CN109368509A - Aircraft engine Intelligent assembly system - Google Patents
Aircraft engine Intelligent assembly system Download PDFInfo
- Publication number
- CN109368509A CN109368509A CN201811371329.3A CN201811371329A CN109368509A CN 109368509 A CN109368509 A CN 109368509A CN 201811371329 A CN201811371329 A CN 201811371329A CN 109368509 A CN109368509 A CN 109368509A
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- China
- Prior art keywords
- axis
- suspender
- main body
- whirlpool
- terminal pad
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B66—HOISTING; LIFTING; HAULING
- B66C—CRANES; LOAD-ENGAGING ELEMENTS OR DEVICES FOR CRANES, CAPSTANS, WINCHES, OR TACKLES
- B66C19/00—Cranes comprising trolleys or crabs running on fixed or movable bridges or gantries
-
- 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
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- 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
- B23P2700/00—Indexing scheme relating to the articles being treated, e.g. manufactured, repaired, assembled, connected or other operations covered in the subgroups
- B23P2700/01—Aircraft parts
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Carriers, Traveling Bodies, And Overhead Traveling Cranes (AREA)
- Load-Engaging Elements For Cranes (AREA)
Abstract
The invention discloses a kind of aircraft engine Intelligent assembly systems, including main body rack, low whirlpool suspender, auxiliary hangar system, crane, X-axis running gear, Y-axis jacking system, fan adjustment suspender, A axis rotary system, gear-box installation vehicle, core engine to load and unload suspender.The invention has the characteristics that being one group of specialized extremely strong horizontal fixed assembly system according to the part component feature design of the technical process and assembly of production assembly.Spatial attitude of the part in assembling process can be adjusted in a short time by the control feedback of system, avoided the responsible operation of stand-type assembly, greatly improved the efficiency of production assembly.The assembling quality of product is greatly enhanced due to increasing the on-line checkings instrument such as precise instrument, level meter in assembly, also the foundation for subsequent engine horizontal production line is taken a firm foundation.
Description
Technical field
The present invention relates to aircraft engines to assemble field, and in particular to a kind of aircraft engine Intelligent assembly system.
Background technique
Assembly is that engine manufactures most important link, and mounting technology level and assembling quality directly affect engine
Reliable life and main performance parameter, airspace engine new material in China's will study application in recent years, part plus
Work, inspection are all greatly improved, but general assembly link has still continued to use the fixed assembly mode stood of early stage, based on solid
Fixed rigid cage is assembled, and tooling technological level is also assembled with traditional assembly method, such as: start in assembly
When thermomechanical components, the height by repeatedly adjusting equipment, the horizontal attitude of hanging component, the pivot angle in space are needed, to guarantee to match
The accuracy of conjunction greatly reduces the efficiency of production in this way.The quality assembled in traditional assembly method not can guarantee, and not have
On-line measurement, such quality it is difficult to ensure that, and to the basic quality of operating personnel require it is also very high.This just makes organization of production mould
The manufacture level of formula and assembly technique and modern engine part component is uncoordinated, it is difficult to meet the needs of space flight.
Summary of the invention
Problem that the purpose of the present invention is to overcome the above shortcomings provides a kind of aircraft engine Intelligent assembly system.
Present invention technical solution used for the above purpose is: aircraft engine Intelligent assembly system, including master
Body support frame, low whirlpool suspender, auxiliary hangar system, crane, X-axis running gear, Y-axis jacking system, fan adjustment suspender, the rotation of A axis
Transfer from one department to another system, gear-box installation vehicle, core engine handling suspender, the X-axis running gear, crane are installed on main body rack, institute
It states Y-axis jacking system to be arranged in X-axis running gear, the auxiliary hangar system, the setting of A axis rotary system go up and down in Y-axis and be
On system, the low whirlpool suspender, fan adjustment suspender, core engine handling suspender are arranged on crane, the X-axis running gear, Y-axis
Jacking system, fan adjustment suspender, A axis rotary system, core engine handling suspender with operating system signal communication.
