CN217914093U - Fixing device for machining aviation equipment - Google Patents
Fixing device for machining aviation equipment Download PDFInfo
- Publication number
- CN217914093U CN217914093U CN202222128540.0U CN202222128540U CN217914093U CN 217914093 U CN217914093 U CN 217914093U CN 202222128540 U CN202222128540 U CN 202222128540U CN 217914093 U CN217914093 U CN 217914093U
- Authority
- CN
- China
- Prior art keywords
- threaded rod
- sliding
- mounting groove
- fixing frame
- plummer
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 238000003754 machining Methods 0.000 title claims description 8
- 230000002457 bidirectional effect Effects 0.000 claims description 6
- 101000623895 Bos taurus Mucin-15 Proteins 0.000 claims 1
- 230000000694 effects Effects 0.000 abstract description 4
- 238000005516 engineering process Methods 0.000 abstract description 2
- 230000001105 regulatory effect Effects 0.000 description 8
- 210000005056 cell body Anatomy 0.000 description 4
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
Images
Landscapes
- Jigs For Machine Tools (AREA)
Abstract
The utility model relates to an aircraft equipment processing technology field especially relates to a fixing device for processing aircraft equipment. The bearing device comprises a bearing table, wherein a first adjusting component and a second adjusting component are arranged on the bearing table, a first fixing structure and a second adjusting component are connected to the first adjusting component and the second adjusting component, the fixing structure comprises a fixing frame, a groove body is formed in the fixing frame, a first threaded rod is connected in the groove body in a rotating mode, the top end of the first threaded rod penetrates through the outside of the fixing frame and is fixedly connected with a first rotating handle, a first moving block is connected to the surface threads of the first threaded rod, a fixing plate is hinged to one side of the first moving block, a second threaded rod is connected to the fixing frame in a rotating mode, a second rotating handle is fixedly connected to the top end of the second threaded rod, and a second moving block is connected to the surface threads of the second threaded rod. The utility model discloses can adjust according to the specification size of aeronautical equipment, the suitability is good, has improved fixed effect, easy operation, convenient to use.
Description
Technical Field
The utility model relates to an aeronautical equipment processing technology field especially relates to a fixing device for processing aeronautical equipment.
Background
With the continuous improvement of productivity and scientific and technical level and the continuous development of the aerospace industry, the aerospace industry integrates a plurality of new achievements of scientific and technical and greatly changes the structure of transportation. In aerospace, a lot of aviation equipment exist, and when the aviation equipment is processed, in order to ensure the stability of the equipment, a fixing device is usually used for fixing the aviation equipment. When the fixing device for processing the aviation equipment is used, the fixing device is usually inconvenient to adjust, can only fix the equipment with the same specification and size, cannot adjust according to the specification and size of the equipment, the surface of some aviation equipment is not horizontal, and the fixing device cannot be more effectively fixed by being attached to the equipment when the equipment is fixed, so that the fixing effect is poor. To this end, we propose a fixture for machining aircraft equipment to solve the above-mentioned problems.
SUMMERY OF THE UTILITY MODEL
The to-be-solved technical problem of the utility model is to provide a can adjust according to the specification size of aeronautical equipment, the suitability is good, and is fixed effectual, easy operation, convenient to use's a fixing device for processing aeronautical equipment.
The utility model discloses a solve above-mentioned problem, the technical scheme who proposes is: the utility model provides a fixing device for processing aviation equipment, includes the plummer, be equipped with regulating assembly one and regulating assembly two on the plummer, all be connected with fixed knot structure on regulating assembly one and the regulating assembly two, fixed knot structure includes the mount, the cell body has been seted up on the mount, the cell body internal rotation is connected with threaded rod one, the top of threaded rod one runs through outside and the fixedly connected with turning handle one of mount, the surface threaded connection of threaded rod one has movable block one, one side of movable block one articulates there is the fixed plate, it is connected with threaded rod two to rotate on the mount, the top fixedly connected with turning handle two of threaded rod two, the surface threaded connection of threaded rod two has movable block two, one side fixedly connected with spliced pole of movable block two, the bottom of spliced pole runs through the mount and extends to the outside of mount, the bottom of spliced pole is articulated with one side that the movable block one was kept away from to the fixed plate, all be equipped with the rubber pad on mount and the fixed plate.
Furthermore, the adjusting component comprises a first mounting groove and a first sliding groove, a bidirectional threaded rod is connected to the first mounting groove in a rotating mode, a first movable block is connected to the two ends of the bidirectional threaded rod in a threaded mode, the first sliding groove is provided with two sliding blocks, the two sliding blocks are connected to the first sliding groove in a sliding mode, the bottom side of the first sliding block is connected with the first movable block respectively, and the top side of the first sliding block is connected with a fixing frame respectively.
Further, the inside at the plummer is seted up to mounting groove one, the upper surface at the plummer is seted up to spout one, spout one is linked together with mounting groove one, the one end of two-way threaded rod runs through to the outside of plummer and fixedly connected with rotates handle one.
Furthermore, the second adjusting component comprises a second mounting groove and a second sliding groove, a third threaded rod is connected in the second mounting groove in a rotating mode, a second movable block is connected to the surface of the third threaded rod in a threaded mode, a second sliding block is connected in the second sliding groove in a sliding mode, the bottom side of the second sliding block is connected with the second movable block, and the top side of the second sliding block is connected with a fixed frame.
Further, mounting groove two, spout two, threaded rod three, movable block two, slider two all are equipped with two, two the inside at the plummer is all seted up to mounting groove two, two the upper surface at the plummer is all seted up to spout two, two spout two communicates with corresponding mounting groove two respectively, two the one end of threaded rod three all runs through to the outside of plummer and fixedly connected with rotates handle two.
Furthermore, the first moving block is connected with the groove body in a sliding mode.
The utility model has the advantages that:
the utility model discloses can treat the aeronautical equipment of processing and effectively fix, can carry out the regulation of distance between the mount according to the size of equipment, can select to use two, three or four mounts to fix according to the specification of equipment, can also be according to the surface condition of equipment, the gradient of adjustment fixed plate to it is more effectual fixed to it, makes its abundant and equipment phase-match use, improves fixed effect, easy operation, convenient to use.
Drawings
Fig. 1 is a schematic structural view of a fixing device for processing aircraft equipment of the present invention.
Fig. 2 is a side view of the utility model discloses a fixing device for processing aircraft equipment.
Fig. 3 is a top view of a carrier table for processing a fixture of an aircraft.
Fig. 4 is an enlarged view of the part a of fig. 2 of a fixing device for processing aircraft equipment according to the present invention.
( 1. A bearing table; 2. a fixed mount; 3. a trough body; 4. a first threaded rod; 5. a first rotating handle; 6. moving a first block; 7. a fixing plate; 8. a second threaded rod; 9. a second rotating handle; 10. moving a second block; 11. connecting columns; 12. a rubber pad; 13. a first mounting groove; 14. a first sliding chute; 15. a bidirectional threaded rod; 16. a first movable block; 17. a first sliding block; 18. rotating the first handle; 19. a second mounting groove; 20. a second chute; 21. a third threaded rod; 22. a second movable block; 23. a second sliding block; 24. rotating handle two )
Detailed Description
The present invention will be further explained with reference to the accompanying drawings.
According to fig. 1, 2, 3 and 4, the utility model provides a fixing device for processing aviation equipment, including the plummer 1, be equipped with regulating assembly one and regulating assembly two on the plummer 1, both be connected with fixed knot structure on regulating assembly one and the regulating assembly two, fixed knot structure includes mount 2, seted up cell body 3 on the mount 2, the internal rotation of cell body 3 is connected with threaded rod one 4, the top of threaded rod one 4 runs through to the outside of mount 2 and fixedly connected with turning handle one 5, the surface threaded connection of threaded rod one 4 has a movable block 6, one side of movable block one 6 articulates there is fixed plate 7, the rotation is connected with threaded rod two 8 on the mount 2, the top fixedly connected with turning handle two 9 of threaded rod two 8, the surface threaded connection of threaded rod two 8 has movable block two 10, one side fixedly connected with spliced pole 11 of movable block two 10, the bottom of spliced pole 11 runs through the mount 2 and extends to the outside of mount 2, the bottom of spliced pole 11 is articulated with one side of fixed plate 7 far away from first 6, rubber pad 12 is equipped with fixed mount 2 and fixed plate 7; the first adjusting component and the second adjusting component are used for adjusting the distance between the fixing structures and adjusting the distance according to the specification and size of the aviation equipment to be processed, the fixing structures can be better fixed with the aviation equipment in a matched mode, the two sides of the fixing plates are hinged to the first moving block and the connecting column respectively, the inclination of the fixing plates can be adjusted, and therefore the fixing plates are better fixed with the aviation equipment in a surface fit mode.
The adjusting part includes mounting groove 13 and spout 14, 13 internal rotations in mounting groove are connected with two-way threaded rod 15, the equal threaded connection in both ends of two-way threaded rod 15 has movable block 16, spout 14 is equipped with two, two equal sliding connection has slider 17 in the spout 14, two the bottom side of slider 17 is connected with two movable block 16 respectively, two the top side of slider 17 is connected with a mount 2 respectively.
