CN207191477U - A kind of multiple material stringer of aircraft, wall panel skin upset docking equipment - Google Patents
A kind of multiple material stringer of aircraft, wall panel skin upset docking equipment Download PDFInfo
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- CN207191477U CN207191477U CN201720799188.XU CN201720799188U CN207191477U CN 207191477 U CN207191477 U CN 207191477U CN 201720799188 U CN201720799188 U CN 201720799188U CN 207191477 U CN207191477 U CN 207191477U
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- corner
- stringer
- crossbeam
- wall panel
- fork
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Abstract
This application discloses a kind of multiple material stringer of aircraft, wall panel skin upset docking equipment, its structure is by column, crossbeam, four axles rotation docking unit, wall panel skin mould tire, stringer places bracket, ground, safety barrier etc. forms, wall panel skin mould tire, stringer is placed bracket and is placed in parallel on ground, the width that two groups of columns place bracket with crossbeam along wall panel skin mould tire and stringer moves back and forth, crossbeam is realized by screw rod transmission with column among two columns and lifted, multigroup four axles rotation docking unit passes through guide rail, rack pinion realizes length direction integral translation, safety barrier is arranged in two groups of column both ends, by column, crossbeam, wall panel skin mould tire, stringer is placed bracket etc. and is surrounded.
Description
Technical field
The application is related to Aircraft tooling manufacturing technology, particularly a kind of technique for aircraft composite stringer, wall panel skin
Upset docking equipment.
Background technology
In aircraft product component, wallboard base part is a lot, and frame sections, wing box, horizontal tail of hanging down all are by wallboard, frame rib, cut
The structure compositions such as corner cut piece, every kind of wall panel assembly is made up of wall panel skin and stringer.Wall panel skin and stringer are formed
, it is necessary to which stringer is accurately navigated on covering during wall panel assembly, this just needs to realize its positioning by related process equipment.
Typically positioned using metal stringer, wall panel skin using assembly jig and locating clamp plate, but work as and run into length
It is the hot-forming last stage during due to its stringer, wall panel skin docking when purlin, wall panel skin are the structure of composite, zero
Part is particularly, and covering major part situation has adhesivity, and manpower, machinery can not contact easily, common positioning means
It is difficult to ensure that it is positioned, its problem place is particularly just more highlighted when this covering exceeds the width of human hand reach.
Stringer, wall panel skin docking for composite type is, it is necessary to realize stringer undercarriage, aerial control on rack
180 ° of system upset, until accurately enter with wall panel skin position the basic function such as dock, it is necessary to it is a kind of be adapted to various stringer upset to position,
It is reliable and stable, automatically control, operate simple, both artistic and practical upset butt-joint process equipment.
The content of the invention
The purpose of the application is to provide general multiple material stringer, wall panel skin upset docking equipment, and it is compound to may be used as aircraft
The stringer of material type, wall panel skin accurately dock.
