CN200981464Y - Horizontal single-arm automatic dismounting machine for aircraft tyre - Google Patents
Horizontal single-arm automatic dismounting machine for aircraft tyre Download PDFInfo
- Publication number
- CN200981464Y CN200981464Y CN 200620168142 CN200620168142U CN200981464Y CN 200981464 Y CN200981464 Y CN 200981464Y CN 200620168142 CN200620168142 CN 200620168142 CN 200620168142 U CN200620168142 U CN 200620168142U CN 200981464 Y CN200981464 Y CN 200981464Y
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- lifting arm
- main
- main shaft
- oil tank
- instrument head
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- 229910000831 Steel Inorganic materials 0.000 claims abstract description 3
- 239000010959 steel Substances 0.000 claims abstract description 3
- 238000003466 welding Methods 0.000 claims description 2
- 238000003825 pressing Methods 0.000 abstract description 2
- 230000005611 electricity Effects 0.000 abstract 2
- 230000003247 decreasing effect Effects 0.000 abstract 1
- 230000000694 effects Effects 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 208000027418 Wounds and injury Diseases 0.000 description 1
- 239000003638 chemical reducing agent Substances 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- 230000006378 damage Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 208000014674 injury Diseases 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 210000002826 placenta Anatomy 0.000 description 1
- 230000000750 progressive effect Effects 0.000 description 1
- 238000012857 repacking Methods 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 238000003756 stirring Methods 0.000 description 1
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Abstract
A horizontal single arm automatic airplane tyre disassembling machine comprises a power device and a main machine. The power device comprises an electricity control cabinet, a hydraulic pressure system and a pneumatic device. The main machine, a bearing seat and a guide rail are welded on the base seat. The bearing seat is provided with the hydraulic pressure system and an electricity control cabinet. A main carriage is arranged on the guide rail by hinge connection with a carriage oil tank. The pneumatic device and an instrument head walking bracket are arranged by hinge connection with an instrument head walking oil tank. The instrument head bracket is fixed on the instrument head walking bracket and provided above with a detachable instrument head. A lifting arm is articulated with the bearing seat. One end of the lifting oil tank is articulated with the other end of the lifting arm on the bearing seat. The lifting arm is provided with a main shaft motor, a speed decreasing machine belt connected with the main shaft motor, a main shaft oil tank fixed on the lifting arm through bonds and bolts. The steel cylinder of the main shaft oil tank is provided with a dialing disk, a central cone, a bearing sleeve and a pad. The horizontal single arm automatic airplane tyre disassembling machine has the advantages of compact structure, small volume, low weight, small occupying area, simple operation and low cost with the pressing and disassembling tyre as an integral horizontal structure.
Description
Technical field
The utility model belongs to the design and the manufacturing technology field of aircraft tyre removing machine, particularly Horizontal Arm Automatic Aircraft Tire Disassembly Machine.It is applicable to dismounting civilian, the military aircraft tire.
Background technology
Present domestic aircraft tyre dismounting is all adopted manually and the hydraulic pressure point is brought realization.Dismounting aircraft tyre labour intensity is big in this way, inefficiency.Particularly radial-ply tyre and wheel hub are had than major injury, influence its service life.This tyre detacher utilizes with the contacting surface relative rolling progressive pressure tire of tyre-pressing disc with tire by electronic and mechanical drive hydraulic pressure, make tire and wheel hub dial from, do not injure the radial of tire and the sealing surface of wheel hub.Its weak point is, it is the gate-type structure, promptly press tire and tear open tire by two components from framework form.Therefore, its volume is big, complex structure, and floor area is big, and complex operation costs an arm and a leg.
Summary of the invention
The purpose of this utility model provides a kind of Horizontal Arm Automatic Aircraft Tire Disassembly Machine.
The technical solution of the utility model is:
Utilizing existing full-sized car tyre dismounting machine technology, through the clamping at main shaft position with press the repacking of tire tool heads, is propulsion source with electric power, hydraulic efficiency pressure system pneumatic system, the aircraft tyre removing machine that to form horizontal single armed blank press structure be one.
Principle of work of the present utility model is:
Aircraft tyre manually is placed on the planker, and planker is delivered to tire on the main shaft that has conical inner body by the hydraulic actuating cylinder traction, clamps tire by hydraulic actuating cylinder with conical inner body again; Lifting arm rises to suitable height by hydraulic actuating cylinder with tire; Motor via reducer passes to main shaft with power, and the dial on the main shaft is stirred revolution with tire; Press the tire tool heads under the atmospheric pressure effect, to realize the rotary head commutation and be fixed on the guide rail, under the hydraulic actuating cylinder effect, press the tire tool heads by tire by the guide rail guiding, with tire and wheel hub dial from, commutate to opposite side again and lean on tire; Dismantle bolt or snap ring make the aircraft tyre split, with detection and the maintenance of carrying out next step.In military aircraft tire when assembling, be contained in wheel hub on the main shaft and with conical inner body and clamp, again with rubber tire be pressed into dress opposite side wheel hub and snap ring installation end by placenta.More than operation is finished by mobile console or remote controller by a people, and its advantage is that to press tire to tear tire open be an integral body, compact conformation, and volume is little, and floor area is little, and is easy and simple to handle, time saving and energy saving, safe and reliable, and price is low.
Description of drawings
Below in conjunction with accompanying drawing the utility model is described further.
Fig. 1 is the utility model structural representation.
Fig. 2 is this left view.
Arrow is represented sense of motion among the figure.
1-planker oil cylinder, 2-supporting seat, 3-guide rail, 4-main shaft oil cylinder, 5-dial, 6-conical inner body, 7-support sleeve, 8-pressure pad, 9-tool heads walking oil cylinder, 10-operating console, 11-tool heads, the 12-instrument headstock, 13-master's planker, 14-hydraulic efficiency pressure system, 15-lifting arm, 16-hoist cylinder, 17-spindle motor, 18-reductor, 19-electrical control cubicles, 20-base, 21-pneumatics, 22-tool heads walker.
The specific embodiment:
The utility model is made up of actuating unit and main frame.
Actuating unit, by electrical control cubicles 19, hydraulic efficiency pressure system 14 and pneumatics 21 are formed.
Main frame is based on base 20, and supporting seat 2 and guide rail 3 tack weldings are connected on the base 20, and hydraulic efficiency pressure system 14 and electrical control cubicles 19 are installed on the supporting seat 2; Main planker 13 is installed on the guide rail 3, and the hinge connection through planker oil cylinder 1 realizes linear reciprocating motion; Pneumatics 21 and tool heads walker 22 are mounted on the main planker 13 by tool heads walking oil cylinder 9 hinges, the clamping of rising and falling of pneumatics 21 implementation tool heads, 11 rotations and tool heads walker 22, the linear reciprocating motion of the tool heads walking oil cylinder 9 implementation tool headstocks 22; The instrument headstock 12 is fixed on the tool heads walker 22, and disconnectable tool heads 11 is housed on it; Lifting arm 15 is connected with supporting seat 2 hinges, and an end of hoist cylinder 16 is hinged on the lifting arm 15, and the other end is hinged on the supporting seat 2, by the flexible rotary and lifting of realizing lifting arm 15; Spindle motor 17 is installed on lifting arm 15, and reductor 18 and main shaft oil cylinder 4 are fixed on the lifting arm 15 by key, bolted connection.18 jiaos of bands of spindle motor 17 and reductor are connected, and dial 5, conical inner body 6, support sleeve 7 and pressure pad 8 are housed on the steel cylinder of main shaft oil cylinder 4.Occupation mode is piston rod contraction bands dynamic pressure pad 8, support sleeve 7 and the conical inner body 6 clamping tires of main shaft oil cylinder 4, and to reductor 18, reductor 18 drives 4 rotations of main shaft oil cylinder again, stirs the tire rotation by dial 5 through the angle strap drive in spindle motor 17 rotations; Operating console 10 is wired mobile controlling equipment in steering range.
The utility model has been made model machine, Beijing Kelland company of material group of CA trial effect ideal in the warp.The result shows: meet diameter 27 '-61 ' fully, the dismounting of wide 7.75 '-23.5 ' aircraft tyre.
