CN104029150B - Aircraft product back segment parts open fittings navigation system - Google Patents
Aircraft product back segment parts open fittings navigation system Download PDFInfo
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- CN104029150B CN104029150B CN201410248730.3A CN201410248730A CN104029150B CN 104029150 B CN104029150 B CN 104029150B CN 201410248730 A CN201410248730 A CN 201410248730A CN 104029150 B CN104029150 B CN 104029150B
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- 238000006243 chemical reaction Methods 0.000 claims description 9
- 210000001015 abdomen Anatomy 0.000 claims description 5
- 238000005553 drilling Methods 0.000 description 8
- 238000004080 punching Methods 0.000 description 4
- 238000000137 annealing Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 229910000679 solder Inorganic materials 0.000 description 3
- 238000009434 installation Methods 0.000 description 2
- 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
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000000153 supplemental effect Effects 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B25—HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
- B25B—TOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FOR FASTENING, CONNECTING, DISENGAGING OR HOLDING
- B25B11/00—Work holders not covered by any preceding group in the subclass, e.g. magnetic work holders, vacuum work holders
- B25B11/02—Assembly jigs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23Q—DETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g. ARRANGEMENTS FOR COPYING OR CONTROLLING; MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OF PARTICULAR DETAILS OR COMPONENTS; COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOT DIRECTED TO A PARTICULAR RESULT
- B23Q3/00—Devices holding, supporting, or positioning work or tools, of a kind normally removable from the machine
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Transportation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Automatic Assembly (AREA)
Abstract
The present invention relates to a kind of aircraft product back segment parts open fittings navigation system, it comprises: a central workbench; One bottom support positioner, this bottom support positioner is arranged at described central workbench; One fixed positioner, this fixed positioner is arranged at described central workbench, is positioned at the relative both sides of described bottom support positioner; One mobile positioning apparatus, this mobile positioning apparatus is arranged at described central workbench, this mobile positioning apparatus comprises portable positioning unit, and this portable positioning unit is positioned at four sides of described bottom support positioner, can move relative to described central workbench; Described fixed positioner, mobile positioning apparatus and bottom support positioner by aircraft product back segment positioning parts to be positioned and can be fixed.
Description
Technical field
The present invention relates to a kind of automated manufacturing equipment, particularly relate to a kind of aircraft product back segment parts open fittings navigation system.
Background technology
Current aircraft assembling is main relies on traditional hand assembled mode, and bound fraction control measure targetedly, aircraft assembly quality can be improved to a certain extent, but the assembly quality technical indicator of distance advanced aircraft harshness also has suitable gap, is mainly reflected in: large scale frame beam framework assembly precision not easily ensures.Because FRAME COMPONENTS full-size reaches more than 4 meters, in part manufacture and assembling process, self-deformation is comparatively large, and assembling process lacks effective detection and control measure, cannot meet designing technique conditional request; Multiple material/titanium alloy, multiple material/aluminium alloy laminated construction drilling difficulty are large, hand-made hole is high to operative's skill set requirements, drilling efficiency is low, the multiple material layering of easy appearance, diameter ellipse, and due to position, hole tilt, draw the inaccurate concavo-convex amount of connector head caused of the nest degree of depth overproof, seriously affect aircraft performance.
Aircraft assembling present situation shows: traditional hand assembled technology can not meet the assembling quality requirement of advanced aircraft, and need fundamentally to change mounting technology means, numeric terminal becomes inevitable choice.The key component of automation drilling numeric terminal, existing aircraft product back segment parts assembling adopts closed frock, but because space interference problem causes the automation drilling that can not realize employing Digit Control Machine Tool, therefore, the layout type of existing closed frock must be transformed, make it to meet the operating space needed for automation drilling.
Summary of the invention
In view of this, necessaryly a kind of aircraft product back segment parts open fittings navigation system is provided, to realize numeric terminal and the automation drilling of aircraft product.
A kind of aircraft product back segment parts open fittings navigation system, it comprises: a central workbench; One bottom support positioner, this bottom support positioner is arranged at described central workbench; One fixed positioner, this fixed positioner is arranged at described central workbench, is positioned at the relative both sides of described bottom support positioner; One mobile positioning apparatus, this mobile positioning apparatus is arranged at described central workbench, this mobile positioning apparatus comprises portable positioning unit, and this portable positioning unit is positioned at four sides of described bottom support positioner, can move relative to described central workbench; Described fixed positioner, mobile positioning apparatus and bottom support positioner by aircraft product back segment positioning parts to be positioned and can be fixed.
A kind of aircraft product back segment parts open fittings navigation system, it comprises: a central workbench, one bottom support positioner, this bottom support positioner is arranged at described central workbench, and is positioned at the bottom of described aircraft product back segment parts to be positioned, one fixed positioner, this fixed positioner is arranged at described central workbench, and is positioned at the left and right sides of described aircraft product back segment parts to be positioned, one mobile positioning apparatus, this mobile positioning apparatus is arranged at described central workbench, this mobile positioning apparatus comprises the first portable positioning unit, second portable positioning unit, 3rd portable positioning unit and the 4th portable positioning unit, this first portable positioning unit and the second portable positioning unit lay respectively at belly and the back of described aircraft product back segment parts to be positioned, can move relative to described central workbench, described 3rd portable positioning unit and the 4th portable positioning unit lay respectively at the left and right sides of described aircraft product back segment parts to be positioned, can move relative to described central workbench, described fixed positioner, mobile positioning apparatus and bottom support positioner by aircraft product back segment positioning parts to be positioned and can be fixed.
Compared with prior art, aircraft product back segment parts open fittings navigation system provided by the invention utilizes fixed positioner, mobile positioning apparatus and bottom support positioner by aircraft product back segment positioning parts to be positioned and can fix, so can realize the numeric terminal of aircraft product.After aircraft product back segment parts to be positioned are accurately located, portable positioning unit in mobile positioning apparatus is removed, now, certain position of aircraft product back segment parts to be positioned opens wide, for follow-up Digit Control Machine Tool automatic punching provides operating space.
Accompanying drawing explanation
Fig. 1 is the perspective view of the aircraft product back segment parts open fittings navigation system that the embodiment of the present invention provides.
Fig. 2 is the perspective view of pectination locating support in the aircraft product back segment parts open fittings navigation system that provides of the embodiment of the present invention.
Fig. 3 is the perspective view of the first portable positioning unit and the second portable positioning unit in the aircraft product back segment parts open fittings navigation system that provides of the embodiment of the present invention.
Fig. 4 is the perspective view of the 3rd portable positioning unit and the 4th portable positioning unit in the aircraft product back segment parts open fittings navigation system that provides of the embodiment of the present invention.
Fig. 5 is the perspective view of bottom support positioner in the aircraft product back segment parts open fittings navigation system that provides of the embodiment of the present invention.
Main element symbol description
| Central authorities' workbench | 11 |
| Bottom support positioner | 12 |
| Base | 121 |
| Support cover | 122 |
| Support column | 123 |
| Locator | 124 |
| First fixed positioner | 131 |
| Second fixed positioner | 132 |
| Pectination locating support | 134 |
| Locator | 135、158 |
| Curb girder | 136、149 |
| Vertical beam | 137 |
| First mobile positioning apparatus | 141 |
| Second mobile positioning apparatus | 142 |
| 3rd mobile positioning apparatus | 151 |
| 4th mobile positioning apparatus | 152 |
| First guide rail | 143 |
| First portable positioning unit | 144 |
| Second guide rail | 145 |
| Second portable positioning unit | 146 |
| "ON" shape locating support | 147 |
| Locator | 148 |
| Crossbeam | 150 |
| 3rd guide rail | 153 |
| 3rd portable positioning unit | 154 |
| 4th guide rail | 155 |
| 4th portable positioning unit | 156 |
| Conversion support | 157 |
| Collateral support | 159 |
| Main body | 160 |
Following detailed description of the invention will further illustrate the present invention in conjunction with above-mentioned accompanying drawing.
Detailed description of the invention
Below in conjunction with the accompanying drawings and the specific embodiments, aircraft product back segment parts open fittings navigation system provided by the invention is described in further detail.
