CN206502049U - A kind of airframe docks numeric terminal layout structure with head - Google Patents
A kind of airframe docks numeric terminal layout structure with head Download PDFInfo
- Publication number
- CN206502049U CN206502049U CN201720211511.7U CN201720211511U CN206502049U CN 206502049 U CN206502049 U CN 206502049U CN 201720211511 U CN201720211511 U CN 201720211511U CN 206502049 U CN206502049 U CN 206502049U
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- China
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- fuselage
- head
- positioning unit
- airframe
- posture adjustment
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Abstract
A kind of airframe docks numeric terminal layout structure with head, belong to aircraft manufacturing mounting technology field, its structure includes two fuselage brackets, head posture adjustment positioning unit, fuselage posture adjustment positioning unit, two laser trackers, two interface operating desks, one fuselage end operating desk, two active operation ladders and an integrated control system operating desk, two fuselage brackets are located at airframe lower section, and head posture adjustment positioning unit and fuselage posture adjustment positioning unit are respectively arranged at the lower section of the head and fuselage；Two described laser trackers are symmetricly set in the both sides in front of head, form aircraft digital measurement field, two interface operating desks are respectively arranged the end that fuselage is arranged in the fuselage end operating desk described in head and fuselage abutment joint both sides, two described active operation ladders are arranged in fuselage both sides, and described integrated control system operating desk is integrated with measuring system, posture adjusting system, process management and Database Systems and completes docking control work.
Description
Technical field
The utility model belongs to aircraft manufacturing mounting technology field, and digitlization is especially docked with head with a kind of airframe
Assemble layout structure relevant.
Background technology
During the entire process of aircraft manufacturing production, the assembly work of aircraft account for general 50% workload, therefore improve
The operating efficiency of aircraft assembling is improved to the efficiency of whole aircraft manufacturing production process and made great sense.At present, it is domestic
The assembling of aircraft all uses traditional assembly method substantially, and aircraft Butt Assembling is carried out using frock, and people's measurement is being passed using station
Unite on working stand, this not only loses time, and add the working strength of personnel, reduction work quality and efficiency.
Utility model content
The purpose of this utility model is to overcome prior art not enough to dock numeral makeup with head there is provided a kind of airframe
With layout structure.
A kind of airframe docks numeric terminal layout structure with head, it is characterized in that, described structure includes two machines
Body bracket, head posture adjustment positioning unit, fuselage posture adjustment positioning unit, two laser trackers, two interface operating desks, one
Fuselage end operating desk, two active operation ladders and an integrated control system operating desk, two fuselage brackets are located at airframe
Lower section, support and protective effect are played to fuselage, in case fuselage lands accident caused by equipment fault, while adding machine
The strong point of body, makes head fuselage assembling process more stablize；
Head posture adjustment positioning unit and fuselage the posture adjustment positioning unit is respectively arranged at the lower section of the head and fuselage,
Head posture adjustment positioning unit and fuselage posture adjustment positioning unit are constituted by four three axis positioners, and each three axis positioner is provided with
Three-dimensional force sensor, to ensure real-time force monitoring when posture adjustment is carried out to head and fuselage；
Two described laser trackers are symmetricly set in the both sides in front of head, form aircraft digital measurement field, often
Platform laser tracker is installed by the laser tracker pedestal lifted based on king bolt, has adapted to light in laser tracker measurement process
Road accessibility and human users' convenience, are realized without dead angle measurement；
Described two interface operating desks are respectively arranged in head and fuselage abutment joint both sides, for realizing aircraft exterior pair
The operation of junction；
Described fuselage end operating desk is arranged at the end of fuselage, enters interior of aircraft docking area as personnel and material
The passage of operation；
Two described active operation ladders are arranged in fuselage both sides, one man operation can voluntarily reach corresponding positions as needed
Put, for entering fuselage interior from external fuselage and completing the measurement work of external fuselage measurement point, and coordinate with locator,
Prevent from colliding with locator and damaging locator；
Described integrated control system operating desk is integrated with measuring system, posture adjusting system, process management and Database Systems
Complete immediately below docking control work, the top view for being arranged at fuselage.
As the supplement to above-mentioned technical proposal and perfect, the utility model also includes following technical characteristic.
