CN216859518U - Military aviation spare anchor clamps convenient to adjust - Google Patents
Military aviation spare anchor clamps convenient to adjust Download PDFInfo
- Publication number
- CN216859518U CN216859518U CN202220679624.0U CN202220679624U CN216859518U CN 216859518 U CN216859518 U CN 216859518U CN 202220679624 U CN202220679624 U CN 202220679624U CN 216859518 U CN216859518 U CN 216859518U
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- threaded rod
- upper base
- clamping
- base
- head
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- 238000009434 installation Methods 0.000 abstract description 20
- 238000000034 method Methods 0.000 description 3
- 238000010276 construction Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
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Abstract
The utility model discloses a military aviation part clamp convenient to adjust, which comprises a lower base, an enclosing table and a threaded rod, wherein the top end of the lower base is provided with an upper base, and the other side of the threaded rod is provided with a chuck structure. According to the military aviation piece clamp, the connecting structure is arranged, an operator can firstly install the lower base on the operating platform through bolts when installing the military aviation piece clamp, after the installation is finished, the upper base can be placed on the lower base, the central positioning rod can be used for positioning, then the limiting platform can be installed, the lower base and the upper base can be connected together by rotating the limiting platform, when the limiting platform is loosened, the upper base can be subjected to auxiliary rotating adjustment, when the military aviation piece clamp is disassembled, the limiting platform can be disassembled, then the upper base is taken down from the lower base, so that the upper base and parts above the upper base can be maintained and cleaned independently, the lower base is left on the operating platform, when the upper base is installed next time, the military aviation piece clamp can be directly positioned, and the separability of the military aviation piece clamp when in use is realized.
Description
Technical Field
The utility model relates to the technical field of military aviation part clamps, in particular to a military aviation part clamp convenient to adjust.
Background
The fixture is a device for fixing a processing object to a correct position in a mechanical manufacturing process so as to receive construction or detection, and is also called a fixture, and broadly speaking, a device for quickly, conveniently and safely installing a workpiece in any process in a technological process is called a fixture, such as a welding fixture, an inspection fixture, an assembly fixture, a machine tool fixture and the like, wherein the machine tool fixture is the most common;
traditional military aviation spare anchor clamps are after installing, and general formula as an organic whole, if the anchor clamps pull down the back and install next time, generally need carry out the location of coordinate again, comparatively inconvenient when using, consequently need improve it, make its use of being convenient for more.
SUMMERY OF THE UTILITY MODEL
Technical problem to be solved
The utility model aims to provide a military aviation piece clamp convenient to adjust, which is used for solving the defect that the existing military aviation piece clamp is inconvenient to disassemble, assemble and position.
(II) contents of utility model
In order to solve the technical problems, the utility model provides the following technical scheme: the utility model provides a for military use aviation spare anchor clamps convenient to adjust, includes base, encloses platform and threaded rod down, the top of base is provided with the base down, the inside of going up the base is provided with connection structure, the top of going up the base is fixed with encloses the platform, the inside of enclosing the platform is provided with the threaded rod, one side of threaded rod is provided with auxiliary structure, the opposite side of threaded rod is provided with chuck structure.
Preferably, the connecting structure comprises a positioning rod, a threaded rod and a limiting table, the positioning rod is arranged inside the upper base, the top end of the positioning rod is provided with the threaded rod, and the limiting table is fixed at the top end of the threaded rod. The separability of the device is achieved.
Preferably, the cross section of the positioning rod is smaller than that of the upper base, and the positioning rod and the upper base form a rotatable structure.
Preferably, the auxiliary structure includes draw-in groove, joint post and runner, the draw-in groove sets up in one side of threaded rod, the inside of draw-in groove is provided with the joint post, one side of joint post is fixed with the runner. The rotating wheel is convenient to disassemble and assemble.
Preferably, the cross section of the clamping groove is larger than that of the clamping column, and the clamping groove and the clamping column form a detachable structure.
Preferably, the chuck structure includes mount pad, installation head, clamping head and rubber pad, the mount pad is fixed in the opposite side of threaded rod, the inside of mount pad is provided with the installation head, one side of installation head is fixed with the clamping head, the rubber pad is installed to one side of clamping head. The damage to the workpiece can be reduced during clamping.
Preferably, the cross section of the mounting seat is larger than that of the mounting head, and the mounting seat and the mounting head form a clamping structure.