The low whirlpool suspender includes low whirlpool suspender main body, low whirlpool terminal pad, the low whirlpool suspender main body and low whirlpool terminal pad
Connection, is equipped with therebetween pressure sensor, low whirlpool suspender turn-screw is equipped in the low whirlpool suspender main body, described low
Hanging sliding block is installed, the hanging sliding block is connect with crane on the suspender turn-screw of whirlpool;The auxiliary hangar system includes auxiliary
Hangar system main body, the right terminal pad in low whirlpool, the left terminal pad in low whirlpool are helped, the auxiliary hanging system body is led by terminal pad movement
Rail is connect with the mobile slide body of terminal pad, and the mobile slide body of the terminal pad opens and closes shaft and the left terminal pad in low whirlpool by terminal pad
Connection, the low left terminal pad in whirlpool are equipped with guide rail and lock scroll wheel, are equipped with core engine hanging on the auxiliary hanging system body
Moving guide rail is equipped with suspended mobile sliding block on the core engine suspended mobile guide rail, is equipped on the suspended mobile sliding block
Core engine hanging auxiliary suspension hook, core engine hang connecting rod, and the low left terminal pad in whirlpool and the right terminal pad in low whirlpool pass through company
The connection of disk latch is connect, has assigned lock screw, connection positioning pin on terminal pad latch, the left terminal pad in the low whirlpool and described
It is mounted on low whirlpool terminal pad locating piece in the low right terminal pad in whirlpool, in the low left terminal pad in whirlpool and the right terminal pad in low whirlpool
Equipped with arc orbit;The X-axis running gear includes X-axis running gear main body, X-axis hoofing part unit, walking roller, described
X-axis hoofing part unit is mounted in X-axis running gear main body, and the walking roller is connect with X-axis hoofing part unit, described
Walking roller is equipped with latch segment, and the latch segment is connect with locking driving unit;The Y-axis jacking system includes Y-axis lifting system
System main body, Y-axis elevation driving unit, the Y-axis jacking system main body are led by Y-axis riser guide, elevating screw and X-axis walking
Body connection, the elevating screw are connect with Y-axis elevation driving unit;The A axis rotary system include A axis rotary system main body,
Fan lifts turning unit, fan lifts rotary motive power unit, and the A axis rotating body turns round shaft by A axis and Y-axis is gone up and down
System body connection, the fan lifting turning unit are mounted in A axis rotary system main body, are equipped with guide rail therebetween
Scroll wheel is locked, the fan lifting turning unit is connect with fan lifting rotary motive power unit, and the fan lifting revolution is single
Fan positioning pin is installed in member;The fan adjustment suspender includes fan adjustment suspender main body, fan adjustment suspender motor, wind
Fan adjustment suspender speed reducer, fan adjustment suspender main body pass sequentially through drive connecting rod, follower link and fan adjustment suspender
Speed reducer connection, the fan adjustment suspender speed reducer are connect with fan adjustment suspender motor, and the fan adjusts suspender main body
Equipped with lifting connection frame moving guide rail, the lifting connection frame moving guide rail is connect by sliding block with lifting connection frame, described to hang
Fixed pin is installed on dress connection frame;The gear-box installation vehicle includes installation vehicle car body, installs and is equipped with deceleration on vehicle car body
Machine support frame, the speed reducer support frame are connect with lifting system;The core engine handling suspender includes core engine suspender main body,
Core engine lifting connecting rod is installed, the core engine suspender main body is equipped with turn-screw, institute in the core engine suspender main body
It states and slide suspension centre is installed on turn-screw.
The A axis rotary system further includes digital display, operating illumination, and the two is mounted in A axis rotary system main body.
Illumination and bar shaped lighting lamp for work are installed in the right terminal pad in low whirlpool.
The invention has the characteristics that being one group designed according to the technical process of production assembly and the part component feature of assembly
Specialized extremely strong horizontal fixed assembly system.Part can be adjusted in a short time in assembling process by the control feedback of system
In spatial attitude, avoid the responsible operation of stand-type assembly, greatly improve production assembly efficiency.Due in assembly
The assembling quality that the on-line checkings instrument such as precise instrument, level meter greatly enhances product is increased, is also started to be subsequent
The foundation of machine horizontal production line is taken a firm foundation.
Detailed description of the invention
Fig. 1 is structural schematic diagram of the invention.
Fig. 2 is low whirlpool suspender schematic diagram of the invention.
Fig. 3 is auxiliary hanging system schematic one of the invention.
Fig. 4 is auxiliary hanging system schematic two of the invention.
Fig. 5 is auxiliary hanging system schematic three of the invention.
Fig. 6 is X-axis running gear schematic diagram of the invention.