Described fuselage end operating desk includes electric up-down counter and the access way of fuselage interior is passed in and out for workman, should
The top of access way sets platform, and lifting counter, which rises the material for needing to use when assembling, to be transported at platform, it is to avoid
The trouble of material is carried above and below workman.
Further, the table surface height of the platform is identical with the floor level in aircraft cabin, facilitates workman to pass in and out fuselage
It is internal.
Further, anti-collision rubber bar is installed close to aircraft side on the platform, it is to avoid misoperation is anticipated
Damaged when outer aircraft.
Described numeric terminal layout structure also includes an internal work being made using aluminium alloy lightweight material
Ladder, internal work ladder is positioned over inside aircraft cabin on joint floor, primarily to being applicable internal docking area adapts to space
Height and the height differences demand of people.
Further, the surrounding of the internal work ladder is provided with anti-collision rubber, in order to avoid working stand collsion damage aircraft.
A technique bracket, machine are correspondingly arranged on respectively on head posture adjustment positioning unit and fuselage the posture adjustment positioning unit
Head and fuselage are respectively placed on each self-corresponding technique bracket, when being mainly to ensure that head and fuselage posture adjustment rigidly avoid posture adjustment
Pull phenomenon.
Described interface operating desk is divided into 2 layers of Liftable type operating desk and base, meets workman and is constructed in arbitrary height,
Using electric model, earth leakage protective, there are jerk, spacing, anticollision device, collision-prevention device.
The utility model can reach following beneficial effect：The utility model integrated application includes digital coordination skill
The various advanced skills such as art, digitalized artificial technology, digital measuring technique, Digital location technology, virtual five axles posture adjustment technology
Art, has set up advanced digitlization Butt Assembling system, has improved efficiency of assembling and assembly precision.
Brief description of the drawings
Fig. 1 is front view of the present utility model.
Fig. 2 is top view of the present utility model.
Fig. 3 is left view of the present utility model.
Fig. 4 is right view of the present utility model.
Embodiment
Embodiment of the present utility model is described in detail below in conjunction with the accompanying drawings.
As shown in Fig. 1 ~ Fig. 4, airframe 2 of the present utility model docks numeric terminal layout structure with head, including
Two fuselage brackets 5, head posture adjustment positioning unit, fuselage posture adjustment positioning unit 7, two laser trackers 10, two interface behaviour
Make platform 8 and internal work is terraced, a fuselage end operating desk 4, two active operations ladders 3 and an integrated control system operating desk 6,
Two fuselage brackets 5 are located at the lower section of airframe 2, and support and protective effect are played to fuselage.
Head posture adjustment positioning unit 9 and fuselage posture adjustment positioning unit 7 are respectively arranged at the lower section of the head 1 and fuselage 2,
A technique bracket, the He of head 1 are correspondingly arranged on respectively on the head posture adjustment positioning unit 9 and fuselage posture adjustment positioning unit 7
Fuselage 2 is respectively placed on each self-corresponding technique bracket, head posture adjustment positioning unit 9 and fuselage posture adjustment positioning unit 7 by
Four three axis positioners compositions, each three axis positioner is provided with three-dimensional force sensor, to ensure to carry out head 1 and fuselage 2
Real-time force monitoring during posture adjustment；
Two described laser trackers 10 are symmetricly set in the both sides in the front of head 1, form aircraft digital measurement field,
Every laser tracker 10 is installed by the pedestal of laser tracker 10 lifted based on king bolt, has been adapted to laser tracker 10 and has been measured
During light path accessibility and human users' convenience；
Described two interface operating desks 8 are respectively arranged in head 1 and the abutment joint both sides of fuselage 2,8 points of interface operating desk
For 2 layers of Liftable type operating desk and base, meet workman and constructed in arbitrary height, using electric model, earth leakage protective, there is urgency
Stop, spacing, anticollision device, collision-prevention device, the operation for realizing aircraft exterior interface；
Described fuselage end operating desk 4 is arranged at the end of fuselage, and fuselage end operating desk 4 includes electric up-down counter
Platform is set with the top for the access way inside workman's turnover fuselage 2, the access way, lifting counter need when will assemble
The material used, which rises, to be transported at platform, and the table surface height of platform is identical with the floor level in aircraft cabin, facilitates workman
Pass in and out inside fuselage 2, anti-collision rubber bar is installed close to aircraft side on platform, it is to avoid misoperation occurs to damage during accident
