CN107160130A - A kind of aircraft engine installs equipment - Google Patents
A kind of aircraft engine installs equipment Download PDFInfo
- Publication number
- CN107160130A CN107160130A CN201710462962.2A CN201710462962A CN107160130A CN 107160130 A CN107160130 A CN 107160130A CN 201710462962 A CN201710462962 A CN 201710462962A CN 107160130 A CN107160130 A CN 107160130A
- Authority
- CN
- China
- Prior art keywords
- axis
- aircraft engine
- screw mandrel
- axle
- slide unit
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P19/00—Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes
-
- 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
- B64F5/50—Handling or transporting aircraft components
Landscapes
- Engineering & Computer Science (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transmission Devices (AREA)
Abstract
A kind of aircraft engine installs equipment, including AGV power chassis, Mecanum wheel, staggered form lifting device, the motor support frock for supporting aircraft engine, Electric Appliance Cabinet and posture adjustment platform mechanism, wherein, Mecanum wheel is arranged on AGV power chassis, many walking mechanisms are installed on AGV power chassis, posture adjustment platform mechanism is connected with AGV power chassis by staggered form lifting device, and motor support frock is connected with posture adjustment platform mechanism；Electric Appliance Cabinet is arranged on AGV power chassis, the aircraft engine being placed in motor support frock is lifted in aircraft engine cabin by staggered form lifting device, and the fine setting of certain position and angle is done by posture adjustment platform mechanism, and then realize the automatic transportation of aircraft engine and semi-automatic installment work, operator's quantity can effectively be reduced and save human resources, shorten the set-up time and improve production efficiency, improve Aircraft Production efficiency, and security is protected and improved.
Description
Technical field
Equipment is installed the present invention relates to aircraft mounting technique field, more particularly to a kind of aircraft engine.
Background technology
Existing aircraft engine installs main be installed in place aircraft engine using manpower mode, it is necessary to which ten come skilled
Workman, which coordinates, to complete, and not only need workman's number numerous, and hand labor intensity is big, install and take many, inefficiency；
Simultaneously because narrow space is not easy to operative, there is certain potential safety hazard.
The content of the invention
Technical problem solved by the invention is that providing a kind of aircraft engine installs equipment, to solve above-mentioned background skill
Shortcoming in art.
Technical problem solved by the invention is realized using following technical scheme：
A kind of aircraft engine installs equipment, including AGV power chassis, Mecanum wheel, staggered form lifting device, for supporting
Motor support frock, Electric Appliance Cabinet and the posture adjustment platform mechanism of aircraft engine, wherein, Mecanum wheel is arranged on AGV power
On chassis, many walking mechanisms are installed on AGV power chassis, posture adjustment platform mechanism is lifted with AGV power chassis by staggered form
Device connection is risen, motor support frock is connected with posture adjustment platform mechanism；Electric Appliance Cabinet is arranged on AGV power chassis, staggered form
The aircraft engine being placed in motor support frock is lifted in aircraft engine cabin by lifting device, and flat by posture adjustment
The fine setting of certain position and angle is done by platform mechanism, and then realizes the automatic transportation of aircraft engine and semi-automatic installment work, energy
The enough operator's quantity that effectively reduces saves human resources, shortens the set-up time and improves production efficiency；Each several part concrete structure is such as
Under：
In AGV power chassis, front axle mechanism is with vehicle frame by being welded to connect, and walking mechanism is arranged on front axle mechanism, back axle machine
Structure is connected with vehicle frame by pin bindiny mechanism, and walking mechanism is arranged on rear bridge mechanism, and Mecanum wheel is arranged on vehicle frame；
In walking mechanism, movable motor is connected with line shaft, and circular cone rod bearing is placed in bearing block, and is sleeved on line shaft
On；
In staggered form lifting device, power is provided using the symmetrical mechanism form of double lead, two drive lead screws pass through chain
Connection, makes lifting platform steadily lift, preceding rocker bar bearing is fixed on vehicle frame with lifting motor, rear hinge to ensure that action is synchronous
Bearing is movably arranged on vehicle frame, is in relative sliding mode with vehicle frame；Lifting motor is connected with drive lead screw, drive lead screw with
Rocker bar bearing is connected afterwards, and transposition arm is connected with preceding rocker bar bearing, rear rocker bar bearing respectively, and lifting platform is fixed on transposition arm top
Portion, by drive lead screw rotate drive after rocker bar bearing so that drive transposition arm cause lifting platform realize up and down motion；
In lifting platform, line slideway slide rail is fixed on vehicle frame with screw mandrel support seat；Rocker bar bearing is clamped with feed screw nut afterwards
Block and straight-line guide rail slide block are fixed as an assembly, and straight-line guide rail slide block is placed on line slideway slide rail, and drive lead screw runs through silk
