CN102249006A - Movement butt joint device for large body part of airplane general assembly - Google Patents
Movement butt joint device for large body part of airplane general assembly Download PDFInfo
- Publication number
- CN102249006A CN102249006A CN2011101199767A CN201110119976A CN102249006A CN 102249006 A CN102249006 A CN 102249006A CN 2011101199767 A CN2011101199767 A CN 2011101199767A CN 201110119976 A CN201110119976 A CN 201110119976A CN 102249006 A CN102249006 A CN 102249006A
- Authority
- CN
- China
- Prior art keywords
- frame body
- bracket
- fuselage
- butt joint
- screw rod
- 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.)
- Pending
Links
- 210000001503 joint Anatomy 0.000 title abstract description 16
- 230000007246 mechanism Effects 0.000 claims abstract description 8
- 238000003032 molecular docking Methods 0.000 claims description 18
- 230000013011 mating Effects 0.000 claims description 7
- 238000004519 manufacturing process Methods 0.000 description 4
- 238000000034 method Methods 0.000 description 3
- 230000008901 benefit Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 230000033772 system development Effects 0.000 description 1
- 230000032258 transport Effects 0.000 description 1
Images
Landscapes
- Automatic Assembly (AREA)
Abstract
The invention discloses a movement butt joint device for a large body part of an airplane general assembly. The device comprises a frame body and a part bracket, wherein the frame body is provided with movable rollers, supporting leg components and an operating platform; the part bracket is fixed on the frame body; the frame body comprises a front body bracket and a rear body bracket; the rear body bracket is connected with the frame body through a fine adjustment mechanism; the fine adjustment mechanism comprises a pull rod, a screw rod which is in threaded connection with the pull rod and a hand wheel which is used for controlling the screw rod to rotate; the screw rod is fixed on the frame body through a bearing; the end head of the pull rod is hinged on the rear body bracket; and the rear body bracket is connected with the frame body in a slidable manner through a roller shaft and a chute. The movement butt joint device is combined with an airplane automation assembling line and an automatic butt joint platform system, so that the automation butt joint of the large body part is realized.
Description
Technical field
The present invention relates to the big parts automation butt joint of aircraft general assembly field, relate in particular to the big parts of fuselage and move docking facilities.
Background technology
Aircraft assembly automation docking technique is the beginning of airplane complete machine general assembly fitting work, also is one of extremely important link in the aircraft manufacturing link, and its assembly quality and efficient directly influence follow-up Assembling Production process.The big parts of airframe butt joint present situation still adopts traditional artificial lifting joint mode, and merging precision is low, inefficiency, labour intensity are bigger, and big parts are long dead time, exist certain safe mass hidden danger in the butt joint.For promoting and guaranteeing fuselage butt joint assembly technique and assembly quality, the joint mode that changes the big parts of tradition lifting aircraft is imperative.Aircraft is aspect big parts butt joint assembly technique at present, towards automated assembly docking platform system development open, that have the strain rate effect ability, the stress that interface produces in the assembling can be eliminated by aircraft automated assembly docking platform system, improve assembly quality, the assembly automation degree improves, production efficiency improves, and the production cycle shortens; Highly versatile; Save a large amount of assembly tooling expenses.
Summary of the invention
Therefore the purpose of this invention is to provide and a kind ofly move docking facilities with the big parts of the matching used airframe of aircraft automated assembly docking platform, this device can change the support attitude of fuselage, the function that realization is installed, parked, transports the big parts butt joint of airframe fine setting, butt joint realizes the unstressed assembling of airframe.
The big parts of aircraft general assembly fuselage of the present invention move docking facilities, contain frame body and parts carriage, frame body is provided with shifting roller and spike assembly, and workplatform, the parts carriage is fixed on the frame body, frame body contains fuselage front rack and fuselage tail-bracket, it is characterized in that described fuselage tail-bracket is connected with frame body by a micro-adjusting mechanism, described micro-adjusting mechanism contains pull bar and forms with pull bar screw rod that is spirally connected and the handwheel that the control screw rod rotates, described screw rod by bearing fixing on frame body, the termination of described pull bar is hinged on the fuselage tail-bracket, and the fuselage tail-bracket is by roller shaft and chute and frame body sliding block joint.
Advantage of the present invention will show following some: 1, can be easily with the big member supporting of airframe on the parts carriage of this device, by shifting roller parts and this device are moved to assigned address on the aircraft automated assembly docking platform together, fix with the spike assembly again, realize the transportation of the big parts of fuselage and park.When 2, airframe being installed, the workplatform that is arranged on the frame body provides standardized job platform for operating personal.3, the arc profile of parts carriage and the big member profile of fuselage are coincide, and micro-adjusting mechanism is eliminated the assembly stress that butt joint produces by the parts carriage being realized the butt joint fine setting to the big parts of fuselage, satisfy the big parts automation butt joint of fuselage requirement.
Below in conjunction with the embodiment accompanying drawing this application is described in further detail:
Description of drawings
The big parts of Fig. 1 aircraft general assembly fuselage move the docking facilities scheme drawing
The big parts of Fig. 2 aircraft general assembly fuselage move the docking facilities lateral plan
The big parts of Fig. 3 aircraft general assembly fuselage move the docking facilities back view
Fig. 4 micro-adjusting mechanism local structure scheme drawing
Fig. 5 the application's the big parts of aircraft general assembly fuselage move docking facilities and the supporting running condition scheme drawing of aircraft automated assembly plateform system
Number description: front rack 1; Tail-bracket 2; Last mating operation platform 3; Holding-down bolt 4; Following mating operation platform 5; Roller 6; Scalable workplatform 7; Slide bar 8; Locating dowel pin 9; Handwheel 10; Chute 11; Roller shaft 12; Pull bar 13; Screw rod 14; Bearing 15; Frame body 16, the big parts 17 of fuselage; Automated assembly plateform system 18
The specific embodiment
Referring to accompanying drawing, the frame body 16 that the big parts of aircraft general assembly fuselage move docking facilities is to be welded by rigid structural member, be respectively equipped with mating operation platform 3 on symmetrical two in the both sides of frame body 16, be provided with mating operation platform 5 down in the inboard of frame body 16, rear side at frame body 16 also is provided with scalable workplatform 7, scalable workplatform 7 is connected the rear side of frame body 16 by slide bar 8 and locating dowel pin 9, and the operator stands on the above-mentioned workplatform can carry out fuselage interface attitude measurement and mating operation; Be provided with roller 6 and holding-down bolt 4 in the bottom of frame body, during transportation, rise holding-down bolt, utilize roller that this device and the big parts of fuselage are moved on the aircraft docking platform, be screwed to aircraft docking platform on fixed together with the big parts of fuselage this device by holding-down bolt 4 again.
In order to support the big parts of fuselage, the parts carriage that is provided with on frame body 16 comprises front rack 1 and tail-bracket 2, and the profile of carriage and fuselage appearance coincide here.Front rack 1 is fixed on the front end of frame body 16, tail-bracket 2 is by flexibly connecting between a fine tuning structure and the frame body 16, as shown in Figure 4, the tail-bracket body is provided with four chutes 11, tail-bracket 2 is movably connected in the rear end of frame body 16 by chute 11 and roller shaft 12, and tail-bracket is finely tuned in the chute tolerance band with respect to frame body.The pull bar 13 of fine tuning structure is threaded with screw rod 14, and screw rod 14 is fixed on the right side of frame body 16 by bearing 15, and the external end head of screw rod 14 is connected with handwheel 10, and the other end and the tail-bracket 2 of the pull bar 13 of fine tuning structure are hinged.During fine setting, rotate handwheel 10, it is flexible to drive pull bar 13 by screw rod 14, realizes the fine setting to tail-bracket, realizes the Installation and Debugging to the left and right motion of the big parts interface of airframe, eliminates the butt joint stress of interface.
Claims (2)
1. the big parts of aircraft general assembly fuselage move docking facilities, contain frame body and parts carriage, frame body is provided with shifting roller and spike assembly, and workplatform, the parts carriage is fixed on the frame body, frame body contains fuselage front rack and fuselage tail-bracket, it is characterized in that described fuselage tail-bracket is connected with frame body by a micro-adjusting mechanism, described micro-adjusting mechanism contains pull bar and forms with pull bar screw rod that is spirally connected and the handwheel that the control screw rod rotates, described screw rod by bearing fixing on frame body, the termination of described pull bar is hinged on the fuselage tail-bracket, and the fuselage tail-bracket is by roller shaft and chute and frame body sliding block joint.
2. the big parts of aircraft general assembly fuselage as claimed in claim 1 move docking facilities, it is characterized in that being respectively equipped with mating operation platform on symmetrical two in the both sides of frame body, be provided with mating operation platform down in the inboard of frame body, rear side at frame body also is provided with scalable workplatform, and scalable workplatform is connected the rear side of frame body by slide bar and locating dowel pin.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011101199767A CN102249006A (en) | 2011-05-11 | 2011-05-11 | Movement butt joint device for large body part of airplane general assembly |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011101199767A CN102249006A (en) | 2011-05-11 | 2011-05-11 | Movement butt joint device for large body part of airplane general assembly |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN102249006A true CN102249006A (en) | 2011-11-23 |
Family
ID=44976661
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011101199767A Pending CN102249006A (en) | 2011-05-11 | 2011-05-11 | Movement butt joint device for large body part of airplane general assembly |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102249006A (en) |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103277645A (en) * | 2013-06-26 | 2013-09-04 | 苏州速腾电子科技有限公司 | Bearing rack |
| CN103286542A (en) * | 2013-06-13 | 2013-09-11 | 沈阳飞机工业（集团）有限公司 | Multi-lug-sheet large-size component movement butt joint unwheeling |
| CN103303491A (en) * | 2012-03-09 | 2013-09-18 | 陕西飞机工业（集团）有限公司 | Abutting technological equipment of airplane large components and abutting method thereof |
| CN103991649A (en) * | 2014-06-12 | 2014-08-20 | 沈阳飞机工业（集团）有限公司 | Folding transportation bracket for large fuselage part section |
| CN104842852A (en) * | 2015-05-27 | 2015-08-19 | 中航（上海）汽车技术有限公司 | Fixing device of large-size aviation component transport trailer |
| CN105189033A (en) * | 2013-03-29 | 2015-12-23 | 三菱重工业株式会社 | Method for bonding fuselage and strong back |
| CN105905312A (en) * | 2016-04-01 | 2016-08-31 | 中航飞机股份有限公司西安飞机分公司 | Installation platform and dismounting method thereof for overall floor of large transport aircraft |
| CN106114906A (en) * | 2011-12-15 | 2016-11-16 | 波音公司 | The automatic assembling of jigsaw airframe |
| CN109264020A (en) * | 2018-11-17 | 2019-01-25 | 大连四达高技术发展有限公司 | Intelligent up-down butt joint system for large components of machine body |
| CN111775980A (en) * | 2020-07-14 | 2020-10-16 | 国人机器人（天津）有限公司 | Load translation equipment |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20080308211A1 (en) * | 2005-12-16 | 2008-12-18 | Airbus Uk Limited | Assembly of Aircraft Components |
| CN101357687A (en) * | 2008-09-26 | 2009-02-04 | 浙江大学 | A Multi-task Aircraft Auxiliary Assembly System Based on Industrial Robot |
| CN102001451A (en) * | 2010-11-12 | 2011-04-06 | 浙江大学 | Airplane component attitude adjusting and butting system based on four numeric control positioners, attitude adjusting platform and mobile bracket and corresponding method |
-
2011
- 2011-05-11 CN CN2011101199767A patent/CN102249006A/en active Pending
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20080308211A1 (en) * | 2005-12-16 | 2008-12-18 | Airbus Uk Limited | Assembly of Aircraft Components |
| CN101357687A (en) * | 2008-09-26 | 2009-02-04 | 浙江大学 | A Multi-task Aircraft Auxiliary Assembly System Based on Industrial Robot |
| CN102001451A (en) * | 2010-11-12 | 2011-04-06 | 浙江大学 | Airplane component attitude adjusting and butting system based on four numeric control positioners, attitude adjusting platform and mobile bracket and corresponding method |
Non-Patent Citations (1)
| Title |
|---|
| 王建华: "飞机总装对接技术", 《航空制造技术》 * |
Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106114906A (en) * | 2011-12-15 | 2016-11-16 | 波音公司 | The automatic assembling of jigsaw airframe |
| CN103303491B (en) * | 2012-03-09 | 2016-03-30 | 陕西飞机工业（集团）有限公司 | A kind of production tooling of Large Aircraft Components docking and docking calculation thereof |
| CN103303491A (en) * | 2012-03-09 | 2013-09-18 | 陕西飞机工业（集团）有限公司 | Abutting technological equipment of airplane large components and abutting method thereof |
| CN105189033A (en) * | 2013-03-29 | 2015-12-23 | 三菱重工业株式会社 | Method for bonding fuselage and strong back |
| CN103286542B (en) * | 2013-06-13 | 2015-10-28 | 沈阳飞机工业（集团）有限公司 | The large parts of many auricles move docking unwheeling |
| CN103286542A (en) * | 2013-06-13 | 2013-09-11 | 沈阳飞机工业（集团）有限公司 | Multi-lug-sheet large-size component movement butt joint unwheeling |
| CN103277645A (en) * | 2013-06-26 | 2013-09-04 | 苏州速腾电子科技有限公司 | Bearing rack |
| CN103991649A (en) * | 2014-06-12 | 2014-08-20 | 沈阳飞机工业（集团）有限公司 | Folding transportation bracket for large fuselage part section |
| CN104842852A (en) * | 2015-05-27 | 2015-08-19 | 中航（上海）汽车技术有限公司 | Fixing device of large-size aviation component transport trailer |
| CN104842852B (en) * | 2015-05-27 | 2017-08-29 | 上海航空特种车辆有限责任公司 | The fixing device of the big part transtainer of aviation |
| CN105905312A (en) * | 2016-04-01 | 2016-08-31 | 中航飞机股份有限公司西安飞机分公司 | Installation platform and dismounting method thereof for overall floor of large transport aircraft |
| CN105905312B (en) * | 2016-04-01 | 2018-07-06 | 中航飞机股份有限公司西安飞机分公司 | A kind of large transport airplane Integral floor mounting platform and its method for dismounting |
| CN109264020A (en) * | 2018-11-17 | 2019-01-25 | 大连四达高技术发展有限公司 | Intelligent up-down butt joint system for large components of machine body |
| CN111775980A (en) * | 2020-07-14 | 2020-10-16 | 国人机器人（天津）有限公司 | Load translation equipment |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN102249006A (en) | Movement butt joint device for large body part of airplane general assembly | |
| CN202763375U (en) | Locating clamping fixture for car body sheet metal parts | |
| CN203356931U (en) | Positioning-pin driving structure and manual telescopic positioning-pin structure | |
| CN204053461U (en) | A kind of assembled camshaft suit frock | |
| CN201900432U (en) | Pneumatic propulsion device for positioning pin of assembling and welding clamp for vehicle body | |
| CN212420146U (en) | Truck longitudinal beam robot welding workstation | |
| CN205817151U (en) | Lightweight robot flexibility location gripping apparatus | |
| CN106166717A (en) | A kind of auxiliary support apparatus on flexible assemble production line | |
| CN101386053A (en) | A rotary automatic riveting manipulator and its use method | |
| CN203679489U (en) | Numerically-controlled H-shaped steel cutting machine | |
| CN204449573U (en) | Straight seam welding machine weld tracker | |
| CN203236201U (en) | Device for assembling transmission shaft for vehicle | |
| CN207255148U (en) | The power synchronous riveting device such as one kind | |
| CN205043411U (en) | Pneumatic upset workstation | |
| CN204277267U (en) | Mobile welder | |
| CN104923855B (en) | A kind of fraising special equipment remanufactured for automatic gearbox of vehicles valve body | |
| CN203992613U (en) | A kind of leaf springs of car blanking shearing machine automatic positioning equipment | |
| CN203196829U (en) | Adhesive dispensing unit in magnetic core assembling machine | |
| CN203141496U (en) | Servo manipulator for oriented double-station electronic assembling | |
| CN102364557A (en) | Production-practicability type assembly, adjustment and repair lathe for teaching purpose | |
| CN104493334A (en) | Welding seam tracking device for straight seam welding machine | |
| CN104742080B (en) | A kind of upset laminating mechanism | |
| CN103451873B (en) | Adjustable shaft drives guiding mechanism | |
| CN102689117B (en) | Flexible manufacturing line for rail wagons and production process thereof | |
| CN210885152U (en) | Forklift capable of moving counterweight back and forth |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20111123 |