CN104002132B - The assembly system of integrated double aircraft product - Google Patents
The assembly system of integrated double aircraft product Download PDFInfo
- Publication number
- CN104002132B CN104002132B CN201410248818.5A CN201410248818A CN104002132B CN 104002132 B CN104002132 B CN 104002132B CN 201410248818 A CN201410248818 A CN 201410248818A CN 104002132 B CN104002132 B CN 104002132B
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- China
- Prior art keywords
- leading portion
- back segment
- parts
- assembly unit
- aircraft product
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- 238000004080 punching Methods 0.000 claims abstract description 27
- 238000005259 measurement Methods 0.000 claims abstract description 18
- 238000005553 drilling Methods 0.000 claims description 50
- 238000009434 installation Methods 0.000 abstract description 4
- 238000005516 engineering process Methods 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 229910001069 Ti alloy Inorganic materials 0.000 description 1
- 238000004364 calculation method Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P21/00—Machines for assembling a multiplicity of different parts to compose units, with or without preceding or subsequent working of such parts, e.g. with programme control
- B23P21/002—Machines for assembling a multiplicity of different parts to compose units, with or without preceding or subsequent working of such parts, e.g. with programme control the units stationary whilst being composed
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Automatic Assembly (AREA)
Abstract
The present invention provides the assembly system of a kind of integrated double aircraft product, including: a leading portion assembly unit, a back segment assembly unit, a planer-type automatic punching lathe, a measurement subsystem and an integrated management and control system, wherein, described leading portion assembly unit and back segment assembly unit are doubling arrangement, and described planer-type automatic punching lathe is movably arranged between leading portion assembly unit and back segment assembly unit；Described measurement subsystem is for detecting aircraft product to be processed installation pose in leading portion assembly unit and back segment assembly unit, and drive leading portion assembly unit and back segment assembly unit, it is achieved being accurately positioned of aircraft product leading portion parts and aircraft product back segment parts；Described integrated management and control subsystem, be managed collectively leading portion assembly unit, back segment assembly unit, planer-type automatic punching lathe and measurement subsystem and control.
Description
Technical field
The invention belongs to automated manufacturing field, especially with respect to the Digital assembly system of a kind of integrated double aircraft product.
Background technology
The assembling of some complex aircraft products at present relies primarily on traditional hand assembled assembling mode, by bound fraction control measure targetedly, can improve aircraft product assembly quality to a certain extent.But the quality of the aircraft product assembled by the way of hand assembled, the assembling quality and technical index that distance improves constantly at present also has suitable gap.Being mainly reflected in: on the one hand, large-size frame assembly precision is difficult to ensure；During reaching more than 4m, part manufacture and assembling due to FRAME COMPONENTS full-size, self-deformation is relatively big, and assembling process lacks effective detection and control measure, it is impossible to meet designing technique condition requirement；On the other hand, multiple material/titanium alloy, multiple material/aluminium alloy laminated construction drilling difficulty are big, hand-made hole is high to operative's skill set requirements and drilling efficiency is low, multiple material layering, diameter ellipse easily occur, and due to position, hole tilt, draw the inaccurate concavo-convex amount of connector head caused of the nest degree of depth overproof, severely impact aircraft properties of product.
As can be seen here, complex aircraft Product Assembly present situation shows that traditional hand assembled technology can not meet the assembling quality requirement improved constantly, needs fundamentally to change mounting technology means.
Summary of the invention
In sum, necessary offer one can effectively detect and control assembling process, and can the Digital assembly system of the accurate integrated double aircraft product of drilling.
A kind of assembly system of integrated double aircraft product, including: a leading portion assembly unit, a back segment assembly unit, a planer-type automatic punching lathe, a measurement subsystem and an integrated management and control system, wherein, described leading portion assembly unit and back segment assembly unit are doubling arrangement, described planer-type automatic punching lathe is movably arranged between leading portion assembly unit and back segment assembly unit, to the aircraft product leading portion parts drilling being arranged in leading portion assembly unit or to the aircraft product back segment parts drilling being arranged in back segment assembly unit；Described measurement subsystem is for detecting aircraft product to be processed installation pose in leading portion assembly unit and back segment assembly unit, and drive leading portion assembly unit and back segment assembly unit, it is achieved being accurately positioned of aircraft product leading portion parts and aircraft product back segment parts；Described integrated management and control subsystem, to leading portion assembly unit, back segment assembly unit, planer-type automatic punching lathe and measure subsystem and be managed collectively and control, it is achieved being accurately positioned and drilling of aircraft product leading portion parts and aircraft product back segment parts.
Compared with prior art, the Digital assembly system of the integrated double aircraft product that the present invention provides, by integrated leading portion assembly unit and back segment assembly unit, have aircraft leading portion parts simultaneously concurrently and back segment parts are accurately positioned assembling, rigging error on-line checking, connecting hole accurate numerical control automatic punching function, improve the assembly precision of described aircraft product, and improve the utilization rate of equipment and installations of described planer-type automatic punching lathe.
Accompanying drawing explanation
Fig. 1 is the structural representation of the Digital assembly system of the integrated double aircraft product that the embodiment of the present invention provides.
Main element symbol description
| Auxiliary table | 1 |
| The electronic working stand of leading portion parts | 2 |
| Leading portion parts assembling drilling station | 3 |
| Planer-type automatic punching lathe | 4 |
| The electronic working stand of back segment parts | 5 |
| Back segment parts assembling drilling station | 6 |
| Back segment parts manual working ladder | 7 |
| Integrated management and control system | 8 |
| Back segment parts assembling positioner | 9 |
| Leading portion parts manual working ladder | 10 |
| Leading portion parts assembling positioner | 11 |
| Central authorities' workbench | 12 |
| Measure subsystem | 13 |
| Line slideway | 14 |
Specific examples below will further illustrate the present invention in conjunction with above-mentioned accompanying drawing.
Detailed description of the invention
The embodiment of the present invention provides the Digital assembly system of a kind of integrated double aircraft product, and described assembly system includes a leading portion assembly unit, a back segment assembly unit, a planer-type automatic punching lathe, a measurement subsystem and an integrated management and control system.Described leading portion assembly unit and back segment assembly unit are that doubling arrangement is arranged, described planer-type automatic punching lathe is arranged between leading portion assembly unit and back segment assembly unit, and can move to leading portion assembly unit or back segment assembly unit and be processed aircraft product.Described measurement subsystem is for being accurately positioned aircraft product component to be processed.Described integrated management and control system are for being managed collectively described leading portion assembly unit, back segment assembly unit and planer-type automatic punching lathe and control.
Refer to Fig. 1, described leading portion assembly unit, back segment assembly unit may be disposed on central authorities' workbench 12, the assembly system of described integrated double aircraft product can farther include two auxiliary tables 1 and be respectively arranged at the both sides that described central authorities workbench 12 is relative, and described planer-type automatic punching lathe 4 is set up on described auxiliary table 1.Described central authorities workbench 12 is arranged between described auxiliary table 1.Said two auxiliary table 1 can be respectively arranged with a line slideway 14, forms two line slideways being parallel to each other 14, and two line slideways 14 on described auxiliary table 1 be arranged in parallel.Described line slideway 14 runs through described leading portion assembly unit and back segment assembly unit.Described planer-type automatic punching lathe 4 may be disposed on described two line slideways 14, and moves along described line slideway 14 to described leading portion assembly unit or back segment assembly unit.