Stem nut grip block is arranged in screw mandrel support seat, and feed screw nut is arranged on drive lead screw, and passes through feed screw nut's grip block
Clamp；
In motor support frock, front end screw mandrel height regulating rod is enclosed on front support screw mandrel and can be suitable around front support screw mandrel
Rotate counterclockwise is so as to adjust front support screw mandrel height；Similarly, screw mandrel height regulating rod in rear end is enclosed on the support screw of rear end
And rear end support frame height can be adjusted along rotate counterclockwise around rear end support screw, support frame lower section in rear end is provided with two
Rear end support screw；Frock connecting plate and frock frame welding, and front support screw mandrel is arranged on frock with rear end support screw
On framework；
In posture adjustment platform mechanism, the comprehensive axle platform that trackslips includes X-axis slide unit, Y-axis slide unit and A axle turntables, and X-axis line slideway is fixed
On lifting platform, X-axis slide unit is arranged on X-axis line slideway, and X-axis stepper motor is connected with X-axis screw mandrel, X-axis screw mandrel and X-axis
Slide unit is connected, and drives X-axis screw mandrel to rotate by X-axis stepper motor so that X-axis slide unit backhauls on X-axis line slideway
It is dynamic；Similarly, Y-axis line slideway is fixed on Y-axis slide unit, and Y-axis slide unit is arranged on Y-axis line slideway, y-axis stepper motor and Y
Axial filament bar is connected, and Y-axis screw mandrel is connected with Y-axis slide unit, drives Y-axis screw mandrel to rotate so that Y-axis slide unit by y-axis stepper motor
Moved back and forth on Y-axis line slideway；A axle turntable bearings are fixed on A axle turntables, and A shaft step motors are connected with A axial filament bars, A
Axial filament bar is connected with A axle turntables, drives A axial filaments bar to rotate so that A axles turntable is in A axle turntable axles by A shaft step motors
Hold and rotate clockwise or counterclockwise, so as to realize to aircraft engine pose adjustment.
In the present invention, anticollision barrier is installed, pedal is connected by screw with anticollision barrier, plays periphery on vehicle frame
Protect the effect of vehicle.
In the present invention, front axle mechanism on rear bridge mechanism with being separately installed with two walking mechanisms.
In the present invention, movable motor is connected by decelerator with line shaft.
In the present invention, bearing pin is installed in the middle part of transposition arm.
In the present invention, lifting platform is concave structure, to save space, as far as possible reduction height.
In the present invention, posture adjustment platform mechanism includes two X-axis line slideways and two Y-axis line slideways.
In the present invention, X-axis handwheel is provided with lifting platform, and X-axis handwheel is connected with X-axis screw mandrel, X-axis screw mandrel and X
Axle slide unit is connected, and drives X-axis screw mandrel to rotate so that X-axis slide unit is moved back and forth on X-axis line slideway by X-axis handwheel.
In the present invention, Y-axis handwheel is provided with lifting platform, and Y-axis handwheel is connected with Y-axis screw mandrel, Y-axis screw mandrel and Y
Axle slide unit is connected, and drives Y-axis screw mandrel to rotate so that Y-axis slide unit is moved back and forth on Y-axis line slideway by Y-axis handwheel.
In the present invention, A axle handwheels are provided with lifting platform, and A axles handwheel is connected with A axial filament bars, A axial filaments bar and A
Axle turntable is connected, drive A axial filaments bars to rotate by A axles handwheel so that A axles turntable on A axle turntable bearings clockwise or
Rotate counterclockwise.
Beneficial effect：The present invention guides transport engine to install car automatically by AGV, to improve existing installation equipment not
Foot, is particularly suitable for automating the technological requirement of pulsating aircraft assembling production, according to putting for aircraft aircraft engine to be installed
Position is different, and hand-held remote controller after automatic path planning to destination, manpower intervention carries out the semi-automatic installation of aircraft engine
Operation, not only saves artificial, shortens the aircraft engine installation exercise time, improve Aircraft Production efficiency, and security is protected
Barrier and raising.
Brief description of the drawings
Fig. 1 is the structural representation of presently preferred embodiments of the present invention.
Fig. 2 is the AGV power chassis structural representations in presently preferred embodiments of the present invention.
Fig. 3 is the walking mechanism structural representation in presently preferred embodiments of the present invention.
Fig. 4 is the staggered form lifting device structural representation in presently preferred embodiments of the present invention.
Fig. 5 is schematic diagram before the staggered form lifting device lifting in presently preferred embodiments of the present invention.
Fig. 6 is schematic diagram after the staggered form lifting device lifting in presently preferred embodiments of the present invention.
Fig. 7 is the line slide rail supporting construction schematic diagram in presently preferred embodiments of the present invention.
Fig. 8 is the posture adjustment platform mechanism side view in presently preferred embodiments of the present invention.
