CN210449617U - Paint spraying tool for airplane wing flap - Google Patents
Paint spraying tool for airplane wing flap Download PDFInfo
- Publication number
- CN210449617U CN210449617U CN201921059901.2U CN201921059901U CN210449617U CN 210449617 U CN210449617 U CN 210449617U CN 201921059901 U CN201921059901 U CN 201921059901U CN 210449617 U CN210449617 U CN 210449617U
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- rocker
- base
- paint spraying
- flap
- wing flap
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Abstract
The utility model discloses a paint spraying tool aiming at an airplane wing flap, which comprises a base and a rocker, wherein the top of the base is provided with a rocker hole site, and the rocker is matched in the rocker hole site; the rocker is provided with a positioning structure for fixing the airplane flap. According to above-mentioned technical scheme, the aircraft wing flap passes through location structure to be fixed on the rocker, and is parallel or close parallel with the rocker, and the operator rotates the rocker, and the wing flap rotates thereupon, so, conveniently sprays paint in the wing flap both sides.
Description
Technical Field
The utility model relates to a paint spraying work of wing flap among general aviation aircraft.
Background
The flap is one of the important components of the aircraft wing and plays an important role in the take-off and landing process. The flap is thin and is mostly in a slender shape, so that the flap is difficult to be stably fixed for painting, and special tools are needed for fixing, so that stable painting operation can be conveniently realized.
SUMMERY OF THE UTILITY MODEL
The utility model solves the technical problem that: the utility model provides a special frock, fixed flap is convenient for carry out the operation of spraying paint to it.
In order to solve the technical problem, the utility model provides a following technical scheme: a paint spraying tool for an airplane flap comprises a base and a rocker, wherein a rocker hole is formed in the top of the base, and the rocker is matched in the rocker hole; the rocker is provided with a positioning structure for fixing the airplane flap.
According to above-mentioned technical scheme, the aircraft wing flap passes through location structure to be fixed on the rocker, and is parallel or close parallel with the rocker, and the operator rotates the rocker, and the wing flap rotates thereupon, so, conveniently sprays paint in the wing flap both sides.
Drawings
The invention will be further explained with reference to the drawings:
FIG. 1 is a schematic view of a painting tool for an aircraft flap;
fig. 2 is an exploded view of fig. 1.
The symbols in the drawings illustrate that:
10. a base; 11. a base body; 12. a connecting rod; 13. a bottom cross bar; 14. a support bar; 15. a reinforcing bar; 16. a connecting rod;
20. a rocker; 21. a positioning structure; 22. a handle;
30. and (6) rocker hole positions.
Detailed Description
With reference to fig. 1 and 2, a paint spraying tool for an aircraft flap comprises a base 10 and a rocker 20.
The base 10 comprises two base bodies 11 and a connecting rod 12, wherein the two base bodies are respectively arranged at two ends of the connecting rod; the base comprises a bottom cross bar 13, a pair of support bars 14 arranged on the bottom cross bar, a reinforcing bar 15 connecting the support bars and the bottom cross bar, and a connecting rod 16 connecting the pair of support bars, wherein the tops of the pair of support bars are provided with rocker hole sites 30; a pair of support rods form a V-shape.
The rocker hole sites 30 may be formed as follows: a section of metal pipe is welded on the top of the support rod 14, and the holes of the metal pipe form the positions of the rocker holes.
The two seat bodies 11 are arranged in bilateral symmetry about the center of the connecting rod 12, and a rocker hole on the left seat body and a corresponding rocker hole on the right seat body form a group of rocker holes; the other rocker hole site on the left seat body and the corresponding other rocker hole site on the right seat body form the other group of rocker hole sites. A rocker 20 is matched in each group of rocker hole sites, and two rocker holes of each group of rocker hole sites are supported at two ends of the rocker to play a role in stable support.
Two rockers 20, have sufficient distance between them and supply two flaps to pass through, so, two rockers can carry out the operation of spraying paint to two flaps simultaneously, improve work efficiency.
Each rocker 20 is provided with a stop between a set of two rocker holes 30 that cooperate with the rocker. The matching of the rocker and the rocker hole positions can adopt the following modes: firstly, a rocker is inserted into a group of rocker hole sites, namely two rocker hole sites; and then, two stop blocks are fixed on the rocker, one stop block is close to one rocker hole site, the other stop block is close to the other rocker hole site, and the two stop blocks are positioned between the two rocker hole sites. Therefore, the rocker does not have axial play and is stably matched with the two rocker holes. Wherein, the stop block can be screwed or welded on the rocker.
The rocker 20 is provided at one end with a handle 22, which is preferably formed by bending the end of the rocker directly, at 90 degrees.
The rocker 20 is provided with a positioning structure 21 for fixing the wing flap of the airplane, and the positioning structure is positioned between a group of two rocker hole sites, so that the gravity center of the wing flap falls between a group of two rocker hole sites, namely between the two base bodies 11, and the wing flap can be stably supported.
The positioning structure 21 is a bolt hole site arranged on the rocker 20, and the bolt hole site corresponds to the flap mounting hole. The number and the positions of the bolt hole sites on one rocker are determined according to the number and the positions of the mounting holes on the flap. Preferably, after the rocker is fitted into the rocker hole 30, a cylindrical rod is welded or screwed on the rocker, and the cylindrical rod is provided with the bolt hole. When the wing flap is fixed, the wing flap mounting hole corresponds to the bolt hole site, and the bolt is matched with the wing flap mounting hole and then is in threaded connection with the bolt hole site, so that the fixing of the wing flap and the rocker is realized.
As an improvement, the bottom of two pedestal 11 sets up the gyro wheel, and the frock that sprays paint of being convenient for removes.
The above description is only for the preferred embodiment of the present invention, and for those skilled in the art, there are variations on the detailed description and the application scope according to the idea of the present invention, and the content of the description should not be construed as a limitation to the present invention.
Claims (6)
1. The utility model provides a frock of spraying paint to aircraft flap, includes base (10) and rocker (20), its characterized in that: a rocker hole site (30) is arranged at the top of the base, and the rocker is matched in the rocker hole site; the rocker is provided with a positioning structure (21) for fixing the airplane flap.
2. The paint spraying tool according to claim 1, characterized in that: two groups of rocker hole sites (30) are arranged on the base (10), and a rocker (20) is matched in each group of rocker hole sites.
3. The paint spraying tool according to claim 2, characterized in that: the base (10) comprises two base bodies (11) and a connecting rod (12), wherein the two base bodies are respectively arranged at two ends of the connecting rod; the base body comprises a bottom cross rod (13), a pair of support rods (14) arranged on the bottom cross rod, a reinforcing rod (15) connecting the support rods and the bottom cross rod, and a connecting rod (16) connecting the pair of support rods, wherein the top parts of the pair of support rods are provided with rocker hole sites (30); a pair of support rods form a V-shape.
4. The paint spraying tool according to claim 2, characterized in that: each rocker (20) is provided with a stop block which is positioned between a group of two rocker hole sites (30) matched with the rockers.
5. The paint spraying tool according to claim 1, characterized in that: the positioning structure (21) is a bolt hole position arranged on the rocker (20), and the bolt hole position corresponds to the flap mounting hole.
6. The paint spraying tool according to claim 1, characterized in that: one end of the rocker (20) is provided with a handle (22).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921059901.2U CN210449617U (en) | 2019-07-09 | 2019-07-09 | Paint spraying tool for airplane wing flap |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921059901.2U CN210449617U (en) | 2019-07-09 | 2019-07-09 | Paint spraying tool for airplane wing flap |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210449617U true CN210449617U (en) | 2020-05-05 |
Family
ID=70444364
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921059901.2U Active CN210449617U (en) | 2019-07-09 | 2019-07-09 | Paint spraying tool for airplane wing flap |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210449617U (en) |
-
2019
- 2019-07-09 CN CN201921059901.2U patent/CN210449617U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20220210 Address after: 312500 No.1-3 (building 1-5), Aofeng Road, Wozhou Town, Xinchang County, Shaoxing City, Zhejiang Province Patentee after: Zhejiang Wanfeng Aircraft Manufacturing Co.,Ltd. Address before: 312500, No.1, Aofeng Road, Xinchang Industrial Park, Shaoxing City, Zhejiang Province Patentee before: Wanfeng Aircraft Industry Co.,Ltd. |