Fig. 7 is Y-axis jacking system schematic diagram one of the invention.
Fig. 8 is Y-axis jacking system and A axis rotary system schematic diagram two of the invention.
Fig. 9 is fan adjustment suspender schematic diagram of the invention.
Figure 10 is gear-box installation vehicle schematic diagram of the invention.
Figure 11 is core of the invention machine handling suspender schematic diagram.
Wherein: 1, main body rack 2, operating system 3, low whirlpool suspender 300, low whirlpool suspender main body 301, low whirlpool connect
Connect disk 302, pressure sensor 303, low whirlpool suspender turn-screw 304, hanging sliding block 4, auxiliary hangar system
400, auxiliary hanging system body 401, the right terminal pad 402 in low whirlpool, low 403 terminal pad latch of whirlpool terminal pad locating piece
404, lock screw 405, connection positioning pin 406, illumination 407, arc guide rail 408, bar shaped lighting lamp for work
409, guide rail locking scroll wheel 410, link disk folding shaft 411, terminal pad moving guide rail 412, the mobile cunning of terminal pad
Block 413, core engine suspended mobile guide rail 414, suspension hook move sliding block 415, core engine hanging assists suspension hook 416,
Core engine hangs connecting rod 417, the left terminal pad 5 in low whirlpool, crane runway 6, crane 7, X-axis running gear 700, X-axis
Running gear main body 701, X-axis hoofing part unit 702, locking driving unit 703, latch segment 704, walking rolling
Take turns 8, Y-axis jacking system 800, Y-axis jacking system main body 801, Y-axis riser guide 802, elevating screw 803, Y
Axis elevation driving unit 11, fan adjustment suspender 1100, fan adjustment suspender main body 1101, fan adjustment suspender slow down
Machine 1102, drive connecting rod 1103, follower link 1104, fan adjustment suspender motor 1105, lifting connection frame are mobile
Guide rail 1106, sliding block 1107, lifting connection frame 1108, fixed pin 12, A axis rotary system 1200, A axis rotation system
Uniting, main body 1201, fan positioning pin 1202, fan lift turning unit 1203, guide rail locks scroll wheel 1204, A axis
Turn round shaft 1205, operating illumination 1206, digital display 1207, fan lifting rotary motive power unit 13, fan
Unit 14, precise instrument 15, gear-box installation vehicle 1500, installation vehicle main body 1501, lifting system 1502, speed reducer
Support frame 1503, speed reducer 16, core engine unit 17, low whirlpool unit 18, core engine load and unload suspender 1800, core
Machine suspender main body 1801, core engine lift connecting rod 1802, drive lead screw 1803, slide suspension centre.
Specific embodiment
As shown in Figure 1, the present invention be a kind of aircraft engine Intelligent assembly system, including main body rack 1, low whirlpool suspender 3,
Hangar system 4, crane 6, X-axis running gear 7, Y-axis jacking system 8, fan is assisted to adjust suspender 11, A axis rotary system 12, tooth
Roller box installs vehicle 15, core engine loads and unloads suspender 18, and the X-axis running gear 7, crane 6 are installed in the crane rail of main body rack 1
On road 5, the Y-axis jacking system 8 is arranged in X-axis running gear 7, and the auxiliary hangar system 4, A axis rotary system 12 are set
It sets on Y-axis jacking system 8, the low whirlpool suspender 3, fan adjustment suspender 11, core engine handling suspender 18 are arranged in crane 6
On, the X-axis running gear 7, Y-axis jacking system 8, fan adjustment suspender 11, A axis rotary system 12, core engine load and unload suspender
18 with 2 signal communication of operating system.
As shown in Fig. 2, the low whirlpool suspender 3 includes low whirlpool suspender main body 300, low whirlpool terminal pad 301, the low whirlpool suspender
Main body 300 is connect with low whirlpool terminal pad 301, is equipped with pressure sensor 302 therebetween, in the low whirlpool suspender main body 300
Low whirlpool suspender turn-screw 303 is installed, hanging sliding block 304, the hanging are installed on the low whirlpool suspender turn-screw 303
Sliding block 304 is connect with crane 6;As in Figure 3-5, the auxiliary hangar system 4 includes auxiliary hanging system body 400, low whirlpool
Right terminal pad 401, the left terminal pad 417 in low whirlpool, the auxiliary hanging system body 400 is by terminal pad moving guide rail 411 and even
It connects the mobile slide body 412 of disk to connect, the mobile slide body 412 of the terminal pad opens and closes shaft 410 and the left company in low whirlpool by terminal pad
The connection of disk 417 is connect, the low left terminal pad 417 in whirlpool is equipped with guide rail and locks scroll wheel 409, and the auxiliary is hung on system body 400
Core engine suspended mobile guide rail 413 is installed, suspended mobile sliding block 414 is installed on the core engine suspended mobile guide rail 413,
Core engine hanging auxiliary suspension hook 415, core engine hanging connecting rod 416, the low whirlpool are installed on the suspended mobile sliding block 414
The right terminal pad 401 of left terminal pad 417 and the low whirlpool is connected by terminal pad latch 403, is assigned on terminal pad latch 403
There are lock screw 404, connection positioning pin 405, is respectively mounted in the low left terminal pad 417 in whirlpool and the right terminal pad 401 in the low whirlpool
There is low whirlpool terminal pad locating piece 402, is equipped with circular arc rail in the low left terminal pad 417 in whirlpool and the right terminal pad 401 in the low whirlpool
Road 407 is equipped with illumination 406 and bar shaped lighting lamp for work 408 in the low right terminal pad 401 in whirlpool;As shown in fig. 6, the X
Axis running gear 7 includes X-axis running gear main body 700, X-axis hoofing part unit 701, walking roller 704, the X-axis walking
Driving unit 701 is mounted in X-axis running gear main body 700, and the walking roller 704 connects with X-axis hoofing part unit 701
It connects, the walking roller 704 is equipped with latch segment 703, and the latch segment 703 is connect with locking driving unit 702;Such as Fig. 7,8 institutes
Show, the Y-axis jacking system 8 includes Y-axis jacking system main body 800, Y-axis elevation driving unit 803, the Y-axis jacking system
Main body 800 is connect by Y-axis riser guide 801, elevating screw 802 with X-axis walking main body 700, the elevating screw 802 and Y
Axis elevation driving unit 803 connects;As shown in Figure 7,8, the A axis rotary system 12 includes A axis rotary system main body 1200, wind
Fan lifting turning unit 1202, fan lift rotary motive power unit 1207, and the A axis rotating body 1200 is turned by the revolution of A axis
Axis 1204 is connect with Y-axis jacking system main body 800, and the fan lifting turning unit 1202 is mounted on A axis rotary system
In main body 1200, it is equipped with guide rail therebetween and locks scroll wheel 1203, the fan lifting turning unit 1202 and fan lift
Rotary motive power unit 1207 connects, and fan positioning pin 1201, the A axis rotation are equipped on the fan lifting turning unit 1202
Turn to be also equipped with digital display 1206, operating illumination 1205 on system body 1200;As shown in figure 9, the fan adjustment is hung
Tool 11 includes fan adjustment suspender main body 1100, fan adjusts suspender motor 1104, fan adjusts suspender speed reducer 1101, described
Fan adjustment suspender main body 1100 passes sequentially through drive connecting rod 1102, follower link 1103 and fan and adjusts suspender speed reducer 1101
Connection, the fan adjustment suspender speed reducer 1101 are connect with fan adjustment suspender motor 1104, and the fan adjusts suspender master
Body 1100 is equipped with lifting connection frame moving guide rail 1105, and the lifting connection frame moving guide rail 1105 passes through sliding block 1106 and lifting
Connection frame 1107 connects, and is equipped with fixed pin 1108 on the lifting connection frame 1107;As shown in Figure 10, the gear-box installation
Vehicle 15 includes installation vehicle car body 1500, installs and is equipped with speed reducer support frame 1502 on vehicle car body 1500, the speed reducer support
Frame 1502 is connect with lifting system 1501;As shown in figure 11, the core engine handling suspender 18 includes core engine suspender main body
1800, core engine lifting connecting rod 1801, the core engine suspender main body 1800 are installed in the core engine suspender main body 1800
It is equipped with turn-screw 1802, slide suspension centre 1803 is installed on the turn-screw 1802.
The course of work is as follows:
1, transport device send fan unit 13 to the preset of installation station, and equipment operator's operating system 2 controls at this time
System drive X-axis running gear 7 drives Y-axis jacking system 8, A axis rotary system 12, the operation of auxiliary hangar system 4 to preset to first
Point;
2,2 control system of operating system driving Y-axis jacking system 8 drives A axis rotary system 12, auxiliary hangar system 4 vertically to transport
Positioning Hoisting Position of the row extremely with fan unit 13;
3,2 control system of operating system connects fan positioning pin 1201, after fan positioning pin 1201 fixes, to fan tune
Whole suspender 11 and fan unit 13 are attached with fixed pin 1108, are adjusted fan unit 13 with fan adjustment suspender 11 after connection
It is whole to horizontal;
4, vehicle 15 is installed with the gear-box for being loaded with speed reducer support frame 1502, loads adjustment and installation speed reducer 1503;
5, after the completion of loading, the pipeline of surrounding is assembled;
6, manual teardown lock screw 404, connection positioning pin 405 will assist the right terminal pad 401 in low whirlpool, low in hangar system 4
The left terminal pad 417 in whirlpool is lifted along Y-direction, then left and right terminal pad can open and close shaft 410 with terminal pad and rotate, in order to core
Machine can be lifted into default rigging position by suspender;
7, core engine unit 16 is transported to predeterminated position by travelling bogie, is connected core engine suspender 18 with crane 6 and is lifted by crane core engine
The abutting joint position of core engine unit 16 and fan unit 13 is reached, connection core engine hanging auxiliary suspension hook 415, core engine are hung
Connecting rod 416 is hung, the position of slide suspension centre 1803 is adjusted by manually adjusting drive lead screw 1802, to adjust core engine
In the assembly posture with fan unit 13, the posture during adjusting is monitored and by digital display unit 16 by precise instrument 14
1206 displays;
8, core engine unit 16 and fan unit 13 are assembled, while the company of core engine unit 16 Yu fan unit 13 is installed
Take over road;
9, it connect core engine suspender 18 with crane 6 with fan adjustment suspender 11 to be cooperated, by fan unit 13 and core engine list
The assembly of member 16 carries out horizontal adjustment posture, to guarantee the installation in low whirlpool;
10, low whirlpool unit 17 is transported to the Hoisting Position of assembly, with crane 6 connect low whirlpool suspender 3 lift low whirlpool unit 17 to
Preset is assembled, low whirlpool component is adjusted to level;
11, low whirlpool unit 17 is installed, after the completion manually along the right terminal pad 401 in the low whirlpool in Y-direction whereabouts, the left terminal pad 417 in low whirlpool, then
Left and right terminal pad can be opened and closed shaft rotation 410 with terminal pad and is harmonious, and be slidably connected disk latch 403, installation locking screw 404,
Terminal pad is harmonious completion by connection positioning pin 405;
12, lifting is connect with low whirlpool cell location with the low whirlpool terminal pad locating piece 402 in low whirlpool terminal pad.When position is improper
When, the adjustment of position can be carried out by terminal pad moving guide rail 411;
13, core engine suspender 18 is removed, core engine is hung into auxiliary suspension hook 415, core engine hanging connecting rod 416 and core engine list
Member 16 separates, and removes low whirlpool suspender 3, removes the detection device instrument of assembly;
14,2 driving fan of operating system lifts rotary motive power unit 1207, is lifted inside turning unit 1202 by driving fan
Dial scale, drive fan lifting turning unit 1202 rotate.The low whirlpool terminal pad when fan lifting turning unit 1202 turns round
Help out and follow rotation, it is therefore intended that guarantee fan unit, core engine unit, low whirlpool unit assemble the half of completion at
Product in the same horizontal line can be stable follow fan lifting rotary motive power unit 1207 turn round;
15, the whole pipeline in periphery of engine is installed.By control fan lift turning unit 1207 gyroscopic pendulum angular motion come
All peripheral pipelines are installed;
16, after all peripheral pipe components are installed, fixed pin 1108, fan positioning pin 1201, the right connection in low whirlpool are dismantled
Disk 401, assembly are completed.
The foregoing is only a preferred embodiment of the present invention, but scope of protection of the present invention is not limited thereto,
Anyone skilled in the art within the technical scope of the present disclosure, according to the technique and scheme of the present invention and its
Inventive concept is subject to equivalent substitution or change, should be covered by the protection scope of the present invention.
Claims (4)
1. aircraft engine Intelligent assembly system, it is characterised in that: including main body rack, low whirlpool suspender, auxiliary hangar system, hang
Vehicle, X-axis running gear, Y-axis jacking system, fan adjustment suspender, A axis rotary system, gear-box installation vehicle, core engine handling are hung
Tool, the X-axis running gear, crane are installed on main body rack, and the Y-axis jacking system is arranged in X-axis running gear,
The auxiliary hangar system, A axis rotary system are arranged on Y-axis jacking system, and the low whirlpool suspender, fan adjust suspender, core
Scheming is loaded and unloaded suspender and is arranged on crane, the X-axis running gear, Y-axis jacking system, fan adjustment suspender, A axis rotation system
System, core engine handling suspender with operating system signal communication.
2. aircraft engine Intelligent assembly system as described in claim 1, it is characterised in that: the low whirlpool suspender includes low whirlpool
Suspender main body, low whirlpool terminal pad, the low whirlpool suspender main body are connect with low whirlpool terminal pad, are equipped with pressure sensing therebetween
Device is equipped with low whirlpool suspender turn-screw in the low whirlpool suspender main body, is equipped with hanging on the low whirlpool suspender turn-screw
Sliding block, the hanging sliding block are connect with crane;The auxiliary hangar system includes auxiliary hanging system body, the right connection in low whirlpool
Disk, the left terminal pad in low whirlpool, the auxiliary hanging system body are connect by terminal pad moving guide rail with the mobile slide body of terminal pad,
The mobile slide body of the terminal pad opens and closes shaft by terminal pad and connect with the left terminal pad in low whirlpool, and the low left terminal pad in whirlpool is equipped with and leads
Rail locks scroll wheel, and core engine suspended mobile guide rail is equipped on the auxiliary hanging system body, and the core engine hanging moves
Suspended mobile sliding block is installed on dynamic guide rail, core engine hanging auxiliary suspension hook, core engine are installed on the suspended mobile sliding block
Connecting rod is hung, the low left terminal pad in whirlpool is connected with the low right terminal pad in whirlpool by terminal pad latch, terminal pad locking
Lock screw, positioning pin have been assigned on plate, and low whirlpool is mounted in the low left terminal pad in whirlpool and the right terminal pad in low whirlpool and is connected
Disk locating piece is connect, is equipped with arc orbit in the low left terminal pad in whirlpool and the right terminal pad in low whirlpool;The X-axis running gear
Including X-axis running gear main body, X-axis hoofing part unit, walking roller, the X-axis hoofing part unit is mounted on X-axis walking
On system body, the walking roller is connect with X-axis hoofing part unit, and the walking roller is equipped with latch segment, the locking
Block is connect with locking driving unit;The Y-axis jacking system includes Y-axis jacking system main body, Y-axis elevation driving unit, the Y
By Y-axis riser guide, elevating screw and X-axis walking main body connection, the elevating screw and Y-axis are gone up and down axis jacking system main body
Driving unit connection;The A axis rotary system includes A axis rotary system main body, fan lifting turning unit, fan lifting revolution
Power unit, the A axis rotating body are turned round shaft by A axis and are connect with Y-axis jacking system main body, the fan lifting
Turning unit is mounted in A axis rotary system main body, is equipped with guide rail therebetween and is locked scroll wheel, the fan lifting revolution is single
Member is connect with fan lifting rotary motive power unit, is equipped with fan positioning pin on the fan lifting turning unit;The fan
Adjustment suspender includes fan adjustment suspender main body, fan adjustment suspender motor, fan adjustment suspender speed reducer, fan adjustment
Suspender main body passes sequentially through drive connecting rod, follower link and fan adjustment suspender speed reducer connection, the fan adjustment suspender and subtracts
Fast machine is connect with fan adjustment suspender motor, and the fan adjustment suspender main body is equipped with lifting connection frame moving guide rail, described to hang
Dress connection frame moving guide rail is connect by sliding block with lifting connection frame, is equipped with fixed pin on the lifting connection frame;The tooth
It includes installation vehicle car body that roller box, which installs vehicle, installs and is equipped with speed reducer support frame on vehicle car body, the speed reducer support frame with mention
The connection of the system of liter;The core engine handling suspender includes core engine suspender main body, is equipped with core in the core engine suspender main body
Scheming lifts connecting rod, and the core engine suspender main body is equipped with turn-screw, is equipped with slide suspension centre on the turn-screw.
3. aircraft engine Intelligent assembly system as claimed in claim 2, it is characterised in that: the A axis rotary system also wraps
Digital display, operating illumination are included, the two is mounted in A axis rotary system main body.
4. aircraft engine Intelligent assembly system as claimed in claim 2, it is characterised in that: pacify in the low right terminal pad in whirlpool
Equipped with illumination and bar shaped lighting lamp for work.
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CN201811371329.3A CN109368509B (en) | 2018-11-18 | 2018-11-18 | Intelligent assembly system for aircraft engine |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110153703A (en) * | 2019-06-21 | 2019-08-23 | 江苏同力日升机械股份有限公司 | A kind of axis drives assembly pipeline automatically |
CN112723180A (en) * | 2020-12-29 | 2021-04-30 | 珠海迪沃航空工程有限公司 | Intelligent airplane engine position changing device and position changing method thereof |
Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102356041A (en) * | 2009-03-17 | 2012-02-15 | 斯奈克玛 | Workshop for preparing aircraft engines for shipping |
CN102666360A (en) * | 2009-11-20 | 2012-09-12 | 斯奈克玛 | Assembly for handling an aircraft engine |
CN103204248A (en) * | 2013-03-25 | 2013-07-17 | 大连理工大学 | Numerical-control electric frame truck for airplane engine mounting |
US20140061559A1 (en) * | 2012-08-31 | 2014-03-06 | Tronair, Inc. | Aircraft Engine Stand |
CN104709469A (en) * | 2013-12-17 | 2015-06-17 | 空中客车运营简化股份公司 | Assembly for an aircraft, aircraft part, aircraft, and removing method |
CN104999268A (en) * | 2015-07-17 | 2015-10-28 | 大连四达高技术发展有限公司 | Auxiliary airplane engine installing system |
WO2015168637A1 (en) * | 2014-05-02 | 2015-11-05 | Morey Joel T | Aircraft engine stand |
CN106275505A (en) * | 2015-06-23 | 2017-01-04 | 罗尔公司 | Install or remove aircraft engine |
CN107352043A (en) * | 2017-06-26 | 2017-11-17 | 大连理工大学 | A kind of six axle posture adjustment platforms for aircraft engine whole machine installation |
CN108284966A (en) * | 2017-12-26 | 2018-07-17 | 中国航发四川燃气涡轮研究院 | A kind of small aero hydraulic pressure assembly vehicle frame |
-
2018
- 2018-11-18 CN CN201811371329.3A patent/CN109368509B/en active Active
Patent Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102356041A (en) * | 2009-03-17 | 2012-02-15 | 斯奈克玛 | Workshop for preparing aircraft engines for shipping |
CN102666360A (en) * | 2009-11-20 | 2012-09-12 | 斯奈克玛 | Assembly for handling an aircraft engine |
US20140061559A1 (en) * | 2012-08-31 | 2014-03-06 | Tronair, Inc. | Aircraft Engine Stand |
CN103204248A (en) * | 2013-03-25 | 2013-07-17 | 大连理工大学 | Numerical-control electric frame truck for airplane engine mounting |
CN104709469A (en) * | 2013-12-17 | 2015-06-17 | 空中客车运营简化股份公司 | Assembly for an aircraft, aircraft part, aircraft, and removing method |
WO2015168637A1 (en) * | 2014-05-02 | 2015-11-05 | Morey Joel T | Aircraft engine stand |
CN106275505A (en) * | 2015-06-23 | 2017-01-04 | 罗尔公司 | Install or remove aircraft engine |
CN104999268A (en) * | 2015-07-17 | 2015-10-28 | 大连四达高技术发展有限公司 | Auxiliary airplane engine installing system |
CN107352043A (en) * | 2017-06-26 | 2017-11-17 | 大连理工大学 | A kind of six axle posture adjustment platforms for aircraft engine whole machine installation |
CN108284966A (en) * | 2017-12-26 | 2018-07-17 | 中国航发四川燃气涡轮研究院 | A kind of small aero hydraulic pressure assembly vehicle frame |
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CN110153703A (en) * | 2019-06-21 | 2019-08-23 | 江苏同力日升机械股份有限公司 | A kind of axis drives assembly pipeline automatically |
CN112723180A (en) * | 2020-12-29 | 2021-04-30 | 珠海迪沃航空工程有限公司 | Intelligent airplane engine position changing device and position changing method thereof |
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