CN209207383U - The mounting tool of aircraft quick-detachable lock - Google Patents
The mounting tool of aircraft quick-detachable lock Download PDFInfo
- Publication number
- CN209207383U CN209207383U CN201822064978.0U CN201822064978U CN209207383U CN 209207383 U CN209207383 U CN 209207383U CN 201822064978 U CN201822064978 U CN 201822064978U CN 209207383 U CN209207383 U CN 209207383U
- Authority
- CN
- China
- Prior art keywords
- fixed column
- product fixed
- plate
- sliding panel
- bottom plate
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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- 238000004519 manufacturing process Methods 0.000 abstract description 6
- 239000000463 material Substances 0.000 abstract description 5
- 239000002699 waste material Substances 0.000 abstract description 5
- 238000009434 installation Methods 0.000 description 3
- 238000005336 cracking Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
Abstract
The mounting tool of aircraft quick-detachable lock, including upper mounted plate (1), support plate (2), bottom plate (3), positioning column (4), sliding panel (5), upper product fixed column (6), lower product fixed column (7) and hydraulic cylinder (8)；The hydraulic cylinder (8) is mounted on upper mounted plate (1)；Between the bottom plate (3) and upper mounted plate (1), it is equipped with positioning column (4) and support plate (2)；The sliding panel (5) is mounted on positioning column (4), and upper product fixed column (6) is equipped with below sliding panel (5)；Lower product fixed column (7) corresponding with upper product fixed column (6) is equipped on the bottom plate (3).The utility model structure is simple, is easy to make, and tooling service efficiency is high；Production efficiency can be greatly improved, the waste of material and mold is reduced.
Description
Technical field
The utility model belongs to mechanical manufacturing field, when relating generally to aircraft quick-detachable lock and being mounted on winged covering.
Background technique
It is existing that the head of quick-detachable lock is withstood using a tooling when installing aircraft quick-detachable lock, in addition with set wound packages stop
Circle is easy to make stopper ring and lock cover out of plumb in this way, causes lock cover surface seriously to pull and cracks with stopper ring, to cause to produce
Product are scrapped, this not only inefficiencies, waste of material, and cause a large amount of economic loss.
Utility model content
The utility model be it is existing when installing aircraft quick-detachable lock in order to solve, withstand quick-detachable lock using a tooling
Head is easy to make in this way stopper ring and lock cover out of plumb in addition with set wound packages stopper ring, cause lock cover surface seriously pull and
Stopper ring cracking, scrap of the product, this not only inefficiencies, waste of material, and the technical issues of cause a large amount of economic loss.
In order to solve the above-mentioned technical problem, the utility model uses following technical proposal:
The mounting tool of aircraft quick-detachable lock, the tooling include upper mounted plate 1, support plate 2, bottom plate 3, positioning column 4, slide
Movable plate 5, upper product fixed column 6, lower product fixed column 7 and hydraulic cylinder 8；
The hydraulic cylinder 8 is mounted on upper mounted plate 1；
Between the bottom plate 3 and upper mounted plate 1, it is equipped with positioning column 4 and support plate 2；
The sliding panel 5 is mounted on positioning column 4, and upper product fixed column 6 is equipped with below sliding panel 5；
Lower product fixed column 7 corresponding with upper product fixed column 6 is equipped on the bottom plate 3.
By adopting the above technical scheme the utility model has the advantages that
1, the utility model structure is simple, is easy to make, and tooling service efficiency is high；
2, the utility model can greatly improve production efficiency, reduce the waste of material and mold.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the utility model;
In figure: 1- upper mounted plate, 2- support plate, 3- bottom plate, 4- positioning column, 5- sliding panel, the upper product of 6- are fixed
Product fixed column, 8- hydraulic cylinder under column, 7-.
Specific embodiment
As shown in Figure 1, the mounting tool of aircraft quick-detachable lock, the tooling include upper mounted plate 1, support plate 2, bottom plate 3,
Positioning column 4, sliding panel 5, upper product fixed column 6, lower product fixed column 7 and hydraulic cylinder 8；
The hydraulic cylinder 8 is mounted on upper mounted plate 1；
Between the bottom plate 3 and upper mounted plate 1, it is equipped with positioning column 4 and support plate 2；
The sliding panel 5 is mounted on positioning column 4, and upper product fixed column 6 is equipped with below sliding panel 5；
Lower product fixed column 7 corresponding with upper product fixed column 6 is equipped on the bottom plate 3.
The utility model is that existing mounting means is converted into assembled tool, needs two people cooperation that could install before, but
After the utility model, a people just carries out installation operation.The height of hydraulic cylinder is adjusted, height and product after each installation
Fitness consistency is very good, and shape appearance is good, high production efficiency, greatly reduces waste of the traditional processing mode to material
And its loss.
It is more convenient that product adjustment is installed.
Using the utility model tooling, product appearance quality after production efficiency and installation is not only increased, and designs letter
Single, easy to implement, significant effect can be widely popularized in mechanical manufacturing field.
Claims (1)
1. the mounting tool of aircraft quick-detachable lock, it is characterized in that: the tooling includes upper mounted plate (1), support plate (2), bottom plate
(3), positioning column (4), sliding panel (5), upper product fixed column (6), lower product fixed column (7) and hydraulic cylinder (8)；
The hydraulic cylinder (8) is mounted on upper mounted plate (1)；
Between the bottom plate (3) and upper mounted plate (1), it is equipped with positioning column (4) and support plate (2)；
The sliding panel (5) is mounted on positioning column (4), and upper product fixed column (6) is equipped with below sliding panel (5)；
Lower product fixed column (7) corresponding with upper product fixed column (6) is equipped on the bottom plate (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822064978.0U CN209207383U (en) | 2018-12-10 | 2018-12-10 | The mounting tool of aircraft quick-detachable lock |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822064978.0U CN209207383U (en) | 2018-12-10 | 2018-12-10 | The mounting tool of aircraft quick-detachable lock |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209207383U true CN209207383U (en) | 2019-08-06 |
Family
ID=67463682
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201822064978.0U Active CN209207383U (en) | 2018-12-10 | 2018-12-10 | The mounting tool of aircraft quick-detachable lock |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209207383U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110802548A (en) * | 2019-10-10 | 2020-02-18 | 中国航空工业集团公司上海航空测控技术研究所 | Quick-release screw assembling device and assembling method |
-
2018
- 2018-12-10 CN CN201822064978.0U patent/CN209207383U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110802548A (en) * | 2019-10-10 | 2020-02-18 | 中国航空工业集团公司上海航空测控技术研究所 | Quick-release screw assembling device and assembling method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: Installation tooling of aircraft quick release lock Effective date of registration: 20221219 Granted publication date: 20190806 Pledgee: China Construction Bank Corporation Zunyi branch Pledgor: GUIZHOU HANGRUI AVIATION PRECISION PARTS MANUFACTURING Co.,Ltd. Registration number: Y2022520000054 |
|
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PC01 | Cancellation of the registration of the contract for pledge of patent right |
Granted publication date: 20190806 Pledgee: China Construction Bank Corporation Zunyi branch Pledgor: GUIZHOU HANGRUI AVIATION PRECISION PARTS MANUFACTURING Co.,Ltd. Registration number: Y2022520000054 |
|
| PC01 | Cancellation of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: Installation tooling for aircraft quick release locks Granted publication date: 20190806 Pledgee: China Construction Bank Corporation Zunyi branch Pledgor: GUIZHOU HANGRUI AVIATION PRECISION PARTS MANUFACTURING Co.,Ltd. Registration number: Y2024520000009 |
|
| PE01 | Entry into force of the registration of the contract for pledge of patent right |