Refer to Fig. 1, first embodiment of the invention provides a kind of aircraft product back segment parts open fittings navigation system, there is the assembling of aircraft product back segment component framework, location and fixing effect, aircraft product framework each several part is made to keep relative position accurately, and provide follow-up to the intensity needed for aircraft product back segment operation of components, rigidity and locus, such as, the operating space needed for follow-up Digit Control Machine Tool automatic punching is provided.
Described aircraft product back segment parts open fittings navigation system comprises central workbench 11, bottom support positioner 12, fixed positioner, mobile positioning apparatus.Described bottom support positioner 12 is arranged at described central workbench 11.Described fixed positioner comprises the first fixed positioner 131 and the second fixed positioner 132, and described first fixed positioner 131 and the second fixed positioner 132 are arranged at described central workbench 11, and lay respectively at the relative both sides of described bottom support positioner 12, can aircraft product back segment parts to be positioned be positioned.
Described mobile positioning apparatus comprises the first mobile positioning apparatus 141, second mobile positioning apparatus 142, the 3rd mobile positioning apparatus 151 and the 4th mobile positioning apparatus 152.Described first mobile positioning apparatus 141 and the second mobile positioning apparatus 142 are arranged at described central workbench 11, and lay respectively at the other both sides of described bottom support positioner 12.Described 3rd mobile positioning apparatus 151 and the 4th mobile positioning apparatus 152 are arranged at described central workbench 11, and lay respectively at the relative both sides that described bottom support positioner 12 is provided with described fixed positioner.That is, described first mobile positioning apparatus 141 and described second mobile positioning apparatus 142 are oppositely arranged in a first direction, described 3rd mobile positioning apparatus 151 and the 4th mobile positioning apparatus 152 are oppositely arranged in a second direction, and described first direction is perpendicular to described second direction.
Described fixed positioner, mobile positioning apparatus and bottom support positioner 12 by aircraft product back segment positioning parts to be positioned and can be fixed.
Described first mobile positioning apparatus 141 is identical with the second mobile positioning apparatus 142 structure.Wherein, described first mobile positioning apparatus 141 comprises the first guide rail 143 and the first portable positioning unit 144, this first guide rail 143 is arranged at described central workbench 11, and be positioned at the side that described bottom support positioner 12 does not arrange fixed positioner, described first portable positioning unit 144 is arranged at described first guide rail 143, and can move on this first guide rail 143.Described second mobile positioning apparatus 142 comprises the second guide rail 145 and the second portable positioning unit 146, this second guide rail 145 is arranged at described central workbench 11, and be positioned at described bottom support positioner 12 with the described first relative side of guide rail 143, described second portable positioning unit 146 is arranged at described second guide rail 145, and can move on this second guide rail 145.That is, described first portable positioning unit 144 and the second portable positioning unit 146 can move along described second direction respectively.
Described 3rd mobile positioning apparatus 151 is identical with the 4th mobile positioning apparatus 152 structure.Wherein, described 3rd mobile positioning apparatus 151 comprises the 3rd guide rail 153 and the 3rd portable positioning unit 154,3rd guide rail 153 is arranged at described central workbench 11, and be positioned at the side that described bottom support positioner 12 is provided with the first fixed positioner 131, described 3rd portable positioning unit 154 is arranged at described 3rd guide rail 153, and can move on the 3rd guide rail 153.Described 4th mobile positioning apparatus 152 comprises the 4th guide rail 155 and the 4th portable positioning unit 156,4th guide rail 155 is arranged at described central workbench 11, and be positioned at the side that described bottom support positioner 12 is provided with the second fixed positioner 132, described 4th portable positioning unit 156 is arranged at described 4th guide rail 155, and can move on the 4th guide rail 155.That is, described 3rd portable positioning unit 154 and the 4th portable positioning unit 156 can move along described second direction respectively.
Fixed positioner 132, first mobile positioning apparatus 141, second mobile positioning apparatus 142 of described first fixed positioner 131, second, the 3rd mobile positioning apparatus 151, the 4th mobile positioning apparatus 152 and bottom support positioner 12 form a space jointly, and this space is for placing aircraft product back segment parts to be positioned.
Concrete, described first fixed positioner 131, second fixed positioner 132 is arranged on the left and right sides of aircraft product back segment parts to be positioned, the first portable positioning unit 144 in described first mobile positioning apparatus 141 is arranged on the belly of aircraft product back segment parts to be positioned, the second portable positioning unit 146 in described second mobile positioning apparatus 142 is arranged on the back of aircraft product back segment parts to be positioned, in 3rd mobile positioning apparatus 151 the 3rd portable positioning unit 154, in 4th mobile positioning apparatus 152 the 4th portable positioning unit 156 is arranged at the left and right sides of aircraft product back segment parts to be positioned.Described bottom support positioner 12 is arranged on the bottom of aircraft product back segment parts to be positioned.
Described first fixed positioner 131 is identical with the second fixed positioner 132 structure, is symmetricly set in the relative both sides of described bottom support positioner 12.Described first fixed positioner 131 and the second fixed positioner 132 are made up of pectination locating support 134 and multiple locator 135.See also Fig. 2, this pectination locating support 134 is made up of a vertical beam 137 and multiple curb girder 136, and the plurality of curb girder 136 is arranged at intervals at the side of described vertical beam 137 respectively.Described multiple locator 135 is arranged at described multiple curb girder 136 respectively.In the present embodiment, described curb girder 136 has four, described locator 135 has four, described vertical beam 137 adopts the heavy wall rectangular tube of 400mm × 400mm × 12mm to be welded, described curb girder 136 adopts Q235-A Plate Welding to form, answer stress relief annealing after integral solder, and then overall processing, add man-hour requirement and ensure flatness between the bottom surface of pectination locating support 134 and curb girder installed surface and the depth of parallelism.Described four locater 135 is arranged at described four curb girders 136 respectively, described locator 135 has the single degree of freedom, installation direction is vertical with the second fixed positioner 132 with described first fixed positioner 131, namely, horizontal direction is installed, and this locator 135 is used for locating hole important in the frame of positioning aircraft product back segment parts and other part.
The first guide rail 143 in described first mobile positioning apparatus 141 is identical with the second guide rail 145 structure in the second mobile positioning apparatus 142, be line slideway, be arranged at the both sides that described central workbench 11 does not arrange described fixed positioner, and extend to described second fixed positioner 132 from described first fixed positioner 131.
Described first portable positioning unit 144 in described first mobile positioning apparatus 141 is identical with portable positioning unit 146 structure of second in described second mobile positioning apparatus 142.See also Fig. 3, described first portable positioning unit 144 and the second portable positioning unit 146 form by "ON" shape locating support 147 and eight locators 148.Described "ON" shape locating support 147 is multilayer "ON" shape locating support, be made up of two vertical beams 149 and four crossbeams 150, described two vertical beams 149 be arranged in parallel, and described four crossbeam 150 parallel interval are arranged at described two vertical beams 149 and vertical with these two vertical beams 149.Described vertical beam 149 adopts the heavy wall rectangular tube of 400mm × 400mm × 12mm to be welded, described crossbeam 150 adopts Q235-A Plate Welding to form, stress relief annealing is answered after integral solder, and then overall processing, add the flatness between man-hour requirement guarantee "ON" shape locating support 147 bottom surface and crossbeam installed surface and the depth of parallelism.Wherein eight locators 148 are arranged at intervals at the two ends of each crossbeam 150 respectively, described locator 148 has the single degree of freedom, installation direction is vertical with the second mobile positioning apparatus 142 with described first mobile positioning apparatus 141 respectively, that is, horizontal direction is installed.Describedly to open " shape locating support 147 is arranged at described first guide rail 143 and the second guide rail 145 respectively, and this first guide rail 143 and the second guide rail 145 can move to the right side of the second fixed positioner 132 relatively respectively.Described locator 148 is used for the framework in supplemental support aircraft product to be positioned back segment parts, coordinates fixed positioner to complete accurate location.
The exact position of described first mobile positioning apparatus 141 and the second mobile positioning apparatus 142 requires it is only the position in its work, middle walking and dodge less demanding to precision of position, therefore, can adopt the accurate locate mode of back to zero.First guide rail 143 of described first mobile positioning apparatus 141 and the second guide rail 145 of described second mobile positioning apparatus 142 are provided with travel switch, when described first mobile positioning apparatus 141 and the walking of the second mobile positioning apparatus 142 arrive the operating position of positioning tool, trigger travel switch, now apply back to zero program, exact position is determined by the precision of the encoder on servomotor, can obtain higher precision at every turn.
