CN203245590U - Aircraft seat part assembling auxiliary device - Google Patents
Aircraft seat part assembling auxiliary device Download PDFInfo
- Publication number
- CN203245590U CN203245590U CN 201320196016 CN201320196016U CN203245590U CN 203245590 U CN203245590 U CN 203245590U CN 201320196016 CN201320196016 CN 201320196016 CN 201320196016 U CN201320196016 U CN 201320196016U CN 203245590 U CN203245590 U CN 203245590U
- Authority
- CN
- China
- Prior art keywords
- gangbar
- aircraft seat
- lifting platform
- round bar
- cylinder
- 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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- Forklifts And Lifting Vehicles (AREA)
Abstract
The utility model discloses an aircraft seat part assembling auxiliary device. The aircraft seat part assembling auxiliary device comprises sliding rails, a lifting platform and a working platform. The bottom portion of the lifting platform is provided with sliding wheels, the sliding wheels are located in the sliding rails and can slide in the sliding rails back and forth, the working platform is connected to a lifting mechanism of the lifting platform, and the working platform comprises a supporting plate, a connecting frame and a clamping control device. According to the aircraft seat part assembling auxiliary device, a seat framework can be automatically turned over according to needs, and installation personnel only need to fixedly stand on a procedure point so that various parts can be installed. Operation is convenient and simple, frequent moving is not needed, labor and materials are saved, and assembling efficiency is greatly improved.
Description
Technical field
The utility model relates to aircraft seat accessory installing apparatus, is specifically related to a kind of aircraft seat accessory assembling servicing unit.
Background technology
Seat is the main device in the aircraft passenger compartment, and after the passenger entered the cabin, main activity was all finished on the seat, so security and comfortableness are to weigh two important standards of aircraft seat.Aircraft seat production installation process need to be with package, such as cotton material, backguy etc. is assembled in the chair framework, assembling mode in the past is to use staff to install one by one, because row's aircraft seat has several seats, if using staff installs, then need often mobile each position of assembling of installation personnel, unreasonable and the wasting phenomenon that in the flow sequence such as storage of material handling, personnel operation, personnel's wait, material, exists, the installation effectiveness of seat part is low, and the security of seat also can not get good assurance.
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 accessory assembling servicing unit, automatic turning seat skeleton as required, and installation personnel only needs fixed station just various accessories can be installed on a flow points; Convenient and simple, do not need frequent movement, significantly improve efficiency of assembling.
For addressing the above problem, the technical scheme that the utility model adopts is as follows:
A kind of aircraft seat accessory assembling servicing unit comprises slide rail, lifting platform, workbench, and the lifting platform bottom is equipped with movable pulley, and movable pulley is arranged in slide rail and can slidably reciprocates at slide rail; Described workbench is connected on the elevating mechanism of lifting platform, and it comprises gripper shoe, link and claming controller;
Be provided with the locating slot vertical with the lifting platform glide direction on the described gripper shoe, round bar is installed in the locating slot, locating slot is all stretched out at the round bar two ends, the one end side fixed head that removably connects;
Described claming controller comprises cylinder, control panel, driving lever and gangbar, wherein cylinder is installed on the link, driving lever is connected on the linking arm of cylinder, gangbar installation parallel with driving lever also connects by jig arm, gangbar can be rotated in jig arm, and wherein a unidirectional end of gangbar and driving lever is fixed on the fixed head of side; Hinged at least two locating pieces on the described gangbar, the locating piece front end is free end, during work, free end is clamped on the round bar and with round bar to be fixed; Described control panel is installed in the work of link one side control cylinder.
The utility model can also be realized by following preferred mode:
Preferred embodiment a kind of as the utility model, on the basis of such scheme, the quantity of described locating slot is two, and two locating slots are set in parallel on the gripper shoe, and described round bar quantity is two, is installed in the locating slot respectively.
Preferred embodiment a kind of as the utility model, on the basis of such scheme, described locating piece is four, and wherein on the gangbar of the both sides of two linking arms that are hinged on cylinder, two other is positioned at the two ends of gangbar.
Preferred embodiment a kind of as the utility model, on the basis of such scheme, the front end of described jig arm extends extension arm, and the position at the corresponding round bar of extension arm place is provided with groove.
Preferred embodiment a kind of as the utility model, on the basis of such scheme, described workbench 360 degree are rotatably connected on lifting platform.
Compared to existing technology, the beneficial effects of the utility model are: aircraft seat accessory assembling servicing unit described in the utility model is the automatic turning seat skeleton as required, and installation personnel only needs fixed station just various accessories can be installed on a flow points; Easy to operate simple, do not need frequent movement, use manpower and material resources sparingly, significantly improve efficiency of assembling.
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 accessory assembling assistant apparatus structure schematic diagram described in the utility model.
The specific embodiment
As shown in Figure 1, aircraft seat accessory assembling servicing unit described in the utility model comprises slide rail 1, lifting platform 2, workbench 3, and lifting platform 2 bottoms are equipped with movable pulley 15, and movable pulley 15 is arranged in slide rail 1 and can slidably reciprocates at slide rail 1; Workbench 5 is connected on the elevating mechanism of lifting platform 2, and it comprises gripper shoe, link and claming controller;
Be provided with the locating slot 16 vertical with lifting platform 2 glide directions on the described gripper shoe, round bar 10 is installed in the locating slot 16, locating slot 16 is all stretched out at round bar 10 two ends, the one end side fixed head 13 that removably connects;
Described claming controller comprises cylinder 4, control panel 3, driving lever 7 and gangbar 9, wherein cylinder 4 is installed on the link, driving lever 7 is connected on the linking arm of cylinder 4, gangbar 9 installation parallel with driving lever also passed through jig arm 6 connections, gangbar 9 can be rotated in jig arm 6, and wherein a unidirectional end of gangbar 9 and driving lever 7 is fixed on the side fixed head 13; Hinged at least two locating pieces 14 on the described gangbar 9, locating piece 14 front ends are free end, during work, free end is clamped on the round bar 10 and with round bar 10 to be fixed; Described control panel 3 is installed in the work of link one side control cylinder 4.
Aircraft seat accessory assembling servicing unit operation principle described in the utility model is as follows: first round bar 10 is put in the locating slot 16, one end is toward being close to side location-plate 13, press the play button on the control panel 3, the locating piece 14 that allows cylinder 4 drive on the gangbar 9 compresses round bar 10, then respective accessory 11 and push away toward centres on from the two ends of round bar 10 toward intermediate sleeve, until the top begins the installation of accessory 11 afterwards again to the solid screw of locating piece 14 rear lockings.
The utility model can also be realized by following preferred mode:
In order to realize simultaneously the more assembling of polygamy spare, further promote operating efficiency, in preferred embodiment of the utility model, on the basis of such scheme, the quantity of described locating slot 16 is two, two locating slots 16 are set in parallel on the gripper shoe, and described round bar 10 quantity are two, are installed in respectively in the locating slot 16.
In order further to strengthen the fixation of gangbar, prevent its swing, preferred embodiment a kind of as the utility model, on the basis of such scheme, described locating piece 14 is four, wherein on the gangbar 9 of two linking arm both sides that are hinged on cylinder, two other is positioned at the two ends of gangbar 9.
Preferred embodiment a kind of as the utility model, on the basis of such scheme, the front end of described jig arm 6 extends extension arm 12, and the position at extension arm 12 corresponding round bars 10 places is provided with groove.
In order to further facilitate the assembling of accessory, preferred embodiment a kind of as the utility model, on the basis of such scheme, described workbench 360 degree are rotatably connected on lifting platform.Workbench 5 can be realized 360 degree rotations at lifting platform 2, and is convenient at the different station installation fitting.
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 (5)
1. an aircraft seat accessory assembles servicing unit, and it is characterized in that: it comprises slide rail, lifting platform, workbench, and the lifting platform bottom is equipped with movable pulley, and movable pulley is arranged in slide rail and can slidably reciprocates at slide rail; Described workbench is connected on the elevating mechanism of lifting platform, comprises gripper shoe, link and claming controller;
Be provided with the locating slot vertical with the lifting platform glide direction on the described gripper shoe, round bar is installed in the locating slot, locating slot is all stretched out at the round bar two ends, the one end side fixed head that removably connects;
Described claming controller comprises cylinder, control panel, driving lever and gangbar, wherein cylinder is installed on the link, driving lever is connected on the linking arm of cylinder, gangbar installation parallel with driving lever also connects by jig arm, gangbar can be rotated in jig arm, and wherein a unidirectional end of gangbar and driving lever is fixed on the fixed head of side; Hinged at least two locating pieces on the described gangbar, the locating piece front end is free end, during work, free end is clamped on the round bar and with round bar to be fixed; Described control panel is installed in the work of link one side control cylinder.
2. aircraft seat accessory according to claim 1 assembles servicing unit, and it is characterized in that: the quantity of described locating slot is two, and two locating slots are set in parallel on the gripper shoe, and described round bar quantity is two, is installed in the locating slot respectively.
3. aircraft seat accessory according to claim 1 assembling servicing unit, it is characterized in that: described locating piece is four, wherein on the gangbar of two linking arm both sides that are hinged on cylinder, two other is positioned at the two ends of gangbar.
4. each described aircraft seat accessory assembles servicing unit according to claim 1-3, and it is characterized in that: the front end of described jig arm extends extension arm, and the position at the corresponding round bar of extension arm place is provided with groove.
5. each described aircraft seat accessory assembles servicing unit according to claim 1-3, it is characterized in that: described workbench 360 degree are rotatably connected on lifting platform.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320196016 CN203245590U (en) | 2013-04-17 | 2013-04-17 | Aircraft seat part assembling auxiliary device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320196016 CN203245590U (en) | 2013-04-17 | 2013-04-17 | Aircraft seat part assembling auxiliary device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203245590U true CN203245590U (en) | 2013-10-23 |
Family
ID=49372051
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201320196016 Expired - Fee Related CN203245590U (en) | 2013-04-17 | 2013-04-17 | Aircraft seat part assembling auxiliary device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203245590U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104476459A (en) * | 2014-12-03 | 2015-04-01 | 重庆红亿机械有限公司 | Clamp for seat assembling |
| CN104942208A (en) * | 2015-06-26 | 2015-09-30 | 芜湖市恒峰科技有限公司 | Rotary working table used for riveting and pressing automobile parts |
-
2013
- 2013-04-17 CN CN 201320196016 patent/CN203245590U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104476459A (en) * | 2014-12-03 | 2015-04-01 | 重庆红亿机械有限公司 | Clamp for seat assembling |
| CN104942208A (en) * | 2015-06-26 | 2015-09-30 | 芜湖市恒峰科技有限公司 | Rotary working table used for riveting and pressing automobile parts |
| CN104942208B (en) * | 2015-06-26 | 2018-03-27 | 芜湖市恒峰科技有限公司 | A kind of rotary table for riveting auto parts machinery |
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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 |