1 closes up tooling platform, it is characterized in that: described air intake duct front end positioning component comprises sliding panel and 2, left and right air inlet keeper, sliding panel can on the base positioning plate two of the left and right sides slide anteroposterior and location, air inlet keeper is arranged on sliding panel, and air inlet keeper profile coordinates with the air intake duct front end internal orifice of composite.
5. unmanned plane body modularization according to claim 1 closes up tooling platform, it is characterized in that: described air intake duct rear end positioning component is arranged on base positioning plate one, comprise positioning table and rear end positioning sleeve and positioning spigot circle, positioning table is connected with base positioning plate one across on body junction component, rear end positioning sleeve is vertically fixed on positioning table, positioning spigot circle coordinates with rear end positioning sleeve, positioning spigot circle seam part coordinates with UAV Inlet rear end inwall, realizes the space orientation in UAV Inlet and body plate frock.
6. unmanned plane body modularization according to claim 1 closes up tooling platform, it is characterized in that: described vertical deckle board positioning seat is divided into left and right two pieces and is arranged on both sides base positioning plate one respectively, ensure the at right angle setting of unmanned plane body deckle board and body lower plate.
7. unmanned plane body modularization according to claim 1 closes up tooling platform, it is characterized in that: described bottom wing installation component is combined by centralized positioning plate and bottom wing locating piece, centralized positioning plate is arranged on basic platform, to locate about platform chute, bottom wing locating piece is arranged on centralized positioning plate, realizes coordinating with bottom wing aerofoil profile locating.
8. unmanned plane body modularization according to claim 1 closes up tooling platform, it is characterized in that: described head installation component is made up of supporting ring in circular seam and circumferential alignment pin, for the body head metal frame of positioning round.
9. unmanned plane body modularization according to claim 1 closes up tooling platform, it is characterized in that: on main frame, install plate press box one, upper plate press box two, upper plate press box one, upper plate press box two match with fuselage upper plate profile for semi-circular; Wing is installed slide unit assembly and is made up of the backup block of the left and right sides, crossbeam, vertical beam, realizes the space orientation that unmanned plane wing installs slide unit assembly; Empennage installation component is made up of the backup block of the left and right sides, crossbeam, crossbeam has 4 empennage locating holes can locate empennage connector.
10. unmanned plane body modularization according to claim 1 closes up the using method of tooling platform, it is characterized in that:
First, assembled body junction component on basic platform, select support bar one and the support bar two of differing heights, wherein support bar one is higher than support bar two, pressing plate is used to be fixed on basic platform by support bar one, support bar two, pressing plate adopts screw rod to be arranged in the matrix form dovetail groove of basic platform, and the two ends of support bar one and support bar two have the locating hole of 4 standards; Base positioning plate one and base positioning plate two have matrix form locating hole, strand drilling screw is utilized to be connected with support bar one by base positioning plate one respectively, base positioning plate two is connected with support bar two, combine, and then utilize connecting plate head and the tail to connect to form left side frame, same assembling method composition right side frame; The use lower plate holding frame one of the framework of arranged on left and right sides, lower plate holding frame two, lower plate holding frame three, lower plate holding frame four, lower plate holding frame five connect respectively, lower plate holding frame one, lower plate holding frame two, lower plate holding frame three, lower plate holding frame four, lower plate holding frame five have the installing hole of uniform sizes and centre-to-centre spacing, the correspondence position of strand drilling screw below base positioning plate one is utilized to be connected and fixed, the installation of body junction component;
Carry out the installation that lower plate closes up part after the installation of body junction component, first, lower plate limiting plate is arranged on respectively the below of base positioning plate one both sides, lower plate limiting plate plays the position-limiting action of the unmanned plane body lower plate left and right sides; Front transmitting fulcrum installation component comprises fixed mounted seat one, plate perforate drill bushing, fulcrum position fixing handle one, rear transmitting fulcrum installation component comprises fixed mounted seat two, plate perforate drill bushing, fulcrum position fixing handle two, and front transmitting fulcrum installation component and rear transmitting fulcrum installation component are arranged on correspondence position below base positioning plate one respectively; Plate super hole cutter cover is used for the perforate location of composite machine body lower plate in frock, unmanned plane lower plate is put into tooling platform, carry out the perforate of lower plate, extraction drill bushing after perforate completes, insert fulcrum position fixing handle one, fulcrum position fixing handle two respectively, launch the location of fulcrum and body lower plate before and after fulcrum position fixing handle one, fulcrum position fixing handle two are respectively used to, quick locking is located;