The 3rd guide rail 153 in described 3rd mobile positioning apparatus 151 is identical with the 4th guide rail 155 structure in the 4th mobile positioning apparatus 152, is line slideway, is arranged at the both sides that described central workbench 11 is provided with described fixed positioner respectively.Described 3rd guide rail 153 extends from described first fixed positioner 131 to the direction away from described first fixed positioner 131.Described 4th guide rail 155 extends from described second fixed positioner 132 to the direction away from described second fixed positioner 132.
Described 3rd portable positioning unit 154 in described 3rd mobile positioning apparatus 151 is identical with portable positioning unit 156 structure of the 4th in described 4th mobile positioning apparatus 152.See also Fig. 4,3rd portable positioning unit 154 and the 4th portable positioning unit 156 form by main body 160, collateral support 159, conversion support 157 and locator 158, described conversion support 157 is arranged at described main body 160, described collateral support 159 is arranged at one end of described conversion support 157, and described locator 158 is arranged at the top of described collateral support 159.The main body 160 of described 3rd portable positioning unit 154 and the 4th portable positioning unit 156 adopts the heavy wall rectangular tube of 400mm × 400mm × 12mm to be welded, collateral support 159 adopts Q235-A Plate Welding to form, stress relief annealing is answered after integral solder, and then overall processing, add the flatness between man-hour requirement guarantee conversion support 157 bottom surface and collateral support 159 installed surface and the depth of parallelism.Described conversion support 157 is arranged at described 3rd guide rail 153 and the 4th guide rail 155 respectively, described 3rd portable positioning unit 154 relatively the 3rd guide rail 153 can move to the left side of described first fixed positioner 131, and relatively described 4th guide rail 155 of described 4th portable positioning unit 156 can move to the right side of described second fixed positioner 132.Described 3rd mobile positioning apparatus 151 and the 4th mobile positioning apparatus 152 can be treated positioning aircraft product side and accurately locate.
See also Fig. 5, described bottom support positioner 12 comprises base 121, support cover 122, multiple support column 123 and two locators 124.Described support cover 122 is arranged on described base 121, this support cover 122 and is provided with two spaced circular holes, for the formation of the working space of product back segment parts.The surrounding of this circular hole is provided with multiple support column 123, and the relative both sides of described support cover 122 are respectively arranged with locator 124.Described multiple support column 123 and two locators 124 are for supporting and locate locating hole important in the frame of aircraft product back segment parts to be positioned and other part.
The aircraft product back segment parts open fittings navigation system that the present embodiment provides in use, first by fixed positioner, mobile positioning apparatus, bottom support positioner 12 is fixed on the assigned address of central workbench 11, ensure the relative position relation between them, then each frame of aircraft product back segment component framework to be positioned and beam are passed through the multiple locators 135 on fixed positioner, multiple locators 148 on mobile positioning apparatus, 158 and multiple support columns 123 of bottom support positioner 12 and two locators 124 accurately locate and fix, wherein fixed positioner is arranged on the left and right sides of aircraft product back segment parts to be positioned, in mobile positioning apparatus first portable positioning unit 144 and the second portable positioning unit 146 are separately positioned on belly and the back of aircraft product back segment parts to be positioned, 3rd portable positioning unit 154 and the 4th portable positioning unit 156 are separately positioned on the left and right sides of aircraft product back segment parts to be positioned, bottom support positioner 12 is arranged on the bottom of aircraft product back segment parts to be positioned, the numeric terminal of aircraft product can be realized.
After aircraft product back segment component framework to be positioned is accurately located, locator 148 on first mobile positioning apparatus 131 and the second mobile positioning apparatus 132 is extracted out from aircraft product back segment component framework, first portable positioning unit 144 and the second portable positioning unit 146 are moved to respectively the right side of the second fixed positioner 132 to the right along the first guide rail 143 and the second guide rail 145, locator 158 on 3rd mobile positioning apparatus 151 and the 4th mobile positioning apparatus 152 is extracted out from aircraft product back segment component framework, 3rd portable positioning unit 154 is moved to the left side of the first fixed positioner 131 left along the 3rd guide rail 153, 4th portable positioning unit 156 is moved on the right side of the second fixed positioner 132 along the 4th guide rail 155 to the right.Now, belly and the back position of aircraft product back segment parts to be positioned open wide, and in addition, described support cover 122 offers two circular holes, and this provides operating space for follow-up Digit Control Machine Tool automatic punching.