Described leading portion assembly unit includes the electronic working stand of leading portion parts 2, leading portion parts assembling drilling station 3, leading portion parts assembling positioner 11 and a leading portion parts manual working ladder 10.Described leading portion parts assembling drilling station 3 is arranged between described two line slideways 14, for carrying aircraft product leading portion parts to be processed；Described leading portion parts assembling positioner 11 is arranged at described leading portion parts assembling drilling station 3 in the side being perpendicular on line slideway 14 direction, for positioning and fixing aircraft leading portion parts to be processed.The described electronic working stand of leading portion parts 2 may be disposed at described leading portion parts assembling drilling station 3 in any side being perpendicular on line slideway 14.Further, described leading portion assembly unit can include two electronic working stands of leading portion parts 2, is respectively arranged at described leading portion parts assembling drilling station 3 in the opposite sides being perpendicular on line slideway 14 direction.The described electronic working stand of leading portion parts 2 can lift in the height direction, and in the horizontal direction closer or far from aircraft leading portion parts to be processed.Described leading portion parts manual working ladder 10 may be disposed at the described leading portion parts assembling drilling station 3 at least side between two line slideways 14.Further, described leading portion assembly unit can include two leading portion parts manual working ladders 10, be respectively arranged at described leading portion parts assembling drilling station 3 between two line slideways 14 relative to both sides.Described leading portion parts manual working ladder 10 can assemble drilling station 3 closer or far from described leading portion parts in the horizontal direction.
Described measurement subsystem 13 is for measuring the pose of described aircraft product leading portion parts to be processed and assess, and pass the measurements to described integrated management and control subsystem 8, with control described leading portion parts assembling positioner 11, the position of described aircraft product leading portion parts to be processed is adjusted so that described aircraft product leading portion parts to be processed are accurately positioned.It is appreciated that position is specifically set can selecting as required of described measurement subsystem 13.In the present embodiment, described measurement subsystem 13 is laser radar.
Described back segment assembly unit includes that subsystem 13 measured by the electronic working stand of back segment parts 5, back segment parts assembling drilling station 6, back segment parts manual working ladder 7, back segment parts assembling positioner 9 and.Described back segment parts assembling drilling station 6 is arranged between described two line slideways 14, described back segment parts assembling positioner 9 is arranged at described back segment parts assembling drilling station 6 in the side being perpendicular on line slideway 14 direction, for positioning and fixing aircraft product back segment parts to be processed.The described electronic working stand of back segment parts 5 may be disposed at described back segment parts assembling drilling station 6 at least side being perpendicular on line slideway 14.Further, described back segment assembly unit can include two electronic working stands of back segment parts 5, is respectively arranged at described back segment parts assembling drilling station 6 in the opposite sides being perpendicular on line slideway 14 direction.The described electronic working stand of back segment parts 5 can lift in the height direction, and in the horizontal direction closer or far from aircraft back segment parts to be processed.Described back segment parts manual working ladder 7 may be disposed at described back segment parts assembling drilling station 6 between two line slideways 14 away from the side of planer-type automatic punching lathe 4.Described back segment parts manual working ladder 7 can assemble drilling station 6 closer or far from described back segment parts in the horizontal direction.
Described measurement subsystem 13 is simultaneously used for the pose of described aircraft product back segment parts to be processed is measured and assessed, and pass the measurements to described integrated management and control system 8, with control described back segment parts assembling positioner 9, the position of described aircraft product leading portion parts to be processed is adjusted so that described aircraft product leading portion parts to be processed are accurately positioned.
Described planer-type automatic punching lathe 4 is arranged on described line slideway 14, and can move along described line slideway 14 to described leading portion parts assembling drilling station 3 or back segment parts assembling drilling station 6, and realize aircraft product leading portion parts to be processed and the automatic punching of back segment parts surfaces externally and internally.
The Digital assembly system of integrated double aircraft product of the present invention is operationally, aircraft product leading portion parts to be processed are arranged on described leading portion parts assembling drilling station 3, aircraft product back segment parts to be processed are arranged on described back segment parts assembling drilling station 6.The installation pose of aircraft leading portion parts and back segment parts is measured respectively by measurement subsystem 13, aircraft leading portion parts and back segment part pose adjustment amount is determined respectively by analytical calculation, automatically leading portion parts assembling positioner 11 is driven to adjust leading portion part pose, back segment parts assembling positioner 9 adjusts back segment part pose, remove the mobile device in leading portion parts assembling positioner 11 and back segment parts assembling positioner the most respectively, planer-type automatic punching machine tool movement is to leading portion parts drilling position, carry out the drilling of leading portion parts surfaces externally and internally each position, and move to back segment parts drilling position, carry out the drilling of back segment parts surfaces externally and internally each position, unified management that above-mentioned each operation is carried out by integrated management with control system 8 and control.
The assembly system of the integrated double aircraft product that the present invention provides, drilling station is assembled by integrated aircraft leading portion parts, back segment parts assembling drilling station and measurement subsystem, compact conformation, have aircraft leading portion parts simultaneously concurrently and back segment parts are accurately positioned assembling, rigging error on-line checking, connecting hole accurate numerical control automatic punching function, and it is good to assemble drilling quality, efficiency is high, one planer-type automatic punching machine can be simultaneously used for aircraft product leading portion parts and the assembling drilling of back segment parts, greatly improve the utilization rate of described planer-type automatic punching lathe.
It addition, those skilled in the art also can make other change in spirit of the present invention, these changes made according to present invention spirit, all should be included in scope of the present invention certainly.
Claims (9)
1. an assembly system for integrated double aircraft product, including: a leading portion assembly unit, after one
Section assembly unit, a planer-type automatic punching lathe, a measurement subsystem and an integrated management and control system
System, it is characterised in that described leading portion assembly unit and back segment assembly unit interval are arranged, described planer-type
Automatic punching lathe is movably arranged between leading portion assembly unit and back segment assembly unit, along a straight line
Move to described leading portion assembly unit or back segment assembly unit, to the flight being arranged in leading portion assembly unit
Device product leading portion parts drilling or to the aircraft product back segment parts system being arranged in back segment assembly unit
Hole；Described measurement subsystem fills at leading portion assembly unit and back segment for detecting aircraft product to be processed
Join the pose in unit, and drive leading portion assembly unit and back segment assembly unit, it is achieved before aircraft product
Section parts and being accurately positioned of aircraft product back segment parts；Described integrated management and control subsystem are right
Leading portion assembly unit, back segment assembly unit, planer-type automatic punching lathe and measurement subsystem are unified
Management with control, it is achieved aircraft product leading portion parts and aircraft product back segment parts be accurately positioned and
Drilling.
The assembly system of integrated double aircraft product the most as claimed in claim 1, it is characterised in that
Described leading portion assembly unit, back segment assembly unit is arranged on central authorities' workbench, described central authorities workbench
Both sides are respectively arranged with an auxiliary table, and described planer-type automatic punching machine tool frame is located at described auxiliary work
In station.
The assembly system of integrated double aircraft product the most as claimed in claim 2, it is characterised in that
It is respectively arranged with a line slideway on the auxiliary table of described central authorities workbench both sides, forms two mutually
Parallel line slideway, described planer-type automatic punching lathe sets up and on described line slideway, and along straight
The direction of line guide rail is moved.
The assembly system of integrated double aircraft product the most as claimed in claim 3, it is characterised in that
Described leading portion assembly unit include an electronic working stand of leading portion parts, one leading portion parts assembling drilling station,
One leading portion parts assembling positioner and leading portion parts manual working ladder, the assembling drilling of described leading portion parts
Station is arranged between two line slideways, for carrying aircraft product leading portion parts to be processed.
The assembly system of integrated double aircraft product the most as claimed in claim 4, it is characterised in that
Described leading portion parts assembling positioner is arranged at described leading portion parts assembling drilling station and is being perpendicular to straight line
Side on guide rail direction, for positioning and fixing the leading portion parts assembling system of aircraft product to be processed
Hole station.
The assembly system of integrated double aircraft product the most as claimed in claim 4, it is characterised in that
The described electronic working stand of leading portion parts is arranged at described leading portion parts assembling drilling station and leads being perpendicular to straight line
Side on rail direction, and lift in the short transverse being perpendicular to central authorities' table surface, and parallel
Closer or far from aircraft leading portion parts to be processed in the horizontal direction of central authorities' workbench；Described leading portion
Parts manual working ladder be arranged at described leading portion parts assembling drilling station between two line slideways extremely
Few side, and assemble drilling station closer or far from described leading portion parts in the horizontal direction.