Air intake duct front end positioning component comprises sliding panel and 2, left and right air inlet keeper, sliding panel can on the base positioning plate two of the left and right sides slide anteroposterior and location, air inlet keeper is arranged on sliding panel, keeper profile coordinates with the air intake duct front end internal orifice of composite, air intake duct rear end positioning component is arranged on base positioning plate one, comprise positioning table and rear end positioning sleeve and positioning spigot circle, positioning table is connected with base positioning plate one across on body junction component, rear end positioning sleeve is vertically fixed on positioning table, positioning spigot circle coordinates with rear end positioning sleeve, positioning spigot circle seam part coordinates with UAV Inlet rear end inwall, realize the space orientation in UAV Inlet and body plate frock, vertical deckle board positioning seat is divided into left and right two pieces and is arranged on both sides base positioning plate one respectively, ensures the at right angle setting of unmanned plane body deckle board and body lower plate, bottom wing installation component is combined by centralized positioning plate and bottom wing locating piece, and centralized positioning plate is arranged on basic platform, and to locate about platform chute, bottom wing locating piece is arranged on centralized positioning plate, realizes coordinating with bottom wing aerofoil profile locating, completing above peace enters after body closes up dress, knocks off in assembling platform by unmanned plane lower plate, can carry out body lower plate and each deckle board, front and back launch fulcrum, air intake duct, bottom wing location and once close up solidification,
Once close up after solidification completes, carry out closing up of body upper plate and lower plate; Extract the positioning spigot cover of air intake duct aft-end assembly first out, take off air intake duct rear end positioning component, take off vertical deckle board positioning seat, unmanned plane body upper plate is combined on lower plate; Head installation component is arranged on the front portion of tooling platform, and utilize the base positioning plate one of the left and right sides to fix, head installation component is made up of supporting ring in circular seam and circumferential alignment pin, for the body head metal frame of positioning round; Body junction component is installed plate press box one, upper plate press box two, and upper plate press box one, upper plate press box two match with fuselage upper plate profile for semi-circular; Wing is installed slide unit assembly and is made up of the backup block of the left and right sides, crossbeam, vertical beam, realizes the space orientation that unmanned plane wing installs slide unit assembly; Empennage installation component is made up of the backup block of the left and right sides, crossbeam, crossbeam has 4 empennage locating holes can locate empennage connector; Finally utilize handle type latch to locate body upper plate limiting plate, upper plate limiting plate is arranged on the top of base positioning plate one both sides respectively, and when upper plate limiting plate can prevent from closing up, upper plate is outwards out of shape; The secondary carrying out body after completing closes up solidification, secondary takes off head installation component, wing slide unit assembly, empennage installation component respectively after closing up solidification, to heading slip air intake duct front end positioning component, seam part is thrown off, forward and backward generation fulcrum positioning sleeve is extracted out, take out the upper plate limiting plate that latch takes off both sides, finally the unmanned plane body closed up is taken out in tooling platform.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201210588222.0A CN103101632B (en) | 2012-12-29 | 2012-12-29 | Unmanned aerial vehicle body modularization folding tool platform and usage of the same |
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| CN201210588222.0A CN103101632B (en) | 2012-12-29 | 2012-12-29 | Unmanned aerial vehicle body modularization folding tool platform and usage of the same |
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| CN103101632B true CN103101632B (en) | 2015-04-22 |
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| US10960458B2 (en) * | 2014-07-09 | 2021-03-30 | The Boeing Company | Mobile platforms for performing operations inside a fuselage assembly |
| CN106625331B (en) * | 2016-12-07 | 2017-10-03 | 中国人民解放军第五七二一工厂 | A kind of aircraft radars device changes the outfit special tooling and costume changing method |
| CN106695328A (en) * | 2017-02-20 | 2017-05-24 | 西安爱生技术集团公司 | Flexible assembly tooling structure for unmanned aerial vehicle |
| CN107128506B (en) * | 2017-03-28 | 2019-03-26 | 浙江大学 | A kind of adaptive support device for composite wing siding |
| CN108516102B (en) * | 2018-04-28 | 2023-09-26 | 中电科芜湖钻石飞机制造有限公司 | Flexible general aircraft support tool |
| CN109465791B (en) * | 2018-11-14 | 2020-11-03 | 中国直升机设计研究所 | Helicopter air inlet channel assembly assembling jig |
| CN111483609B (en) * | 2020-05-18 | 2024-06-04 | 西安爱生技术集团公司 | Middle wing part gluing and folding tool for small and medium-sized unmanned aerial vehicle |
| CN115026570A (en) * | 2022-06-17 | 2022-09-09 | 四川腾盾科技有限公司 | Non-hoisting type disassembling and assembling equipment for medium and large unmanned aerial vehicle |
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