CN213319739U - Flexible tool for detecting and processing profile of aircraft wing wallboard - Google Patents
Flexible tool for detecting and processing profile of aircraft wing wallboard Download PDFInfo
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- CN213319739U CN213319739U CN202021915329.8U CN202021915329U CN213319739U CN 213319739 U CN213319739 U CN 213319739U CN 202021915329 U CN202021915329 U CN 202021915329U CN 213319739 U CN213319739 U CN 213319739U
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- 238000001514 detection method Methods 0.000 claims description 2
- 239000006096 absorbing agent Substances 0.000 claims 1
- 239000000463 material Substances 0.000 abstract description 5
- 238000009434 installation Methods 0.000 abstract 2
- 239000002131 composite material Substances 0.000 description 24
- 238000004519 manufacturing process Methods 0.000 description 5
- 238000000034 method Methods 0.000 description 5
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
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Abstract
The utility model discloses an aircraft wing wallboard shape face detects flexible frock of processing relates to flexible frock technical field for the wing processing, including base, slide rail, support frame, servo electric cylinder, first movable block, electronic jar, flexible post, first servo motor, first lead screw, second movable block, first installation piece, second servo motor, second lead screw, first auxiliary rod, third movable block, first grip block, second installation piece, third servo motor, third lead screw, second auxiliary rod, fourth movable block, flexible motor and baffle. The utility model discloses a set up first lead screw and second lead screw, can adjust wing combined material's height at any time in a flexible way, adapt to the processing demand of different wings, through setting up third servo motor and fourth movable block, fix the support frame, reduce the probability that takes place the skew between electronic jar of device during operation and the wing combined material, guaranteed the accuracy nature of device during operation.
Description
Technical Field
The utility model relates to a wing processing specifically is an aircraft wing wallboard profile detects flexible frock of processing with flexible frock technical field.
Background
Because the aircraft flies in the air and has high speed, each part on the aircraft needs to have good strength and rigidity so as to bear huge aerodynamic load and ensure the flight safety of the aircraft. The composite material of the airplane wing is an important ring in the manufacturing link of the airplane, the shape of the composite material is complex, the composite material is generally composed of multiple curved surfaces, and the composite material is difficult to manufacture and mold. The method dynamically generates required tool positioning through means of adjustment, control and the like, and is called as a flexible tool. The flexible tool can avoid designing and manufacturing special fixed frames and clamps for assembling various parts, can reduce the manufacturing cost of the tool, shorten the preparation period of the tool, reduce the production land and greatly improve the assembly productivity.
The existing flexible tool for detecting and processing the profile of the wing panel of the airplane has a single fixed position for wing composite materials, and the adjustment mode is not flexible enough, so that the processing requirements of different wings are difficult to meet.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a flexible frock of aircraft wing wallboard shape face detection processing to solve the problem that proposes among the above-mentioned background art.
In order to solve the technical problem, the utility model provides a following technical scheme: a flexible tool for detecting and processing the profile of an airplane wing wall panel comprises a base, slide rails are symmetrically arranged on two sides of the top of the base, a plurality of support frames which are connected in a sliding mode are arranged on the tops of the slide rails, a servo electric cylinder is arranged in the center of the top of each support frame, a first moving block is sleeved on an output shaft of the servo electric cylinder on the inner side of each support frame, a plurality of electric cylinders are arranged at the bottom of each first moving block, a plurality of telescopic columns are arranged on the top of the base, a plurality of first servo motors are symmetrically arranged on two sides of the outer wall of each slide rail, a first lead screw is sleeved on an output shaft of each first servo motor, one end of each first lead screw extends between the two slide rails, a second moving block is sleeved on the outer wall of each first lead screw in a matching mode, the second moving block is connected with the top of the, a second lead screw is sleeved on the output shaft of the second servo motor, one end of the second lead screw extends to the bottom of the inner side of the first mounting block, a first auxiliary rod is arranged on one side of the second lead screw on the inner wall of the first mounting block, the second lead screw and the first auxiliary rod are movably sleeved with a same third moving block, a telescopic motor is arranged in the third moving block, a first clamping block is sleeved on the upper portion of the third moving block on the output shaft of the telescopic motor, a second clamping block matched with the first clamping block is arranged on one side of the third moving block away from the first servo motor, second mounting blocks are symmetrically arranged at the bottoms of two sides of the outer wall of the support frame, a third servo motor is arranged at the top of the second mounting block, a third lead screw is sleeved on the output end of the third servo motor, one end of the third lead screw extends to the lower portion of the base, and a second auxiliary rod is arranged at the bottom of the second mounting block on one side, the third screw rod and the second auxiliary rod are movably sleeved with a same fourth moving block, and the fourth moving block is located below the base.
Furthermore, the top of the telescopic column is provided with a sucker, the sucker is parallel to the base, and the contact between the sucker and the bottom of the composite material ensures the stability of the composite material during processing.
Furthermore, the top of the base is provided with a sliding groove matched with the second moving block, so that the moving range of the second moving block is limited, and the stability of the second moving block during movement is ensured.
Furthermore, the first auxiliary rod is connected with the third moving block in a sliding mode, a first lead screw nut is arranged inside the third moving block, and the first lead screw nut is matched with the second lead screw, so that the stability of the third moving block during movement is guaranteed.
Furthermore, the second auxiliary rod is connected with the fourth moving block in a sliding mode, a second lead screw nut is arranged inside the fourth moving block, and the second lead screw nut is matched with the third lead screw, so that the stability of the fourth moving block during movement is guaranteed.
Furthermore, the rubber block is arranged on one side, adjacent to the outer wall of the second clamping block, of the first clamping block, friction force between the device and the composite material is increased through the rubber block, and stability during clamping is guaranteed.
Furthermore, a baffle is arranged on one side of the base and is perpendicular to the base, so that the movement of the composite material is limited, and the stability of the device during operation is ensured.
Furthermore, a limiting block is arranged at the bottom end of the second auxiliary rod, and safety of the device in operation is guaranteed by limiting the movement range of the fourth moving block.
Compared with the prior art, the utility model discloses the beneficial effect who reaches is:
1. the utility model discloses a set up first servo motor, first lead screw, second movable block, second servo motor, second lead screw, first grip block and second grip block, when work goes on, can adjust wing combined material's height at any time in a flexible way, adapt to the processing demand of different wings.
2. The utility model discloses a set up third servo motor, third lead screw, second auxiliary rod and fourth movable block, fix to the support frame, reduce the probability that takes place the skew between electronic jar of device during operation and the wing combined material, guaranteed the accuracy nature of device during operation.
Drawings
The accompanying drawings are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention, and together with the description serve to explain the invention and not to limit the invention. In the drawings:
FIG. 1 is a front cross-sectional view of the present invention in its entirety;
FIG. 2 is an enlarged schematic view of the present invention at A in FIG. 1;
fig. 3 is a side view of the utility model in its entirety;
fig. 4 is an enlarged schematic view of fig. 1 at B according to the present invention;
in the figure: 1, a base; 2, a slide rail; 3, supporting a frame; 4, servo electric cylinder; 5 a first moving block; 6 electric cylinders; 7, a telescopic column; 8 a first servo motor; 9 a first lead screw; 10 a second moving block; 11 a first mounting block; 12 a second servo motor; 13 a second lead screw; 14 a first auxiliary lever; 15 a third moving block; 16 a first clamping block; 17 a second clamping block; 18 a second mounting block; 19 a third servo motor; 20 a third screw rod; 21 a second auxiliary lever; 22 a fourth moving block; 23 a telescopic motor; 24 baffle.
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. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-4, the present invention provides a technical solution: a flexible tool for detecting and processing the profile of an airplane wing wall panel comprises a base 1, slide rails 2 are symmetrically arranged on two sides of the top of the base 1, a plurality of support frames 3 which are connected in a sliding mode are arranged on the top of each slide rail 2, a servo electric cylinder 4 is arranged in the center of the top of each support frame 3, a first moving block 5 is sleeved on the inner side of each support frame 3 through an output shaft of each servo electric cylinder 4, a plurality of electric cylinders 6 are arranged at the bottom of each first moving block 5, a plurality of telescopic columns 7 are arranged on the top of the base 1, a plurality of first servo motors 8 are symmetrically arranged on two sides of the outer wall of each slide rail 2, a first lead screw 9 is sleeved on the output shaft of each first servo motor 8, one end of each first lead screw 9 extends to a position between every two slide rails 2, a second moving block 10 is sleeved on the, the top of the second moving block 10 is provided with a first mounting block 11, the top of the first mounting block 11 is provided with a second servo motor 12, an output shaft of the second servo motor 12 is sleeved with a second lead screw 13, one end of the second lead screw 13 extends to the bottom of the inner side of the first mounting block 11, a first auxiliary rod 14 is arranged on one side of the second lead screw 13 on the inner wall of the first mounting block 11, a same third moving block 15 is movably sleeved on the second lead screw 13 and the first auxiliary rod 14, a telescopic motor 23 is arranged inside the third moving block 15, a first clamping block 16 is sleeved on an output shaft of the telescopic motor 23 above the third moving block 15, and a second clamping block 17 matched with the first clamping block 16 is arranged on one side of the third moving block 15 far away from the first servo motor 8.
The top of the telescopic column 7 is provided with a sucker which is parallel to the base 1, and the contact between the sucker and the bottom of the composite material ensures the stability of the composite material during processing.
The top of the base 1 is provided with a sliding groove matched with the second moving block 10, so that the moving range of the second moving block 10 is limited, and the stability of the second moving block 10 during movement is ensured.
The first auxiliary rod 14 is slidably connected with the third moving block 15, a first lead screw nut is arranged inside the third moving block 15, and the first lead screw nut is matched with the second lead screw 13, so that the stability of the third moving block 15 during movement is ensured.
The rubber blocks are arranged on one sides, adjacent to the outer walls of the first clamping block 16 and the second clamping block 17, of the rubber blocks, friction force between the device and a composite material is increased, and stability during clamping is guaranteed.
A baffle 24 is arranged on one side of the base 1, the baffle 24 is perpendicular to the base 1, movement of the composite material is limited, and stability of the device in operation is guaranteed.
The implementation mode is specifically as follows: when the airplane wing composite material clamping device is used, the airplane wing composite material is placed above the telescopic column 7 through the arrangement of the first servo motor 8, the first lead screw 9, the second moving block 10, the second servo motor 12, the second lead screw 13, the first clamping block 16 and the second clamping block 17, the first servo motor 8 works to drive the first lead screw 9 to rotate, the first lead screw 9 and the second moving block 10 rotate relatively to drive the second moving block 10 to move along the direction of the first lead screw 9, the second servo motor 12 works to drive the second lead screw 13 to rotate, the third moving block 15 and the second lead screw 13 rotate relatively to drive the third moving block 15 to move along the direction of the first auxiliary rod 14, the telescopic motor 23 works to drive the first clamping block 16 to move, the airplane wing composite material is clamped between the first clamping block 16 and the second clamping block 17, the servo cylinder 4 works to drive the first moving block 5 to move, the electric cylinder 6 moves along with the first moving block 5, different pressures are applied to the composite material of the airplane wing, flexible tooling work is carried out on the composite material, and the height of the composite material of the airplane wing can be flexibly adjusted at any time when the composite material of the airplane wing works, so that the composite material of the airplane wing can meet the processing requirements of different wings.
Referring to fig. 1 and 3, the present invention provides a technical solution: the flexible tool for detecting and processing the profile of the wall plate of the airplane wing further comprises second mounting blocks 18 symmetrically arranged at the bottoms of the two sides of the outer wall of the support frame 3, a third servo motor 19 is arranged at the top of each second mounting block 18, a third lead screw 20 is sleeved at the output end of the third servo motor 19, one end of the third lead screw 20 extends to the lower portion of the base 1, a second auxiliary rod 21 is arranged at one side of the third lead screw 20 at the bottom of each second mounting block 18, a same fourth moving block 22 is movably sleeved on the third lead screw 20 and the second auxiliary rod 21, and the fourth moving block 22 is located below the base 1.
The second auxiliary rod 21 is slidably connected with the fourth moving block 22, a second lead screw nut is arranged inside the fourth moving block 22, and the second lead screw nut is matched with the third lead screw 20, so that the stability of the fourth moving block 22 during movement is ensured.
The bottom end of the second auxiliary rod 21 is provided with a limiting block, and the safety of the device in operation is ensured by limiting the movement range of the fourth moving block 22.
The implementation mode is specifically as follows: during the use, through setting up third servo motor 19, third lead screw 20, second auxiliary rod 21 and fourth movable block 22, support frame 3 slides on slide rail 2, when sliding to required position, third servo motor 19 work, drive third lead screw 20 and rotate, third lead screw 20 and fourth movable block 22 rotate relatively, drive fourth movable block 22 and carry out the motion along the direction of second auxiliary rod 21, stop when moving to fourth movable block 22 top in close contact with base 1 bottom, fix support frame 3, reduce the probability that takes place the skew between electronic jar 6 and the combined material during device work, the accuracy of device during operation has been guaranteed.
The utility model discloses a theory of operation:
referring to the attached drawings 1-4 in the specification, by arranging the first servo motor 8, the first lead screw 9, the second moving block 10, the second servo motor 12, the second lead screw 13, the first clamping block 16 and the second clamping block 17, the height of the composite material of the wing can be flexibly adjusted at any time during work, so that the composite material of the wing can meet the processing requirements of different wings.
Further, referring to the attached drawings 1 and 3 of the specification, the supporting frame 3 is fixed by arranging a third servo motor 19, a third screw rod 20, a second auxiliary rod 21 and a fourth moving block 22, so that the probability of deviation between the electric cylinder 6 and a wing composite material when the device works is reduced, and the accuracy of the device in working is ensured.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments described in the foregoing embodiments, or equivalents may be substituted for elements thereof. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (8)
1. The utility model provides a flexible frock of aircraft wing wallboard shape face detection processing, includes base (1), its characterized in that: the sliding rail type electric shock absorber is characterized in that sliding rails (2) are symmetrically arranged on two sides of the top of the base (1), a plurality of support frames (3) which are connected in a sliding mode are arranged on the top of each sliding rail (2), a servo electric cylinder (4) is arranged in the center of the top of each support frame (3), a first moving block (5) is sleeved on the inner side of each support frame (3) through an output shaft of each servo electric cylinder (4), a plurality of electric cylinders (6) are arranged at the bottom of each first moving block (5), a plurality of telescopic columns (7) are arranged on the top of the base (1), a plurality of first servo motors (8) are symmetrically arranged on two sides of the outer wall of each sliding rail (2), a first lead screw (9) is sleeved on the output shaft of each first servo motor (8), one end of each first lead screw (9) extends to a position between the two sliding rails (2), a second moving block (10) is sleeved on, a first mounting block (11) is arranged at the top of the second moving block (10), a second servo motor (12) is arranged at the top of the first mounting block (11), a second lead screw (13) is sleeved on an output shaft of the second servo motor (12), one end of the second lead screw (13) extends to the bottom of the inner side of the first mounting block (11), a first auxiliary rod (14) is arranged on one side of the second lead screw (13) on the inner wall of the first mounting block (11), a same third moving block (15) is movably sleeved on the second lead screw (13) and the first auxiliary rod (14), a telescopic motor (23) is arranged inside the third moving block (15), a first clamping block (16) is sleeved on the upper portion of the output shaft of the telescopic motor (23) above the third moving block (15), and a second clamping block (17) matched with the first clamping block (16) is arranged on one side of the third moving block (15) far away from the first servo motor (8), the novel support is characterized in that second mounting blocks (18) are symmetrically arranged at the bottoms of the two sides of the outer wall of the support frame (3), a third servo motor (19) is arranged at the top of each second mounting block (18), a third lead screw (20) is sleeved at the output end of the third servo motor (19), one end of the third lead screw (20) extends to the position below the base (1), a second auxiliary rod (21) is arranged at one side of the third lead screw (20) at the bottom of each second mounting block (18), a same fourth moving block (22) is movably sleeved on the third lead screw (20) and the second auxiliary rod (21), and the fourth moving block (22) is located below the base (1).
2. The flexible tool for detecting and processing the shape of the wall plate of the airplane wing according to claim 1, wherein the flexible tool comprises: the top of the telescopic column (7) is provided with a sucker which is parallel to the base (1).
3. The flexible tool for detecting and processing the shape of the wall plate of the airplane wing according to claim 1, wherein the flexible tool comprises: the top of the base (1) is provided with a sliding groove matched with the second moving block (10).
4. The flexible tool for detecting and processing the shape of the wall plate of the airplane wing according to claim 1, wherein the flexible tool comprises: the first auxiliary rod (14) is connected with the third moving block (15) in a sliding mode, a first lead screw nut is arranged inside the third moving block (15), and the first lead screw nut is matched with the second lead screw (13).
5. The flexible tool for detecting and processing the shape of the wall plate of the airplane wing according to claim 1, wherein the flexible tool comprises: the second auxiliary rod (21) is connected with the fourth moving block (22) in a sliding mode, a second lead screw nut is arranged inside the fourth moving block (22), and the second lead screw nut is matched with the third lead screw (20).
6. The flexible tool for detecting and processing the shape of the wall plate of the airplane wing according to claim 1, wherein the flexible tool comprises: and a rubber block is arranged on one side of the first clamping block (16) adjacent to the outer wall of the second clamping block (17).
7. The flexible tool for detecting and processing the shape of the wall plate of the airplane wing according to claim 1, wherein the flexible tool comprises: one side of the base (1) is provided with a baffle (24), and the baffle (24) is perpendicular to the base (1).
8. The flexible tool for detecting and processing the shape of the wall plate of the airplane wing according to claim 1, wherein the flexible tool comprises: the bottom end of the second auxiliary rod (21) is provided with a limiting block.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021915329.8U CN213319739U (en) | 2020-09-04 | 2020-09-04 | Flexible tool for detecting and processing profile of aircraft wing wallboard |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021915329.8U CN213319739U (en) | 2020-09-04 | 2020-09-04 | Flexible tool for detecting and processing profile of aircraft wing wallboard |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN213319739U true CN213319739U (en) | 2021-06-01 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021915329.8U Active CN213319739U (en) | 2020-09-04 | 2020-09-04 | Flexible tool for detecting and processing profile of aircraft wing wallboard |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN213319739U (en) |
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2020
- 2020-09-04 CN CN202021915329.8U patent/CN213319739U/en active Active
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| Date | Code | Title | Description |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP01 | Change in the name or title of a patent holder |
Address after: No.23, Hongbin Road, Yuhong District, Shenyang City, Liaoning Province Patentee after: Liaoning Huatian Aviation Technology Co.,Ltd. Address before: No.23, Hongbin Road, Yuhong District, Shenyang City, Liaoning Province Patentee before: SHENZHEN HUATIAN AVIATION MACHINERY CO.,LTD. |
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| CP01 | Change in the name or title of a patent holder |