Be appreciated that the concrete structure of locating support in described fixed positioner and mobile positioning apparatus is not limited to the structure of the present embodiment, can design according to the concrete structure of aircraft product back segment parts to be positioned.Quantity and the position of described locator are not limit, and can be distributed in the different crossbeam of each positioner or the diverse location of curb girder and each crossbeam or curb girder, can by the accurate positioning instant of aircraft product back segment parts to be positioned as long as meet.
The each part of aircraft product back segment parts open fittings navigation system that the embodiment of the present invention provides is arranged separately in space and has relative position accurately, this system architecture is compact, opening character good, have the accurate orientation assemble of framework, rigging error on-line checkingi, outer covering piece connecting hole accurate numerical control automatic punching function concurrently simultaneously, and assembling drilling quality is good, efficiency is high, machine tool utilization rate is high.And achieve numeric terminal and the automation drilling of aircraft product.
In addition, those skilled in the art can also do other change in spirit of the present invention, and these changes done according to the present invention's spirit all should be included in the present invention's scope required for protection.
Claims (8)
1. an aircraft product back segment parts open fittings navigation system, it comprises:
One central workbench;
One bottom support positioner, this bottom support positioner is arranged at described central workbench;
One fixed positioner, this fixed positioner is arranged at described central workbench, be positioned at the relative both sides of described bottom support positioner, this fixed positioner is made up of the first fixed positioner and the second fixed positioner, this first fixed positioner and the second fixed positioner lay respectively at the relative both sides of described bottom support positioner, described first fixed positioner, second fixed positioner includes pectination locating support and multiple locator, the plurality of locator is arranged at described pectination locating support, for locating aircraft product back segment parts to be positioned,
One mobile positioning apparatus, this mobile positioning apparatus is arranged at described central workbench, this mobile positioning apparatus comprises portable positioning unit, and this portable positioning unit is positioned at four sides of described bottom support positioner, can move relative to described central workbench;
Described fixed positioner, mobile positioning apparatus and bottom support positioner by aircraft product back segment positioning parts to be positioned and can be fixed.
2. aircraft product back segment parts open fittings navigation system as claimed in claim 1, it is characterized in that, described mobile positioning apparatus is made up of the first mobile positioning apparatus, the second mobile positioning apparatus, the 3rd mobile positioning apparatus and the 4th mobile positioning apparatus.
3. aircraft product back segment parts open fittings navigation system as claimed in claim 2, it is characterized in that, described first mobile positioning apparatus comprises the first portable positioning unit and the first guide rail, this first portable positioning unit is arranged at this first guide rail, and can move relative to this first guide rail; Described second mobile positioning apparatus comprises the second portable positioning unit and the second guide rail, and described second portable positioning unit is arranged at this second guide rail, and can move relative to this second guide rail; Described 3rd mobile positioning apparatus comprises the 3rd portable positioning unit and the 3rd guide rail, and the 3rd portable positioning unit is arranged at the 3rd guide rail, and can move relative to the 3rd guide rail; Described 4th mobile positioning apparatus comprises the 4th portable positioning unit and the 4th guide rail, and the 4th portable positioning unit is arranged at the 4th guide rail, and can move relative to the 4th guide rail.
4. aircraft product back segment parts open fittings navigation system as claimed in claim 3, it is characterized in that, described first portable positioning unit and the second portable positioning unit include "ON" shape locating support and multiple locator, the plurality of locator is arranged at described "ON" shape locating support, for supporting and locating aircraft product back segment parts to be positioned.
5. aircraft product back segment parts open fittings navigation system as claimed in claim 3, it is characterized in that, described 3rd portable positioning unit and the 4th portable positioning unit are by main body, collateral support, conversion support and locator composition, described conversion support is arranged at described main body, described collateral support is arranged at one end of described conversion support, and described locator is arranged at the top of described collateral support.
6. aircraft product back segment parts open fittings navigation system as claimed in claim 1, it is characterized in that, described bottom support positioner comprises base, is arranged at the support cover of described base, is arranged at multiple support column of described support cover and two locators.