The assembly system of integrated double aircraft product the most as claimed in claim 2, it is characterised in that
Described back segment assembly unit include one back segment parts electronic working stand one back segment parts assembling drilling station, one
Back segment parts manual working ladder, a back segment parts assembling positioner, described back segment parts assembling drilling work
Position is arranged between two line slideways.
The assembly system of integrated double aircraft product the most as claimed in claim 7, it is characterised in that
Described back segment parts assembling positioner be arranged at described back segment parts assembling drilling station with line slideway
The perpendicular side on direction, to position and fix aircraft product back segment parts to be processed.
The assembly system of integrated double aircraft product the most as claimed in claim 7, it is characterised in that
The described electronic working stand of back segment parts is arranged at described back segment parts assembling drilling station and is being perpendicular to straight line
At least side on guide rail, and lift in the height direction and in horizontal direction closer or far from described back segment
Parts assembling drilling station；Described back segment parts manual working ladder is arranged at the assembling drilling of described back segment parts
Station away from the side of planer-type automatic punching lathe, and leans between two line slideways in the horizontal direction
Drilling station is assembled close or remote from described back segment parts.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410248818.5A CN104002132B (en) | 2014-06-06 | 2014-06-06 | The assembly system of integrated double aircraft product |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410248818.5A CN104002132B (en) | 2014-06-06 | 2014-06-06 | The assembly system of integrated double aircraft product |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104002132A CN104002132A (en) | 2014-08-27 |
| CN104002132B true CN104002132B (en) | 2016-08-24 |
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ID=51363194
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410248818.5A Active CN104002132B (en) | 2014-06-06 | 2014-06-06 | The assembly system of integrated double aircraft product |
Country Status (1)
| Country | Link |
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| CN (1) | CN104002132B (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110893547B (en) * | 2019-12-09 | 2021-09-17 | 中航沈飞民用飞机有限责任公司 | Layout method for composite material vertical tail assembly production line of civil airliner |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2520787B2 (en) * | 1990-11-28 | 1996-07-31 | 本田技研工業株式会社 | Vehicle rear floor processing line |
| JP2763505B2 (en) * | 1995-03-16 | 1998-06-11 | 本田技研工業株式会社 | Method and apparatus for assembling automotive parts |
| DE102006020076B4 (en) * | 2006-04-29 | 2009-02-12 | Bayerische Motoren Werke Aktiengesellschaft | Method for connecting body parts and device for carrying out the method |
| CN102658478B (en) * | 2012-05-11 | 2014-11-05 | 山东海华汽车部件有限公司 | Leaf spring assembly line |
| CN202934395U (en) * | 2012-10-17 | 2013-05-15 | 颜希艇 | Complex machine tool with double-end processing function |
| CN203197225U (en) * | 2013-04-22 | 2013-09-18 | 杭州古月机电设备有限公司 | Double-station cast-weld machine structure |
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| Publication number | Publication date |
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| CN104002132A (en) | 2014-08-27 |
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| C41 | Transfer of patent application or patent right or utility model | ||
| CB03 | Change of inventor or designer information |
Inventor after: Chen Ken Inventor after: Song Libin Inventor after: Liu Li Inventor after: Zhang Jiwen Inventor after: Zheng Linbin Inventor after: Wu Dan Inventor after: Yin Huabin Inventor after: Chen Xuemei Inventor after: Zhou Kai Inventor after: Xu Jing Inventor after: Wang Guolei Inventor after: Yang Xiangdong Inventor before: Chen Ken Inventor before: Yang Dongchao Inventor before: Wu Dan Inventor before: Zhou Kai Inventor before: Wang Guolei Inventor before: Yang Xiangdong Inventor before: Song Libin Inventor before: Li Jinquan Inventor before: Xu Jing Inventor before: Liu Li |
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| COR | Change of bibliographic data | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20160704 Address after: 100084 Beijing Beijing 100084-82 mailbox Applicant after: Tsinghua University Applicant after: Chengdu Airplane Industry (Group) Corp., Ltd. Address before: 100084 Beijing Beijing 100084-82 mailbox Applicant before: Tsinghua University |
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