Claims (1)
1, Horizontal Arm Automatic Aircraft Tire Disassembly Machine is made up of actuating unit and main frame, and main frame is made up of base, planker, lifting arm, clamping mechanism and dismounting mechanism for tire and annex thereof, it is characterized in that horizontal type structure, constitute by actuating unit and main frame,
Actuating unit, by electrical control cubicles (19), hydraulic efficiency pressure system (14) and pneumatics (21) constitute,
Main frame, supporting seat (2) and guide rail (3) tack welding are connected on the base (20), supporting seat (2) is gone up hydraulic efficiency pressure system (14) and electrical control cubicles (19) is installed, main planker (13) is installed in guide rail (3) and upward connects through supporting plate oil cylinder (1) hinge, pneumatics (21) and tool heads walker (22) are installed on the main planker (13) by tool heads walking oil cylinder (9) hinge, the instrument headstock (12) is fixed on the tool heads walker (22), disconnectable tool heads (11) is housed on it, lifting arm (15) is connected with supporting seat (2) hinge, hoist cylinder (16) one ends are hinged on the lifting arm (15), on the hinged supporting seat of the other end (2), lifting arm (15) is gone up dress spindle motor (17), reductor (18) passes through key with main shaft oil cylinder (4), bolted connection is fixed on the lifting arm (15), spindle motor (17) is connected by the angle band with reductor (18), and dial (5) is installed on the steel cylinder of main shaft oil cylinder (4), conical inner body (6), support sleeve (7) and pressure pad (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200620168142 CN200981464Y (en) | 2006-12-11 | 2006-12-11 | Horizontal single-arm automatic dismounting machine for aircraft tyre |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200620168142 CN200981464Y (en) | 2006-12-11 | 2006-12-11 | Horizontal single-arm automatic dismounting machine for aircraft tyre |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN200981464Y true CN200981464Y (en) | 2007-11-28 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 200620168142 Expired - Lifetime CN200981464Y (en) | 2006-12-11 | 2006-12-11 | Horizontal single-arm automatic dismounting machine for aircraft tyre |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN200981464Y (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101289052B (en) * | 2007-04-18 | 2011-06-15 | 施耐宝仪器股份有限公司 | Apparatus for positioning tyred wheels on a tyre changer machine |
| CN102774245A (en) * | 2012-07-21 | 2012-11-14 | 营口天辅铝业有限公司 | Pressurizing transmission locking mechanism for pneumatic tire mounting and demounting machine free of large plate |
| CN107776908A (en) * | 2017-10-23 | 2018-03-09 | 晨龙飞机（荆门）有限公司 | A kind of aircraft wheel hub changes device |
| CN110203026A (en) * | 2019-05-13 | 2019-09-06 | 合肥海川汽车部件系统有限公司 | Device is used in a kind of disassembly of automobile tire |
-
2006
- 2006-12-11 CN CN 200620168142 patent/CN200981464Y/en not_active Expired - Lifetime
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101289052B (en) * | 2007-04-18 | 2011-06-15 | 施耐宝仪器股份有限公司 | Apparatus for positioning tyred wheels on a tyre changer machine |
| CN102774245A (en) * | 2012-07-21 | 2012-11-14 | 营口天辅铝业有限公司 | Pressurizing transmission locking mechanism for pneumatic tire mounting and demounting machine free of large plate |
| CN102774245B (en) * | 2012-07-21 | 2015-03-18 | 营口天辅铝业有限公司 | Pressurizing transmission locking mechanism for pneumatic tire mounting and demounting machine free of large plate |
| CN107776908A (en) * | 2017-10-23 | 2018-03-09 | 晨龙飞机（荆门）有限公司 | A kind of aircraft wheel hub changes device |
| CN110203026A (en) * | 2019-05-13 | 2019-09-06 | 合肥海川汽车部件系统有限公司 | Device is used in a kind of disassembly of automobile tire |
| CN110203026B (en) * | 2019-05-13 | 2021-08-10 | 合肥海川汽车部件系统有限公司 | Device for dismounting automobile tire |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| EE01 | Entry into force of recordation of patent licensing contract |
Assignee: BRIGHT TECHNOLOGY CO., LTD. Assignor: Wei Engui Contract fulfillment period: 2009.3.24 to 2017.3.24 Contract record no.: 2009210000058 Denomination of utility model: Horizontal single-arm automatic dismounting machine for aircraft tyre Granted publication date: 20071128 License type: Exclusive license Record date: 20090326 |
|
| LIC | Patent licence contract for exploitation submitted for record |
Free format text: EXCLUSIVE LICENSE; TIME LIMIT OF IMPLEMENTING CONTACT: 2009.3.24 TO 2017.3.24; CHANGE OF CONTRACT Name of requester: YINGKOU BRIGHT TECHNOLOGY CO. TD Effective date: 20090326 |
|
| ASS | Succession or assignment of patent right |
Owner name: BRIGHT TECHNOLOGY CO., LTD. Free format text: FORMER OWNER: WEI ENGUI Effective date: 20140718 |
|
| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20140718 Address after: 115001, Ma Ying 8, Lunan Road, old border area, Liaoning, Yingkou Patentee after: BRIGHT TECHNOLOGY CO., LTD. Address before: Yingkou City, Liaoning province 115001 Zhanqian District jianfeng Street No. 23, Tunli Patentee before: Wei Engui |
|
| CX01 | Expiry of patent term |
Granted publication date: 20071128 |
|
| EXPY | Termination of patent right or utility model |