Fig. 9 is the posture adjustment platform mechanism top view in presently preferred embodiments of the present invention.
Figure 10 is the motor support tool structure schematic diagram in presently preferred embodiments of the present invention.
Embodiment
In order that the technical means, the inventive features, the objects and the advantages of the present invention are readily apparent from clearly, tie below
Conjunction is specifically illustrating, and the present invention is expanded on further.
Equipment, including AGV are installed referring to a kind of Fig. 1 aircraft engine（Automated Guided Vehicle are automatic
Guide car）Power chassis 1, walking mechanism 2, Mecanum wheel 3, anticollision barrier 4, pedal 5, staggered form lifting device 6, it is used for
Motor support frock 7, Electric Appliance Cabinet 8 and the posture adjustment platform mechanism 9 of aircraft engine are supported, wherein, walking mechanism 2 is received with Mike
Nurse wheel 3 is arranged on AGV power chassis 1 by bolt, constitutes AGV homing guidance transport sections；Anticollision barrier 4 and pedal 5
It is arranged on after being bolted on AGV power chassis 1, constitutes collision protection part；AGV power chassis 1 and posture adjustment platform machine
Structure 9 connects and composes semi-automatic lifting and posture adjustment part by staggered form lifting device 6；Motor support frock 7 and posture adjustment platform
Mechanism 9 is bolted；Electric Appliance Cabinet 8 is arranged on AGV power chassis 1 by bolt, constitutes the power-control section of vehicle,
Aircraft engine in motor support frock 7 is lifted in aircraft engine cabin by semi-automatic lifting and posture adjustment part
And the fine setting of certain position and angle is done by posture adjustment platform mechanism 9, so as to realize the automatic transportation and half of aircraft engine certainly
Dynamic installment work；Each several part concrete structure is as follows：
It is shown in Figure 2, AGV power chassis 1 include walking mechanism 2, Mecanum wheel 3, front axle mechanism 10, rear bridge mechanism 11,
Pin bindiny mechanism 12 and vehicle frame 13, front axle mechanism 10 is with vehicle frame 13 by being welded to connect, and two walking mechanisms 2 are pacified by bolt
On front axle mechanism 10, rear bridge mechanism 11 is connected with vehicle frame 13 by pin bindiny mechanism 12, and two walking mechanisms 2 pass through spiral shell
Bolt is arranged on rear bridge mechanism 11, and anticollision barrier 4 is arranged on vehicle frame 13 by bolt, and pedal 5 is protected by screw and anticollision
Column 4 is connected, and plays a part of periphery protection vehicle；Four Mecanum wheels 3 are arranged on vehicle frame 13, in actual applications, wheat
The requirement that Ke Namu takes turns 3 pairs of ground flat degrees is more strict, is realized from Mecanum wheel control principle and learns that four wheels are all
Power output wheel, belongs to four-wheel four-drive control, therefore it is required that four Mecanum wheels 3 simultaneously with ground good contact, to ensure
Four Mecanum wheels 3 are contacted simultaneously with ground, so as to provide enough frictional force to drive vehicle to move, due to actual ground not
It is smooth cause AGV power chassis 1 from by all wheel Complete Binds in one plane, it is desirable to have certain suspension floating energy
Power, it is contemplated that the use particularity of the car and the rigidity property requirement to vehicle, can not use the spring similar to automobile herein
Floating suspension mechanism, is considered as three-point support structure form, i.e., to simplify structure design and improving reliability：The propons machine of car
Structure 10 is fixed as one with vehicle frame 13, the rear ralocatable mode of bridge mechanism 11, and the chassis structure form of AGV power chassis 1 is similar to fork truck；
Due to the particularity of the operation principle of Mecanum wheel 3, make connected line shaft not only by radial load, moment of flexure,
Torsion, also axial force, common deep groove ball bearing are difficult to meet use requirement, therefore walking mechanism 2 is using to dress circular cone rod
Bearing 24 supports line shaft 25, and driving movable motor 21 is connected through decelerator 22 with the line shaft 25, and circular cone rod bearing 24 is pacified
In bearing block 23, wheelboss flange disk 26 is used to fasten circular cone rod bearing 24, and concrete structure is shown in Figure 3；
Referring to shown in Fig. 4~7, staggered form lifting device 6 is that aircraft engine is given rise into correct position, is needed with reference to actual use
Ask, space requirement is compact and lift height is higher, therefore be more adapted to using " staggered form " elevating mechanism, by staggered form lift
Structure principle understands, no matter two be hinged wait how the angle between long poles changes, the line at rod member two ends all the time with level
Face keeping parallelism, and it is vertical with the line of adjacent rod end, it is made according to this principle, the agency cost is low, make
With convenient, simple in construction, easy to manufacture, can using less mould and frock to be manufactured and be assembled the advantages of, in height
Had a very wide range of applications in the daily lifes such as idle job, transport work；Including lifting platform 61, preceding rocker bar bearing 62, after
