CN218109415U - Perforating device is used in production of unmanned aerial vehicle spare part - Google Patents
Perforating device is used in production of unmanned aerial vehicle spare part Download PDFInfo
- Publication number
- CN218109415U CN218109415U CN202222035900.2U CN202222035900U CN218109415U CN 218109415 U CN218109415 U CN 218109415U CN 202222035900 U CN202222035900 U CN 202222035900U CN 218109415 U CN218109415 U CN 218109415U
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- Prior art keywords
- fixed
- aerial vehicle
- unmanned aerial
- fastening
- spare part
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- 238000004519 manufacturing process Methods 0.000 title claims abstract description 21
- 238000004080 punching Methods 0.000 claims abstract description 28
- 235000017166 Bambusa arundinacea Nutrition 0.000 claims abstract description 12
- 235000017491 Bambusa tulda Nutrition 0.000 claims abstract description 12
- 241001330002 Bambuseae Species 0.000 claims abstract description 12
- 235000015334 Phyllostachys viridis Nutrition 0.000 claims abstract description 12
- 239000011425 bamboo Substances 0.000 claims abstract description 12
- 238000003825 pressing Methods 0.000 claims description 27
- 238000009434 installation Methods 0.000 claims description 15
- 238000001125 extrusion Methods 0.000 claims description 8
- 238000003466 welding Methods 0.000 claims description 3
- 230000007423 decrease Effects 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005056 compaction Methods 0.000 description 1
- 238000005553 drilling 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
- 238000003860 storage Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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Abstract
The utility model discloses a perforating device for producing unmanned aerial vehicle parts, which comprises a base, wherein a vertical rod is fixed on the base, a lifting clamping block is sleeved on the vertical rod, a perforating machine head is fixed at one end of the lifting clamping block, a chuck is arranged at the bottom end of the perforating machine head, a perforating drill bit is connected to the chuck, a clamping screw is connected to the lifting clamping block, a fastening rotating plate is connected to the clamping screw, a handle is fixed at one end of the fastening rotating plate, and a stop disc is fixed on the surface of the other end of the fastening rotating plate; the utility model discloses a design end a fixture block, an equipment section of thick bamboo and end a set, end a set and install and be used for on the fastening commentaries on classics board that adds fastening screw pivoted, finish the back when its fastening, go into the end inslot that ends a set lateral wall through ending fixture block one end card, realize rotating to the fastening commentaries on classics board and end the position, effectually avoid it to receive the mistake and bump and cause the rotation, make the high emergence of its aircraft nose that punches change, improve the precision of the production depth of punching of unmanned aerial vehicle spare part.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle spare part punches, concretely relates to punching device is used in production of unmanned aerial vehicle spare part.
Background
Unmanned aerial vehicle spare part is in production, and for the easy to assemble fixed and threading equipment, need adopt perforating device to contact with spare part through the drill bit on the aircraft nose that punches, then punch the processing to spare part, and when perforating device punched unmanned aerial vehicle spare part production, its is small, the operation of being convenient for, and the precision of just punching is high.
Present perforating device is used in unmanned aerial vehicle spare part production when using, it is rotatory through changeing the board to the fastening, it is not hard up to realize the tight piece of lift clamp, then adjust the height of perforating aircraft nose, it is fixed to position locking to realize through clamping screw once more, but when the operation of actually punching, the fastening commentaries on classics board is touched to easy mistake, it is rotatory to make it drive clamping screw, it is not hard up to cause the tight piece of lift clamp, thereby lead to when punching to unmanned aerial vehicle spare part man-hour, the aircraft nose takes place to move down, cause the degree of depth of punching to change, influence the problem of unmanned aerial vehicle spare part precision of punching, for this reason we propose perforating device for unmanned aerial vehicle spare part production.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a perforating device is used in production of unmanned aerial vehicle spare part to solve the perforating device is used in production of unmanned aerial vehicle spare part that proposes in the above-mentioned background art in the use, the mistake is bumped easily and is leaded to the clamping screw rotatory, and leads to the tight piece of lift clamp not hard up, makes its perforating aircraft nose take place to move down in the operation, causes the problem that the degree of depth of punching changed.
In order to achieve the above object, the utility model provides a following technical scheme: perforating device is used in unmanned aerial vehicle spare part production, the on-line screen storage device comprises a base, be fixed with the pole setting on the base, the cover is equipped with the tight piece of lift clamp in the pole setting, the one end of the tight piece of lift clamp is fixed with the punch head, the bottom of punch head is provided with the chuck, be connected with the drill bit on the chuck, be connected with clamping screw on the tight piece of lift clamp, be connected with the fastening commentaries on classics board on classics on the clamping screw, the one end of fastening commentaries on classics board is fixed with the handle, the other end fixed surface of fastening commentaries on classics board has the end position dish, the lateral wall of end position dish is circular array and has seted up the end position groove, the lateral wall of clamping piece is fixed with an equipment section of thick bamboo, the inside sliding connection of an equipment section of thick bamboo has the end position fixture block, the one end of end position fixture block extends to corresponding end position inslot portion, the other end of end position fixture block is provided with the top spring, and the top spring is located inside an equipment section of thick bamboo.
Preferably, a strip-shaped sliding hole is formed in the surface of the assembly cylinder, a pressing block is arranged on the inner side of the strip-shaped sliding hole, and one end of the pressing block is fixed on the surface of the stop fixture block.
Preferably, the cross section of the pressing block is of a convex structure, and the cross section of the assembling cylinder is of a rectangular structure.
Preferably, the bottom of drill bit is provided with the clamp plate, the fixed surface of clamp plate has four installation section of thick bamboo, and the inside of installation section of thick bamboo is provided with installation slide bar and extrusion spring, and extrusion spring is located the bottom of installation slide bar, the installation slide bar is fixed in the punch head bottom.
Preferably, the longitudinal section of the installation slide rod is of a T-shaped structure, and the cross section of the pressing plate is of a circular structure.
Preferably, the central axis of the pressure plate and the central axis of the perforating drill bit are overlapped, and the pressure plate and the mounting cylinder are fixed through welding.
Preferably, the side part of the perforating machine head is provided with an operating case, and the bottom end of the base is provided with a ground foot.
Compared with the prior art, the beneficial effects of the utility model are that:
(1) Stop the position fixture block through the design, an equipment section of thick bamboo and end the position dish, end the position dish and install and be used for on being used for fastening commentaries on classics board with fastening screw pivoted, after its fastening finishes, go into the position groove that ends of ending a position dish lateral wall through ending position fixture block one end card, realize rotating the position to fastening commentaries on classics board, effectually avoid it to receive the mistake and bump and cause the rotation, make the high emergence of its frame head change, improve the precision of unmanned aerial vehicle spare part production drilling depth, top spring through the design, top spring exerts the spring action to ending the position fixture block, it is more stable at ending the position inslot to promote its one end card, be difficult for breaking away from, press the briquetting through the design, the convenience shifts down the promotion to ending the position fixture block that is in an equipment section of thick bamboo.
(2) Through the installation slide bar, extrusion spring, clamp plate and the installation section of thick bamboo of design, the clamp plate is connected to the puncher overhead through installation slide bar and installation section of thick bamboo, when making its decline punch, and the clamp plate extrudees with spare part, makes it compress tightly the punching part position, when avoiding it to punch, and this region is in fluffy state and leads to punching counterpoint not accurate, improves the precision of punching.
Drawings
Fig. 1 is a schematic structural view of the present invention;
FIG. 2 is an enlarged view of the point A of FIG. 1 according to the present invention;
FIG. 3 is a rear view of the fastening rotary plate, the stop disc and the stop block of the present invention;
FIG. 4 is an assembled cross-sectional view of the pressing plate, the mounting cylinder and the mounting slide bar of the present invention;
in the figure: 1. a base; 2. erecting a rod; 3. a handle; 4. fastening the rotating plate; 5. a perforating machine head; 6. operating the case; 7. a drill bit; 8. mounting the cylinder; 9. pressing a plate; 10. installing a sliding rod; 11. a stop fixture block; 12. an assembly cartridge; 13. a spring is supported; 14. a strip-shaped slide hole; 15. pressing the block; 16. a stop disc; 17. a stop groove; 18. extruding the spring; 19. and lifting the clamping block.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the 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.
Examples
Referring to fig. 1 to 4, the present invention provides a technical solution: the perforating device for the production of the unmanned aerial vehicle parts comprises a base 1, wherein a vertical rod 2 is fixed on the base 1, a lifting clamping block 19 is sleeved on the vertical rod 2, a perforating machine head 5 is fixed at one end of the lifting clamping block 19, a chuck is arranged at the bottom end of the perforating machine head 5, a perforating drill bit 7 is connected on the chuck, a clamping screw is connected on the lifting clamping block 19, a fastening rotating plate 4 is connected on the clamping screw, a handle 3 is fixed at one end of the fastening rotating plate 4, a stop disc 16 is fixed on the surface of the other end of the fastening rotating plate 4, stop grooves 17 are formed in the side wall of the stop disc 16 in a circular array, an assembling cylinder 12 is fixed on the side wall of the clamping block, a stop clamping block 11 is connected in the assembling cylinder 12 in a sliding manner, the stop clamping block 11, the assembling cylinder 12 and the stop disc 16 are designed, the stop disc 16 is installed on the fastening rotating plate 4 for rotating the clamping screw, after the fastening is finished, one end of a stop fixture block 11 is clamped into a stop groove 17 on the side wall of a stop disc 16, so that the rotation stop of a fastening rotating plate 4 is realized, the rotation caused by the error collision is effectively avoided, the height of a punching head 5 of the punching head is changed, the punching depth precision of the unmanned aerial vehicle part production is improved, one end of the stop fixture block 11 extends into the corresponding stop groove 17, the other end of the stop fixture block 11 is provided with a top spring 13, the top spring 13 exerts an elastic action on the stop fixture block 11 through the designed top spring 13 to push one end of the stop fixture block to be clamped in the stop groove 17 more stably and not to be separated easily, the top spring 13 is positioned in an assembling cylinder 12, the surface of the assembling cylinder 12 is provided with a strip-shaped sliding hole 14, the inner side of the strip-shaped sliding hole 14 is provided with a pressing block 15, the downward movement of the stop fixture block 11 in the assembling cylinder 12 is facilitated through the designed pressing block 15, one end of the pressing block 15 is fixed on the surface of the stop fixture block 11, the cross section of the pressing block 15 is of a convex structure, and the cross section of the assembly cylinder 12 is of a rectangular structure.
In the embodiment, preferably, a pressing plate 9 is arranged at the bottom end of the punching drill 7, four mounting cylinders 8 are fixed on the surface of the pressing plate 9, mounting slide rods 10 and extrusion springs 18 are arranged inside the mounting cylinders 8, the mounting slide rods 10, the extrusion springs 18, the pressing plate 9 and the mounting cylinders 8 are designed, the pressing plate 9 is connected to the punching machine head 5 through the mounting slide rods 10 and the mounting cylinders 8, and when the pressing plate descends to punch, the pressing plate 9 is pressed against parts to compress the punching parts, so that punching misalignment caused by the punching parts being in a fluffy state is avoided, punching precision is improved, the extrusion springs 18 are arranged at the bottom end of the mounting slide rods 10, the mounting slide rods 10 are fixed at the bottom of the punching machine head 5, the longitudinal section of the mounting slide rods 10 is of a T-shaped structure, the cross section of the pressing plate 9 is of a circular structure, the central axis of the pressing plate 9 and the central axis of the punching drill 7 are mutually overlapped, the pressing plate 9 and the mounting cylinders 8 are fixed by welding, an operating cabinet 6 is arranged on the side portion of the punching machine head 5, and the bottom end of the base 1 is provided with feet.
The utility model discloses a theory of operation and use flow: the utility model discloses in use, the tight piece 19 of lift clamp that becomes flexible is changeed through fastening commentaries on classics board 4, so that adjust the whole height of aircraft nose 5 that punches, when tight piece 19 of lift clamp that becomes flexible, press down the position fixture block 11 to ending through pressing the briquetting 15, make its one end break away from in ending the position groove 17, and then can rotate fastening commentaries on classics board 4, realize the tight piece 19 tightness adjustment of clamp that goes up and down, treat that it adjusts the back that finishes, will end position fixture block 11 one end card once more and go into the position groove 17 inside that ends position dish 16, rotate the position that ends to fastening commentaries on classics board 4, avoid its mistake to bump and cause aircraft nose 5 that punches to become flexible, change the height, influence unmanned aerial vehicle spare part precision of punching, the utility model discloses in punching, aircraft nose 5 decline in-process, clamp plate 9 presses in the region of punching, to its face compaction that punches, avoid it to take place the covering or awning on and cause the location not accurate.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various 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 (7)
1. Perforating device is used in production of unmanned aerial vehicle spare part, including base (1), be fixed with pole setting (2) on base (1), the cover is equipped with the tight piece (19) of lift clamp on pole setting (2), the one end of the tight piece (19) of lift clamp is fixed with puncher head (5), the bottom of puncher head (5) is provided with the chuck, be connected with drill bit (7) on the chuck, be connected with clamping screw on the tight piece (19) of lift clamp, the last fastening that is connected with of clamping screw changes board (4), the one end of fastening commentaries on classics board (4) is fixed with handle (3), its characterized in that: the surface of the other end of the fastening rotating plate (4) is fixed with a stop disc (16), the side wall of the stop disc (16) is a circular array and is provided with a stop groove (17), the side wall of the clamping block is fixed with an assembling cylinder (12), the inside of the assembling cylinder (12) is connected with a stop fixture block (11) in a sliding mode, one end of the stop fixture block (11) extends to the inside of the corresponding stop groove (17), the other end of the stop fixture block (11) is provided with a top spring (13), and the top spring (13) is located inside the assembling cylinder (12).
2. Perforating device is used in production of unmanned aerial vehicle spare part according to claim 1, characterized in that: the surface of the assembling cylinder (12) is provided with a strip-shaped sliding hole (14), the inner side of the strip-shaped sliding hole (14) is provided with a pressing block (15), and one end of the pressing block (15) is fixed on the surface of the stop clamping block (11).
3. The perforating device is used in production of unmanned aerial vehicle spare part of claim 2, characterized in that: the cross section of the pressing block (15) is of a convex structure, and the cross section of the assembling cylinder (12) is of a rectangular structure.
4. Perforating device is used in production of unmanned aerial vehicle spare part according to claim 1, characterized in that: the bottom of punch bit (7) is provided with clamp plate (9), the fixed surface of clamp plate (9) has four installation section of thick bamboo (8), and the inside of installation section of thick bamboo (8) is provided with installation slide bar (10) and extrusion spring (18), and extrusion spring (18) are located the bottom of installation slide bar (10), installation slide bar (10) are fixed in punch aircraft nose (5) bottom.
5. The perforating device is used in production of unmanned aerial vehicle spare part of claim 4, characterized in that: the longitudinal section of the mounting sliding rod (10) is of a T-shaped structure, and the cross section of the pressing plate (9) is of a circular structure.
6. The perforating device is used in production of unmanned aerial vehicle spare part of claim 5, characterized in that: the central axis of the pressing plate (9) and the central axis of the punching drill bit (7) are overlapped, and the pressing plate (9) and the mounting cylinder (8) are fixed through welding.
7. The perforating device is used in production of unmanned aerial vehicle spare part of claim 4, characterized in that: the side part of the punching machine head (5) is provided with an operating machine box (6), and the bottom end of the base (1) is provided with a ground foot.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222035900.2U CN218109415U (en) | 2022-08-04 | 2022-08-04 | Perforating device is used in production of unmanned aerial vehicle spare part |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222035900.2U CN218109415U (en) | 2022-08-04 | 2022-08-04 | Perforating device is used in production of unmanned aerial vehicle spare part |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218109415U true CN218109415U (en) | 2022-12-23 |
Family
ID=84522121
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202222035900.2U Expired - Fee Related CN218109415U (en) | 2022-08-04 | 2022-08-04 | Perforating device is used in production of unmanned aerial vehicle spare part |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218109415U (en) |
-
2022
- 2022-08-04 CN CN202222035900.2U patent/CN218109415U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20221223 |