The inside at plummer 1 is seted up to mounting groove one 13, the upper surface at plummer 1 is seted up to spout one 14, spout one 14 is linked together with mounting groove one 13, the one end of two-way threaded rod 15 runs through to the outside of plummer 1 and fixedly connected with rotates handle one 18.
The second adjusting component comprises a second mounting groove 19 and a second sliding groove 20, a third threaded rod 21 is rotationally connected in the second mounting groove 19, a second movable block 22 is connected to the surface of the third threaded rod 21 in a threaded manner, a second sliding block 23 is slidably connected in the second sliding groove 20, the bottom side of the second sliding block 23 is connected with the second movable block 22, and the top side of the second sliding block 23 is connected with the fixed frame 2.
Two 19 mounting grooves, two 20 spout, three 21 threaded rods, two movable blocks 22, two 23 sliders all are equipped with two, two 19 mounting grooves are all seted up in the inside of plummer 1, two the upper surface at plummer 1 is all seted up to two 20 spouts, two 20 spout respectively with two 19 intercommunications of corresponding mounting grooves, two the one end of three 21 threaded rods all runs through to the outside of plummer 1 and fixedly connected with rotates handle two 24.
The moving block I6 is connected with the groove body 3 in a sliding mode.
The working principle is as follows:
when the utility model is used, the positions of four fixed frames 2 are adjusted according to the size of the aeronautical equipment to be processed, the first rotating handle 18 is rotated to drive the bidirectional threaded rod 15 to rotate, and the first two movable blocks 16 can be close to or far away from each other under the sliding connection of the first slide block 17 and the first slide groove 14, so that the first slide block 14 drives the fixed frames 2 to be close to or far away from each other, and the specific position between the fixed frames 2 is adjusted, as shown in fig. 2; the second rotating handle 9 is rotated to drive the third threaded rod 21 to rotate, the movable block 22 is moved under the limitation of the sliding connection between the second sliding block 23 and the second sliding groove 20, the second sliding block 23 drives the fixed frame 2 to move, as shown in figure 1, the two rotating handles 24 are respectively rotated, and the distance between the fixed frames 2 is specifically adjusted according to the size of the equipment; four sides of equipment are placed on four fixing frames 2 respectively, two or three fixing frames 2 can be selected for use according to the specification of the equipment, after the equipment is placed, a first rotating handle 5 and a second rotating handle 9 are rotated respectively, the first rotating handle 5 is rotated, a first threaded rod 4 is rotated, a first moving block 6 drives a fixing plate 7 to move downwards, and meanwhile, the second rotating handle 9 is rotated, so that a second moving block 10 drives a connecting column 11 to move downwards, the fixing plate 7 is driven to move downwards, the fixing plate 7 is pressed on the equipment, and the aviation equipment is fixed during machining.
When aviation equipment surface level, rotate turning handle one 5 and turning handle two 9 simultaneously, make the horizontally pressure of fixed plate 7 on the equipment, if the equipment surface is uneven, then corresponding rotation turning handle one 5 and turning handle two 9, the both ends of fixed plate 7 are articulated with movable block one 6 and spliced pole 11 respectively, when the distance that movable block one 6 and movable block two 10 removed is inconsistent, the distance that the fixed plate 7 both ends removed is different, fixed plate 7 can take place the slope, thereby what more match presses at the equipment top, fix the equipment, improve fixed effect, rubber pad 12 plays the guard action to the equipment.
Although the present invention has been described with reference to the preferred embodiments, it should be understood that various changes and modifications can be made by those skilled in the art without departing from the spirit and scope of the invention.
Claims (6)
1. A fixing device for processing aircraft equipment, includes plummer (1), its characterized in that: the novel rubber pad bearing device is characterized in that a first adjusting assembly and a second adjusting assembly are arranged on the bearing table (1), a fixing structure is connected to the first adjusting assembly and the second adjusting assembly, the fixing structure comprises a fixing frame (2), a groove body (3) is formed in the fixing frame (2), a first threaded rod (4) is rotatably connected to the groove body (3), the top end of the first threaded rod (4) penetrates through the first fixing frame (2) and is fixedly connected with a first rotating handle (5), a first moving block (6) is connected to the surface of the first threaded rod (4), a fixing plate (7) is hinged to one side of the first moving block (6), a second threaded rod (8) is rotatably connected to the fixing frame (2), a second rotating handle (9) is fixedly connected to the top end of the second threaded rod (8), a second moving block (10) is connected to the surface of the second threaded rod (8), a connecting column (11) is fixedly connected to one side of the second moving block (10), the bottom end of the connecting column (11) penetrates through the fixing frame (2) and extends to the outside of the connecting column (2), rubber pads are hinged to one side of the fixing frame (7), and rubber pads are arranged on the fixing frame (2) and rubber pads (12).