To achieve the above objectives, the application, which adopts the following technical scheme that, is achieved：
A kind of aircraft stringer, wall panel skin upset docking equipment, including column, crossbeam, four axles rotation docking unit, wallboard
Covering mould tire, stringer place bracket, ground, and ground is provided with two slide rails that are parallel and being engaged with column bottom, crossbeam
It is connected among two columns and with column by lead screw transmission mechanism, two columns are connected with crossbeam with slide rail, horizontal
Multigroup four axle rotation docking unit is equidistantly provided with beam, wall panel skin mould tire, stringer are placed bracket and lain in successively among slide rail
Ground on；Two columns are translated with crossbeam, four axles rotation docking unit by guide rail screw rod transmission along beam width direction；
Crossbeam is moved by guide rail screw rod transmission along column above-below direction；Described four axles rotation docking unit includes telescopic mast, corner
Fork, rotation clamp assembly, telescopic mast are that can carry out the flexible electric cylinder class formation moved up and down；Corner fork upper end is by leading
Rail, screw rod transmission and telescopic mast form transverse movement relation, and corner fork lower end is the fork configuration of 45 ° or so of corner；Rotation
Clamp assembly is made up of corner arm, compact heap, electromagnet, pin of giving up the throne, gear hobbing, roller etc., corner arm one end be auricle structure with
Corner fork forms fork ear and center of rotation is formed in fork ear junction with merging, and corner arm other end top is reverse L type structure, L
Bottom sets guide groove and mounting hole for setting end；Compact heap is arranged in the guide groove of corner arm, is inverted L shape, with corner arm
Reverse L type form mutual buckle structure；Electromagnet face compact heap bottom is arranged on the mounting hole of corner arm；Pin one of giving up the throne is platform
Rank, under step optical axis be provided with compression spring and corner arm outer wall formed it is counter push away, other end is twisted inwards to be threaded through corner arm
Enter compact heap bottom；The center of rotation that gear hobbing axle center is formed by corner fork and corner arm is fixed on the outside of corner arm；Roller
It is cylindrical with gear hobbing is tangent is fixed on corner fork；Telescopic mast on four axles rotation docking unit is by guide rail screw rod transmission along upper
Lower direction moves up and down, and corner fork, along the translational motion of beam width direction, rotates clamp assembly by guide rail screw rod transmission
It is driven by guide rail gear hobbing roller along axis of rotation and does 180 ° of rotations, the compact heap for rotating clamp assembly is opened by electromagnetic action
It is opened and closed resultant motion.
The spatial pose that the advantages of the application is to plan with motion control using automatically controlling realizes variable interface
Stringer in the upset in space, and realize it and docked with the accurate of wall panel skin, its is simple in construction, versatile, relative into
The features such as this is low, full-automatic, the metal wallboard for having the stringer of composite class, wall panel skin docking even common is docked equal
With general applicability.
The application is described in further detail below in conjunction with drawings and Examples.
Brief description of the drawings
The general multiple material stringers of Fig. 1, wallboard upset docking equipment configuration figure；
The axles of Fig. 2 tetra- rotation docking cellular construction figure；
Fig. 3 lifts by crane stringer state diagram；
Docking scheme after the upset of Fig. 4 stringers wallboard.
In Fig. 1~Fig. 3：1st, column；2nd, crossbeam；3rd, four axles rotation docking unit；4th, wall panel skin mould tire；5th, stringer is placed
Bracket；6th, ground；7th, telescopic mast；8th, corner fork；9th, clamp assembly is rotated；10th, corner arm；11st, compact heap；12nd, electromagnet；
13rd, give up the throne pin；14th, gear hobbing；15th, roller；16th, stringer；17th, wall panel skin.
Embodiment
Referring to Fig. 1~Fig. 4, a kind of aircraft stringer, wall panel skin upset docking equipment, including the rotation of column 1, crossbeam 2, four axles
Turn to place 3 yuan of order, wall panel skin mould tire 4, stringer on bracket 5, ground 6, ground 6 be provided with two it is parallel and with column 1
The slide rail that bottom is engaged, crossbeam 2 are arranged among two columns 1 and are connected with column 1 by lead screw transmission mechanism, and two vertical
