CN219633206U - Spare part processing fixing device for space flight - Google Patents
Spare part processing fixing device for space flight Download PDFInfo
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- CN219633206U CN219633206U CN202321225127.4U CN202321225127U CN219633206U CN 219633206 U CN219633206 U CN 219633206U CN 202321225127 U CN202321225127 U CN 202321225127U CN 219633206 U CN219633206 U CN 219633206U
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- 238000003466 welding Methods 0.000 claims description 10
- 210000001503 joint Anatomy 0.000 claims description 6
- 239000011825 aerospace material Substances 0.000 description 3
- 230000018109 developmental process Effects 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 230000032683 aging Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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Abstract
The utility model discloses a processing and fixing device for parts for spaceflight, which relates to the field of spaceflight parts and comprises a supporting bottom plate, wherein fixed side blocks are horizontally and symmetrically welded at two ends of the supporting bottom plate, fixing through holes are uniformly formed in the top surface of the fixed side blocks, a control panel is obliquely welded at one side edge of the supporting bottom plate, end cylinders are horizontally and symmetrically connected at two ends of the supporting bottom plate, a movable ejector block is horizontally arranged on the top surface of the supporting bottom plate, a telescopic ejector rod is fixedly connected with the top surface of the movable ejector block through bolts, a fixing column is horizontally abutted to one side edge of the telescopic ejector rod, an abutting screw is in threaded connection with one side edge of the fixing column, and a rotating end block is abutted to one end far from the telescopic ejector rod, so that the clamping and fixing operation of various parts can be met by adopting an adjustable structure, and meanwhile, the adjustable angle can be used more in a manual rotating operation.
Description
Technical Field
The utility model relates to the technical field of aerospace parts, in particular to a processing and fixing device for aerospace parts.
Background
Aerospace materials refer to various materials used for aircrafts and power devices, accessories and instruments thereof, are one of decisive factors for the development of aerospace engineering technology, and aerospace material science is also one branch of development in material science. The aerospace material has excellent high and low temperature resistance, ageing resistance and corrosion resistance, and can adapt to space environment.
When processing current space component, it is required to fix the component, and the traditional fixing adopts an integrated fixed clamping structure, so that only one end of the component can be clamped and fixed, unstable conditions can be formed during the operation, and the fixed specification and size are limited to a certain extent, thereby influencing the efficiency of the component processing operation.
Disclosure of Invention
The utility model aims to provide a processing and fixing device for aerospace parts, which is used for solving the problems that the prior aerospace parts are required to be fixed during processing in the prior art, an integrated fixed clamping structure is adopted in traditional fixing, so that only one end of each part can be clamped and fixed, unstable conditions can be formed during the operation, the fixed specification and size are limited to a certain extent, and the efficiency of the processing operation of the parts is influenced.
In order to achieve the above purpose, the present utility model provides the following technical solutions:
the utility model provides a spare part processing fixing device for space flight, includes supporting baseplate, the horizontal symmetry welding in both ends of supporting baseplate has fixed side piece, fixed through-hole has evenly been seted up to the top surface of fixed side piece, the incline welding in one side of supporting baseplate has control panel, the horizontal symmetry bolted connection in both ends of supporting baseplate has an end cylinder, the top surface level of supporting baseplate is provided with the removal kicking block, the top surface bolt fixedly connected with telescopic ejector rod of removal kicking block, the side horizontal butt joint of telescopic ejector rod has a fixed cylinder, the side threaded connection of fixed cylinder has a butt joint screw rod, the fixed cylinder has a rotation end piece in the one end butt joint of keeping away from telescopic ejector rod, the rotation end piece has the clamping ring in the one end welding of keeping away from fixed cylinder, the inboard side horizontal internal groove horizontal joint has a bottom fixture block, the inboard side vertical direction bolted connection of telescopic ejector rod has an extension cylinder, the side screw hole has been seted up to one side of telescopic ejector rod, the one end horizontal welding of fixed cylinder has an end screw rod, the fixed cylinder has a rotation end at the one end of keeping away from the side clamping plate, the clamping ring has a rotation end piece, the clamping ring has a rotation end flat connection.
As a preferred embodiment of the present utility model: the number of the fixed side blocks is two, the two fixed side blocks are arranged in parallel, the two fixed side blocks are horizontally and fixedly arranged at the bottom surfaces of the two ends of the supporting bottom plate, and the control panel is fixedly arranged at the top surface of one side edge of the supporting bottom plate close to one end.
As a preferred embodiment of the present utility model: the end air cylinders are horizontally and fixedly arranged at the top surfaces of the two ends of the supporting bottom plate, the output ends of the end air cylinders horizontally penetrate through the two ends of the supporting bottom plate and extend to the inner side edges of the horizontal inner grooves, and the extending ends are fixedly connected to the side edges of the bottom clamping blocks in a one-to-one correspondence mode.
As a preferred embodiment of the present utility model: the number of the movable jacking blocks is two, the two movable jacking blocks are arranged in parallel, one end of the fixed column body is horizontally abutted to the position of the opening end of the side screw hole, one end of the jacking screw penetrates through the side wall of the fixed column body to extend to the inner side edge of the end clamping hole, and the extending ends are abutted to the outer side edge of the clamping block.
As a preferred embodiment of the present utility model: one end horizontal welding of end fixture block sets up and is close to the bottom position at the side of removing the kicking block, extends the vertical axis position that sets up at flexible ejector pin to fixed, and the side screw is seted up and is close to the top position at the side of flexible ejector pin.
As a preferred embodiment of the present utility model: the end screw rod threaded fixed connection establishes the medial side at the side screw, and joint piece joint sets up the medial side at the end draw-in hole, and the output of rotation motor extends to the inside internal portion of the inboard centre gripping of grip ring and a plurality of grip blocks mechanical connection setting each other.
Compared with the prior art, the utility model has the beneficial effects that:
according to the utility model, after the supporting bottom plate is horizontally arranged at a designated position, the fixed side blocks are fixedly connected and arranged at the designated position through the bolts after penetrating through the fixed through holes, after the supporting bottom plate is fixed, the parts are horizontally placed at the positions between the telescopic ejector rods, the control panel is controlled to control the end cylinder to extend, so that the output end extrudes the bottom clamping block to horizontally move in the horizontal inner groove, the movable ejector blocks are driven to move, the telescopic ejector rods on the top surface fold and move towards the central position, the clamping rings at the two ends are buckled at the two ends of the parts, after the rotating motor rotates, the mechanical rotation treatment is driven to fold and clamp the parts at the central position, when the parts are required to be lifted or lowered after being fixed, the parts are driven to rotate to a designated angle through controlling the extending cylinder, and after the jacking screw rotates, the jacking and fixing clamping blocks are driven to fix the parts in the inner parts of the end clamping holes, and the clamping blocks can meet the requirement of various parts by adopting an adjustable structure, and simultaneously the manual rotation angle can be adjusted.
Drawings
Other features, objects and advantages of the present utility model will become more apparent upon reading of the detailed description of non-limiting embodiments, given with reference to the accompanying drawings in which:
FIG. 1 is a schematic perspective view of a processing and fixing device for aerospace components;
FIG. 2 is a schematic structural view of a connection detail of a front cross section of a support base plate of a component tooling fixture for aerospace;
FIG. 3 is a schematic view of a structural schematic diagram of a support base plate side view cross-section connection detail of a aerospace component tooling fixture;
FIG. 4 is a schematic structural view of a telescopic ram of a aerospace component tooling fixture in elevation cross-section connection detail;
fig. 5 is a schematic structural view of a fixing post of a fixing device for processing parts for aerospace in front section connection detail.
In the figure: 1. a support base plate; 2. fixing the side blocks; 3. a fixing through hole; 4. a control panel; 5. an end cylinder; 6. moving the top block; 7. a telescopic ejector rod; 8. a fixed column; 9. a screw rod is propped up; 10. rotating the end block; 11. a clamping ring; 12. a horizontal inner tank; 13. a bottom clamping block; 14. an extension cylinder; 15. a side screw hole; 16. an end screw; 17. an end clamping hole; 18. a clamping block; 19. a rotating motor; 20. and a clamping block.
Detailed Description
Referring to fig. 1, in the embodiment of the utility model, a processing and fixing device for parts for aerospace comprises a supporting bottom plate 1, two ends of the supporting bottom plate 1 are symmetrically welded with fixed side blocks 2 horizontally, the top surfaces of the fixed side blocks 2 are uniformly provided with fixing through holes 3, one side edge of the supporting bottom plate 1 is obliquely welded with a control panel 4, the number of the fixed side blocks 2 is two, the two fixed side blocks 2 are arranged in parallel, the two fixed side blocks 2 are horizontally fixed at the bottom surfaces of the two ends of the supporting bottom plate 1, the control panel 4 is fixedly arranged at the position, close to one end, of the top surface of one side edge of the supporting bottom plate 1, two ends of the supporting bottom plate 1 are horizontally and symmetrically connected with end air cylinders 5, the end air cylinders 5 are horizontally and fixedly arranged at the top surfaces of the two ends of the supporting bottom plate 1, the output ends of the end air cylinders 5 horizontally penetrate through the two ends of the supporting bottom plate 1 and extend to the inner side edges of a horizontal inner groove 12, the extending ends are horizontally and fixedly connected at the side edge positions of the bottom clamping blocks 13 in a one-to-one correspondence manner, the top surface of the supporting bottom plate 1 is horizontally provided with the movable jacking blocks 6, the top surface bolts of the movable jacking blocks 6 are fixedly connected with the telescopic jacking rods 7, one side edge of each telescopic jacking rod 7 is horizontally abutted with the fixed column body 8, the side edges of the fixed column bodies 8 are in threaded connection with the jacking screw rods 9, the number of the movable jacking blocks 6 is two, the two movable jacking blocks 6 are mutually arranged in parallel, one ends of the fixed column bodies 8 are horizontally abutted with each other and are arranged at the opening end positions of the side screw holes 15, one ends of the jacking screw rods 9 penetrate through the side walls of the fixed column bodies 8 and extend to the inner side edges of the end clamping holes 17, the extending ends are abutted with the outer side edges of the clamping blocks 18, one ends of the fixed column bodies 8 far away from the telescopic jacking rods 7 are abutted with the rotating end blocks 10, the rotary end block 10 is welded with a clamping ring 11 at one end far away from the fixed column 8;
referring to fig. 2-5, in the embodiment of the utility model, a horizontal inner groove 12 is horizontally disposed on an inner side of a supporting base plate 1, a bottom clamping block 13 is horizontally clamped on an inner side of the horizontal inner groove 12, an extension cylinder 14 is vertically connected to an inner side of a telescopic ejector rod 7 through bolts, a side screw hole 15 is disposed on one side of the telescopic ejector rod 7, one end of the bottom clamping block 13 is horizontally welded on a side edge of the movable ejector rod 6 near a bottom end position, the extension cylinder 14 is vertically and fixedly disposed on a central axis position of the telescopic ejector rod 7, the side screw hole 15 is disposed on a side edge of the telescopic ejector rod 7 near a top end position, an end screw 16 is horizontally welded on one end of a fixed cylinder 8, an end clamping hole 17 is disposed on one end of the fixed cylinder 8 far from the end screw 16, a clamping block 18 is welded on one end of the rotating end block 10, a rotating motor 19 is horizontally bolted on an inner side of the fixed cylinder 8, a clamping block 20 is uniformly disposed on an inner side of the clamping ring 11, the end screw 16 is fixedly connected to an inner side of the side screw hole 15 through threads, the clamping block 18 is clamped on an inner side of the end clamping hole 17, and the clamping block 19 is connected to a plurality of clamping blocks 20 extending to the inner side of the clamping bodies of the clamping ring 11.
The working principle of the utility model is as follows:
after the supporting bottom plate 1 is horizontally arranged at a designated position, the fixing side blocks 2 are fixedly connected and arranged at the designated position to finish the installation operation after the bolts penetrate through the fixing through holes 3, the parts are horizontally placed between the telescopic ejector rods 7 after the supporting bottom plate 1 is fixed, the control panel 4 is controlled to control the end cylinder 5 to extend, the output end extrudes the bottom clamping block 13 to horizontally move in the horizontal inner groove 12, the movable ejector block 6 is driven to move, the telescopic ejector rods 7 on the top surface fold and move towards the central position, the clamping rings 11 on the two ends are buckled and arranged at the two ends of the parts, the rotating motor 19 rotates and then drives the mechanical rotating process to fold and fix the parts at the central position, when the parts are required to be lifted or lowered after the parts are fixed, the parts are driven to rotate to a designated angle through the control of the extension cylinder 14, and the jacking and fixing clamping blocks 18 are driven to rotate at the inner sides of the clamping holes 17 after the jacking screw 9 rotates.
The foregoing description is only a preferred embodiment of the present utility model, but the scope of the present utility model is not limited thereto, and any person skilled in the art, who is within the scope of the present utility model, should make equivalent substitutions or modifications according to the technical solution of the present utility model and the inventive concept thereof, and should be covered by the scope of the present utility model.
Claims (6)
1. The utility model provides a spare part processing fixing device for space flight, includes supporting baseplate (1), a serial communication port, the horizontal symmetry welding in both ends of supporting baseplate (1) has fixed side piece (2), fixed through-hole (3) have evenly been seted up to the top surface of fixed side piece (2), the one side oblique welding of supporting baseplate (1) has control panel (4), the horizontal symmetry bolted connection in both ends of supporting baseplate (1) has end cylinder (5), the top surface level of supporting baseplate (1) is provided with movable ejector shoe (6), the top surface bolt fixedly connected with telescopic ejector rod (7) of movable ejector shoe (6), the horizontal butt joint of one side limit of telescopic ejector rod (7) has fixed cylinder (8), the side threaded connection of fixed cylinder (8) has butt screw rod (9), the butt joint of one end of fixed cylinder (8) at keeping away from telescopic ejector rod (7) has rotation end block (10), rotation end block (10) are in the one end welding of keeping away from fixed cylinder (8) have end cylinder (11), the inboard horizontal joint of supporting baseplate (1) has flexible ejector rod (12), the horizontal butt joint (14) of side horizontal joint cylinder (13) has inside groove (14) to the horizontal expansion joint of inner tank (13), side screw (15) have been seted up to a side of flexible ejector pin (7), the one end horizontal welding of fixed cylinder (8) has end screw rod (16), end clamping hole (17) have been seted up in the one end of keeping away from end screw rod (16) to fixed cylinder (8), the one end welding of rotating end piece (10) has joint piece (18), the medial side horizontal bolted connection of fixed cylinder (8) has rotation motor (19), the medial side of holding ring (11) evenly is provided with grip block (20).
2. The processing and fixing device for the aerospace parts according to claim 1, wherein the number of the fixing side blocks (2) is two, the two fixing side blocks (2) are arranged in parallel, the two fixing side blocks (2) are horizontally and fixedly arranged at the bottom surfaces of two ends of the supporting bottom plate (1), and the control panel (4) is fixedly arranged at the position, close to one end, of the top surface of one side edge of the supporting bottom plate (1).
3. The processing and fixing device for parts for aerospace according to claim 1, wherein the end air cylinders (5) are horizontally and fixedly arranged at the top surfaces of two ends of the supporting bottom plate (1), the output ends of the end air cylinders (5) horizontally penetrate through two ends of the supporting bottom plate (1) and extend to the inner side edges of the horizontal inner grooves (12), and the extending ends are horizontally and fixedly connected and arranged at the side edge positions of the bottom clamping blocks (13) in a one-to-one correspondence mode.
4. The processing and fixing device for parts for aerospace according to claim 1, wherein the number of the movable jacking blocks (6) is two, the two movable jacking blocks (6) are arranged in parallel, one end of the fixing column body (8) is horizontally abutted to the opening end position of the side screw hole (15), one end of the jacking screw (9) penetrates through the side wall of the fixing column body (8) to extend to the inner side edge of the end clamping hole (17), and the extending end is abutted to the outer side edge of the clamping block (18).
5. The processing and fixing device for the aerospace parts according to claim 1, wherein one end of the bottom clamping block (13) is horizontally welded and arranged at the side edge of the movable ejector block (6) close to the bottom end, the extension cylinder (14) is vertically and fixedly arranged at the central axis position of the telescopic ejector rod (7), and the side screw hole (15) is formed at the side edge of the telescopic ejector rod (7) close to the top end.
6. The processing and fixing device for parts for aerospace according to claim 1, wherein the end screw (16) is fixedly connected to the inner side of the side screw hole (15), the clamping block (18) is clamped to the inner side of the end clamping hole (17), and the output end of the rotating motor (19) extends to the inner side of the inner clamping body of the clamping ring (11) to be mechanically connected with the clamping blocks (20).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321225127.4U CN219633206U (en) | 2023-05-19 | 2023-05-19 | Spare part processing fixing device for space flight |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321225127.4U CN219633206U (en) | 2023-05-19 | 2023-05-19 | Spare part processing fixing device for space flight |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219633206U true CN219633206U (en) | 2023-09-05 |
Family
ID=87806950
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321225127.4U Active CN219633206U (en) | 2023-05-19 | 2023-05-19 | Spare part processing fixing device for space flight |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN219633206U (en) |
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2023
- 2023-05-19 CN CN202321225127.4U patent/CN219633206U/en active Active
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