Aircraft；Internal work ladder 12 is positioned over inside aircraft cabin on joint floor, and the surrounding of the internal work ladder 12 is provided with
Anti-collision rubber, in order to avoid working stand collsion damage aircraft, the terraced 12 plug-in battery-type electric lights of each internal work are with improving
Portion operates brightness, and each working stand 12 is made up of two faces, and one of face possesses elevating function and adapts to space height and people's
Height differences demand；Two described active operation ladders 3 are arranged in the both sides of fuselage 2, are power by reliable motorized motions, use
Moving lifting car form, single-grip control, you can relevant position is voluntarily reached with one man operation as needed, for from fuselage 2
Outside enters the inside of fuselage 2 and completes the measurement work of the externally measured point of fuselage 2, and coordinates with locator, prevents and positions
Device collides and damages locator, and can be acted with variable raising and lowering speed control rise and reduction, active operation
Ladder 3 uses compact design, it is allowed to rotated around the axletree of oneself, and the limited space of turnover is lighter, reliable motorized motions
Lasting power is provided for lift truck, built-in automatic charger can be realized to be filled soon, for entering from the outside of fuselage 2 in fuselage 2
Portion and complete the externally measured point of fuselage 2 measurement work, i.e., one can directly open this driver and hold target ball or T-Probe
Completion measurement work is without again as conventional conventional operation ladder needs people first to move ladder high and low's realization measurement, and with determining again
Position device hight coordinate；Described integrated control system operating desk 6 is integrated with measuring system, posture adjusting system, process management and data
Storehouse system completes docking control work, is arranged at the side-lower of fuselage 2.
Airframe 2 of the present utility model docks numeric terminal layout method with head, comprises the following steps：First
Step, System self-test is carried out by integrated control system operating desk；Second step, digitized measurement is built by two laser trackers 10
；3rd step, enters position to head posture adjustment positioning unit 9, by the corresponding technique bracket correspondence of fuselage by die process bracket correspondence
Enter position to fuselage posture adjustment positioning unit 7；4th step, lifts position to the corresponding technique bracket of fuselage, to fuselage by forebody 2
2 realize flexible support；5th step, measures the measurement point of fuselage 2 using active operation ladder 3 and passes through fuselage posture adjustment positioning unit 7
Posture adjustment；6th step, lifts position to the corresponding technique bracket 11 of head by head 1, flexible support is realized to head 1；7th
Step, measures head measurement point using active operation ladder 3 and passes through the posture adjustment of head posture adjustment positioning unit 9；8th step, by fuselage support
Frame 5, interface operating desk 8, fuselage end operating desk 4, internal work ladder 12 enter position and complete related docking operation；9th step, will
Terraced 12 returns of fuselage bracket 5, interface operating desk 8, fuselage end operating desk 4, internal work；Tenth step, by the machine after docking
Body 2 and the overall distancing of head 1, complete Butt Assembling.
Claims (8)
1. a kind of airframe docks numeric terminal layout structure with head, it is characterised in that：Described structure includes two machines
Body bracket, head posture adjustment positioning unit, fuselage posture adjustment positioning unit, two laser trackers, two interface operating desks, one
Fuselage end operating desk, two active operation ladders and an integrated control system operating desk, two fuselage brackets are located under airframe
Side, support and protective effect are played to fuselage, and head posture adjustment positioning unit and fuselage posture adjustment positioning unit are respectively arranged at described
The lower section of head and fuselage, head posture adjustment positioning unit and fuselage posture adjustment positioning unit are constituted by four three axis positioners, respectively
Individual three axis positioner is provided with three-dimensional force sensor；
Two described laser trackers are symmetricly set in the both sides in front of head, form aircraft digital measurement field, every is swashed
Optical tracker system is installed by the laser tracker pedestal lifted based on king bolt；
Described two interface operating desks are respectively arranged in head and fuselage abutment joint both sides；
Described fuselage end operating desk is arranged at the end of fuselage, is operated as personnel and material into interior of aircraft docking area
Passage；
Two described active operation ladders are arranged in fuselage both sides, one man operation can voluntarily reach relevant position as needed；
Described integrated control system operating desk is integrated with measuring system, posture adjusting system, process management and Database Systems and completed
Docking control work, is arranged at fuselage side-lower.
2. a kind of airframe docks numeric terminal layout structure with head according to claim 1, it is characterised in that：Institute
The fuselage end operating desk stated includes electric up-down counter and the access way of fuselage interior is passed in and out for workman, the access way
Top sets platform, and lifting counter, which rises the material for needing to use when assembling, to be transported at platform.
3. a kind of airframe docks numeric terminal layout structure with head according to claim 2, it is characterised in that：Institute
The table surface height for stating platform is identical with the floor level in aircraft cabin.
4. a kind of airframe docks numeric terminal layout structure with head according to claim 3, it is characterised in that：Institute
State close aircraft side on platform and anti-collision rubber bar is installed.
5. a kind of airframe docks numeric terminal layout structure with head according to claim 4, it is characterised in that：Institute
The numeric terminal layout structure stated also includes an internal work ladder being made using aluminium alloy lightweight material, internal work
Ladder is positioned over inside aircraft cabin on joint floor.
6. a kind of airframe docks numeric terminal layout structure with head according to claim 5, it is characterised in that：Institute
The surrounding for stating internal work ladder is provided with anti-collision rubber.
7. a kind of airframe docks numeric terminal layout structure with head according to claim 6, it is characterised in that：Institute
State and be correspondingly arranged on a technique bracket on head posture adjustment positioning unit and fuselage posture adjustment positioning unit respectively, head and fuselage point
It is not positioned on each self-corresponding technique bracket.
8. a kind of airframe docks numeric terminal layout structure with head according to claim 7, it is characterised in that：Institute
The interface operating desk stated is divided into 2 layers of Liftable type operating desk and base.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720211511.7U CN206502049U (en) | 2017-03-06 | 2017-03-06 | A kind of airframe docks numeric terminal layout structure with head |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720211511.7U CN206502049U (en) | 2017-03-06 | 2017-03-06 | A kind of airframe docks numeric terminal layout structure with head |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206502049U true CN206502049U (en) | 2017-09-19 |
Family
ID=59841747
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720211511.7U Expired - Fee Related CN206502049U (en) | 2017-03-06 | 2017-03-06 | A kind of airframe docks numeric terminal layout structure with head |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206502049U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108791947A (en) * | 2018-05-28 | 2018-11-13 | 成都飞机工业（集团）有限责任公司 | A kind of anti-tailspin mounting device and localization method |
| CN111266822A (en) * | 2020-03-12 | 2020-06-12 | 散裂中子源科学中心 | Remote self-positioning installation equipment and method for vacuum box of waste beam station |
| CN112570987A (en) * | 2020-10-27 | 2021-03-30 | 成都飞机工业（集团）有限责任公司 | Flexible posture-adjusting and involuting tool and assembling method thereof |
| CN113247297A (en) * | 2021-06-28 | 2021-08-13 | 成都飞机工业（集团）有限责任公司 | Integrated system for machining and testing large part of machine body |
-
2017
- 2017-03-06 CN CN201720211511.7U patent/CN206502049U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108791947A (en) * | 2018-05-28 | 2018-11-13 | 成都飞机工业（集团）有限责任公司 | A kind of anti-tailspin mounting device and localization method |
| CN111266822A (en) * | 2020-03-12 | 2020-06-12 | 散裂中子源科学中心 | Remote self-positioning installation equipment and method for vacuum box of waste beam station |
| CN112570987A (en) * | 2020-10-27 | 2021-03-30 | 成都飞机工业（集团）有限责任公司 | Flexible posture-adjusting and involuting tool and assembling method thereof |
| CN113247297A (en) * | 2021-06-28 | 2021-08-13 | 成都飞机工业（集团）有限责任公司 | Integrated system for machining and testing large part of machine body |
| CN113247297B (en) * | 2021-06-28 | 2021-12-10 | 成都飞机工业（集团）有限责任公司 | Integrated system for machining and testing large part of machine body |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170919 |