(III) advantageous effects
The utility model provides a military aviation spare anchor clamps convenient to adjust, its advantage lies in: through the arrangement of the connecting structure, during installation, an operator can firstly install the lower base on the operating platform through bolts, after the lower base is installed, the upper base can be placed on the lower base, the central positioning rod can be used for positioning, then the limiting platform can be installed, the lower base and the upper base can be connected together by rotating the limiting platform, and when the limiting platform is loosened, the upper base can be subjected to auxiliary rotating adjustment;
the auxiliary structure is arranged, the clamping groove is formed in the end of the threaded rod, and the clamping column at the side end of the rotating wheel is inserted into the clamping groove, so that the rotating wheel can be rotated to rotate the threaded rod, and along with the completion of the operation, an operator can directly pull the rotating wheel down, thereby avoiding the influence on the trend of a cutter due to the existence of the rotating wheel and realizing the safety of the clamp for military aviation parts during use;
through being provided with the chuck structure, the holding head is inserted on the mount pad of threaded rod front end through the installation head, and when the rubber pad of the overhead installation of holding can avoid the holding head to compress tightly the work piece, causes the damage to the work piece, and the detachability of holding head, and the operating personnel of being convenient for changes it, has realized the convenience when this for military use aviation spare anchor clamps holding head is changed.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly introduced below, and it is obvious that the drawings in the following description are some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without creative efforts.
FIG. 1 is a schematic front sectional view of the present invention;
FIG. 2 is a schematic top view of the present invention;
FIG. 3 is a schematic three-dimensional structure of the connection structure of the present invention;
FIG. 4 is a schematic front sectional view of the auxiliary structure of the present invention;
FIG. 5 is a schematic diagram of a cross-sectional front view of the chuck structure of the present invention.
In the figure: 1. a lower base; 2. a connecting structure; 201. positioning a rod; 202. screwing; 203. a limiting table; 3. an upper base; 4. enclosing the platform; 5. an auxiliary structure; 501. a card slot; 502. a clamping column; 503. a rotating wheel; 6. a threaded rod; 7. a chuck structure; 701. a mounting seat; 702. a mounting head; 703. a clamping head; 704. and (7) a rubber pad.
Detailed Description
In order to make the objects, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are some, but not all, embodiments of the present invention. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without any inventive step, are within the scope of the present invention.
In the description of the present invention, it should be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, e.g., as meaning either a fixed connection, a removable connection, or an integral connection; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.
Example one
Referring to fig. 1-5, an embodiment of the present invention is shown: a military aviation spare part clamp convenient to adjust comprises a lower base 1, an enclosing table 4 and a threaded rod 6, wherein the top end of the lower base 1 is provided with an upper base 3, the inside of the upper base 3 is provided with a connecting structure 2, the connecting structure 2 comprises a positioning rod 201, a threaded rod 202 and a limiting table 203, the positioning rod 201 is arranged inside the upper base 3, the top end of the positioning rod 201 is provided with the threaded rod 202, the top end of the threaded rod 202 is fixed with the limiting table 203, the cross section of the positioning rod 201 is smaller than that of the upper base 3, the positioning rod 201 and the upper base 3 form a rotatable structure, the top end of the upper base 3 is fixed with the enclosing table 4, the inside of the enclosing table 4 is provided with the threaded rod 6, one side of the threaded rod 6 is provided with an auxiliary structure 5, and the other side of the threaded rod 6 is provided with a chuck structure 7;
specifically, when in use, firstly, an operator can firstly install the lower base 1 on the operating platform through bolts, after the lower base 1 is installed, the upper base 3 can be placed on the lower base 1, the central positioning rod 201 can be used for positioning, then the limiting platform 203 can be installed, the lower base 1 and the upper base 3 can be connected together by rotating the limiting platform 203, when the limiting platform 203 is loosened, the upper base 3 can be subjected to auxiliary rotation adjustment, when the device is disassembled, the limiting platform 203 can be disassembled, then the upper base 3 is taken down from the lower base 1, so that the upper base 3 and parts above the upper base 3 can be maintained and cleaned independently, the lower base 1 is left on the operating platform, when the upper base 3 is installed next time, the positioning can be directly carried out, or the operator can directly install the upper base 3 on the operating platform, the through groove at the center can be used for collecting scraps to prevent the scraps from influencing the processing process, along with the completion of installation, operating personnel alright put the work piece in enclosing the inside of platform 4, rotate threaded rod 6 and carry out the centre gripping to the work piece can.
Example two
This embodiment still includes: the auxiliary structure 5 comprises a clamping groove 501, a clamping column 502 and a rotating wheel 503, the clamping groove 501 is arranged on one side of the threaded rod 6, the clamping column 502 is arranged inside the clamping groove 501, the rotating wheel 503 is fixed on one side of the clamping column 502, the cross section of the clamping groove 501 is larger than that of the clamping column 502, the clamping groove 501 and the clamping column 502 form a detachable structure, the chuck structure 7 comprises an installation seat 701, an installation head 702, a clamping head 703 and a rubber pad 704, the installation seat 701 is fixed on the other side of the threaded rod 6, the installation head 702 is arranged inside the installation seat 701, the clamping head 703 is fixed on one side of the installation head 702, the rubber pad 704 is installed on one side of the clamping head 703, the cross section of the installation seat 701 is larger than that of the installation head 702, and the installation seat 701 and the installation head 702 form a clamping structure;
specifically, during the use, processing has draw-in groove 501 in the end department of threaded rod 6, the joint post 502 of runner 503 side inserts in draw-in groove 501, so can rotate runner 503 and come to carry out the pivoted operation to threaded rod 6, along with the operation finishes, operating personnel can directly pull out runner 503, can avoid runner 503 to exist, influence the cutter trend, pull down back runner 503 simultaneously, operating personnel is through continuing to rotate threaded rod 6, can pull down threaded rod 6, be convenient for change its maintenance, simultaneously, clamping head 703 inserts on the mount pad 701 of threaded rod 6 front end through installation head 702, when the rubber pad 704 of installation on clamping head 703 can avoid clamping head 703 to compress tightly the work piece, cause the damage to the work piece, and clamping head's detachability, the operating personnel of being convenient for change it.
In the description of the present invention, it should be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, e.g., as meaning either a fixed connection, a removable connection, or an integral connection; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.
The above-described embodiments of the apparatus are merely illustrative, and the units described as separate parts may or may not be physically separate, and parts displayed as units may or may not be physical units, may be located in one place, or may be distributed on a plurality of network units. Some or all of the modules may be selected according to actual needs to achieve the purpose of the solution of the present embodiment. One of ordinary skill in the art can understand and implement it without inventive effort.
Finally, it should be noted that: the above examples are only intended to illustrate the technical solution of the present invention, but not to limit it; although the present invention has been described in detail with reference to the foregoing embodiments, it will be understood by those of ordinary skill in the art that: the technical solutions described in the foregoing embodiments may still be modified, or some technical features may be equivalently replaced; and such modifications or substitutions do not depart from the spirit and scope of the corresponding technical solutions of the embodiments of the present invention.
Claims (7)
1. The utility model provides a military aviation spare anchor clamps convenient to adjust, includes lower base (1), encloses platform (4) and threaded rod (6), its characterized in that: the top end of the lower base (1) is provided with an upper base (3);
a connecting structure (2) is arranged inside the upper base (3), and a surrounding table (4) is fixed at the top end of the upper base (3);
enclose the inside of platform (4) and be provided with threaded rod (6), one side of threaded rod (6) is provided with auxiliary structure (5), the opposite side of threaded rod (6) is provided with chuck structure (7).
2. The military aerial part clamp of claim 1, wherein: the connecting structure (2) comprises a positioning rod (201), a threaded rod (202) and a limiting table (203), the positioning rod (201) is arranged inside the upper base (3), the threaded rod (202) is arranged at the top end of the positioning rod (201), and the limiting table (203) is fixed at the top end of the threaded rod (202).
3. The military aerial part clamp of claim 2, wherein: the cross section of the positioning rod (201) is smaller than that of the upper base (3), and the positioning rod (201) and the upper base (3) form a rotatable structure.
4. The military aerial part clamp of claim 1, wherein: auxiliary structure (5) include draw-in groove (501), joint post (502) and runner (503), draw-in groove (501) set up in one side of threaded rod (6), the inside of draw-in groove (501) is provided with joint post (502), one side of joint post (502) is fixed with runner (503).
5. The military aerial part clamp of claim 4, wherein: the cross section of the clamping groove (501) is larger than that of the clamping column (502), and the clamping groove (501) and the clamping column (502) form a detachable structure.
6. The military aerial part clamp of claim 1, wherein: the clamping head structure (7) comprises a mounting seat (701), a mounting head (702), a clamping head (703) and a rubber pad (704), wherein the mounting seat (701) is fixed to the other side of the threaded rod (6), the mounting head (702) is arranged inside the mounting seat (701), the clamping head (703) is fixed to one side of the mounting head (702), and the rubber pad (704) is installed on one side of the clamping head (703).
7. The military aerial part clamp of claim 6, wherein: the cross section of the mounting seat (701) is larger than that of the mounting head (702), and the mounting seat (701) and the mounting head (702) form a clamping structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220679624.0U CN216859518U (en) | 2022-03-25 | 2022-03-25 | Military aviation spare anchor clamps convenient to adjust |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220679624.0U CN216859518U (en) | 2022-03-25 | 2022-03-25 | Military aviation spare anchor clamps convenient to adjust |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216859518U true CN216859518U (en) | 2022-07-01 |
Family
ID=82124673
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202220679624.0U Expired - Fee Related CN216859518U (en) | 2022-03-25 | 2022-03-25 | Military aviation spare anchor clamps convenient to adjust |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216859518U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115401481A (en) * | 2022-09-20 | 2022-11-29 | 江苏太平洋精锻科技股份有限公司 | Device for positioning workpiece by positioning fixture for lathe machining |
-
2022
- 2022-03-25 CN CN202220679624.0U patent/CN216859518U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115401481A (en) * | 2022-09-20 | 2022-11-29 | 江苏太平洋精锻科技股份有限公司 | Device for positioning workpiece by positioning fixture for lathe machining |
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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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20220701 |