CN203245771U - Aircraft seat framework assembly jig - Google Patents
Aircraft seat framework assembly jig Download PDFInfo
- Publication number
- CN203245771U CN203245771U CN 201320195905 CN201320195905U CN203245771U CN 203245771 U CN203245771 U CN 203245771U CN 201320195905 CN201320195905 CN 201320195905 CN 201320195905 U CN201320195905 U CN 201320195905U CN 203245771 U CN203245771 U CN 203245771U
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- CN
- China
- Prior art keywords
- keel
- control block
- seat
- mobile control
- fixed head
- 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.)
- Expired - Fee Related
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Abstract
The utility model discloses an aircraft seat framework assembly jig which comprises a movable control seat and an assembly jig assembly which is placed on the movable control seat, wherein the assembly jig assembly comprises a keel, a fixing plate, a clamping assembly, a movable limiting piece and at least two supporting seats. According to the aircraft seat framework assembly jig, the relative positions of a framework main keel and armrests and the relative positions of the framework main keel and seat feet can be flexibly adjusted, the framework main keel, the armrests and the seat feet can be flexibly clamped, the whole framework can be assembled only through one person after fixation, and the aircraft seat framework assembly jig is very convenient to operate.
Description
Technical field
The utility model relates to a kind of aircraft seat accessory installing apparatus, is specifically related to a kind of aircraft seat Skeleton assembly anchor clamps.
Background technology
Seat is the main device in the aircraft passenger compartment, and after the passenger entered the cabin, most of the time all finished on the seat, so security and comfortableness are to weigh two important standards of aircraft seat.The installation of aircraft seat is the important step in the aircraft manufacturing process.
The part that aircraft seat relates to is a lot, and assembling in the past generally needs a plurality of staff to finish.When the installation of chair framework, people is the relative position of main joist, handrail, seat pin fixedly, another one people's installation connecting element (such as bolt, gnu etc.) and because aircraft seat one row has a plurality of seats, handrail and seat pin are all more, generally one by one staff fixed installation is more time-consuming.
The utility model content
In order to overcome the deficiencies in the prior art, the purpose of this utility model is to provide a kind of aircraft seat Skeleton assembly anchor clamps, can adjust flexibly relative position with clamping skeleton main joist and handrail, seat pin by anchor clamps, and the fixing assembling that only needs afterwards a people can finish whole skeleton, easy to operate.
For addressing the above problem, the technical scheme that the utility model adopts is as follows:
A kind of support chair Skeleton assembly anchor clamps comprise mobile control block and are positioned at assembling jig assembly on the mobile control block that described assembling jig assembly comprises keel, fixed head, clamping assembly, movable locating part and at least two supporting seats; Described fixed head is fixed on the end on the mobile control block top board, and fixed head is provided with the shrinkage pool that keel are installed; Described supporting seat is fixed on the mobile control block top board on fixed head right side, its top is provided with Baltimore groove, described keel installation rises at the supported mounting of the Baltimore groove of supporting seat, and the left end of keel is buckled in the shrinkage pool on the fixed head, and several backrest frames are socketed on the keel; Described clamping assembly comprises support bar and tong arm, and support bar is fixed on the mobile control block top board, and tong arm is hinged on the support bar, and the front end of tong arm is provided with clamping part, and clamping part be used for to clamp and fixing keel; Described movable locating part is hinged on supporting seat one side, is used for preventing that keel from swinging; Described assembling jig assembly also comprises catch, and described catch lower end is fixed on the mobile control block top board, and the upper end of catch is used for fixedly keel away from an end of fixed head.
The utility model can also be realized by following preferred scheme:
As the utility model a kind of preferred embodiment in, on the basis of such scheme, described keel quantity is two, two keel are installed in parallel on the supporting seat, wherein are socketed backrest frames on keel, socket seat angle on another root keel.。
Compared to existing technology, the beneficial effects of the utility model are: aircraft seat Skeleton assembly anchor clamps described in the utility model can be adjusted the relative position with clamping skeleton main joist and handrail, seat pin flexibly, and only need a people can finish the assembling of whole skeleton after fixing, operation is very easy.
Below in conjunction with the drawings and specific embodiments the utility model is described in further detail.
Description of drawings
Fig. 1 is aircraft seat Skeleton assembly clamp structure schematic diagram described in the utility model.
The specific embodiment
As shown in Figure 1, support chair Skeleton assembly anchor clamps described in the utility model, comprise mobile control block and be positioned at assembling jig assembly on the mobile control block, described assembling jig assembly comprises keel 5, fixed head 1, clamping assembly 7, movable locating part 6 and at least two supporting seats 2; Described fixed head 1 is fixed on the end on the mobile control block top board, and fixed head 1 is provided with the shrinkage pool that keel 5 are installed; Described supporting seat 2 is fixed on the mobile control block top board on fixed head 1 right side, its top is provided with Baltimore groove, the supported seat of the Baltimore groove that described keel 5 are installed in supporting seat 22 is erected, and the left end of keel 5 is buckled in the shrinkage pool on the fixed head, and several backrest frames 3 are socketed on the keel; Described clamping assembly comprises support bar and tong arm, and support bar is fixed on the mobile control block top board, and tong arm is hinged on the support bar, and the front end of tong arm is provided with clamping part, and clamping part be used for to clamp and fixing keel 5; Described movable locating part 6 is hinged on supporting seat one side, is used for preventing that keel 5 from swinging; Described assembling jig assembly also comprises catch, and described catch lower end is fixed on the mobile control block top board, and the upper end of catch is used for fixedly keel 5 away from an end of fixed head.
The utility model can also be realized by following preferred scheme:
In preferred embodiment of the utility model, on the basis of such scheme, described keel 5 quantity are two, and two keel 5 are installed in parallel on the supporting seat 2, wherein are socketed backrest frames 3 on keel, socket seat angle 4 on another root keel.
Above-mentioned embodiment only is preferred embodiment of the present utility model; can not limit with this scope of the utility model protection, the variation of any unsubstantiality that those skilled in the art does on basis of the present utility model and replacement all belong to the utility model scope required for protection.
Claims (2)
1. aircraft seat Skeleton assembly anchor clamps, it is characterized in that: comprise mobile control block and be positioned at assembling jig assembly on the mobile control block, described assembling jig assembly comprises keel, fixed head, clamping assembly, movable locating part and at least two supporting seats; Described fixed head is fixed on the end on the mobile control block top board, and fixed head is provided with the shrinkage pool that keel are installed; Described supporting seat is fixed on the mobile control block top board on fixed head right side, its top is provided with Baltimore groove, described keel installation rises at the supported mounting of the Baltimore groove of supporting seat, and the left end of keel is buckled in the shrinkage pool on the fixed head, and several backrest frames are socketed on the keel; Described clamping assembly comprises support bar and tong arm, and support bar is fixed on the mobile control block top board, and tong arm is hinged on the support bar, and the front end of tong arm is provided with clamping part, and clamping part be used for to clamp and fixing keel; Described movable locating part is hinged on supporting seat one side, is used for preventing that keel from swinging; Described assembling jig assembly also comprises catch, and described catch lower end is fixed on the mobile control block top board, and the upper end of catch is used for fixedly keel away from an end of fixed head.
2. aircraft seat Skeleton assembly anchor clamps according to claim 1, it is characterized in that: described keel quantity is two, two keel are installed in parallel on the supporting seat, wherein are socketed backrest frames on keel, socket seat angle on another root keel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320195905 CN203245771U (en) | 2013-04-17 | 2013-04-17 | Aircraft seat framework assembly jig |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320195905 CN203245771U (en) | 2013-04-17 | 2013-04-17 | Aircraft seat framework assembly jig |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203245771U true CN203245771U (en) | 2013-10-23 |
Family
ID=49372232
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201320195905 Expired - Fee Related CN203245771U (en) | 2013-04-17 | 2013-04-17 | Aircraft seat framework assembly jig |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203245771U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105414958A (en) * | 2015-12-05 | 2016-03-23 | 重庆创力工贸有限公司 | Assembly method of car seat cushion |
| CN106112476A (en) * | 2016-07-13 | 2016-11-16 | 宁波高格汽车装备有限公司 | A kind of Assembling Special Equipment of chair framework |
| CN110405709A (en) * | 2019-07-01 | 2019-11-05 | 安徽瑞佑自动化科技有限公司 | A kind of seat slide mounting work station |
-
2013
- 2013-04-17 CN CN 201320195905 patent/CN203245771U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105414958A (en) * | 2015-12-05 | 2016-03-23 | 重庆创力工贸有限公司 | Assembly method of car seat cushion |
| CN106112476A (en) * | 2016-07-13 | 2016-11-16 | 宁波高格汽车装备有限公司 | A kind of Assembling Special Equipment of chair framework |
| CN106112476B (en) * | 2016-07-13 | 2019-01-29 | 宁波安川汽车装备有限公司 | A kind of Assembling Special Equipment of chair framework |
| CN110405709A (en) * | 2019-07-01 | 2019-11-05 | 安徽瑞佑自动化科技有限公司 | A kind of seat slide mounting work station |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C56 | Change in the name or address of the patentee |
Owner name: ZHONGSHAN?XINHUI PRECISION?TECHNOLOGY CO.,?LTD. Free format text: FORMER NAME: ZHONGSHAN XINHUI AUTOMOBILE MOULD INDUSTRIAL CO., LTD. |
|
| CP03 | Change of name, title or address |
Address after: 528437, Guangdong Province, Zhongshan Torch Development Zone, 13 East River Road, Yu Industrial Park, third first floor, the first first, third floors Patentee after: Zhong Shanxinhui microtechnic limited company Address before: 528437, third first floor, Yu Da Industrial Park, 13 East Yanjiang Road, Torch Development Zone, Guangdong, Zhongshan Patentee before: Xinhui Automobile Industrial Co., Ltd. |
|
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20131023 Termination date: 20180417 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |