CN212683679U - Multi-station automatic clamp for long beam of airplane - Google Patents
Multi-station automatic clamp for long beam of airplane Download PDFInfo
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- CN212683679U CN212683679U CN202021212273.XU CN202021212273U CN212683679U CN 212683679 U CN212683679 U CN 212683679U CN 202021212273 U CN202021212273 U CN 202021212273U CN 212683679 U CN212683679 U CN 212683679U
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Abstract
The utility model provides an automatic anchor clamps of long roof beam multistation of aircraft. Automatic anchor clamps of long roof beam multistation of aircraft include: mounting blocks; the fixing block is arranged on one side of the mounting block; the square block is fixedly arranged on the outer wall of one side of the fixed block; the rotating rod is rotatably arranged on the square block; the first motor is fixedly arranged at the top of the square block; the first gear is fixedly sleeved on the rotating rod; and the second gear is fixedly arranged on the output shaft of the first motor and is meshed with the first gear. The utility model provides an automatic anchor clamps of long roof beam multistation of aircraft has the centre gripping of carrying out perpendicular or level and inclined position to the aircraft roof beam, uses manpower sparingly, the advantage to the aircraft roof beam protection among the clamping process.
Description
Technical Field
The utility model relates to an aircraft length roof beam anchor clamps technical field especially relates to an aircraft length roof beam multistation automatic clamp.
Background
With the rapid development of the modern aviation industry and the acceleration of the modernization process of our country, the aviation manufacturing industry is rapidly developed under the modern high-tech conditions, and generally, the aircraft manufacturing only refers to the manufacturing of parts of an aircraft body, the assembly of parts, the general assembly of a whole machine and the like. Other parts of the aircraft, such as aircraft engines, instruments, onboard equipment, hydraulic systems and accessories, etc., are manufactured by specialized factories and are not included in the aircraft manufacturing scope.
The quality and automation of structural parts of an airplane are always difficult problems to solve in the aviation industry, and most of the structural parts are manually clamped on workpieces, so that the time and the labor are consumed, and the structural parts of the airplane are possibly damaged.
Therefore, it is necessary to provide a multi-station automatic clamp for long beams of airplanes to solve the above technical problems.
SUMMERY OF THE UTILITY MODEL
The utility model provides a technical problem provide a have the centre gripping of carrying out perpendicular or level and inclined position to the aircraft roof beam, use manpower sparingly, the aircraft long beam multistation automatic clamp to the aircraft roof beam protection among the clamping process.
In order to solve the technical problem, the utility model provides an automatic anchor clamps of long roof beam multistation of aircraft, include: mounting blocks; the fixing block is arranged on one side of the mounting block; the square block is fixedly arranged on the outer wall of one side of the fixed block; the rotating rod is rotatably arranged on the square block; the first motor is fixedly arranged at the top of the square block; the first gear is fixedly sleeved on the rotating rod; the second gear is fixedly arranged on an output shaft of the first motor and is meshed with the first gear; the stabilizing block is fixedly arranged at one end of the rotating rod, which is far away from the fixing block; the first sliding groove is formed in the outer wall of one side of the stabilizing block; the round rod is fixedly arranged in the first sliding groove; the hydraulic cylinder is fixedly arranged at the top of the stabilizing block; the first clamping block is slidably mounted on the round rod, and the top of the first clamping block is fixedly connected with the output shaft of the hydraulic cylinder; the cavity is arranged in the first clamping block; the sliding rod is slidably mounted in the cavity, and two ends of the sliding rod extend out of the first clamping block; the steel ring is arranged in the cavity and fixedly sleeved on the sliding rod; the spring is fixedly arranged in the cavity, the spring is movably sleeved on the sliding rod, the bottom end of the spring is fixedly arranged at the top of the steel ring, and the top end of the spring is fixedly arranged on the inner wall of the top of the cavity; the second clamping block is fixedly arranged on the outer wall of one side of the stabilizing block; the connecting block is fixedly arranged at the top of the second clamping block; and the two arc-shaped chucks are fixedly arranged at the bottom end of the sliding rod and the top of the connecting block respectively.
Preferably, arc-shaped rubber protection pads are installed in the two arc-shaped chucks.
Preferably, a through hole is formed in the top of the first clamping block, a ball is movably embedded in the through hole, and the round rod penetrates through the through hole and is in contact with the ball.
Preferably, the outer wall of one side of the mounting block is fixedly connected with the outer wall of one side of the fixing block.
Preferably, the fixed block activity sets up one side of installation piece, the second spout has been seted up on one side outer wall of fixed block, fixed mounting has the dead lever in the second spout, the top of installation piece is seted up flutedly, slidable mounting has the slider on the dead lever, the screwed pipe is installed in the installation piece rotation, the one end of screwed pipe extends to in the recess, the threaded rod is installed to the screwed pipe internal thread, the one end of threaded rod extends to in the recess and fixed mounting has first articulated piece, first articulated piece with one side outer wall of slider is articulated mutually, fixed cover is equipped with the third gear on the screwed pipe, the top fixed mounting of installation piece has the second motor, fixed mounting has the fourth gear on the output shaft of second motor, the fourth gear with the third gear meshes mutually.
Preferably, a square groove is formed in the outer wall of one side of the mounting block, a second hinge block is fixedly mounted on the inner wall of one side of the square groove, and the second hinge block is hinged to the outer wall of one side of the fixing block.
Preferably, one end of the threaded rod is fixedly provided with a limiting block.
Compared with the prior art, the utility model provides an automatic anchor clamps of long roof beam multistation of aircraft has following beneficial effect:
the utility model provides an airplane long beam multi-station automatic clamp, a first motor is started to drive a second gear, the first gear rotates and a rotating rod rotates, the rotating rod drives a stabilizing block to rotate by different angles, the automatic clamp has the advantage of vertical or horizontal clamping of an airplane beam, a hydraulic cylinder is started to drive a first clamping block to slide downwards, when an arc rubber protection pad in an arc clamping head touches a flying frame, the arc clamping head at the bottom of a sliding rod drives the sliding rod and a steel ring to slide upwards under the action of pressure to extrude a spring, the spring and the arc rubber protection pad have certain elasticity while tightening the flying frame, the airplane frame can be protected, the automatic clamp has the function of protecting the airplane beam in the clamping process, when clamping of an inclination angle of some workpieces or airplane beams is desired, the second motor is started to drive a fourth gear, a third gear and a screwed pipe rotate, the screwed pipe drives a threaded rod to move left and right, can produce thrust to promote the slider and upwards or the lapse, through the articulated of activity, can make the fixed block form a firm angle, make the arc chuck can carry out the centre gripping of some inclination by work piece or aircraft roof beam, have the inclined position centre gripping and use manpower sparingly advantage.
Drawings
Fig. 1 is a schematic front view of a first embodiment of the multi-station automatic clamp for a long beam of an airplane according to the present invention;
fig. 2 is a schematic front view of a second embodiment of the multi-station automatic clamp for a long beam of an airplane according to the present invention;
FIG. 3 is an enlarged schematic view of portion A shown in FIG. 2;
reference numbers in the figures: 1. mounting blocks; 2. a fixed block; 3. a square block; 4. rotating the rod; 5. a first motor; 6. a first gear; 7. a second gear; 8. a stabilizing block; 9. a first chute; 10. a round bar; 11. a hydraulic cylinder; 12. a first clamping block; 13. a cavity; 14. a slide bar; 15. steel rings; 16. a spring; 17. a second clamp block; 18. connecting blocks; 19. an arc-shaped chuck; 20. a second chute; 21. fixing the rod; 22. a groove; 23. a slider; 24. a threaded pipe; 25. a threaded rod; 26. a third gear; 27. a second motor; 28. a fourth gear.
Detailed Description
The present invention will be further described with reference to the accompanying drawings and embodiments.
First embodiment
Referring to fig. 1, in a first embodiment of the present invention, an aircraft long beam multi-station automatic clamp includes: a mounting block 1; the fixing block 2 is arranged on one side of the mounting block 1; the square 3 is fixedly arranged on the outer wall of one side of the fixed block 2; the rotating rod 4 is rotatably arranged on the square block 3; the first motor 5, the said first motor 5 is fixedly mounted on the top of the said square 3; the first gear 6 is fixedly sleeved on the rotating rod 4; the second gear 7 is fixedly arranged on the output shaft of the first motor 5, and the second gear 7 is meshed with the first gear 6; the stabilizing block 8 is fixedly arranged at one end of the rotating rod 4 far away from the fixing block 2; the first sliding groove 9 is formed in the outer wall of one side of the stabilizing block 8; the round rod 10 is fixedly arranged in the first sliding chute 9; the hydraulic cylinder 11 is fixedly arranged at the top of the stabilizing block 8; the first clamping block 12 is slidably mounted on the round rod 10, and the top of the first clamping block 12 is fixedly connected with an output shaft of the hydraulic cylinder 11; the cavity 13 is formed in the first clamping block 12; the sliding rod 14 is slidably mounted in the cavity 13, and two ends of the sliding rod 14 extend out of the first clamping block 12; the steel ring 15 is arranged in the cavity 13, and the steel ring 15 is fixedly sleeved on the sliding rod 14; the spring 16 is fixedly arranged in the cavity 13, the spring 16 is movably sleeved on the sliding rod 14, the bottom end of the spring 16 is fixedly arranged at the top of the steel ring 15, and the top end of the spring 16 is fixedly arranged on the inner wall of the top of the cavity 13; the second clamping block 17 is fixedly arranged on the outer wall of one side of the stabilizing block 8; the connecting block 18 is fixedly arranged at the top of the second clamping block 17; and the two arc-shaped clamping heads 19 are respectively and fixedly arranged at the bottom end of the sliding rod 14 and the top of the connecting block 18.
Arc-shaped rubber protection pads are arranged in the two arc-shaped chucks 19.
The top of the first clamping block 12 is provided with a through hole, a ball is movably embedded in the through hole, and the round rod 10 penetrates through the through hole and is in contact with the ball.
The outer wall of one side of the mounting block 1 is fixedly connected with the outer wall of one side of the fixing block 2.
In this embodiment:
the first step is as follows: install this device on the machine that bears this device, when needing to carry out the centre gripping to horizontal target, start pneumatic cylinder 11 and drive first clamp splice 12 and slide downwards, when the arc rubber protection pad in the arc chuck 19 touches the aircraft roof beam, the arc chuck 19 that is located slide bar 14 bottom drives slide bar 14 and steel ring 15 extrusion spring 16 that slides upwards under the effect of pressure, spring 16 and arc rubber protection pad have certain elasticity when stepping up the frame, can protect the aircraft frame.
The second step is that: when needing to carry out perpendicular centre gripping to the aircraft roof beam, start first motor 5 and drive second gear 7 and rotate, second gear 7 drives first gear 6 and rotates, first gear 6 drives dwang 4 and rotates, dwang 4 drives firm piece 8 and rotates 90, start hydraulic cylinder 11 and drive first clamp splice 12 and slide down, when the arc rubber protection pad in the arc chuck 19 touches and flies the frame, the arc chuck 19 that is located slide bar 14 bottom drives slide bar 14 and the 15 extrusion springs that slide upwards of steel ring 16 under the effect of pressure, fly the frame to the aircraft frame and carry out the centre gripping.
Compared with the prior art, the utility model provides an automatic anchor clamps of long roof beam multistation of aircraft has following beneficial effect: start first motor 5 and drive second gear 7, first gear 6 rotates and dwang 4 rotates, dwang 4 drives the different angles of 8 rotations of stabilizing block, the advantage of the perpendicular or horizontally of centre gripping has to the aircraft roof beam, start hydraulic cylinder 11 and drive first clamp splice 12 and slide down, arc rubber protection pad in the arc chuck 19 touches when flying the frame, the arc chuck 19 that is located slide bar 14 bottom drives slide bar 14 and steel ring 15 extrusion spring 16 that slides upwards under the effect of pressure, spring 16 and arc rubber protection pad have certain elasticity when stepping up and fly the frame, can protect the aircraft frame, the effect to aircraft roof beam protection in having the clamping process.
Second embodiment:
based on the long roof beam multistation automatic clamp of aircraft that the first embodiment of this application provided, the second embodiment of this application provides another kind of long roof beam multistation automatic clamp of aircraft. The second embodiment is merely a preferred way of the first embodiment, and the implementation of the second embodiment does not affect the implementation of the first embodiment alone.
The second embodiment of the present invention will be further explained with reference to the drawings and the embodiments.
Referring to fig. 2-3 in combination, in a second embodiment of the multi-station automatic clamp for the long beam of the airplane provided by the present invention, the fixed block 2 is movably disposed on one side of the mounting block 1, a second chute 20 is disposed on an outer wall of one side of the fixed block 2, a fixed rod 21 is fixedly mounted in the second chute 20, a groove 22 is disposed on a top of the mounting block 1, a slider 23 is slidably mounted on the fixed rod 21, a threaded pipe 24 is rotatably mounted in the mounting block 1, one end of the threaded pipe 24 extends into the groove 22, a threaded rod 25 is mounted in the threaded pipe 24, one end of the threaded rod 25 extends into the groove 22 and is fixedly mounted with a first hinge block, the first hinge block is hinged to an outer wall of one side of the slider 23, a third gear 26 is fixedly mounted on the threaded pipe 24, a second motor 27 is fixedly mounted on a top of the mounting block 1, a fourth gear 28 is fixedly mounted on an output shaft of the second motor 27, and the fourth gear 28 is engaged with the third gear 26.
The square groove has been seted up on one side outer wall of installation piece 1, the articulated piece of second of one side inner wall fixed mounting in square groove, the articulated piece of second with one side outer wall of fixed block 2 is articulated mutually.
One end of the threaded rod 25 is fixedly provided with a limiting block.
In this embodiment:
when wanting to carry out inclination's centre gripping to some work pieces or aircraft roof beam, start second motor 27 and drive fourth gear 28, third gear 26 and screwed pipe 24 and rotate, screwed pipe 24 drives threaded rod 25 and moves about, can produce thrust to promote slider 23 and upwards or slide downwards, through the articulated of activity, can make fixed block 2 form a firm angle, make arc chuck 19 can carry out some inclination's centre gripping by work piece or aircraft roof beam, have the advantage of slant position centre gripping and using manpower sparingly.
The above only is the embodiment of the present invention, not limiting the scope of the present invention, all the equivalent structures or equivalent processes of the present invention are used in the specification and the attached drawings, or directly or indirectly applied to other related technical fields, and the same principle is included in the protection scope of the present invention.
Claims (7)
1. The utility model provides an automatic anchor clamps of long roof beam multistation of aircraft which characterized in that includes:
mounting blocks;
the fixing block is arranged on one side of the mounting block;
the square block is fixedly arranged on the outer wall of one side of the fixed block;
the rotating rod is rotatably arranged on the square block;
the first motor is fixedly arranged at the top of the square block;
the first gear is fixedly sleeved on the rotating rod;
the second gear is fixedly arranged on an output shaft of the first motor and is meshed with the first gear;
the stabilizing block is fixedly arranged at one end of the rotating rod, which is far away from the fixing block;
the first sliding groove is formed in the outer wall of one side of the stabilizing block;
the round rod is fixedly arranged in the first sliding groove;
the hydraulic cylinder is fixedly arranged at the top of the stabilizing block;
the first clamping block is slidably mounted on the round rod, and the top of the first clamping block is fixedly connected with the output shaft of the hydraulic cylinder;
the cavity is arranged in the first clamping block;
the sliding rod is slidably mounted in the cavity, and two ends of the sliding rod extend out of the first clamping block;
the steel ring is arranged in the cavity and fixedly sleeved on the sliding rod;
the spring is fixedly arranged in the cavity, the spring is movably sleeved on the sliding rod, the bottom end of the spring is fixedly arranged at the top of the steel ring, and the top end of the spring is fixedly arranged on the inner wall of the top of the cavity;
the second clamping block is fixedly arranged on the outer wall of one side of the stabilizing block;
the connecting block is fixedly arranged at the top of the second clamping block;
and the two arc-shaped chucks are fixedly arranged at the bottom end of the sliding rod and the top of the connecting block respectively.
2. The long beam multi-station automatic clamp for the airplane according to claim 1, wherein arc-shaped rubber protection pads are installed in the two arc-shaped chucks.
3. The long beam multi-station automatic clamp for the airplane according to claim 1, wherein a through hole is formed in the top of the first clamping block, a ball is movably embedded in the through hole, and the round rod penetrates through the through hole and is in contact with the ball.
4. The long beam multi-station automatic clamp for the airplane according to claim 1, wherein the outer wall of one side of the mounting block is fixedly connected with the outer wall of one side of the fixing block.
5. The long beam multi-station automatic clamp of the aircraft as claimed in claim 1, wherein the fixed block is movably disposed on one side of the mounting block, a second chute is disposed on an outer wall of one side of the fixed block, a fixed rod is fixedly mounted in the second chute, a groove is disposed on a top of the mounting block, a slider is slidably mounted on the fixed rod, a threaded pipe is rotatably mounted in the mounting block, one end of the threaded pipe extends into the groove, a threaded rod is mounted in the threaded pipe, one end of the threaded rod extends into the groove and is fixedly mounted with a first hinge block, the first hinge block is hinged to an outer wall of one side of the slider, a third gear is fixedly mounted on the threaded pipe, a second motor is fixedly mounted on a top of the mounting block, and a fourth gear is fixedly mounted on an output shaft of the second motor, the fourth gear is meshed with the third gear.
6. The long beam multi-station automatic clamp for the airplane according to claim 5, wherein a square groove is formed in the outer wall of one side of the mounting block, a second hinge block is fixedly mounted on the inner wall of one side of the square groove, and the second hinge block is hinged to the outer wall of one side of the fixing block.
7. The long-beam multi-station automatic clamp for the aircraft according to claim 5, wherein a limiting block is fixedly arranged at one end of the threaded rod.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021212273.XU CN212683679U (en) | 2020-06-28 | 2020-06-28 | Multi-station automatic clamp for long beam of airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021212273.XU CN212683679U (en) | 2020-06-28 | 2020-06-28 | Multi-station automatic clamp for long beam of airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212683679U true CN212683679U (en) | 2021-03-12 |
Family
ID=74894700
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021212273.XU Active CN212683679U (en) | 2020-06-28 | 2020-06-28 | Multi-station automatic clamp for long beam of airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212683679U (en) |
-
2020
- 2020-06-28 CN CN202021212273.XU patent/CN212683679U/en active Active
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