Rocker bar bearing 63, lifting motor 64, chain 65, drive lead screw 66, transposition arm 67 and bearing pin 68, using the symmetrical machine of double lead
Configuration formula provides power, and two drive lead screws 66 are connected by chain 65 makes the steadily liter of lifting platform 61 to ensure that action is synchronous
Drop, preceding rocker bar bearing 62 is fixed on vehicle frame 13 with lifting motor 64, and rear rocker bar bearing 63 is movably arranged on vehicle frame 13, with
Vehicle frame 13 is in relative sliding mode；Lifting motor 64 is connected with drive lead screw 66, and drive lead screw 66 is connected with rear rocker bar bearing 63,
Transposition arm 67 is connected with preceding rocker bar bearing 62, rear rocker bar bearing 63 respectively, and bearing pin 68 is arranged on the middle part of transposition arm 67, lifting platform
61 are fixed on the top of transposition arm 67, and rocker bar bearing 63 and then drive transposition arm 67 are so that lift after being driven by the rotation of drive lead screw 66
Realize for peaceful 61 and move up and down；
Because rocker bar bearing 62 is fixed on vehicle frame 13 before staggered form lifting device 6, rear rocker bar bearing 63 is relative on vehicle frame 13
Slide, simply by rolling bearing it can not be supported to slide for reasons in structure, and support force can not be carried by drive lead screw 66
For, therefore lifting platform 61 is supported using line slide rail 615, the axis of line slide rail 615 and the axis perfect parallelism of drive lead screw 66；By
More in the bottom appendix of aircraft engine, when aircraft engine is to be installed, bottom is relatively low from the ground, to meet this requirement,
Lifting platform 61 needs to save space, as far as possible reduction height, is that lifting platform 61 is designed to concave structure by this, lifting is flat
Platform 61 includes line slide rail supporting construction 610, and line slide rail supporting construction 610 includes feed screw nut's grip block 611, feed screw nut
612nd, screw mandrel support seat 613, straight-line guide rail slide block 614 and line slideway slide rail 615, line slideway slide rail 615 are supported with screw mandrel
Seat 613 is bolted on vehicle frame 13；Rocker bar bearing 63 and feed screw nut's grip block 611 and straight-line guide rail slide block 614 afterwards
It is bolted as an assembly, straight-line guide rail slide block 614 is arranged on line slideway slide rail 615 and used cooperatively；Driving wire
Bar 66 is arranged in screw mandrel support seat 613 through feed screw nut's grip block 611, and feed screw nut 612 is arranged on drive lead screw 66,
And clamped by feed screw nut's grip block 611；
Referring to shown in Fig. 8~9, posture adjustment platform mechanism 9 includes A axles handwheel 91, X-axis handwheel 92, Y-axis handwheel 93, X-axis screw mandrel 94, Y
Axial filament bar 95, y-axis stepper motor 96, X-axis stepper motor 97, A shaft step motors 98, A axle turntables bearing 99, X-axis line slideway
910th, A axial filaments bar 911, Y-axis line slideway 912 and comprehensive axle trackslip platform 913；The comprehensive axle platform 913 that trackslips includes X-axis slide unit, Y-axis
Slide unit and A axle turntables, two X-axis line slideways 910 are fixed by screws on lifting platform 61, and it is straight that X-axis slide unit is arranged on X-axis
On line guide rail 910, by driving X-axis screw mandrel 94 to rotate so that X-axis slide unit is in X in X-axis handwheel 92 or X-axis stepper motor 97
Moved back and forth on axle line slideway 910；Similarly, two Y-axis line slideways 912 are fixed by screws on Y-axis slide unit, and Y-axis is slided
Platform is arranged on Y-axis line slideway 912, by Y-axis handwheel 93 or y-axis stepper motor 96 drive Y-axis screw mandrel 95 to rotate so as to
So that Y-axis slide unit is moved back and forth on Y-axis line slideway 912；A axle turntables bearing 99 is fixed by screws on A axle turntables, is led to
Cross A axles handwheel 91 or A shaft step motors 98 drive A axial filaments bar 911 to rotate so that A axles turntable is on A axle turntables bearing 99
Rotate clockwise or counterclockwise；
Shown in Figure 10, motor support frock 7 is the excessive attachment structure part of aircraft engine and AGV power chassis 1,
The front and rear strong point of motor support frock 7 must match with aircraft engine mount point, be that rear support point use before this can
The screw mandrel of regulation as main support shaft, including front support screw mandrel 71, front end screw mandrel height regulating rod 72, frock connecting plate 73,
Frock framework 74, rear end screw mandrel height regulating rod 75, rear end support screw 76 and rear end support frame 77, front end screw mandrel are highly adjusted
Bar 72 is enclosed on front support screw mandrel 71 and can adjust the height of front support screw mandrel 71 along rotate counterclockwise around it；Together
Reason, rear end screw mandrel height regulating rod 75 be enclosed on rear end support screw 76 and can around its along rotate counterclockwise so as to adjusting rear end branch
The height of support 77, the lower section of rear end support frame 77 is provided with two rear end support screws 76；Frock connecting plate 73 and frock framework
74 weld together, and front support screw mandrel 71 is arranged on frock framework 74 with rear end support screw 76.
The general principle and principal character and advantages of the present invention of the present invention has been shown and described above.The technology of the industry
Personnel are it should be appreciated that the present invention is not limited to the above embodiments, and the simply explanation described in above-described embodiment and specification is originally
The principle of invention, without departing from the spirit and scope of the present invention, various changes and modifications of the present invention are possible, these changes
Change and improvement all fall within the protetion scope of the claimed invention.The claimed scope of the invention by appended claims and its
Equivalent thereof.
Claims (10)
1. a kind of aircraft engine installs equipment, it is characterised in that including AGV power chassis, Mecanum wheel, staggered form lifting
Device, the motor support frock for supporting aircraft engine, Electric Appliance Cabinet and posture adjustment platform mechanism, wherein, Mecanum wheel
On AGV power chassis, many walking mechanisms, posture adjustment platform mechanism and AGV power chassis are installed on AGV power chassis
Connected by staggered form lifting device, motor support frock is connected with posture adjustment platform mechanism；Electric Appliance Cabinet is arranged on AGV power bottom
On disk, the aircraft engine being placed in motor support frock is lifted in aircraft engine cabin by staggered form lifting device,
And do the fine setting of certain position and angle by posture adjustment platform mechanism, and then realize the automatic transportation of aircraft engine and semi-automatic
Installment work；Each several part concrete structure is as follows：
In AGV power chassis, front axle mechanism is with vehicle frame by being welded to connect, and walking mechanism is arranged on front axle mechanism, back axle machine
Structure is connected with vehicle frame by pin bindiny mechanism, and walking mechanism is arranged on rear bridge mechanism, and Mecanum wheel is arranged on vehicle frame；
In walking mechanism, movable motor is connected with line shaft, and circular cone rod bearing is placed in bearing block, and is sleeved on line shaft
On；
In staggered form lifting device, power is provided using the symmetrical mechanism form of double lead, two drive lead screws pass through chain
Connection, makes lifting platform steadily lift, preceding rocker bar bearing is fixed on vehicle frame with lifting motor, rear hinge to ensure that action is synchronous
Bearing is movably arranged on vehicle frame, is in relative sliding mode with vehicle frame；Lifting motor is connected with drive lead screw, drive lead screw with
Rocker bar bearing is connected afterwards, and transposition arm is connected with preceding rocker bar bearing, rear rocker bar bearing respectively, and lifting platform is fixed on transposition arm top
Portion, by drive lead screw rotate drive after rocker bar bearing so that drive transposition arm cause lifting platform realize up and down motion；
In lifting platform, line slideway slide rail is fixed on vehicle frame with screw mandrel support seat；Rocker bar bearing is clamped with feed screw nut afterwards
Block and straight-line guide rail slide block are fixed as an assembly, and straight-line guide rail slide block is placed on line slideway slide rail, and drive lead screw runs through silk
Stem nut grip block is arranged in screw mandrel support seat, and feed screw nut is arranged on drive lead screw, and passes through feed screw nut's grip block
Clamp；
In motor support frock, front end screw mandrel height regulating rod is enclosed on front support screw mandrel and can be suitable around front support screw mandrel
Rotate counterclockwise is so as to adjust front support screw mandrel height；Similarly, screw mandrel height regulating rod in rear end is enclosed on the support screw of rear end
And rear end support frame height can be adjusted along rotate counterclockwise around rear end support screw, support frame lower section in rear end is provided with two
Rear end support screw；Frock connecting plate and frock frame welding, and front support screw mandrel is arranged on frock with rear end support screw
On framework；
In posture adjustment platform mechanism, the comprehensive axle platform that trackslips includes X-axis slide unit, Y-axis slide unit and A axle turntables, and X-axis line slideway is fixed
On lifting platform, X-axis slide unit is arranged on X-axis line slideway, and X-axis stepper motor is connected with X-axis screw mandrel, X-axis screw mandrel and X-axis
Slide unit is connected, and drives X-axis screw mandrel to rotate by X-axis stepper motor so that X-axis slide unit backhauls on X-axis line slideway
It is dynamic；Similarly, Y-axis line slideway is fixed on Y-axis slide unit, and Y-axis slide unit is arranged on Y-axis line slideway, y-axis stepper motor and Y
Axial filament bar is connected, and Y-axis screw mandrel is connected with Y-axis slide unit, drives Y-axis screw mandrel to rotate so that Y-axis slide unit by y-axis stepper motor
Moved back and forth on Y-axis line slideway；A axle turntable bearings are fixed on A axle turntables, and A shaft step motors are connected with A axial filament bars, A
Axial filament bar is connected with A axle turntables, drives A axial filaments bar to rotate so that A axles turntable is in A axle turntable axles by A shaft step motors
Hold and rotate clockwise or counterclockwise, so as to realize to aircraft engine pose adjustment.
2. a kind of aircraft engine according to claim 1 installs equipment, it is characterised in that anticollision shield is provided with vehicle frame
Column, pedal is connected by screw with anticollision barrier.
3. a kind of aircraft engine according to claim 1 installs equipment, it is characterised in that front axle mechanism and rear bridge mechanism
On be separately installed with two walking mechanisms.
4. a kind of aircraft engine according to claim 1 installs equipment, it is characterised in that movable motor passes through decelerator
It is connected with line shaft.
5. a kind of aircraft engine according to claim 1 installs equipment, it is characterised in that be provided with pin in the middle part of transposition arm
Axle.
6. a kind of aircraft engine according to claim 1 installs equipment, it is characterised in that lifting platform is spill knot
Structure.
7. a kind of aircraft engine according to claim 1 installs equipment, it is characterised in that posture adjustment platform mechanism includes two
Root X-axis line slideway and two Y-axis line slideways.
8. a kind of aircraft engine according to claim 1 installs equipment, it is characterised in that X is provided with lifting platform
Axle handwheel, and X-axis handwheel is connected with X-axis screw mandrel, X-axis screw mandrel is connected with X-axis slide unit, is passed through X-axis handwheel and is driven X-axis screw mandrel to rotate
So that X-axis slide unit is moved back and forth on X-axis line slideway.
9. a kind of aircraft engine according to claim 1 installs equipment, it is characterised in that Y is provided with lifting platform
Axle handwheel, and Y-axis handwheel is connected with Y-axis screw mandrel, Y-axis screw mandrel is connected with Y-axis slide unit, is passed through Y-axis handwheel and is driven Y-axis screw mandrel to rotate
So that Y-axis slide unit is moved back and forth on Y-axis line slideway.
10. a kind of aircraft engine according to claim 1 installs equipment, it is characterised in that A is provided with lifting platform
Axle handwheel, and A axles handwheel is connected with A axial filament bars, A axial filaments bar is connected with A axle turntables, is passed through A axles handwheel and is driven A axial filaments bar to rotate
So that A axles turntable is rotated clockwise or counterclockwise on A axle turntable bearings.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710462962.2A CN107160130B (en) | 2017-06-19 | 2017-06-19 | A kind of aircraft engine installation equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710462962.2A CN107160130B (en) | 2017-06-19 | 2017-06-19 | A kind of aircraft engine installation equipment |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107160130A true CN107160130A (en) | 2017-09-15 |
| CN107160130B CN107160130B (en) | 2018-11-27 |
Family
ID=59819856
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710462962.2A Active CN107160130B (en) | 2017-06-19 | 2017-06-19 | A kind of aircraft engine installation equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107160130B (en) |
Cited By (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108284959A (en) * | 2017-12-08 | 2018-07-17 | 西安飞机工业（集团）有限责任公司 | A kind of six degree of freedom mounting platform |
| CN108382439A (en) * | 2018-01-16 | 2018-08-10 | 昆明云内动力股份有限公司 | A kind of engine cylinder body transport trolley and transportation system |
| CN108857602A (en) * | 2018-08-03 | 2018-11-23 | 辽宁科技大学 | A kind of spatial complex bend pipe inner surface magnetic grinder and method |
| CN109019434A (en) * | 2018-08-23 | 2018-12-18 | 江苏哈工联合精密传动有限公司 | A kind of small-sized heavily loaded omnidirectional AGV trolley lifted |
| CN109759998A (en) * | 2019-01-08 | 2019-05-17 | 扬州万方电子技术有限责任公司 | A kind of installation vehicle for turbofan aircraft engine |
| CN110406696A (en) * | 2019-08-07 | 2019-11-05 | 沈阳飞机工业（集团）有限公司 | Aircraft landing system intercepts the multi-functional resetting equipment of part |
| CN110589012A (en) * | 2019-09-20 | 2019-12-20 | 西安飞机工业（集团）有限责任公司 | Aircraft engine plug-in mounting device and mounting method |
| CN110961908A (en) * | 2019-12-04 | 2020-04-07 | 江西洪都航空工业集团有限责任公司 | Automatic butt joint posture-adjusting installation system for aircraft engine |
| CN110979722A (en) * | 2019-12-04 | 2020-04-10 | 江西洪都航空工业集团有限责任公司 | A trailer that is used for automatic walking of aircraft engine to dock |
| CN111022392A (en) * | 2019-12-04 | 2020-04-17 | 江西洪都航空工业集团有限责任公司 | Hydraulic lifting posture-adjusting system |
| CN111203830A (en) * | 2020-03-10 | 2020-05-29 | 中烜航空科技(上海)有限公司 | Equipment with universal adjusting function for assembling airplane parts |
| CN111571210A (en) * | 2020-06-15 | 2020-08-25 | 国电联合动力技术(保定)有限公司 | Wind-powered electricity generation complete machine intelligence assembly flowing water platform equipment |
| CN111824451A (en) * | 2020-06-23 | 2020-10-27 | 成都飞机工业（集团）有限责任公司 | Aircraft part transports guarantor type device |
| CN112374063A (en) * | 2020-11-24 | 2021-02-19 | 江苏赛愽智能制造研究院有限公司 | Transfer robot for aerospace manufacturing and working method thereof |
| CN114212272A (en) * | 2021-12-17 | 2022-03-22 | 江西洪都航空工业集团有限责任公司 | Quick loading and unloading mechanism |
| CN114589486A (en) * | 2022-04-02 | 2022-06-07 | 江苏长虹智能装备股份有限公司 | Automobile front axle balance adjusting equipment on automobile flow production line |
| CN114940459A (en) * | 2022-06-16 | 2022-08-26 | 国营芜湖机械厂 | Multifunctional aircraft hanger mounting vehicle |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201136762Y (en) * | 2007-11-09 | 2008-10-22 | 成都飞机工业（集团）有限责任公司 | Longeron installation vehicle |
| US20090266275A1 (en) * | 2008-04-24 | 2009-10-29 | Eaton Corporation | Shipping system for objects such as an aircraft engine |
| CN202016825U (en) * | 2011-04-06 | 2011-10-26 | 成都立航科技有限公司 | Omni-directional aeroengine mounting vehicle |
| CN103639973A (en) * | 2013-11-28 | 2014-03-19 | 江西洪都航空工业集团有限责任公司 | Aircraft engine installing device |
| CN105923568A (en) * | 2016-06-15 | 2016-09-07 | 沈阳飞机工业（集团）有限公司 | Mechanical engine mounting car |
| CN205952324U (en) * | 2016-07-30 | 2017-02-15 | 深圳市劲拓自动化设备股份有限公司 | Accurate appearance mounting platform of transferring of omnidirectional movement type engine |
-
2017
- 2017-06-19 CN CN201710462962.2A patent/CN107160130B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201136762Y (en) * | 2007-11-09 | 2008-10-22 | 成都飞机工业（集团）有限责任公司 | Longeron installation vehicle |
| US20090266275A1 (en) * | 2008-04-24 | 2009-10-29 | Eaton Corporation | Shipping system for objects such as an aircraft engine |
| CN202016825U (en) * | 2011-04-06 | 2011-10-26 | 成都立航科技有限公司 | Omni-directional aeroengine mounting vehicle |
| CN103639973A (en) * | 2013-11-28 | 2014-03-19 | 江西洪都航空工业集团有限责任公司 | Aircraft engine installing device |
| CN105923568A (en) * | 2016-06-15 | 2016-09-07 | 沈阳飞机工业（集团）有限公司 | Mechanical engine mounting car |
| CN205952324U (en) * | 2016-07-30 | 2017-02-15 | 深圳市劲拓自动化设备股份有限公司 | Accurate appearance mounting platform of transferring of omnidirectional movement type engine |
Cited By (23)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108284959A (en) * | 2017-12-08 | 2018-07-17 | 西安飞机工业（集团）有限责任公司 | A kind of six degree of freedom mounting platform |
| CN108382439A (en) * | 2018-01-16 | 2018-08-10 | 昆明云内动力股份有限公司 | A kind of engine cylinder body transport trolley and transportation system |
| CN108857602A (en) * | 2018-08-03 | 2018-11-23 | 辽宁科技大学 | A kind of spatial complex bend pipe inner surface magnetic grinder and method |
| CN109019434A (en) * | 2018-08-23 | 2018-12-18 | 江苏哈工联合精密传动有限公司 | A kind of small-sized heavily loaded omnidirectional AGV trolley lifted |
| CN109019434B (en) * | 2018-08-23 | 2024-04-02 | 江苏哈工联合精密传动有限公司 | Small-size heavy load qxcomm technology AGV dolly that can lift |
| CN109759998B (en) * | 2019-01-08 | 2022-02-25 | 扬州万方科技股份有限公司 | Installation vehicle for turbofan aircraft engine |
| CN109759998A (en) * | 2019-01-08 | 2019-05-17 | 扬州万方电子技术有限责任公司 | A kind of installation vehicle for turbofan aircraft engine |
| CN110406696A (en) * | 2019-08-07 | 2019-11-05 | 沈阳飞机工业（集团）有限公司 | Aircraft landing system intercepts the multi-functional resetting equipment of part |
| CN110589012A (en) * | 2019-09-20 | 2019-12-20 | 西安飞机工业（集团）有限责任公司 | Aircraft engine plug-in mounting device and mounting method |
| CN110979722A (en) * | 2019-12-04 | 2020-04-10 | 江西洪都航空工业集团有限责任公司 | A trailer that is used for automatic walking of aircraft engine to dock |
| CN111022392A (en) * | 2019-12-04 | 2020-04-17 | 江西洪都航空工业集团有限责任公司 | Hydraulic lifting posture-adjusting system |
| CN110961908A (en) * | 2019-12-04 | 2020-04-07 | 江西洪都航空工业集团有限责任公司 | Automatic butt joint posture-adjusting installation system for aircraft engine |
| CN111203830A (en) * | 2020-03-10 | 2020-05-29 | 中烜航空科技(上海)有限公司 | Equipment with universal adjusting function for assembling airplane parts |
| CN111571210A (en) * | 2020-06-15 | 2020-08-25 | 国电联合动力技术(保定)有限公司 | Wind-powered electricity generation complete machine intelligence assembly flowing water platform equipment |
| CN111824451B (en) * | 2020-06-23 | 2021-09-07 | 成都飞机工业（集团）有限责任公司 | Aircraft part transports guarantor type device |
| CN111824451A (en) * | 2020-06-23 | 2020-10-27 | 成都飞机工业（集团）有限责任公司 | Aircraft part transports guarantor type device |
| CN112374063A (en) * | 2020-11-24 | 2021-02-19 | 江苏赛愽智能制造研究院有限公司 | Transfer robot for aerospace manufacturing and working method thereof |
| CN114212272A (en) * | 2021-12-17 | 2022-03-22 | 江西洪都航空工业集团有限责任公司 | Quick loading and unloading mechanism |
| CN114212272B (en) * | 2021-12-17 | 2024-04-02 | 江西洪都航空工业集团有限责任公司 | Quick loading and unloading mechanism |
| CN114589486A (en) * | 2022-04-02 | 2022-06-07 | 江苏长虹智能装备股份有限公司 | Automobile front axle balance adjusting equipment on automobile flow production line |
| CN114589486B (en) * | 2022-04-02 | 2023-01-20 | 江苏长虹智能装备股份有限公司 | Automobile front axle balance adjusting equipment on automobile flow production line |
| CN114940459A (en) * | 2022-06-16 | 2022-08-26 | 国营芜湖机械厂 | Multifunctional aircraft hanger mounting vehicle |
| CN114940459B (en) * | 2022-06-16 | 2023-09-19 | 国营芜湖机械厂 | Multifunctional aircraft hanger mounting vehicle |
Also Published As
| Publication number | Publication date |
|---|---|
| CN107160130B (en) | 2018-11-27 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN107160130A (en) | A kind of aircraft engine installs equipment | |
| CN107188080A (en) | A kind of lifting trolley | |
| CN206767536U (en) | A kind of novel elevating chassis | |
| CN109202356A (en) | H profile steel overturns centering body | |
| CN108750562A (en) | A kind of goods transportation industry manufacture AGV robots | |
| CN103344420A (en) | Multi-shaft bolt tightening test bed | |
| CN107792771A (en) | A kind of arrangements for automotive doors assembles power-assisted assembly | |
| CN104986199A (en) | Device for dismounting and mounting tire | |
| CN208150334U (en) | A kind of double lifting AGV trolleies | |
| CN208467676U (en) | A kind of removable car front-rear axle assembly tooling | |
| CN103894813A (en) | Mobile robot hole forming platform based on composite axle structure | |
| CN202106145U (en) | Rotating mechanism for welding | |
| CN111170199B (en) | Air bag lifter for assembly of passenger car | |
| CN216269184U (en) | High-altitude operation car with locomotive stabilizing mean | |
| CN110815158A (en) | Mobile device for detecting automobile chassis system | |
| CN109454348A (en) | A kind of fixed device of improved welding head | |
| CN206010127U (en) | A kind of automatic material blanking mechanism and the double projection welder with which | |
| CN205527529U (en) | Climbing mechanism of AGV car | |
| CN107825092A (en) | One kind upset assembling device | |
| CN112850038A (en) | Anti-shaking device for frame for aerial assembly line | |
| CN220807308U (en) | Aeroengine mounting vehicle | |
| CN106563903B (en) | A kind of automobile chassis robot welding system | |
| KR102460315B1 (en) | Movable nut runner derived from articulated robot system | |
| CN113233116B (en) | Turning lifting rail car | |
| CN220761459U (en) | Box closing table |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |