CN218745979U - Just, move formula wing upset support device - Google Patents
Just, move formula wing upset support device Download PDFInfo
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- CN218745979U CN218745979U CN202223100139.2U CN202223100139U CN218745979U CN 218745979 U CN218745979 U CN 218745979U CN 202223100139 U CN202223100139 U CN 202223100139U CN 218745979 U CN218745979 U CN 218745979U
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Abstract
The utility model discloses a just, formula wing upset support device moves, including fore-stock, after-poppet, the rotatable formula is equipped with wing root bracket seat on the fore-stock, be equipped with the support auricle on the wing root bracket seat, the both sides of wing root bracket seat are equipped with the locating pin hole, be equipped with a plurality of locating pin subassemblies on the fore-stock, the effect end of locating pin subassembly can penetrate the locating pin downthehole or break away from locating pin hole department to realize that control wing root bracket seat rotates and the final mesh that realizes supplementary upset wing of locating angle, the rotatable formula is equipped with wing little diaphragm on the after-poppet, the wing is little diaphragm along with wing root bracket seat is driven, the bottom of fore-stock and after-poppet all is equipped with the removal subassembly, treats the wing of upset aircraft through setting up two common fixes of bracket around, sets up wing root bracket seat and wing little diaphragm rotatable formula, and through locating pin subassembly control wing root bracket seat pivoted angle, and easy operation can make the fore-and back bracket all can carry out the position removal through setting up the removal subassembly, and is very convenient.
Description
Technical Field
The utility model relates to a technical field of wing parts overturn in the assembling process especially relates to a just, move formula wing upset support device.
Background
The wings of the medium-large unmanned aerial vehicle need to be turned over when the wings of the medium-large unmanned aerial vehicle are painted, polished, beautified, assembled under a frame, installed with equipment and the like, the turning of the wings is limited by factors such as space, region, cost and the like in the turning mode commonly used at present, the turning of the wings is finished mainly by a manual carrying mode under the conditions of requiring operation speed and being limited by space and topography, the method is rough, wing parts are easy to damage in the operation process, and the risk of manual uncontrollable exists.
SUMMERY OF THE UTILITY MODEL
In order to overcome the defects of the prior art, the utility model aims to provide a just, move formula wing upset support device to solve the technical problem that the background art mentioned.
For solving the technical problem, the utility model discloses a following technical scheme realizes:
the utility model provides a just, move formula wing upset support device, includes fore-stock, after-poppet, the last rotatable formula of fore-stock is equipped with wing root bracket holder, be equipped with the support auricle on the wing root bracket holder, the both sides of wing root bracket holder are equipped with the locating pin hole, be equipped with a plurality of locating pin subassemblies on the fore-stock, the effect end of locating pin subassembly can penetrate in the locating pin hole or break away from locating pin hole department to realize that control wing root bracket holder rotates and the final mesh that realizes supplementary upset wing of angle of location, the last rotatable formula of after-poppet is equipped with wing slightly diaphragm, wing slightly diaphragm is driven along with wing root bracket holder, the bottom of fore-stock and after-poppet all is equipped with the removal subassembly.
Further, be equipped with centre shaft hole on the wing root bracket seat, the last position that corresponds centre shaft hole of fore-stock is equipped with the center pin fixing base, be equipped with the center pin in the center pin fixing base, the center pin penetrates the rotatable of realizing wing root bracket seat in the center shaft hole, locating pin subassembly includes bracket pinhole, locating pin, the bracket pinhole is located the fore-stock, the locating pin can stretch out and retract in the bracket pinhole, and when locating pinhole on the wing root bracket seat just rotated and is coaxial with the bracket pinhole, the locating pin stretched out and can fix a position wing root bracket seat, when needs rotate wing root bracket seat, only need with the locating pin withdrawal can, be equipped with the after-poppet pivot on the after-poppet, the wing diaphragm relies on the after-poppet pivot to realize rotating slightly, the removal subassembly is adjustable universal wheel.
Furthermore, the locating pin subassembly has two sets ofly, and one of them group sets up in the upper end horizontal position of fore-stock, and another group installs in the axis lower extreme position of fore-stock, and two sets of locating pin subassemblies can be fixed wing root bracket seat in level and vertical direction to satisfy the operation needs under most wing frame.
Furthermore, the left side and the right side of the upper end of the front bracket are respectively wrapped with a left process pin shaft fixing plate and a right process pin shaft fixing plate, a bracket pin hole of one group of positioning pin assemblies penetrates through the left process pin shaft fixing plate, a positioning pin shaft seat is further arranged on the bracket seat, and a bracket pin hole of the other group of positioning pin assemblies is located on the positioning pin shaft seat.
Furthermore, the locating pin includes locating pin main part and handle, the handle is located the side of locating pin main part and perpendicular to locating pin main part to make things convenient for people to control the locating pin by hand and stretch into and stretch out in bracket pinhole, be equipped with spacing frame on the bracket seat, the handle is located spacing frame, prevents that the locating pin from deviating from and losing
Compared with the prior art, the beneficial effects of the utility model reside in that:
the wing of treating the upset aircraft is fixed jointly through two brackets around setting up, sets into rotatable formula with wing root bracket seat and wing tip diaphragm, and controls wing root bracket seat pivoted angle through the dowel subassembly, easy operation can make the front and back bracket all can carry out the position through setting up the removal subassembly and remove, and is very convenient.
Drawings
FIG. 1: the structure schematic diagram of the front bracket and the rear bracket of the wing overturning bracket of the utility model is shown;
FIG. 2: the front bracket structure of the wing overturning bracket of the utility model is exploded;
FIG. 3: the front bracket structure of the wing overturning bracket of the utility model is a radial exploded view;
FIG. 4: the schematic view of the wing root bracket seat on the front bracket of the wing overturning bracket of the utility model is rotated by 90 degrees;
FIG. 5 is a schematic view of: the structure of the positioning pin in the wing overturning bracket of the utility model is shown schematically;
in the figure: the device comprises a front bracket 1, a central shaft fixing seat 11, a central shaft 12, a bracket pin hole 13, a process pin shaft left fixing plate 14, a process pin shaft right fixing plate 15, a positioning pin shaft seat 16 and a limiting frame 17;
a rear bracket 2, a wing tip transverse plate 21 and a rear bracket rotating shaft 22;
the wing root bracket seat 3, the supporting lug plate 31, the positioning pin hole 32 and the central shaft hole 33;
a moving assembly 4;
locating pin 5, locating pin main part 51, handle 52.
Detailed Description
The present invention will be further described with reference to the accompanying drawings and the detailed description, and it should be noted that the embodiments or technical features described below can be arbitrarily combined to form a new embodiment without conflict.
Referring to fig. 1 to 5:
example 1: refer to fig. 1 to 2 earlier, the utility model discloses a formula wing upset support device just moves, including fore-stock 1, after-poppet 2, the rotatable formula is equipped with wing root bracket seat 3 on the fore-stock 1, be equipped with supporting lug piece 31 on the wing root bracket seat 3, the both sides of wing root bracket seat 3 are equipped with locating pin hole 32, be equipped with multiunit locating pin subassembly on the fore-stock 1, the effect end of locating pin subassembly can penetrate in locating pin hole 32 or break away from locating pin hole 32 to realize that control wing root bracket seat 3 rotates and the final purpose that realizes supplementary upset wing of location angle, the rotatable formula is equipped with wing little diaphragm 21 on after-poppet 2, wing little diaphragm 21 is along with wing root bracket seat 3 from the diaphragm, the bottom of fore-stock 1 and after-poppet 2 all is equipped with removal subassembly 4.
Referring to fig. 2: in a specific technical scheme, a central shaft hole 33 is formed in the center position of the wing root bracket seat 3, a central shaft fixing seat 11 is arranged at a position, corresponding to the central shaft hole 33, on the front bracket 1, a central shaft 12 is arranged in the central shaft fixing seat 11, the central shaft 12 penetrates into the central shaft hole 33 to achieve rotation of the wing root bracket seat 3, the positioning pin assembly comprises a bracket pin hole 13 and a positioning pin 5, the bracket pin hole 13 is located on the front bracket 1, the positioning pin 5 can extend out and retract in the bracket pin hole 13, when the positioning pin hole 32 on the wing root bracket seat 3 just rotates to be coaxial with the bracket pin hole 13, the positioning pin 5 extends out to position the wing root bracket seat 3, when the wing root bracket seat 3 needs to be rotated, only the positioning pin 5 needs to be manually retracted, a rear bracket rotating shaft 22 is arranged on the rear bracket 2, the wing tip transverse plate 21 depends on the rear bracket rotating shaft 22 to achieve rotation, the movable assembly 4 is an adjustable universal wheel, and the adjustable universal wheel is provided with an adjusting and an adjusting fixing assembly capable of locking and unlocking the adjustable universal wheel.
Referring to fig. 1 and 2, in particular, there are two sets of dowel pin assemblies, one set is arranged at the upper horizontal position of the front bracket 1, the other set is arranged at the lower position of the central axis of the front bracket 1, and the two sets of dowel pin assemblies can fix the wing root bracket seat 3 in the horizontal and vertical directions, so as to meet the requirements of most under-wing-frame operations.
When the wing support device is used, two support lugs 31 (the support lugs 31 comprise a front beam support lug 31 and a rear beam support lug 31, which are collectively called as the support lugs 31) on the front bracket 1 are inserted into lug gaps of a front joint and a rear joint of an aircraft wing, the corresponding positioning pins 5 of the front joint and the rear joint of the aircraft wing are inserted, the positioning shafts on the wing tip transverse plates 21 are inserted into corresponding holes of ribs at the tail ends of the aircraft wing, the aircraft wing needs to be turned over when the wing support device works under the shelf, the positioning pins 5 are pulled out to be separated from the positioning pin holes 32 on the wing root bracket seats 3, the wing root bracket seats 3 are rotated by hands, the wing root bracket seats 3 rotate around the central shaft 12, and the aircraft tail on the wing tip transverse plates 21 is driven to rotate around the rear bracket rotating shafts 22. When the rotation is +/-90 degrees, the positioning pins 5 of one group of positioning pin assemblies are used for locking; the rotation of + -180 deg. is locked using the dowel pins 5 of the other set of dowel assemblies.
Specifically, the left side and the right side of the upper end of the front bracket 1 are respectively wrapped with a left process pin shaft fixing plate 14 and a right process pin shaft fixing plate 15, wherein a bracket pin hole 13 of one group of positioning pin assemblies penetrates through the left process pin shaft fixing plate 14, a positioning pin shaft seat 16 is further arranged on the bracket seat, and a bracket pin hole 13 of the other group of positioning pin assemblies is positioned on the positioning pin shaft seat 16.
Referring to fig. 5: the positioning pin 5 comprises a positioning pin main body 51 and a handle 52, the handle 52 is positioned at the side of the positioning pin main body 51 and is perpendicular to the positioning pin main body 51 so as to facilitate the manual operation of the positioning pin 5 to extend into and extend out of the bracket pin hole 13, the bracket seat is provided with a limiting frame 17, the handle 52 is positioned in the limiting frame 17 to prevent the positioning pin 5 from being removed and lost, and it should be noted that in another group of positioning pin assemblies, because the bracket pin hole 13 is arranged on the positioning pin shaft seat 16, the limiting frame 17 is the area formed between the two positioning pin shaft seats 16.
The above embodiments are only preferred embodiments of the present invention, and the protection scope of the present invention cannot be limited thereby, and any insubstantial changes and substitutions made by those skilled in the art based on the present invention are all within the protection scope of the present invention.
Claims (5)
1. The utility model provides a just, move formula wing upset support device which characterized in that: including fore-stock, after-poppet, the last rotatable formula of fore-stock is equipped with wing root bracket holder, be equipped with the support lug piece on the wing root bracket holder, the both sides of wing root bracket holder are equipped with the locating pin hole, be equipped with a plurality of locating pin subassemblies on the fore-stock, the effect end of locating pin subassembly can penetrate in the locating pin hole or break away from locating pin hole department to realize controlling wing root bracket holder and rotate and finally realize the purpose of supplementary upset wing with angle of orientation, the last rotatable formula of after-poppet is equipped with the wing and is slightly diaphragm, the wing is slightly diaphragm along with wing root bracket holder is driven, the bottom of fore-stock and after-poppet all is equipped with the removal subassembly.
2. The portable wing overturning bracket device of claim 1, wherein: be equipped with centre bore on the wing root bracket seat, the last position that corresponds centre bore hole of fore-stock is equipped with the center pin fixing base, be equipped with the center pin in the center pin fixing base, the center pin penetrates the downthehole rotatable of realizing wing root bracket seat of center pin, locating pin subassembly includes bracket pinhole, locating pin, the bracket pinhole is located the fore-stock, the locating pin can stretch out and the withdrawal in the bracket pinhole, and when locating pinhole on the wing root bracket seat just rotated with bracket pinhole coaxial, the locating pin stretched out and can fix a position wing root bracket seat, when needs rotate wing root bracket seat, only need with the locating pin withdrawal can, be equipped with the after-poppet pivot on the after-poppet, the wing slightly diaphragm relies on the after-poppet pivot to realize rotating, the removal subassembly is adjustable universal wheel.
3. The portable wing overturning bracket device according to any one of claims 1-2, characterized in that: the locating pin subassembly has two sets ofly, and one of them group sets up in the upper end horizontal position of fore-stock, and another group installs in the axis lower extreme position of fore-stock, and two sets of locating pin subassemblies can be fixed wing root bracket seat in level and vertical direction to satisfy the operation needs under most wing frame.
4. The portable wing overturning bracket device of claim 1, wherein: the left and right sides of the upper end of the front bracket are respectively wrapped with a left process pin shaft fixing plate and a right process pin shaft fixing plate, a bracket pin hole of one group of positioning pin assemblies penetrates through the left process pin shaft fixing plate, a positioning pin shaft seat is further arranged on the bracket seat, and a bracket pin hole of the other group of positioning pin assemblies is positioned on the positioning pin shaft seat.
5. The portable wing overturning bracket device of claim 1, wherein: the locating pin includes locating pin main part and handle, the handle is located the side of locating pin main part and perpendicular to locating pin main part to make things convenient for the manual control locating pin of people to stretch into in bracket pinhole and stretch out, be equipped with spacing frame on the bracket seat, the handle is located spacing frame, prevents that the locating pin from deviating from and losing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223100139.2U CN218745979U (en) | 2022-11-22 | 2022-11-22 | Just, move formula wing upset support device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223100139.2U CN218745979U (en) | 2022-11-22 | 2022-11-22 | Just, move formula wing upset support device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218745979U true CN218745979U (en) | 2023-03-28 |
Family
ID=85651740
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202223100139.2U Active CN218745979U (en) | 2022-11-22 | 2022-11-22 | Just, move formula wing upset support device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218745979U (en) |
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2022
- 2022-11-22 CN CN202223100139.2U patent/CN218745979U/en active Active
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