Post 1 is connected with crossbeam 2 with slide rail, and multigroup four axle rotation docking unit 3, wall panel skin mould tire 4, length are equidistantly provided with crossbeam 2
Place bracket 5 and lie in successively on the ground 6 among slide rail in purlin；Two columns 1 are logical with crossbeam 2, four axles rotation docking unit 3
Guide rail screw rod transmission is crossed to translate along the width of crossbeam 2；Crossbeam 2 is moved by guide rail screw rod transmission along the above-below direction of column 1；Institute
The four axles rotation docking unit 3 stated includes telescopic mast 7, corner fork 8, rotation clamp assembly 9, and telescopic mast 7 is to be stretched
The electric cylinder class formation moved up and down；The upper end of corner fork 8 forms transverse movement by guide rail, screw rod transmission and telescopic mast 7 and closed
System, the lower end of corner fork 8 are the fork configuration of 45 ° or so of corner；Clamp assembly 9 is rotated by corner arm 10, compact heap 11, electricity
Magnet 12, pin 13 of giving up the throne, gear hobbing 14, roller 15 etc. form, and the one end of corner arm 10 is that auricle structure forms fork ear with corner fork 8
Center of rotation is formed in fork ear junction with merging, the other end top of corner arm 10 is reverse L type structure, and L bottoms set for setting end
Put guide groove and mounting hole；Compact heap 11 is arranged in the guide groove of corner arm 10, is inverted L shape, the reverse L type shape with corner arm 10
Into mutual buckle structure；The face compact heap bottom of electromagnet 12 is arranged on the mounting hole of corner arm 10；Pin 13 1 of giving up the throne is step,
Under step optical axis be provided with compression spring and the outer wall of corner arm 10 formed it is counter push away, other end is twisted inwards to be threaded through corner arm 10
Enter compact heap bottom；The center of rotation that the axle center of gear hobbing 14 is formed by corner fork 8 and corner arm 10 is fixed on outside corner arm 10
Side；Roller 15 it is cylindrical with gear hobbing 14 is tangent is fixed on corner fork 8；Telescopic mast 7 on four axles rotation docking unit 3 is by leading
Rail screw rod transmission is moved up and down along the vertical direction, and corner fork 8 is translated along the width of crossbeam 2 by guide rail screw rod transmission and transported
Dynamic, rotation clamp assembly 9 is driven along axis of rotation by guide rail gear hobbing roller and does 180 ° of rotations, rotates the compression of clamp assembly 9
Block 11 does opening and closing motion by electromagnetic action.
Multiple material stringer 16, the upset pair of wall panel skin 17 are carried out using a kind of multiple material stringer, wall panel skin upset docking equipment
Upset butt-joint process method and process when connecing is as follows：
1st, stringer 16 is placed upside down in stringer and placed on bracket 5；
2nd, four axles first are rotated into the rotation clamp assembly 9 on docking unit 3 to overturn upwards；
3rd, according to the section position angle of stringer 16 calculated, the axle of each group four rotation docking unit 3 on crossbeam 2 is existed
Space allocation is to the sectional position posture of stringer 16；
4th, column 1 is moved to above the placement location of stringer 16 with crossbeam 2, multigroup four axle rotation docking unit 3, the edge of crossbeam 2
Column 1 moves up and down the lower section of stringer 16 that the axle of each group four is rotated docking unit 3 and is adjusted on stringer placement bracket 5；
5th, electromagnet 12 is powered, and rotation clamp assembly 9 opens, and crossbeam 2 drives the axle of each group four rotation docking unit 3 along column
Move up and down by stringer 16 stand rib be caught in rotation clamp assembly 9 notch after, the axle of each group four rotation docking the synchronization lifting of unit 3,
Hold up stringer 16 leave to completely disengage stringer place bracket 5；
6th, the dead electricity of electromagnet 12, rotation clamp assembly 9 close, and rotation clamp assembly 9 clamps stringer 16；
7th, upset docking equipment is overall moves to 500mm above the theoretical position of wall panel skin 17 on wall panel skin mould tire 4；
8th, the axle of each group four rotation docking unit 13 deforms according to control system according to the precalculated stringer 16 that do not influence
Spatial pose path carry out space flip-flop movement, stringer 16 overturn 180 °, stringer 16 is in and docks shape with covering 17
State；
9th, crossbeam 2 drives synchronous decline of each group four axle rotation docking unit 3 to complete the accurate of stringer 16 and wall panel skin 17
Docking.
Claims (1)
1. a kind of multiple material stringer of aircraft, wall panel skin upset docking equipment, it is characterised in that including column, crossbeam, the rotation of four axles
Dock unit, wall panel skin mould tire, stringer and place bracket, ground, ground be provided with two it is parallel and match with column bottom
The slide rail of conjunction, crossbeam are arranged among two columns and are connected with column by lead screw transmission mechanism, and two columns are with crossbeam
It is connected with slide rail, multigroup four axle rotation docking unit is equidistantly provided with crossbeam, wall panel skin mould tire, stringer are placed bracket and put down successively
It is placed on the ground among slide rail；Two columns are with crossbeam, four axles rotation docking unit by guide rail screw rod transmission along crossbeam
Width translates；Crossbeam is moved by guide rail screw rod transmission along column above-below direction；Described four axles rotation docking unit bag
Telescopic mast, corner fork, rotation clamp assembly are included, telescopic mast is that can carry out the flexible electric cylinder class formation moved up and down；Corner
Fork upper end forms transverse movement relation by guide rail, screw rod transmission and telescopic mast, and corner fork lower end is 45 ° or so of corner
Fork configuration；Rotating clamp assembly includes corner arm, compact heap, electromagnet, pin of giving up the throne, gear hobbing, roller, and corner arm one end is ear
Chip architecture forms fork ear with merging in fork ear junction formation center of rotation with corner fork, and corner arm other end top is reverse L
Type structure, L bottoms set guide groove and mounting hole for setting end；Compact heap is arranged in the guide groove of corner arm, is inverted L shape,
Mutual buckle structure is formed with the reverse L type of corner arm；Electromagnet face compact heap bottom is arranged on the mounting hole of corner arm；Give up the throne pin
One is step, under step optical axis be provided with compression spring and corner arm outer wall formed it is counter push away, other end is is threaded through corner
Arm is screwed into compact heap bottom inwards；The center of rotation that gear hobbing axle center is formed by corner fork and corner arm is fixed on outside corner arm
Side；Roller it is cylindrical with gear hobbing is tangent is fixed on corner fork；Telescopic mast on four axles rotation docking unit passes through guide rail screw mandrel
Transmission is moved up and down along the vertical direction, and corner fork, along the translational motion of beam width direction, is rotated by guide rail screw rod transmission
Clamp assembly is driven along axis of rotation by guide rail gear hobbing roller and does 180 ° of rotations, and the compact heap for rotating clamp assembly passes through electromagnetism
Work is used as opening and closing motion.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720799188.XU CN207191477U (en) | 2017-07-04 | 2017-07-04 | A kind of multiple material stringer of aircraft, wall panel skin upset docking equipment |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720799188.XU CN207191477U (en) | 2017-07-04 | 2017-07-04 | A kind of multiple material stringer of aircraft, wall panel skin upset docking equipment |
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| Publication Number | Publication Date |
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| CN207191477U true CN207191477U (en) | 2018-04-06 |
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| CN201720799188.XU Active CN207191477U (en) | 2017-07-04 | 2017-07-04 | A kind of multiple material stringer of aircraft, wall panel skin upset docking equipment |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112173161A (en) * | 2020-09-21 | 2021-01-05 | 中航复合材料有限责任公司 | Auxiliary manufacturing device for composite material fuselage wallboard |
| CN117508630A (en) * | 2024-01-04 | 2024-02-06 | 成都市鸿侠科技有限责任公司 | Size-adjustable aircraft side aileron assembly type frame |
-
2017
- 2017-07-04 CN CN201720799188.XU patent/CN207191477U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112173161A (en) * | 2020-09-21 | 2021-01-05 | 中航复合材料有限责任公司 | Auxiliary manufacturing device for composite material fuselage wallboard |
| CN112173161B (en) * | 2020-09-21 | 2023-05-30 | 中航复合材料有限责任公司 | Auxiliary manufacturing device for composite material fuselage wall plate |
| CN117508630A (en) * | 2024-01-04 | 2024-02-06 | 成都市鸿侠科技有限责任公司 | Size-adjustable aircraft side aileron assembly type frame |
| CN117508630B (en) * | 2024-01-04 | 2024-04-05 | 成都市鸿侠科技有限责任公司 | Size-adjustable aircraft side aileron assembly type frame |
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