CN216461927U - Aviation standard component perforating device - Google Patents
Aviation standard component perforating device Download PDFInfo
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- CN216461927U CN216461927U CN202123164851.4U CN202123164851U CN216461927U CN 216461927 U CN216461927 U CN 216461927U CN 202123164851 U CN202123164851 U CN 202123164851U CN 216461927 U CN216461927 U CN 216461927U
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- 230000007246 mechanism Effects 0.000 claims abstract description 37
- 238000004080 punching Methods 0.000 claims abstract description 28
- 230000000670 limiting effect Effects 0.000 claims description 9
- 230000002950 deficient Effects 0.000 abstract description 2
- 238000009434 installation Methods 0.000 description 8
- 230000005540 biological transmission Effects 0.000 description 5
- 230000000694 effects Effects 0.000 description 5
- 230000033001 locomotion Effects 0.000 description 4
- 239000000203 mixture Substances 0.000 description 2
- 239000007858 starting material Substances 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 230000001360 synchronised effect Effects 0.000 description 1
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Abstract
The utility model discloses an aviation standard component perforating device, including the bottom plate, still include: four symmetrically arranged clamping devices: the four clamping devices are arranged on the upper end face of the bottom plate and used for clamping a standard part to be machined; two symmetrically arranged adjustment mechanisms: the two adjusting mechanisms are arranged on the upper end surface of the bottom plate; the punching mechanism comprises: the punching mechanism is arranged on the upper end surface of the adjusting mechanism; the utility model can realize the height adjustment of the punching mechanism by arranging the adjusting mechanism, thereby realizing the punching purpose of workpieces with different heights; can guarantee to treat the centre gripping purpose of processing standard component through setting up clamping device, can guarantee the precision of punching of reality to can promote the quality of punching effectively, reduce the defective rate effectively.
Description
Technical Field
The utility model belongs to the technical field of aviation standard component processing equipment, concretely relates to aviation standard component perforating device.
Background
The standard parts refer to common parts such as screw thread parts, keys, pins, rolling bearings and the like which are completely standardized in all aspects of structure, size, drawing, marking and the like and are produced by professional factories. The mechanical parts and elements with high standardization degree and strong industrial universality are also called universal parts. Broadly, it includes standardized mechanical parts such as fasteners, couplings, transmission members, seals, hydraulic components, pneumatic components, bearings, springs, etc. The narrow sense includes only standardized fasteners. The commonly known standard component in China is the abbreviation of a standard fastener, is a narrow concept, but cannot exclude the existence of a broad concept. In addition, the industrial standard parts, such as automobile standard parts, mold standard parts and the like, also belong to the broad standard parts.
Aviation standard component need punch through perforating device when processing man-hour, nevertheless various perforating device still has various problems in the market, and the perforating device among the prior art punches is inefficient, and adjusts loaded down with trivial details, has great limitation, for this reason, we propose an aviation standard component perforating device.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an aviation standard component perforating device to solve the problem that proposes among the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides an aviation standard perforating device, includes the bottom plate, still includes:
four symmetrically arranged clamping devices: the four clamping devices are arranged on the upper end face of the bottom plate and are used for clamping a standard part to be processed;
two symmetrically arranged adjusting mechanisms: the two adjusting mechanisms are mounted on the upper end face of the bottom plate and comprise supporting plates, a motor is located on the upper end face of each supporting plate, a driving wheel is sleeved on the circumferential surface of the outer end face of a motor shaft of the motor, driving teeth are fixedly mounted on the circumferential surface of the driving wheel and meshed with driving teeth, a moving plate is fixedly mounted on the inner end face of each driving tooth, and a limiting plate is movably mounted at the lower end of each moving plate;
the punching mechanism: the punching mechanism is arranged on the upper end surface of the adjusting mechanism.
Preferably, the clamping device comprises a fixed plate, an air cylinder is fixedly mounted on an inner end face of the fixed plate, a telescopic column is mounted at an output end of the air cylinder, and a clamping plate is fixedly mounted on an inner end face of the telescopic column.
Preferably, four cylinders are connected with the same controller together.
Preferably, the lower terminal surface fixed mounting of grip block has the movable block, the confession has been seted up to the up end of bottom plate the gliding spout of movable block, just the mounting groove has been seted up to the up end of bottom plate, the fixed plate with the cylinder is installed in the mounting groove.
Preferably, the upper end face of the supporting plate is provided with a groove, and the motor is installed in the groove.
Preferably, the motors are double-shaft motors, and the two motors are connected with the same controller.
Preferably, a moving block is fixedly mounted on the lower end surface of the moving plate, and a sliding groove for the moving block to slide is formed in the limiting plate.
Preferably, the punching mechanism comprises a top plate, a driving machine is installed inside the top plate, and a drill bit is fixedly installed on the lower end face of a driving shaft of the driving machine.
Preferably, a through hole matched with the outer diameter of the driving machine is formed in the center of the top plate, the driving machine is installed in the through hole, and a positioning block is fixedly installed on the upper end face of the driving machine.
Compared with the prior art, the beneficial effects of the utility model are that:
(1) this aviation standard component perforating device, can drive the motor shaft at both ends and the drive wheel and the drive tooth rotation of circumferential surface behind the starter motor, can realize promptly that the driving tooth is along perpendicular reverse movement, thereby can realize the altitude mixture control of movable plate, can realize the lift of mechanism of punching promptly, and same controller is connected to two motors, the rotation opposite direction of two motors, can realize the synchronous motion of movable plate through this kind of setting, can realize the lift of mechanism of punching promptly, can realize the purpose of punching of the work piece of co-altitude not.
(2) This aviation standard component perforating device, can realize the interval regulation of grip block under the effect of cylinder and flexible post, thereby can satisfy the centre gripping purpose of not unidimensional standard component, thereby can guarantee actual result of use, the lower terminal surface fixed mounting of grip block has the movable block, the up end of bottom plate is seted up and is supplied the gliding spout of movable block, provide the space for the removal of movable block through setting up the spout, and have spacing purpose concurrently, thereby can guarantee the actual precision of punching, the defective index has been reduced effectively.
Drawings
Fig. 1 is a perspective view of the present invention;
fig. 2 is a side sectional view of the present invention;
fig. 3 is a schematic perspective view of the middle bottom plate of the present invention;
fig. 4 is a schematic perspective view of the clamping device of the present invention;
fig. 5 is a schematic perspective view of the adjusting mechanism of the present invention;
fig. 6 is a schematic perspective view of the middle punching mechanism of the present invention.
In the figure: 1. a base plate; 2. a clamping device; 201. a fixing plate; 202. a cylinder; 203. a telescopic column; 204. A clamping plate; 205. a movable block; 3. an adjustment mechanism; 301. a support plate; 302. a motor; 303. a motor shaft; 304. a drive wheel; 305. a drive tooth; 306. a transmission gear; 307. moving the plate; 308. a limiting plate; 4. a punching mechanism; 401. a top plate; 402. a driver; 403. a drive shaft; 404. a drill bit.
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. 1-6, the utility model provides an aviation standard component perforating device, including bottom plate 1, still include:
four symmetrically arranged clamping devices 2: the four clamping devices 2 are all arranged on the upper end face of the bottom plate 1, and the four clamping devices 2 are used for clamping a standard part to be processed;
two symmetrically arranged adjusting mechanisms 3: the two adjusting mechanisms 3 are mounted on the upper end face of the bottom plate 1, each adjusting mechanism 3 comprises a supporting plate 301, a motor 302 is located on the upper end face of the supporting plate 301, a driving wheel 304 is sleeved on the circumferential surface of the outer end face of a motor shaft 303 of the motor 302, driving teeth 305 are fixedly mounted on the circumferential surface of the driving wheel 304, the driving teeth 305 are meshed with transmission teeth 306, a moving plate 307 is fixedly mounted on the inner end face of the transmission teeth 306, and a limiting plate 308 is movably mounted at the lower end of the moving plate 307; after the motor 302 is started, the motor shaft 303 at two ends, the driving wheel 304 on the circumferential surface of the motor shaft and the driving tooth 305 can be driven to rotate, that is, the transmission tooth 306 can move along the vertical direction, so that the height of the moving plate 307 can be adjusted, that is, the punching mechanism 4 can be lifted, the moving path of the moving plate 307 can be limited by arranging the limiting plate 308, and the limiting effect is good;
the punching mechanism 4: the punching mechanism 4 is mounted on the upper end surface of the adjusting mechanism 3.
In this embodiment, preferably, the clamping device 2 includes a fixing plate 201, an air cylinder 202 is fixedly mounted on an inner end surface of the fixing plate 201, a telescopic column 203 is mounted on an output end of the air cylinder 202, and a clamping plate 204 is fixedly mounted on an inner end surface of the telescopic column 203; can guarantee the installation stability of cylinder 202 through setting up fixed plate 201, can realize the interval regulation of grip block 204 under the effect of cylinder 202 and flexible post 203 to can satisfy the centre gripping purpose of different size standard components, thereby can guarantee actual result of use, the practicality is strong.
In this embodiment, preferably, the four cylinders 202 are connected to the same controller; through the arrangement, the four clamping plates 204 can be synchronously moved, the operation steps are simplified, the processing time is saved, the clamping stability is good, and the practicability is high.
In this embodiment, preferably, the lower end surface of the clamping plate 204 is fixedly provided with a movable block 205, the upper end surface of the bottom plate 1 is provided with a sliding groove for the movable block 205 to slide, the upper end surface of the bottom plate 1 is provided with an installation groove, and the fixed plate 201 and the cylinder 202 are installed in the installation groove; through setting up the spout for the removal of movable block 205 provides the space, and have spacing purpose concurrently, the practicality is strong, and can guarantee the installation stability of fixed plate 201 and cylinder 202 through setting up the mounting groove to can guarantee the centre gripping purpose of reality, the practicality is strong, and the result of use is good.
In this embodiment, preferably, a groove is formed on the upper end surface of the supporting plate 301, and the motor 302 is installed in the groove; the installation stability of the motor 302 can be ensured by arranging the support plate 301 and the groove, so that the actual using effect can be ensured.
In this embodiment, preferably, the motors 302 are dual-shaft motors, and the two motors 302 are connected to the same controller; and the rotation directions of the two motors 302 are opposite, so that the moving plate 307 can synchronously move, namely the lifting of the punching mechanism 4 can be realized, the punching purpose of workpieces with different heights can be realized, and the practicability is high.
In this embodiment, preferably, a moving block is fixedly mounted on the lower end surface of the moving plate 307, and a sliding groove for the moving block to slide is formed in the limiting plate 308; the purpose that the moving plate 307 slides in the moving plate can be achieved by arranging the sliding grooves, the moving of the moving plate 307 can be limited by arranging the sliding grooves, the practicability is high, and the using effect is good.
In this embodiment, preferably, the hole punching mechanism 4 includes a top plate 401, a driving machine 402 is installed inside the top plate 401, and a drill 404 is fixedly installed on a lower end surface of a driving shaft 403 of the driving machine 402; can guarantee driving machine 402's installation stability through setting up roof 401, can realize the rotation of drive shaft 403 and drill bit 404 after starting driving machine 402 to can realize the purpose of punching, easy operation, the practicality is strong.
In this embodiment, preferably, a through hole adapted to the outer diameter of the driving machine 402 is formed in the center of the top plate 401, the driving machine 402 is installed in the through hole, and a positioning block is fixedly installed on the upper end surface of the driving machine 402; can guarantee driving machine 402's installation purpose through setting up the through-hole, and can guarantee driving machine 402's stable installation through setting up the locating piece, the practicality is strong.
The utility model discloses a theory of operation and use flow: when the device is used, a workpiece to be machined is placed on the upper end face of the bottom plate 1, the air cylinder 202 is started, the distance adjustment of the clamping plate 204 can be realized under the action of the air cylinder 202 and the telescopic column 203, so that the clamping purpose of standard parts with different sizes can be met, and the actual using effect can be ensured;
can drive the motor shaft 303 at both ends and the drive wheel 304 and the drive tooth 305 on circumferential surface rotate behind the starter motor 302, can realize promptly that driving tooth 306 follows vertical reverse movement, thereby can realize the altitude mixture control of moving plate 307, can realize the lift of mechanism 4 of punching promptly, and same controller is connected to two motors 302, the rotation opposite direction of two motors 302, can realize the simultaneous movement of moving plate 307 through this kind of setting, can realize the lift of mechanism 4 of punching promptly, can realize the purpose of punching of the work piece of co-altitude not.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (9)
1. The utility model provides an aviation standard component perforating device, includes bottom plate (1), its characterized in that still includes:
four symmetrically arranged clamping devices (2): the four clamping devices (2) are all arranged on the upper end face of the bottom plate (1), and the four clamping devices (2) are used for clamping a standard part to be processed;
two symmetrically arranged adjusting mechanisms (3): the two adjusting mechanisms (3) are mounted on the upper end face of the bottom plate (1), each adjusting mechanism (3) comprises a supporting plate (301), a motor (302) is located on the upper end face of each supporting plate (301), a driving wheel (304) is sleeved on the circumferential surface of the outer end face of a motor shaft (303) of each motor (302), driving teeth (305) are fixedly mounted on the circumferential surface of each driving wheel (304), the driving teeth (305) are connected with driving teeth (306) in a meshed mode, a moving plate (307) is fixedly mounted on the inner end face of each driving tooth (306), and a limiting plate (308) is movably mounted at the lower end of each moving plate (307);
punching mechanism (4): the punching mechanism (4) is installed on the upper end face of the adjusting mechanism (3).
2. The aviation standard perforating device of claim 1, wherein: clamping device (2) include fixed plate (201), the inner terminal surface fixed mounting of fixed plate (201) has cylinder (202), flexible post (203) is installed to the output of cylinder (202), the inner terminal surface fixed mounting of flexible post (203) has grip block (204).
3. The aviation standard perforating device of claim 2, wherein: the four cylinders (202) are connected with the same controller together.
4. The aviation standard perforating device of claim 2, wherein: the lower terminal surface fixed mounting of grip block (204) has movable block (205), the confession has been seted up to the up end of bottom plate (1) the gliding spout of movable block (205), just the mounting groove has been seted up to the up end of bottom plate (1), fixed plate (201) with cylinder (202) are installed in the mounting groove.
5. The aviation standard perforating device of claim 1, wherein: the upper end face of the supporting plate (301) is provided with a groove, and the motor (302) is arranged in the groove.
6. The aviation standard perforating device of claim 1, wherein: the motor (302) is a double-shaft motor, and the two motors (302) are connected with the same controller.
7. The aviation standard perforating device of claim 1, wherein: the lower end face of the moving plate (307) is fixedly provided with a moving block, and a sliding groove for the moving block to slide is formed in the limiting plate (308).
8. The aviation standard perforating device of claim 1, wherein: the punching mechanism (4) comprises a top plate (401), a driving machine (402) is installed inside the top plate (401), and a drill (404) is fixedly installed on the lower end face of a driving shaft (403) of the driving machine (402).
9. The aviation standard perforating device of claim 8, wherein: the center of the top plate (401) is provided with a through hole matched with the outer diameter of the driving machine (402), the driving machine (402) is installed in the through hole, and a positioning block is fixedly installed on the upper end face of the driving machine (402).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202123164851.4U CN216461927U (en) | 2021-12-16 | 2021-12-16 | Aviation standard component perforating device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202123164851.4U CN216461927U (en) | 2021-12-16 | 2021-12-16 | Aviation standard component perforating device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216461927U true CN216461927U (en) | 2022-05-10 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202123164851.4U Active CN216461927U (en) | 2021-12-16 | 2021-12-16 | Aviation standard component perforating device |
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| Country | Link |
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| CN (1) | CN216461927U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115194499A (en) * | 2022-05-31 | 2022-10-18 | 中国第二重型机械集团德阳万航模锻有限责任公司 | Clamping tool, die forging and die forging numerical control machining method |
-
2021
- 2021-12-16 CN CN202123164851.4U patent/CN216461927U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115194499A (en) * | 2022-05-31 | 2022-10-18 | 中国第二重型机械集团德阳万航模锻有限责任公司 | Clamping tool, die forging and die forging numerical control machining method |
| CN115194499B (en) * | 2022-05-31 | 2023-12-22 | 中国第二重型机械集团德阳万航模锻有限责任公司 | Clamping tool, die forging and numerical control machining method for die forging |
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| Date | Code | Title | Description |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20221125 Address after: 610100 No. 6, Hangtian South Road, Chengdu Economic and Technological Development Zone, Sichuan Province Patentee after: CHENGDU XINGYU PRECISION CASTING Co.,Ltd. Address before: 610100 No. 356, Checheng East seventh Road, Chengdu Economic and Technological Development Zone (Longquanyi District), Longquanyi District, Chengdu, Sichuan Patentee before: Chengdu Xingyu Kaimai Aviation Technology Co.,Ltd. |