CN215146943U - Processing tool for airplane slide rail rib parts - Google Patents
Processing tool for airplane slide rail rib parts Download PDFInfo
- Publication number
- CN215146943U CN215146943U CN202121055711.0U CN202121055711U CN215146943U CN 215146943 U CN215146943 U CN 215146943U CN 202121055711 U CN202121055711 U CN 202121055711U CN 215146943 U CN215146943 U CN 215146943U
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- China
- Prior art keywords
- slide rail
- rail rib
- screw
- anchor clamps
- rib
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Abstract
The utility model relates to a processing frock technical field just discloses an aircraft slide rail rib parts machining frock, including anchor clamps platform and slide rail rib, the inside of anchor clamps platform is equipped with two U type supporting seats, the slide rail rib is and transversely is located two the inside of U type supporting seat, the both sides of U type supporting seat all are equipped with and are used for the fixture fixed with the slide rail rib, the equal screw thread in the left and right sides of anchor clamps platform is provided with first screw rod, the fixed removal seat that sets up with first screw rod screw thread that is equipped with in bottom of U type supporting seat, the one end of first screw rod extends to the outside of anchor clamps platform and fixes and be equipped with first rocking handle. The utility model discloses convenient operation is convenient for accomplish the clamping to the slide rail rib, and easily adjusts the flexible position of slide rail rib, has improved the machining efficiency of slide rail rib.
Description
Technical Field
The utility model relates to a processing frock technical field especially relates to an aircraft slide rail rib parts machining frock.
Background
The existing machining clamp for the sliding rail rib part of the airplane is convenient for machining the sliding rail rib part, but the clamping effect of the machining clamp for the sliding rail rib part of the airplane is not strong in the actual using process, and the machining of the part is possibly inaccurate due to slight movement under the condition that precise machining is needed, so that the assembly failure of the airplane is caused. Wherein patent number is CN208629312U, discloses an aircraft slide rail rib part machining frock, including anchor clamps platform and first slide rail, the positive fixedly connected with fixed block of anchor clamps platform, the inside swing joint of fixed block has the pivot, the outside swing joint of pivot has the clamp plate, the bottom fixedly connected with fixture block of clamp plate, the positive fixedly connected with joint piece of anchor clamps platform, joint piece and fixture block joint, the left side fixedly connected with auxiliary block of first slide rail, auxiliary block contacts with the clamp plate, the hole has been seted up in the front of first slide rail, the rightmost side hole inside threaded connection has set screw, the fixed slot has been seted up in the front of anchor clamps platform, fixed slot and set screw threaded connection, the first curb plate of positive fixedly connected with of anchor clamps platform.
Although the slide rail rib can be stably clamped in the scheme, the position of the slide rail rib is fixed by the aid of the screw, and the telescopic position needs to be adjusted continuously in the machining process, so that the operation is complex, and the machining efficiency of parts is reduced.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving and having adopted the screw among the prior art with slide rail rib position fixing, but need not stop in the course of working make flexible position control, will cause the phenomenon of operation complicacy like this, reduced the machining efficiency's of part problem, and the aircraft slide rail rib spot facing work frock that proposes.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
the utility model provides an aircraft slide rail rib parts machining frock, includes anchor clamps platform and slide rail rib, the inside of anchor clamps platform is equipped with two U type supporting seats, the slide rail rib is transversely to be located two the inside of U type supporting seat, the both sides of U type supporting seat all are equipped with and are used for the fixture fixed with the slide rail rib, the equal screw thread in the left and right sides of anchor clamps platform is provided with first screw rod, the fixed removal seat that sets up with first screw rod screw thread that is equipped with in bottom of U type supporting seat, the one end of first screw rod extends to the outside of anchor clamps platform and fixes and be equipped with first rocking handle.
Preferably, fixture includes second screw rod, splint and second rocking handle, second screw rod screw thread sets up on the lateral wall of U type supporting seat, the lateral wall of splint rotates and sets up on one end of second screw rod, the other end of second screw rod extends to the outside of U type supporting seat and fixes and be equipped with the second rocking handle.
Preferably, the side wall of the clamp table is provided with a strip-shaped opening for the second screw to extend out.
Preferably, the two U-shaped supporting seats positioned inside the fixture table are arranged at different heights.
Preferably, the top of the jig table is provided with scale marks along the length direction thereof.
Preferably, the slide rail ribs are respectively provided with three sections, and the sizes of the sections of the slide rail ribs are different.
Compared with the prior art, the utility model provides an aircraft slide rail rib parts machining frock possesses following beneficial effect:
this aircraft slide rail rib parts machining frock, through setting up the second screw rod in U type supporting seat is inside, splint and second rocking handle, can clip the both sides of slide rail rib to can fix the slide rail rib clamping in the inside of U type supporting seat, through setting up the first screw rod and the removal seat in anchor clamps platform both sides, can adjust the position of U type supporting seat in anchor clamps platform is inside, thereby can adjust the flexible position of slide rail rib, and then can accomplish the quick clamping to the slide rail rib, the machining efficiency of slide rail rib has been improved.
The part that does not relate to among the device all is the same with prior art or can adopt prior art to realize, the utility model discloses convenient operation is convenient for accomplish the clamping to the slide rail rib, and easily adjusts the flexible position of slide rail rib, has improved the machining efficiency of slide rail rib.
Drawings
Fig. 1 is a top view of the tooling for machining a rib part of an aircraft slide rail provided by the present invention;
fig. 2 is the utility model provides an elevation of aircraft slide rail rib parts machining frock.
In the figure: 1 anchor clamps platform, 2 slide rail ribs, 3U type supporting seat, 4 first screws, 5 remove the seat, 6 first rocking handles, 7 second screws, 8 splint, 9 second rocking handles, 10 bar mouths, 11 scale marks.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments.
In the description of the present invention, it is to be understood that the terms "upper", "lower", "front", "rear", "left", "right", "top", "bottom", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplicity of description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention.
Referring to fig. 1-2, an aircraft slide rail rib part processing tool comprises an anchor clamps platform 1 and slide rail ribs 2, the slide rail ribs 2 are respectively provided with three sections, each section of the slide rail ribs 2 is different in size, two U-shaped supporting seats 3 are arranged inside the anchor clamps platform 1, the slide rail ribs 2 are transversely arranged inside the two U-shaped supporting seats 3, clamping mechanisms used for fixing the slide rail ribs 2 are arranged on two sides of each U-shaped supporting seat 3, first screw rods 4 are arranged on the left side and the right side of the anchor clamps platform 1 in a threaded mode, a moving seat 5 in threaded arrangement with the first screw rods 4 is fixedly arranged at the bottom of each U-shaped supporting seat 3, and one ends of the first screw rods 4 extend to the outside of the anchor clamps platform 1 and are fixedly provided with first rocking handles 6.
The clamping mechanism comprises a second screw 7, a clamping plate 8 and a second rocking handle 9, the second screw 7 is arranged on the side wall of the U-shaped supporting seat 3 in a threaded mode, the side wall of the clamping plate 8 is arranged at one end of the second screw 7 in a rotating mode, and the other end of the second screw 7 extends to the outside of the U-shaped supporting seat 3 and is fixedly provided with the second rocking handle 9.
The side wall of the fixture table 1 is provided with a strip-shaped opening 10 for extending the second screw 7, so that the second screw 7 can be ensured to pass through and move in the horizontal direction.
Two U type supporting seats 3 that are located inside the anchor clamps platform 1 are the difference setting of height, because every section size of slide rail rib 2 is different, consequently the design here can guarantee effectively to hold up slide rail rib 2 and fix its clamping.
The top of the fixture table 1 is provided with scale marks 11 along the length direction, so that the staff can observe the telescopic length of the slide rail rib 2 conveniently.
The utility model discloses in, during the use, the staff puts into the inside at 1 inside two U type supporting seats 3 of anchor clamps platform with slide rail rib 2, then the hand rotates second rocking handle 9 and makes second screw rod 7 rotatory and promote splint 8 and remove, make splint 8 and slide rail rib 2's lateral wall counterbalance contact, thereby can accomplish the quick installation to slide rail rib 2, when the flexible position of slide rail rib 2 needs to be adjusted, staff's hand rotates first rocking handle 6 and makes first screw rod 4 rotatory and drive removal seat 5 move in the inside of anchor clamps platform 1, thereby can adjust slide rail rib 2's flexible position, because here is the mode that adopts screw drive, can ensure the steadiness of the clamping of slide rail rib 2, the machining precision and the efficiency of slide rail rib 2 have been improved.
The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.
Claims (6)
1. The utility model provides an aircraft slide rail rib parts machining frock, includes anchor clamps platform (1) and slide rail rib (2), its characterized in that, the inside of anchor clamps platform (1) is equipped with two U type supporting seats (3), slide rail rib (2) are transversely to be located two the inside of U type supporting seat (3), the both sides of U type supporting seat (3) all are equipped with and are used for the fixture fixed with slide rail rib (2), the equal screw thread in both sides is provided with first screw rod (4) about anchor clamps platform (1), the fixed removal seat (5) that are equipped with first screw rod (4) screw thread setting in bottom of U type supporting seat (3), the one end of first screw rod (4) extends to the outside of anchor clamps platform (1) and is fixed and is equipped with first rocking handle (6).
2. The processing tool for the rib part of the aircraft slide rail according to claim 1, wherein the clamping mechanism comprises a second screw (7), a clamping plate (8) and a second rocking handle (9), the second screw (7) is arranged on the side wall of the U-shaped supporting seat (3) in a threaded manner, the side wall of the clamping plate (8) is arranged on one end of the second screw (7) in a rotating manner, and the other end of the second screw (7) extends to the outside of the U-shaped supporting seat (3) and is fixedly provided with the second rocking handle (9).
3. The processing tool for the aircraft slide rail rib part according to claim 2, characterized in that a strip-shaped opening (10) for extending the second screw (7) is formed in the side wall of the clamp table (1).
4. The processing tool for the rib part of the aircraft slide rail according to claim 1, wherein the two U-shaped supporting seats (3) positioned inside the fixture table (1) are arranged at different heights.
5. The processing tool for the rib part of the aircraft slide rail according to claim 1, wherein the top of the clamp table (1) is provided with scale marks (11) along the length direction of the clamp table.
6. The aircraft sliding rail rib part machining tool according to claim 1 is characterized in that the sliding rail ribs (2) are respectively provided with three sections, and the sizes of the sections of the sliding rail ribs (2) are different.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121055711.0U CN215146943U (en) | 2021-05-18 | 2021-05-18 | Processing tool for airplane slide rail rib parts |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121055711.0U CN215146943U (en) | 2021-05-18 | 2021-05-18 | Processing tool for airplane slide rail rib parts |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215146943U true CN215146943U (en) | 2021-12-14 |
Family
ID=79370744
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121055711.0U Active CN215146943U (en) | 2021-05-18 | 2021-05-18 | Processing tool for airplane slide rail rib parts |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215146943U (en) |
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2021
- 2021-05-18 CN CN202121055711.0U patent/CN215146943U/en active Active
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