2. A fixture for machining aircraft equipment according to claim 1, wherein: the adjusting part comprises a first mounting groove (13) and a first sliding groove (14), a first bidirectional threaded rod (15) is connected to the first mounting groove (13) in a rotating mode, a first movable block (16) is connected to the two ends of the first bidirectional threaded rod (15) in a threaded mode, the first sliding groove (14) is provided with two sliding blocks (17) and two sliding blocks (17) are connected to the first sliding block (14) in the sliding groove (14) in a sliding mode, the bottom side of the first sliding block (17) is connected with the first movable block (16) respectively, and the top side of the first sliding block (17) is connected with a fixing frame (2) respectively.
3. A fixing device for machining aircraft equipment according to claim 2, characterized in that: the inside in plummer (1) is seted up in mounting groove (13), the upper surface in plummer (1) is seted up in spout (14), spout (14) are linked together with mounting groove (13), the one end of two-way threaded rod (15) runs through to the outside of plummer (1) and fixedly connected with rotates handle (18).
4. A fixture for machining aircraft equipment according to claim 1, wherein: the adjusting component II comprises a second mounting groove (19) and a second sliding groove (20), a third threaded rod (21) is connected to the second mounting groove (19) in a rotating mode, a second movable block (22) is connected to the surface of the third threaded rod (21) in a threaded mode, a second sliding block (23) is connected to the second sliding groove (20) in a sliding mode, the bottom side of the second sliding block (23) is connected with the second movable block (22), and the top side of the second sliding block (23) is connected with the fixed frame (2).
5. A fixture for use in processing aircraft equipment, according to claim 4, wherein: mounting groove two (19), spout two (20), threaded rod three (21), movable block two (22), slider two (23) all are equipped with two, two the inside at plummer (1) is all seted up in mounting groove two (19), two the upper surface at plummer (1) is all seted up in spout two (20), two spout two (20) communicate with corresponding mounting groove two (19) respectively, two the one end of threaded rod three (21) all runs through to the outside of plummer (1) and fixedly connected with rotates handle two (24).
6. A fixture for machining aircraft equipment according to claim 1, wherein: the first moving block (6) is connected with the groove body (3) in a sliding mode.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222128540.0U CN217914093U (en) | 2022-08-15 | 2022-08-15 | Fixing device for machining aviation equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222128540.0U CN217914093U (en) | 2022-08-15 | 2022-08-15 | Fixing device for machining aviation equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN217914093U true CN217914093U (en) | 2022-11-29 |
Family
ID=84155303
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202222128540.0U Active CN217914093U (en) | 2022-08-15 | 2022-08-15 | Fixing device for machining aviation equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN217914093U (en) |
-
2022
- 2022-08-15 CN CN202222128540.0U patent/CN217914093U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN217914093U (en) | Fixing device for machining aviation equipment | |
| CN213202848U (en) | Sealed glue filling device that glues of cavity glass | |
| CN212043904U (en) | Device for flange trimming | |
| CN115958219A (en) | Multi-point drilling device for machining disc parts | |
| CN218534015U (en) | Steel member grinding device | |
| CN117984183A (en) | MPP electric pipe clamping and polishing equipment | |
| CN114193170B (en) | Multifunctional drilling device for furniture design and drilling method thereof | |
| CN208391249U (en) | A kind of hot press | |
| CN211289301U (en) | Equipment rack that possesses fixed function | |
| CN221474732U (en) | Fixed quartz stone polishing machine | |
| CN222245221U (en) | A high-efficiency template slotting machine with adjustable depth | |
| CN215509966U (en) | Seamless steel pipe cutting device | |
| CN223347261U (en) | Built-in USB interface mounting structure of notebook computer | |
| CN219666596U (en) | Water pump maintenance is with supporting device | |
| CN221334839U (en) | Spraying fixture capable of conveniently overturning metal piece | |
| CN110846216A (en) | Microscopic monitor for embryo development | |
| CN220178877U (en) | A kind of router shell edge processing equipment | |
| CN223656825U (en) | End cover machining clamp | |
| CN222844239U (en) | A PCB board separation device | |
| CN218024462U (en) | A textile rack for weaving | |
| CN222939760U (en) | Automatic inserting piece equipment for transformer production | |
| CN218312612U (en) | Part polisher | |
| CN216232484U (en) | Transfer equipment is used in car seat production | |
| CN223328158U (en) | Calculation auxiliary device for engineering cost | |
| CN222482039U (en) | Cell phone case detection device that wear-resistants |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |