CN211517557U - Stable aviation scissors - Google Patents
Stable aviation scissors Download PDFInfo
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- CN211517557U CN211517557U CN201922416838.XU CN201922416838U CN211517557U CN 211517557 U CN211517557 U CN 211517557U CN 201922416838 U CN201922416838 U CN 201922416838U CN 211517557 U CN211517557 U CN 211517557U
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Abstract
The utility model provides a firm type aviation is cut, including the rotating pin, firm piece, spacing piece, a fixing member, a fastening piece, first fixed orifices, the mounting groove, installation piece and second fixed orifices, the installation piece is installed in the inside left side of scissors handle, the inside second fixed orifices of having seted up of installation piece, first fixed orifices has been seted up in the inside left side of scissors handle, first fixed orifices internally mounted has the mounting, the welding of installation piece left end face has firm piece, the mounting groove has been seted up to firm piece inside, inside scissors sword right side installation to the mounting groove, firm piece and firm piece cross section install the rotating pin, firm piece up end is installed spacing piece, bilateral symmetry installs the fastening piece around the spacing piece up end, this design has solved the not good enough problem of original aviation firm effect, the utility model discloses rational in infrastructure, increase aviation and cut stability in use, firm effectual.
Description
Technical Field
The utility model relates to a firm type aviation is cut belongs to the aviation and cuts technical field.
Background
The scissors are double-edge tools for cutting sheet or linear objects such as cloth, paper, steel plates, ropes, round steel and the like, and the two edges are staggered and can be opened and closed. In China, due to the development of the textile industry, the scissors and scissors industry are distinguished. If a user cuts a knife, the user is called a scissors, the shape of the scissors is like an iron column which is folded in half, the tip of the scissors is opposite to a knife edge, and the lady's red silk is commonly used for weaving. Wherein, aviation scissors also belongs to one kind of scissors.
Present aviation is cut firm effect not good enough, and the scissors sword of aviation is connected with the scissors handle, but the steadiness of scissors sword and scissors handle junction is not good enough, and the scissors sword breaks away from the scissors handle easily, and the problem that above-mentioned appearance appears is cut to firm type aviation of now urgent need.
Disclosure of Invention
Not enough to prior art exists, the utility model aims at providing a firm type aviation is cut to solve the problem that proposes in the above-mentioned background art, the utility model discloses rational in infrastructure increases the aviation and cuts stability in use, and is firm effectual.
In order to achieve the above purpose, the present invention is realized by the following technical solution: a stable aviation scissors comprises a scissors blade, an axis pin, a stable component and a scissors handle, wherein the axis pin is installed at the intersection of the scissors blade, the scissors handle is installed on the right side of the scissors blade, the stable component is arranged at the joint of the scissors handle and the scissors blade, the stable component comprises a rotating pin, a stable block, a limiting piece, a fixing piece, a fastener, a first fixing hole, a mounting groove, a mounting block and a second fixing hole, the mounting block is installed on the left side inside the scissors handle, a second fixing hole is formed inside the mounting block, the first fixing hole is formed on the left side inside the scissors handle, the fixing piece is installed inside the first fixing hole, the stable block is welded on the left end face of the mounting block, the mounting groove is formed inside the stable block, the right side of the scissors blade is installed inside the mounting groove, and the rotating pin is installed at the intersection of the stable block and the, the upper end face of the stabilizing block is provided with a limiting piece, and the front side and the rear side of the upper end face of the limiting piece are symmetrically provided with fasteners.
Furthermore, fastening holes are formed in the fixing blocks and matched with the fastening pieces.
Further, the stabilizing block is matched with the mounting groove.
Furthermore, the aperture of the first fixing hole is the same as that of the second fixing hole, the first fixing hole is matched with the fixing piece, and the second fixing hole is matched with the fixing piece.
Furthermore, a pin hole is formed in the left side of the inner portion of the stabilizing block and is matched with the rotating pin.
Further, the stabilizing blocks are provided with two groups, the specifications of the two groups of stabilizing blocks are the same, the sizes of the two groups of mounting blocks are the same, and the specifications of the two fixing pieces are the same.
The utility model has the advantages that: the utility model discloses a firm type aviation is cut, because of the utility model discloses added rotational pin, firm piece, spacing piece, mounting, fastener, first fixed orifices, mounting groove, installation piece and second fixed orifices, this design has increased the use steadiness that the aviation was cut, has solved original aviation and has cut firm effect not good enough problem, has improved the utility model discloses a stability in use.
Because of the inside fastening hole of having seted up of firm piece, and fastening hole and fastener phase-match, make things convenient for the installation of fastener, because of firm piece and mounting groove phase-match, make things convenient for firm piece to install inside the mounting groove, because of first fixed orifices aperture is the same with second fixed orifices aperture, first fixed orifices and mounting phase-match, second fixed orifices and mounting phase-match, make things convenient for inside the mounting imbeds to first fixed orifices and second fixed orifices, because of the pinhole has been seted up in the inside left side of firm piece, and pinhole and rotating pin phase-match, make things convenient for the installation of rotating pin, the utility model discloses it is rational in infrastructure, increase aviation and cut stability in utilization, it is firm effectual.
Drawings
Other features, objects and advantages of the invention will become more apparent upon reading of the detailed description of non-limiting embodiments with reference to the following drawings:
fig. 1 is a top view of a steady type aviation shears of the present invention;
fig. 2 is a top view of a stabilizing assembly in the stabilizing type aviation shears of the present invention;
fig. 3 is a top view of a scissor handle in the stable aviation scissor of the present invention;
fig. 4 is a front sectional view of a stabilizing block in the stabilizing type aviation shears of the present invention;
in the figure: 1-scissor edge, 2-axle center pin, 3-stabilizing component, 4-scissor handle, 31-rotating pin, 32-stabilizing block, 33-limiting piece, 34-fixing piece, 35-fastening piece, 36-first fixing hole, 37-mounting groove, 38-mounting block, 39-second fixing hole and 351-fastening hole.
Detailed Description
In order to make the technical means, creation features, achievement purposes and functions of the present invention easy to understand, the present invention is further described below with reference to the following embodiments.
Referring to fig. 1-4, the present invention provides a technical solution: the utility model provides a firm type aviation is cut, includes shear blade 1, axle center round pin 2, stabilizes subassembly 3 and shear handle 4, and axle center round pin 2 is installed to shear blade 1 cross, and shear handle 4 is installed to shear blade 1 right side, and shear handle 4 is provided with stabilizes subassembly 3 with shear blade 1 junction.
Fastening hole 351 has been seted up to firm piece 32 inside, and fastening hole 351 and fastener 35 phase-match, make things convenient for the installation of fastener 35, firm piece 32 and mounting groove 37 phase-match, make things convenient for firm piece 32 to install inside mounting groove 37, first fixed orifices 36 aperture is the same with second fixed orifices 39 aperture, first fixed orifices 36 and mounting 34 phase-match, second fixed orifices 39 and mounting 34 phase-match, make things convenient for mounting 34 to imbed inside first fixed orifices 36 and second fixed orifices 39, the pinhole has been seted up to the inside left side of firm piece 32, and pinhole and rotating pin 31 phase-match, make things convenient for the installation of rotating pin 31, firm piece 32 is equipped with two sets ofly, and two sets of firm piece 32 specifications are the same, mounting piece 38 is equipped with two sets ofly, and two sets of 38 specifications of mounting piece are the same, mounting 34 is equipped with two, and two 34 specifications of mounting are the same, increase.
As an embodiment of the present invention: inside steady piece 32 right side is embedded into scissors handle 4, fixing member 34 is embedded into inside first fixed orifices 36 and second fixed orifices 39 in proper order, firm piece 32 realizes firm the connection with scissors handle 4, mounting groove 37 has been seted up to the inside left side of firm piece 32, it is inside that shear blade 1 right side is embedded into mounting groove 37, spacing piece 33 is installed at firm piece 32 up end, fastener 35 is embedded into inside fastening hole 351, shear blade 1 realizes firm the connection with firm piece 32, and rotating pin 31 is installed to two sets of firm piece 32 intersections, pass through fastener 35, firm piece 32, spacing piece 33 and fixing member 34's interpolation, the use steadiness of aviation scissors has effectively been increased.
The basic principles and the main features of the invention and the advantages of the invention have been shown and described above, it will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrative embodiments, but that the invention may be embodied in other specific forms without departing from the spirit or essential characteristics of the invention. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Furthermore, it should be understood that although the present description refers to embodiments, not every embodiment may contain only a single embodiment, and such description is for clarity only, and those skilled in the art should integrate the description, and the embodiments may be combined as appropriate to form other embodiments understood by those skilled in the art.
Claims (6)
1. The utility model provides a firm type aviation is cut, includes scissors sword, axle center round pin, firm subassembly and scissors handle, its characterized in that: a pivot pin is arranged at the intersection of the shear blades, a shear handle is arranged on the right side of the shear blades, and a stabilizing component is arranged at the joint of the shear handle and the shear blades;
the fixing component comprises a rotating pin, a fixing block, a limiting piece, a fixing piece, a fastener, a first fixing hole, a mounting groove, a mounting block and a second fixing hole, the mounting block is installed on the left side inside the shear handle, the second fixing hole is formed inside the mounting block, the first fixing hole is formed in the left side inside the shear handle, the fixing piece is installed inside the first fixing hole, the fixing piece is welded to the left end face of the mounting block, the mounting groove is formed inside the fixing block, the right side of the shear blade is installed inside the mounting groove, the rotating pin is installed at the intersection of the fixing block and the fixing block, the limiting piece is installed on the upper end face of the fixing block, and the fastener is symmetrically installed on the front side and the rear side of the upper end.
2. A robust aerial shear as defined in claim 1, wherein: the inside fastening hole that has seted up of firm piece, and fastening hole and fastener match.
3. A robust aerial shear as defined in claim 1, wherein: the stabilizing block is matched with the mounting groove.
4. A robust aerial shear as defined in claim 1, wherein: the first fixing hole is the same as the second fixing hole in diameter, the first fixing hole is matched with the fixing piece, and the second fixing hole is matched with the fixing piece.
5. A robust aerial shear as defined in claim 1, wherein: the left side of the inner part of the stabilizing block is provided with a pin hole, and the pin hole is matched with the rotating pin.
6. A robust aerial shear as defined in claim 1, wherein: the fixing device is characterized in that the fixing blocks are two groups, the specifications of the two groups of fixing blocks are the same, the sizes of the two groups of mounting blocks are the same, and the specifications of the two fixing pieces are the same.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922416838.XU CN211517557U (en) | 2019-12-30 | 2019-12-30 | Stable aviation scissors |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922416838.XU CN211517557U (en) | 2019-12-30 | 2019-12-30 | Stable aviation scissors |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211517557U true CN211517557U (en) | 2020-09-18 |
Family
ID=72447975
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201922416838.XU Active CN211517557U (en) | 2019-12-30 | 2019-12-30 | Stable aviation scissors |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211517557U (en) |
-
2019
- 2019-12-30 CN CN201922416838.XU patent/CN211517557U/en active Active
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