CN209051607U - A kind of aircraft components assembly jig - Google Patents

A kind of aircraft components assembly jig Download PDF

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Publication number
CN209051607U
CN209051607U CN201821906149.6U CN201821906149U CN209051607U CN 209051607 U CN209051607 U CN 209051607U CN 201821906149 U CN201821906149 U CN 201821906149U CN 209051607 U CN209051607 U CN 209051607U
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CN
China
Prior art keywords
fixture block
locating rod
assembly jig
card slot
push plate
Prior art date
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Application number
CN201821906149.6U
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Chinese (zh)
Inventor
马新权
孟大伟
伍岗
亓保学
任耀龙
张晋嘉
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Xi'an Eagle Aircraft Machinery Manufacturing Co Ltd
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Xi'an Eagle Aircraft Machinery Manufacturing Co Ltd
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Priority to CN201821906149.6U priority Critical patent/CN209051607U/en
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Abstract

The utility model discloses a kind of aircraft components assembly jigs, including assembly jig ontology, first fixture block component, second fixture block component and bracket, first fixture block component includes the first fixture block, first card slot and the second card slot, second fixture block component includes the second fixture block, inner cavity, first locating rod, second locating rod, push plate, reset spring, square groove, strip groove, circular trough, compression spring, small fixture block, slide post, force column, connecting rod and pressing plate, push plate is slidably connected in the first locating rod and the second locating rod, reset spring is socketed in the second locating rod, square groove is provided with the upper and lower surface of the second fixture block, strip groove is provided with the upper and lower surface of the second fixture block, circular trough is provided with the upper and lower surface of the second fixture block, the lower end of compression spring is fixedly connected on the right side of push plate, small fixture block is slidably connected in square groove, slide post sliding connects It connects in strip groove, the lower end of connecting rod is fixedly connected on the left side of push plate.

Description

A kind of aircraft components assembly jig
Technical field
The utility model relates to assembly jig technique for fixing field, specially a kind of aircraft components assembly jig.
Background technique
Aircraft needs to use assembly jig, after assembling aircraft, needs to dismantle assembly jig in assembling, so as to In the outbound of aircraft, but it is all more troublesome in assembling and disassembly between each bracket of traditional assembly jig, it needs to expend very much Time, it is therefore desirable to a kind of time saving and energy saving convenient assembly jig.
Utility model content
The purpose of this utility model is to provide a kind of aircraft components assembly jigs, to solve to propose in above-mentioned background technique The problem of.
To achieve the above object, the utility model provides the following technical solutions: a kind of aircraft components assembly jig, including dress With type frame ontology, the first fixture block component, the second fixture block component and bracket, the assembly jig ontology by the first fixture block component, Second fixture block component and bracket assembled are fixedly connected, and the both ends of the bracket are welded with the first fixture block component or the second fixture block group Part.
The first fixture block component includes the first fixture block, the first card slot and the second card slot, and the inside of first fixture block is set It is equipped with first card slot and second card slot.
The second fixture block component includes the second fixture block, inner cavity, the first locating rod, the second locating rod, push plate, resets bullet Spring, square groove, strip groove, circular trough, compression spring, small fixture block, slide post, force column, connecting rod and pressing plate, the inner cavity open up It is fixedly connected on the upper lower wall of the inner cavity at the both ends of the inside of second fixture block, first locating rod, described The both ends of two locating rods are fixedly connected on the upper lower wall of the inner cavity, the push plate be slidably connected at first locating rod and In second locating rod, in second locating rod, the square groove is provided with second fixture block for the reset spring socket Upper and lower surface, the strip groove are provided with the upper and lower surface of second fixture block, and the circular trough is provided with second fixture block Upper and lower surface, the lower end of the compression spring is fixedly connected on the right side of the push plate, and the small fixture block is slidably connected at institute It states in square groove, the slide post is slidably connected in the strip groove, and the force column is fixedly connected on a left side for the slide post End, the lower end of the connecting rod are fixedly connected on the left side of the push plate, and the pressing plate is fixedly connected in the connecting rod.
Preferably, second card slot is located at the two sides of first card slot and is attached thereto logical.
Preferably, the push plate is run through at the both ends of first locating rod.
Preferably, the push plate is run through at the both ends of second locating rod.
Preferably, the square groove and the central part of the strip groove coincide.
Preferably, the upper end of the compression spring is fixedly connected on the lower surface of the small fixture block.
Preferably, the numerical value that the length of the slide post subtracts the width of the force column is equal to a left side for second card slot Hold the distance values of first fixture block left end.
Compared with prior art, the utility model has the beneficial effects that the aircraft components assembly jig:
(1), the first fixture block component and the second fixture block component can be fixed to each other by internal structure realization, the first card Slot can make the second fixture block into the inside of the first fixture block, and the second card slot can be clamped with small fixture block, the first locating rod and second Locating rod can provide support for push plate, can also anti-thrust plate shift when moving, reset spring can push away for two sides Plate provides the elastic force for reset, and compression spring can provide thrust for lesser calorie block, and small fixture block can be in the effect of compression spring Under slided on square groove, slide post and force column can slide in strip groove under external force, and connecting rod and pressing plate can be with It is slided under external force along circular trough.
Detailed description of the invention
Fig. 1 is the utility model bracket port schematic cross-sectional view;
Fig. 2 is the utility model appearance diagram;
Fig. 3 is the utility model bracket port schematic top plan view;
Fig. 4 is that the utility model bracket connects schematic cross-sectional view.
In figure: 1 assembly jig ontology, 2 first fixture block components, 21 first fixture blocks, 22 first card slots, 23 second card slots, 3 Second fixture block component, 31 second fixture blocks, 32 inner cavities, 33 first locating rods, 34 second locating rods, 35 push plates, 36 reset springs, 37 square grooves, 38 strip grooves, 39 circular troughs, 301 compression springs, 302 small fixture blocks, 303 slide posts, 304 force columns, 305 connections Bar, 306 pressing plates, 4 brackets.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work Every other embodiment obtained, fall within the protection scope of the utility model.
Fig. 1-4 is please referred to, the utility model provides a kind of technical solution: a kind of aircraft components assembly jig, including assembly Type frame ontology 1, the first fixture block component 2, the second fixture block component 3 and bracket 4, assembly jig ontology 1 by the first fixture block component 2, Second fixture block component 3 and the assembling of bracket 4 are fixedly connected, and the both ends of bracket 4 are welded with the first fixture block component 2 or the second fixture block Component 3, the first fixture block component 2 and the second fixture block component 3 can be fixed to each other by internal structure realization.
First fixture block component 2 includes the first fixture block 21, the first card slot 22 and the second card slot 23, and the inside of the first fixture block 21 is set It is equipped with the first card slot 22 and the second card slot 23, the first card slot 22 can make the inside of the second fixture block 31 the first fixture block 21 of entrance, Second card slot 23 is located at the two sides of the first card slot 22 and is attached thereto logical, and the second card slot 23 can be clamped with small fixture block 302.
Second fixture block component 3 include the second fixture block 31, inner cavity 32, the first locating rod 33, the second locating rod 34, push plate 35, Reset spring 36, square groove 37, strip groove 38, circular trough 39, compression spring 301, small fixture block 302, slide post 303, force column 304, connecting rod 305 and pressing plate 306, inner cavity 32 are provided with the inside of the second fixture block 31, and the both ends of the first locating rod 33 are fixed to be connected It connects on the upper lower wall of inner cavity, push plate 35 is run through at the both ends of the first locating rod 33, and the both ends of the second locating rod 34 are fixedly connected on On the upper lower wall of inner cavity, push plate 35 is run through at the both ends of the second locating rod 34, and the first locating rod 33 and the second locating rod 34 can be Push plate 35 provide support, can also anti-thrust plate 35 shift when moving, push plate 35 be slidably connected at the first locating rod 33 and In second locating rod 34, reset spring 36 is socketed in the second locating rod 34, and reset spring 36 can mention for the push plate 35 of two sides For the elastic force for reset, square groove 37 is provided with the upper and lower surface of the second fixture block 31, and strip groove 38 is provided with the second fixture block 31 Upper and lower surface, square groove 37 and the central part of strip groove 38 coincide, and circular trough 39 is provided with the upper following table of the second fixture block 31 Face, the lower end of compression spring 301 are fixedly connected on the right side of push plate 35, and the upper end of compression spring 301 is fixedly connected on small fixture block 302 lower surface, this can provide thrust in elastically-deformable compression spring 301 for lesser calorie block 302, and small fixture block 302 slides It is connected in square groove 37, small fixture block 302 can slide on square groove 37 under the action of compression spring 301, and slide post 303 is sliding Dynamic to be connected in strip groove 38, force column 304 is fixedly connected on the left end of slide post 303, the length of slide post 303 subtract by The numerical value of the width of power column 304 be equal to the second card slot 23 left end to 21 left end of the first fixture block distance values, slide post 303 and Force column 304 can slide in strip groove 38 under external force, and the lower end of connecting rod 305 is fixedly connected on a left side for push plate 35 Side, connecting rod 305 and pressing plate 306 can be slided along circular trough 39 under external force, and pressing plate 306 is fixedly connected on connecting rod On 305.
When assembling assembly jig, bracket and one end of the one end with the first fixture block component 2 is selected to have the second fixture block component 3 Two brackets, then by the second fixture block 31 be aligned the first fixture block 21 the first card slot 22, then hand push move the second fixture block component 3, push it into the first fixture block 21, force column 304 also under the action of the outer wall of the first fixture block 21, drive slide post 303 to Outer movement, when slide post 303 just leaves on small fixture block 302, small fixture block 302 can pass through under the action of compression spring 301 Square groove 37 enters in the second card slot 23 to be clamped therewith, completes the fixation of two brackets at this time.
When disassembly, hand is placed on pressing plate 306 and presses, and pressing plate 306 drives connecting rod 305 to move down, and drives push plate 35 move down simultaneously compression reseting spring 36, and compression spring 301 can pull downward on lower fixture block 301, make under the action of push plate 35 With the second card slot 23 be detached from, then the second fixture block component 3 can be taken out from the first fixture block component 2, after taking-up, pin pressure Plate 306, another hand push the other end of force column 304 toward strip groove 38, are allowed to be placed in by small fixture block 302, so as under Secondary use.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art, It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.

Claims (7)

1. a kind of aircraft components assembly jig, including assembly jig ontology (1), the first fixture block component (2), the second fixture block component (3) and bracket (4), it is characterised in that: the assembly jig ontology (1) passes through the first fixture block component (2), the second fixture block component (3) and bracket (4) assembling is fixedly connected, and the both ends of the bracket (4) are welded with the first fixture block component (2) or the second fixture block group Part (3);
The first fixture block component (2) includes the first fixture block (21), the first card slot (22) and the second card slot (23), first card Block (21) is internally provided with first card slot (22) and second card slot (23);
The second fixture block component (3) includes the second fixture block (31), inner cavity (32), the first locating rod (33), the second locating rod (34), push plate (35), reset spring (36), square groove (37), strip groove (38), circular trough (39), compression spring (301), lesser calorie Block (302), slide post (303), force column (304), connecting rod (305) and pressing plate (306), the inner cavity (32) are provided with described The both ends of the inside of second fixture block (31), first locating rod (33) are fixedly connected on the upper lower wall of the inner cavity, described The both ends of second locating rod (34) are fixedly connected on the upper lower wall of the inner cavity, and the push plate (35) is slidably connected at described On a positioning rod (33) and the second locating rod (34), the reset spring (36) is socketed on second locating rod (34), institute The upper and lower surface that square groove (37) is provided with second fixture block (31) is stated, the strip groove (38) is provided with second fixture block (31) upper and lower surface, the circular trough (39) are provided with the upper and lower surface of second fixture block (31), the compression spring (301) lower end is fixedly connected on the right side of the push plate (35), and the small fixture block (302) is slidably connected at the square groove (37) Interior, the slide post (303) is slidably connected in the strip groove (38), and the force column (304) is fixedly connected on the cunning The left end of dynamic column (303), the lower end of the connecting rod (305) is fixedly connected on the left side of the push plate (35), the pressing plate (306) it is fixedly connected on the connecting rod (305).
2. a kind of aircraft components assembly jig according to claim 1, it is characterised in that: second card slot (23) is located at The two sides of first card slot (22) are simultaneously attached thereto logical.
3. a kind of aircraft components assembly jig according to claim 1, it is characterised in that: first locating rod (33) The push plate (35) are run through at both ends.
4. a kind of aircraft components assembly jig according to claim 1, it is characterised in that: second locating rod (34) The push plate (35) are run through at both ends.
5. a kind of aircraft components assembly jig according to claim 1, it is characterised in that: the square groove (37) and the item The central part of shape slot (38) coincides.
6. a kind of aircraft components assembly jig according to claim 1, it is characterised in that: the compression spring (301) Upper end is fixedly connected on the lower surface of the small fixture block (302).
7. a kind of aircraft components assembly jig according to claim 1, it is characterised in that: the length of the slide post (303) The numerical value that degree subtracts the width of the force column (304) is equal to the left end of second card slot (23) to first fixture block (21) The distance values of left end.
CN201821906149.6U 2018-11-19 2018-11-19 A kind of aircraft components assembly jig Active CN209051607U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201821906149.6U CN209051607U (en) 2018-11-19 2018-11-19 A kind of aircraft components assembly jig

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201821906149.6U CN209051607U (en) 2018-11-19 2018-11-19 A kind of aircraft components assembly jig

Publications (1)

Publication Number Publication Date
CN209051607U true CN209051607U (en) 2019-07-02

Family

ID=67053697

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201821906149.6U Active CN209051607U (en) 2018-11-19 2018-11-19 A kind of aircraft components assembly jig

Country Status (1)

Country Link
CN (1) CN209051607U (en)

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