7. the aircraft product back segment parts open fittings navigation system as described in claim 1,4 or 5, it is characterized in that, described locator has the single degree of freedom, and horizontal direction is installed.
8. an aircraft product back segment parts open fittings navigation system, it comprises:
One central workbench;
One bottom support positioner, this bottom support positioner is arranged at described central workbench, and is positioned at the bottom of aircraft product back segment parts to be positioned;
One fixed positioner, this fixed positioner is arranged at described central workbench, and is positioned at the left and right sides of described aircraft product back segment parts to be positioned;
One mobile positioning apparatus, this mobile positioning apparatus is arranged at described central workbench, this mobile positioning apparatus comprises the first portable positioning unit, second portable positioning unit, 3rd portable positioning unit and the 4th portable positioning unit, this first portable positioning unit and the second portable positioning unit lay respectively at belly and the back of described aircraft product back segment parts to be positioned, can move relative to described central workbench, described 3rd portable positioning unit and the 4th portable positioning unit lay respectively at the left and right sides of described aircraft product back segment parts to be positioned, can move relative to described central workbench,
Described fixed positioner, mobile positioning apparatus and bottom support positioner by aircraft product back segment positioning parts to be positioned and can be fixed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410248730.3A CN104029150B (en) | 2014-06-06 | 2014-06-06 | Aircraft product back segment parts open fittings navigation system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410248730.3A CN104029150B (en) | 2014-06-06 | 2014-06-06 | Aircraft product back segment parts open fittings navigation system |
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| Publication Number | Publication Date |
|---|---|
| CN104029150A CN104029150A (en) | 2014-09-10 |
| CN104029150B true CN104029150B (en) | 2016-04-27 |
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| CN201410248730.3A Active CN104029150B (en) | 2014-06-06 | 2014-06-06 | Aircraft product back segment parts open fittings navigation system |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN107081697B (en) * | 2017-06-02 | 2018-10-19 | 秀卓自动化设备（湖北）有限公司 | A kind of automobile front positioning assembly tooling |
| CN116834967A (en) * | 2023-06-25 | 2023-10-03 | 成都飞机工业（集团）有限责任公司 | Multi-station transfer device and transfer method thereof |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102008044262A1 (en) * | 2008-12-02 | 2010-06-10 | Airbus Deutschland Gmbh | Device for automated supply of side shell in site for manufacturing fuselage section of aircraft, has side shell carrier for introducing side shells, and positioning drums for operating and aligning side shells inside device |
| CN102528698A (en) * | 2010-12-08 | 2012-07-04 | 现代自动车株式会社 | Panel jig apparatus for vehicle |
| CN102556366A (en) * | 2012-02-18 | 2012-07-11 | 沈阳飞机工业（集团）有限公司 | Locator bottom surface supporting device for butt joint of airplane components |
| CN102680262A (en) * | 2012-05-15 | 2012-09-19 | 上海交通大学 | Assembly simulation experiment table for edge strip of airplane wing |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102004056286B4 (en) * | 2004-11-22 | 2015-12-24 | Airbus Operations Gmbh | Device and method for shape and / or dimension independent assembly and stitching of several individual components to form intrinsically rigid, transportable sections for transport, especially for aircraft |
-
2014
- 2014-06-06 CN CN201410248730.3A patent/CN104029150B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102008044262A1 (en) * | 2008-12-02 | 2010-06-10 | Airbus Deutschland Gmbh | Device for automated supply of side shell in site for manufacturing fuselage section of aircraft, has side shell carrier for introducing side shells, and positioning drums for operating and aligning side shells inside device |
| CN102528698A (en) * | 2010-12-08 | 2012-07-04 | 现代自动车株式会社 | Panel jig apparatus for vehicle |
| CN102556366A (en) * | 2012-02-18 | 2012-07-11 | 沈阳飞机工业（集团）有限公司 | Locator bottom surface supporting device for butt joint of airplane components |
| CN102680262A (en) * | 2012-05-15 | 2012-09-19 | 上海交通大学 | Assembly simulation experiment table for edge strip of airplane wing |
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| CN104029150A (en) | 2014-09-10 |
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