CN202716261U - Double-shaft moving working ladder for assembling aircraft - Google Patents
Double-shaft moving working ladder for assembling aircraft Download PDFInfo
- Publication number
- CN202716261U CN202716261U CN2012202627254U CN201220262725U CN202716261U CN 202716261 U CN202716261 U CN 202716261U CN 2012202627254 U CN2012202627254 U CN 2012202627254U CN 201220262725 U CN201220262725 U CN 201220262725U CN 202716261 U CN202716261 U CN 202716261U
- Authority
- CN
- China
- Prior art keywords
- working
- aircraft
- slide rail
- ladder
- sliding rails
- 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
Links
Images
Landscapes
- Ladders (AREA)
Abstract
The utility model relates to a double-shaft moving working ladder for assembling an aircraft, which comprises a working bracket, working supporting legs and a working ladder, wherein the working supporting legs are arranged at the two ends of the bottom of one end of the working bracket, two sliding rails I are arranged on the bottom of the other end of the working bracket in parallel, and are provided with slide blocks I, the slide blocks I are commonly connected with a supporting plate, sliding rails II are arranged on the supporting plate in parallel, the direction of the sliding rails II is vertical to the direction of the sliding rails I, slide blocks II are arranged in the sliding rails II, two supporting rods are movably connected under the side of the outer end of the supporting plate, and the bottom ends of the supporting rods are connected with supporting bases. According to the working ladder, the structure is simple; the position of the working supporting plate can be freely adjusted, so that more parts of the aircraft can be assembled by one working ladder, and in the actual work, the whole working ladder does not need to be moved; and the working ladder is used for a tool for assembling the aircraft, and meanwhile, the working ladder is prevented from being interfered with the aircraft or the tool.
Description
Technical field
But the utility model relates to the aircraft rigger work ladder that a kind of twin shaft moves, and is used for the aircraft assembling process.
Background technology
Aircaft configuration is complicated, needs the occupation of land space large, and its assembling process specification requirement is higher, and thousands of parts need to position, connect, assemble, and workload is very large.Tradition turning over type working stand is because the usage space that needs is larger, and very flexible, as using in baroque aircraft assembling, tends to interfere with aircraft or work because free space is limited.The carrying out that this has not only affected workman's assembly work increased work difficulty, simultaneously also so that the job security reduction.The above-mentioned drawback of work on hand ladder has directly affected the efficiency of assembling of aircraft, has prolonged the aircraft development cycle, can not satisfy the demand that present generation aircraft develops rapidly.
Summary of the invention
But the technical problems to be solved in the utility model provides the aircraft rigger work ladder that twin shaft moves, this working stand is not only simple in structure, but and the position free adjustment of work gripper shoe, thereby realized a working stand to aircraft more multiple location assemble, and in real work, do not need mobile whole working stand, and can well be used for the aircraft rigger dress, avoided interfering between working stand and aircraft or frock simultaneously yet.
For overcoming the above problems, concrete technical scheme of the present utility model is as follows: but the aircraft rigger that a kind of twin shaft moves is made ladder, comprise falsework, work leg and working stand, the work leg is arranged on the two ends of falsework one bottom section, and the twice slide rail I that be arranged in parallel in falsework other end bottom is provided with slide block in the slide rail I, slide block connects gripper shoe jointly, be provided with parallel slide rail II in gripper shoe, the perpendicular direction of slide rail II is in the direction of slide rail I, and slide block is arranged in the slide rail II simultaneously; Be flexibly connected two support bars, support bar bottom connecting support seat at the outer end of gripper shoe side-lower.
Described slide block is provided with locking device in the position of slide rail I and slide rail II.
But be somebody's turn to do the aircraft rigger work ladder employing said structure that twin shaft moves, can carry out horizontal and vertical movement to gripper shoe by the slide block on the horizontal and vertical guide rail, get final product the direction support bar after arriving application position, make supporting seat be positioned at ground, working stand can use, and then has improved the aircraft efficiency of assembling.
Description of drawings
But the aircraft rigger that Fig. 1 moves for twin shaft is made the structural representation of ladder.
But the aircraft rigger that Fig. 2 moves for twin shaft is made the application schematic diagram of ladder.
The specific embodiment
As shown in Figure 1, but the aircraft rigger that a kind of twin shaft moves is made ladder, comprise falsework 1, work leg 2 and working stand 3, work leg 2 is arranged on the two ends of falsework 1 one bottom sections, and the twice slide rail I 4 that be arranged in parallel in falsework 1 other end bottom is provided with slide block 7 in slide rail I 4, the slide block 7 common gripper shoes 8 that connect, be provided with parallel slide rail II 9 in gripper shoe 8, the perpendicular direction of slide rail II 9 is in the direction of slide rail I 4, and slide block 7 is arranged in the slide rail II 9 simultaneously; Be flexibly connected two support bars 5 at the outer end of gripper shoe 8 side-lower, support bar bottom connecting support seat 6, when gripper shoe 8 is moved, support bar can be packed up, place the lower surface of gripper shoe 8, when moving to correct position, support bar is put down, it is fixed, and further guarantees security and the convenience of work.Described slide block 7 is provided with locking device in the position of slide rail I 4 and slide rail II 9, to guarantee between gripper shoe 8 and falsework without relatively moving assurance workman's safety.
As shown in Figure 2, but the aircraft rigger that moves when two twin shafts is done the gripper shoe installation site of ladder when symmetrical, the aircraft rigger that but two groups of twin shafts can be moved is made ladder and is merged, then adopt locking device that it is locked, like this work gripper shoe area increase, working range broaden simultaneously, have also guaranteed security performance.
Claims (2)
1. but the aircraft rigger that moves of a twin shaft is made ladder, comprise falsework (1), work leg (2) and working stand (3), it is characterized in that: work leg (2) is arranged on the two ends of falsework (1) one bottom section, twice slide rail I (4) be arranged in parallel in falsework (1) other end bottom, be provided with slide block (7) in slide rail I (4), slide block (7) connects gripper shoe (8) jointly, be provided with parallel slide rail II (9) in gripper shoe (8), the perpendicular direction of slide rail II (9) is in the direction of slide rail I (4), and slide block (7) is arranged in the slide rail II (9) simultaneously; Be flexibly connected two support bars (5), support bar bottom connecting support seat (6) at the outer end of gripper shoe (8) side-lower.
2. but the aircraft rigger that moves of twin shaft as claimed in claim 1 is made ladder, and it is characterized in that: described slide block (7) is provided with locking device in the position of slide rail I (4) and slide rail II (9).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012202627254U CN202716261U (en) | 2012-06-06 | 2012-06-06 | Double-shaft moving working ladder for assembling aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012202627254U CN202716261U (en) | 2012-06-06 | 2012-06-06 | Double-shaft moving working ladder for assembling aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202716261U true CN202716261U (en) | 2013-02-06 |
Family
ID=47618098
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2012202627254U Expired - Fee Related CN202716261U (en) | 2012-06-06 | 2012-06-06 | Double-shaft moving working ladder for assembling aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202716261U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104002993A (en) * | 2014-06-13 | 2014-08-27 | 沈阳飞机工业（集团）有限公司 | Flexible device for assembling airplane shell and assembly method of flexible device |
| CN105345739A (en) * | 2015-11-17 | 2016-02-24 | 瓦锡兰玉柴发动机有限公司 | Marine diesel engine assembling table |
| CN106514594A (en) * | 2016-12-26 | 2017-03-22 | 郑州游爱网络技术有限公司 | Lifting seat provided with protective device and used for wall painting |
-
2012
- 2012-06-06 CN CN2012202627254U patent/CN202716261U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104002993A (en) * | 2014-06-13 | 2014-08-27 | 沈阳飞机工业（集团）有限公司 | Flexible device for assembling airplane shell and assembly method of flexible device |
| CN104002993B (en) * | 2014-06-13 | 2016-04-20 | 沈阳飞机工业（集团）有限公司 | A kind of flexible apparatus to the assembling of aircraft housing and assembly method thereof |
| CN105345739A (en) * | 2015-11-17 | 2016-02-24 | 瓦锡兰玉柴发动机有限公司 | Marine diesel engine assembling table |
| CN106514594A (en) * | 2016-12-26 | 2017-03-22 | 郑州游爱网络技术有限公司 | Lifting seat provided with protective device and used for wall painting |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN202716261U (en) | Double-shaft moving working ladder for assembling aircraft | |
| CN203160661U (en) | Movable construction hanging basket | |
| CN210695213U (en) | Novel greenhouse skeleton structure | |
| CN205247763U (en) | Similar material simulation experiment table | |
| CN208105469U (en) | A kind of vertical telescopic device adjusting indoor arrangement | |
| CN202249149U (en) | Magnetically-connected fence | |
| CN205822584U (en) | Adjustable high strength I-beam structure | |
| CN203709513U (en) | Table frame | |
| CN202097684U (en) | Hand-operated positioning device | |
| CN205255022U (en) | Metallurgical special purpose machinery popularity claw | |
| CN205088798U (en) | Two -way sliding support node of H shaped steel roof beam with two -way limit function | |
| CN204552274U (en) | A kind of slewing experiment protective screening | |
| CN203321528U (en) | Operation platform for mine shaft heading face | |
| CN203547512U (en) | Multifunctional herringbone ladder | |
| CN205148519U (en) | Production sophisticated planer hydraulic system link for wooden toy | |
| CN204952951U (en) | Remove physics testboard | |
| CN203474399U (en) | Arm frame device and high-altitude operation car comprising same | |
| CN201420384Y (en) | Combined scaffold capable of simply moving for plastering | |
| CN205366511U (en) | Telescopic gasengine support frame | |
| CN203653178U (en) | Gantry lifting device assembly | |
| CN202657567U (en) | Flow assembly track of machine cabinet | |
| CN204238393U (en) | Cross stay cable fixture | |
| CN203742101U (en) | Pop-up glass guard bar | |
| CN203191580U (en) | Rapid electric power communication engineering welding workbench | |
| CN207549525U (en) | A kind of feeding device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20130206 Termination date: 20150606 |
|
| EXPY | Termination of patent right or utility model |