CN210255809U - Tool for aviation parts - Google Patents
Tool for aviation parts Download PDFInfo
- Publication number
- CN210255809U CN210255809U CN201920698648.9U CN201920698648U CN210255809U CN 210255809 U CN210255809 U CN 210255809U CN 201920698648 U CN201920698648 U CN 201920698648U CN 210255809 U CN210255809 U CN 210255809U
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- positioning
- screw
- platform
- base
- clamping part
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Abstract
The utility model discloses a frock for aviation spare part, include: the positioning device comprises a platform, wherein positioning chutes are formed in the platform, two positioning blocks are arranged in each positioning chute, positioning screws are arranged on the positioning blocks, positioning nuts are sleeved on the positioning screws, a positioning plate is further arranged on the platform, two positioning holes are formed in one side of the positioning plate, a sliding rail is arranged on the other side of the positioning plate, a fixture is arranged on the sliding rail and comprises a base and a clamping part, a second screw hole is formed in the top of the base, a second limiting screw is arranged in the second screw hole, a limiting nut is sleeved on the second limiting screw, and the clamping part is located between the base and the limiting nut; through the position of adjustment locating piece in the location spout to the position of adjustment locating plate on the platform, moreover, the position of anchor clamps and clamping part is nimble adjustable, can press from both sides tightly the aviation spare part of different width, has solved among the prior art and can't press from both sides tight problem to the aviation spare part of difference.
Description
Technical Field
The application relates to the technical field of aviation part machining equipment, in particular to a tool for aviation parts.
Background
In the field of aviation manufacturing, a tool needs to be used for clamping aviation parts, the existing tool comprises a platform and clamping equipment, the aviation parts are placed on the platform, and the aviation parts are clamped through the clamping equipment. However, the shapes of the aviation parts are different, the widths are different, the existing tool cannot clamp different aviation parts, and each aviation part needs a specific tool.
SUMMERY OF THE UTILITY MODEL
An object of this application is to provide a frock for aviation spare part to solve among the prior art and can't press from both sides tight problem to different aviation spare parts.
A tooling for an aerospace component, comprising: the positioning device comprises a platform, wherein two positioning chutes are arranged on the platform, the two positioning chutes are in a T shape, the two positioning chutes are parallel to each other, two positioning blocks are arranged in each positioning chute, the positioning blocks are matched with the positioning chutes, positioning screws are arranged on the positioning blocks, and positioning nuts are sleeved on the positioning screws;
the platform is also provided with two positioning plates, the two positioning plates are positioned between the two positioning chutes, one side of each positioning plate is provided with two positioning holes, the other side of each positioning plate is provided with a slide rail, the positioning holes are sleeved on the positioning screw rods, the positioning plates are positioned between the platform and the positioning nuts, the slide rails are provided with clamps, each clamp comprises a base and a clamping part, one side of the base is provided with a first screw hole, one end of the first screw hole is attached to the slide rail, a first limiting screw rod is arranged in the first screw hole, one end of the first limiting screw rod, which is far away from the slide rails, is provided with a rotating handle, the top of the base is provided with a second screw hole, a second limiting screw rod is arranged in the second screw hole, and a limiting nut is sleeved on the second limiting screw rod, the clamping part is provided with a fixing hole, the fixing hole is sleeved on the second limiting screw rod, and the clamping part is located between the base and the limiting nut.
Optionally, a first gasket is arranged between the positioning nut and the positioning plate.
Optionally, a second gasket is arranged between the limiting nut and the clamping part.
Optionally, one end of the clamping portion, which is far away from the fixing hole, is provided with a rubber anti-slip pad.
The application provides a tool for aviation parts, wherein a positioning plate is arranged between a platform and a positioning nut, and the position of the positioning plate on the platform can be adjusted by adjusting the position of a positioning block in a positioning chute, so that the aviation parts with different widths can be clamped; further, the clamp is arranged on the slide rail and can move on the slide rail, the position of the clamp can be adjusted as required, the first limit screw is used for fixing the clamp, the clamping part is provided with a fixing hole, the fixing hole is sleeved on the second limit screw, the clamping part can rotate in the circumferential direction on the second limit screw, the angle between the clamping part and the base can be adjusted, the limit nut is used for fixing the clamping part, the positions of the clamp and the clamping part are flexible and adjustable, the clamp can be suitable for aviation parts of different sizes, and different aviation parts can be clamped.
Drawings
In order to more clearly explain the technical solution of the present application, the drawings needed to be used in the embodiments will be briefly described below, and it is obvious to those skilled in the art that other drawings can be obtained according to the drawings without any creative effort.
Fig. 1 is a schematic top view of a tooling for an aerospace component according to an embodiment of the present disclosure.
Fig. 2 is a left-side sectional view schematically illustrating a tooling for an aviation component according to an embodiment of the present application.
Fig. 3 is a schematic front cross-sectional view of a tooling for an aviation component according to an embodiment of the present application.
Fig. 4 is an enlarged schematic view of a portion a of fig. 3.
Illustration of the drawings: 1-platform, 2-positioning chute, 3-positioning plate, 4-clamp, 5-first limit screw, 6-second limit screw, 7-first gasket, 8-second gasket, 21-positioning block, 22-positioning screw, 23-positioning nut, 31-positioning hole, 32-sliding rail, 41-base, 42-clamping part, 51-rotating handle, 61-limiting nut, 411-first screw hole, 412-second screw hole, 421-fixing hole, 422-rubber anti-skid pad.
Detailed Description
Examples
Referring to fig. 1 to 4, a tooling for an aviation component according to an embodiment of the present application includes: platform 1 is provided with location spout 2 on the platform 1, and location spout 2 is two, and location spout 2 is the T shape, and is parallel to each other between two location spout 2, all is provided with two locating pieces 21 in every location spout 2, and locating piece 21 and location spout 2 looks adaptation are provided with positioning screw 22 on the locating piece 21, and the cover is equipped with set nut 23 on the positioning screw 22.
The platform 1 is further provided with two positioning plates 3, the positioning plates 3 are positioned between the two positioning chutes 2, one side of each positioning plate 3 is provided with two positioning holes 31, the other side of each positioning plate 3 is provided with a slide rail 32, the positioning holes 31 are sleeved on the positioning screws 22, the positioning plates 3 are positioned between the platform 1 and the positioning nuts 23, the slide rails 32 are provided with clamps 4, each clamp 4 comprises a base 41 and a clamping part 42, one side of the base 41 is provided with a first screw hole 411, one end of the first screw hole 411 is attached to the slide rail 32, a first limit screw 5 is arranged in the first screw hole 411, one end of the first limit screw 5, which is far away from the slide rail 32, is provided with a rotating handle 51, the top of the base 41 is provided with a second screw hole 412, a second limit screw 6 is arranged in the second screw hole 412, the second limit screw 6 is sleeved with a, the fixing hole 421 is sleeved on the second limit screw 6, and the clamping portion 42 is located between the base 41 and the limit nut 61.
The locating piece 21 can move in the locating chute 2, and through locating positioning hole 31 cover on positioning screw 22, make locating plate 3 be located between platform 1 and set nut 23, set nut 23 is used for fixing locating plate 3, can be through the position of adjustment locating piece 21 in locating chute 2 to the position of adjustment locating plate 3 on platform 1 can be realized pressing from both sides the tight aviation spare part of different widths.
Be provided with fixed orifices 421 on the clamping part 42, on second stop screw 6 was located to fixed orifices 421 cover, circumferential direction's rotation can be carried out on second stop screw 6 to clamping part 42 to can adjust the angle between clamping part 42 and the base 41, stop nut 61 is used for fixing clamping part 42, anchor clamps 4 and clamping part 42's position is nimble adjustable, can be applicable to not unidimensional aviation spare part, can press from both sides tightly the aviation spare part of difference.
Optionally, a first gasket 7 is disposed between the positioning nut 23 and the positioning plate 3, and the first gasket 7 plays a role in preventing looseness.
Optionally, a second gasket 8 is disposed between the limiting nut 61 and the clamping portion 42, and the second gasket 8 plays a role in preventing loosening.
Optionally, one end of the clamping portion 42 away from the fixing hole 421 is provided with a rubber non-slip pad 422, and the rubber non-slip pad 422 plays a role in non-slip.
According to the technical scheme, the positioning plate 3 is arranged between the platform 1 and the positioning nut 23, and the position of the positioning plate 3 on the platform can be adjusted by adjusting the position of the positioning block 21 in the positioning chute 2, so that the aviation parts with different widths can be clamped; further, set up anchor clamps 4 on slide rail 32, anchor clamps 4 can move on slide rail 32, can adjust the position of anchor clamps 4 as required, first stop screw 5 is used for fixing anchor clamps 4, be provided with fixed orifices 421 on the clamping part 42, fixed orifices 421 cover are located on second stop screw 6, clamping part 42 can carry out circumferencial direction's rotation on second stop screw 6, thereby can adjust the angle between clamping part 42 and the base 41, stop nut 61 is used for fixing clamping part 42, the position of anchor clamps 4 and clamping part 42 is nimble adjustable, can be applicable to not unidimensional aviation spare part, can press from both sides tightly different aviation spare parts.
In particular, the drawings are only schematic, and for convenience of explanation and explanation of the technical solutions, in the same drawings, a part of the structure is processed by a section, a part of the structure is not processed by a section for convenience of presentation, and in the case that a person skilled in the art can implement the technical solutions by technical means commonly used in the art, a part of the structure not affecting the technical solutions is omitted.
Other embodiments of the invention will be apparent to those skilled in the art from consideration of the specification and practice of the invention disclosed herein. This application is intended to cover any variations, uses, or adaptations of the invention following, in general, the principles of the invention and including such departures from the present disclosure as come within known or customary practice within the art to which the invention pertains. It is intended that the specification and examples be considered as exemplary only, with a true scope and spirit of the invention being indicated by the following claims.
The above embodiments of the present application do not limit the scope of the present application.
Claims (4)
1. The utility model provides a frock for aviation spare part which characterized in that includes: the positioning device comprises a platform (1), wherein two positioning chutes (2) are arranged on the platform (1), the two positioning chutes (2) are T-shaped, the two positioning chutes (2) are parallel to each other, two positioning blocks (21) are arranged in each positioning chute (2), the positioning blocks (21) are matched with the positioning chutes (2), positioning screws (22) are arranged on the positioning blocks (21), and positioning nuts (23) are sleeved on the positioning screws (22); the platform is characterized in that the platform (1) is further provided with two positioning plates (3), the two positioning plates (3) are arranged, the two positioning plates (3) are positioned between the two positioning sliding grooves (2), one side of each positioning plate (3) is provided with two positioning holes (31), the other side of each positioning plate (3) is provided with a sliding rail (32), the positioning holes (31) are sleeved on the positioning screws (22), the positioning plates (3) are positioned between the platform (1) and the positioning nuts (23), the sliding rails (32) are provided with clamps (4), each clamp (4) comprises a base (41) and a clamping part (42), one side of each base (41) is provided with a first screw hole (411), one end of each first screw hole (411) is attached to the corresponding sliding rail (32), and each first screw hole (411) is internally provided with a first limiting screw rod (5), keep away from first stop screw (5) the one end of slide rail (32) is provided with rotates handle (51), the top of base (41) is provided with second screw (412), be provided with second stop screw (6) in second screw (412), the cover is equipped with stop nut (61) on second stop screw (6), be provided with fixed orifices (421) on clamping part (42), fixed orifices (421) cover is located on second stop screw (6), clamping part (42) are located base (41) with between stop nut (61).
2. The tooling for the aeronautical component according to claim 1, wherein a first gasket (7) is arranged between the positioning nut (23) and the positioning plate (3).
3. The tooling for aeronautical parts according to claim 1, characterized in that a second shim (8) is provided between the limit nut (61) and the clamping portion (42).
4. The tooling for the aeronautical component according to claim 1, wherein one end of the clamping portion (42) away from the fixing hole (421) is provided with a rubber anti-skid pad (422).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920698648.9U CN210255809U (en) | 2019-05-15 | 2019-05-15 | Tool for aviation parts |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920698648.9U CN210255809U (en) | 2019-05-15 | 2019-05-15 | Tool for aviation parts |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210255809U true CN210255809U (en) | 2020-04-07 |
Family
ID=70025110
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920698648.9U Expired - Fee Related CN210255809U (en) | 2019-05-15 | 2019-05-15 | Tool for aviation parts |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210255809U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117226549A (en) * | 2023-11-13 | 2023-12-15 | 哈尔滨安宇迪航空工业股份有限公司 | Tool for aviation parts |
-
2019
- 2019-05-15 CN CN201920698648.9U patent/CN210255809U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117226549A (en) * | 2023-11-13 | 2023-12-15 | 哈尔滨安宇迪航空工业股份有限公司 | Tool for aviation parts |
| CN117226549B (en) * | 2023-11-13 | 2024-01-26 | 哈尔滨安宇迪航空工业股份有限公司 | Tool for aviation parts |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200407 Termination date: 20210515 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |