CN105216561A - A kind of aircraft tyre dismounting auxiliary device - Google Patents
A kind of aircraft tyre dismounting auxiliary device Download PDFInfo
- Publication number
- CN105216561A CN105216561A CN201510684940.1A CN201510684940A CN105216561A CN 105216561 A CN105216561 A CN 105216561A CN 201510684940 A CN201510684940 A CN 201510684940A CN 105216561 A CN105216561 A CN 105216561A
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- Prior art keywords
- board
- portable plate
- slide block
- flexibly
- aircraft tyre
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- 238000005096 rolling process Methods 0.000 claims abstract description 20
- 238000009434 installation Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 1
- 238000006011 modification reaction Methods 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
Abstract
The invention discloses a kind of aircraft tyre dismounting auxiliary device, comprise base, the surface of described base is provided with two parallel T slots, and the top of base is provided with portable plate, the bottom surface of described portable plate is provided with the T-shaped slide block matched with T slot, and T-shaped slide block is flexibly connected with T slot, the surface of described portable plate is also provided with two parallel chutes, the top of described portable plate is provided with device board, the bottom surface of described device board is provided with the slide block matched with chute, and slide block is flexibly connected with chute, and the surface of device board is provided with hydraulic actuating cylinder, the upper surface of described hydraulic actuating cylinder is connected with expansion link, the side of described expansion link is provided with pipe link, described pipe link is flexibly connected the center of rolling disc, described rolling disc is provided with position-limited lever away from the one side of pipe link.This aircraft tyre dismounting auxiliary device, can realize the stable accurately mobile, time saving and energy saving of tire, improve maintenance efficiency.
Description
Technical field
The present invention relates to aircraft repair technical field, be specially a kind of aircraft tyre dismounting auxiliary device.
Background technology
The dismounting of current existing aircraft tyre, mainly come by manpower, because aircraft tyre is heavier, can not be stable dismantle or aim at mounting hole, and can not dismounting aircraft tyre rapidly, and the personnel that change during use need the strength just dismantled and assembled aircraft tyre that costs a lot of money, so not only waste time and energy, and reduce maintenance efficiency, for this reason, we propose a kind of aircraft tyre dismounting auxiliary device.
Summary of the invention
The object of the present invention is to provide a kind of aircraft tyre dismounting auxiliary device, to solve the problem proposed in above-mentioned background technology.
For achieving the above object, the invention provides following technical scheme: a kind of aircraft tyre dismounting auxiliary device, comprise base, the surface of described base is provided with two parallel T slots, and the top of base is provided with portable plate, the bottom surface of described portable plate is provided with the T-shaped slide block matched with T slot, and T-shaped slide block is flexibly connected with T slot, the surface of described portable plate is provided with groove along axis, be provided with leading screw in a groove, and the two ends of leading screw are flexibly connected with the both ends of the surface of groove respectively, and the side of one end through-going recess of leading screw connects runner, the surface of described portable plate is also provided with two parallel chutes, the top of described portable plate is provided with device board, the bottom surface of described device board is provided with the slide block matched with chute, and slide block is flexibly connected with chute, the bottom surface of described device board is also provided with fixed block, described fixed block is provided with tapped bore, described leading screw coordinates with tapped bore to be installed, and the surface of device board is provided with hydraulic actuating cylinder, the upper surface of described hydraulic actuating cylinder is connected with expansion link, the side of described expansion link is provided with pipe link, described pipe link is flexibly connected the center of rolling disc, described rolling disc is provided with position-limited lever away from the one side of pipe link.
Preferably, the surface middle part of described device board is provided with mounting groove, and described hydraulic actuating cylinder is located in mounting groove.
Preferably, described pipe link is parallel with T slot.
Preferably, described pipe link is socketed with bearing away from one end of expansion link, and the center of rolling disc is provided with mounting hole, and described bearing is located in mounting hole.
Preferably, described position-limited lever is three, and position-limited lever is along the surperficial circumferential direction equidistant arrangement of rolling disc.
Compared with prior art, the invention has the beneficial effects as follows: this aircraft tyre dismounting auxiliary device, the T-shaped slide block matched with T slot is provided with by the lower surface being provided with portable plate, the surface of portable plate is provided with two parallel chutes, the lower surface of device board is provided with the slide block matched with chute, and in device board, be provided with hydraulic actuating cylinder, rolling disc is flexibly connected by pipe link in the side of expansion link, can fixed tire by position-limited lever on rolling disc, the stable accurately mobile of tire can be realized, ensure that the screw on tire aims at bolt, convenient installation, and also can be stable when dismantling take away tire, time saving and energy saving, improve maintenance efficiency.
Accompanying drawing explanation
Fig. 1 is structural representation of the present invention;
Fig. 2 is device board structural representation of the present invention;
Fig. 3 is rolling disc structural representation of the present invention.
In figure: 1 base, 2T shape groove, 3 portable plates, 4T shape slide block, 5 chutes, 6 grooves, 7 leading screws, 8 device board, 9 slide blocks, 10 fixed blocks, 11 tapped bore, 12 hydraulic actuating cylinders, 13 expansion links, 14 pipe links, 15 rolling discs, 16 mounting holes, 17 position-limited levers, 18 runners.
Detailed description of the invention
Below in conjunction with the accompanying drawing in the embodiment of the present invention, be clearly and completely described the technical scheme in the embodiment of the present invention, obviously, described embodiment is only the present invention's part embodiment, instead of whole embodiments.Based on the embodiment in the present invention, those of ordinary skill in the art, not making the every other embodiment obtained under creative work prerequisite, belong to the scope of protection of the invention.
Refer to Fig. 1-3, the invention provides a kind of technical scheme: a kind of aircraft tyre dismounting auxiliary device, comprises base 1, the surface of base 1 is provided with two parallel T slots 2, and the top of base 1 is provided with portable plate 3, the bottom surface of portable plate 3 is provided with the T-shaped slide block 4 matched with T slot 2, and T-shaped slide block 4 is flexibly connected with T slot 2, the surface of portable plate 3 is provided with groove 6 along axis, leading screw 7 is provided with in groove 6, and the two ends of leading screw 7 are flexibly connected with the both ends of the surface of groove 6 respectively, and the side of one end through-going recess 6 of leading screw 7 connects runner 18, can rotating wheel 18, leading screw 7 is rotated, thus drive makes device board about 8 movable, the surface of portable plate 3 is also provided with two parallel chutes 5, the top of portable plate 3 is provided with device board 8, the bottom surface of device board 8 is provided with the slide block 9 matched with chute 5, and slide block 9 is flexibly connected with chute 5, the bottom surface of device board 8 is also provided with fixed block 10, fixed block 10 is provided with tapped bore 11, leading screw 7 coordinates with tapped bore 11 to be installed, the surface middle part of device board 8 is provided with mounting groove, the upper surface that hydraulic actuating cylinder 12 is located at hydraulic actuating cylinder 12 in mounting groove is connected with expansion link 13, height can be changed, the side of expansion link 13 is provided with pipe link 14, pipe link 14 is parallel with T slot 2, pipe link 14 is socketed with bearing away from one end of expansion link 13, and the center of rolling disc 15 is provided with mounting hole 16, bearing is located in mounting hole 16, rolling disc 15 is provided with position-limited lever 17 away from the one side of pipe link 14, position-limited lever 17 is three, and position-limited lever 17 is along the surperficial circumferential direction equidistant arrangement of rolling disc 15, can position-limited lever 17 be inserted in the hole at the middle part of tire, this aircraft tyre dismounting auxiliary device, the T-shaped slide block 4 matched with T slot 2 is provided with by the lower surface being provided with portable plate 3, the surface of movable 3 plates is provided with two parallel chutes 5, the lower surface of device board 8 is provided with the slide block 9 matched with chute 5, and in device board 8, be provided with hydraulic actuating cylinder 12, rolling disc 15 is flexibly connected by pipe link 14 in the side of expansion link 13, can fixed tire by position-limited lever 17 on rolling disc 15, the stable accurately mobile of tire can be realized, the setting of rolling disc 15 ensure that the screw on tire aims at bolt, convenient installation, and also stably can take away tire when dismantling, time saving and energy saving, improve maintenance efficiency.
Although illustrate and describe embodiments of the invention, for the ordinary skill in the art, be appreciated that and can carry out multiple change, amendment, replacement and modification to these embodiments without departing from the principles and spirit of the present invention, scope of the present invention is by claims and equivalents thereof.
Claims (5)
1. an aircraft tyre dismounting auxiliary device, comprise base (1), it is characterized in that: the surface of described base (1) is provided with two parallel T slots (2), and the top of base (1) is provided with portable plate (3), the bottom surface of described portable plate (3) is provided with the T-shaped slide block (4) matched with T slot (2), and T-shaped slide block (4) is flexibly connected with T slot (2), the surface of described portable plate (3) is provided with groove (6) along axis, leading screw (7) is provided with in groove (6), and the two ends of leading screw (7) are flexibly connected with the both ends of the surface of groove (6) respectively, and the side of one end through-going recess (6) of leading screw (7) connects runner (18), the surface of described portable plate (3) is also provided with two parallel chutes (5), the top of described portable plate (3) is provided with device board (8), the bottom surface of described device board (8) is provided with the slide block (9) matched with chute (5), and slide block (9) is flexibly connected with chute (5), the bottom surface of described device board (8) is also provided with fixed block (10), described fixed block (10) is provided with tapped bore (11), described leading screw (7) coordinates with tapped bore (11) to be installed, and the surface of device board (8) is provided with hydraulic actuating cylinder (12), the upper surface of described hydraulic actuating cylinder (12) is connected with expansion link (13), the side of described expansion link (13) is provided with pipe link (14), described pipe link (14) is flexibly connected the center of rolling disc (15), described rolling disc (15) is provided with position-limited lever (17) away from the one side of pipe link (14).
2. a kind of aircraft tyre dismounting auxiliary device according to claim 1, it is characterized in that: the surface middle part of described device board (8) is provided with mounting groove, described hydraulic actuating cylinder (12) is located in mounting groove.
3. a kind of aircraft tyre dismounting auxiliary device according to claim 1, is characterized in that: described pipe link (14) is parallel with T slot (2).
4. a kind of aircraft tyre dismounting auxiliary device according to claim 1, it is characterized in that: described pipe link (14) is socketed with bearing away from one end of expansion link (13), and the center of rolling disc (15) is provided with mounting hole (16), described bearing is located in mounting hole (16).
5. a kind of aircraft tyre dismounting auxiliary device according to claim 1, is characterized in that: described position-limited lever (17) is three, and position-limited lever (17) is along the surperficial circumferential direction equidistant arrangement of rolling disc (15).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510684940.1A CN105216561A (en) | 2015-10-20 | 2015-10-20 | A kind of aircraft tyre dismounting auxiliary device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510684940.1A CN105216561A (en) | 2015-10-20 | 2015-10-20 | A kind of aircraft tyre dismounting auxiliary device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105216561A true CN105216561A (en) | 2016-01-06 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510684940.1A Pending CN105216561A (en) | 2015-10-20 | 2015-10-20 | A kind of aircraft tyre dismounting auxiliary device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105216561A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106080031A (en) * | 2016-06-30 | 2016-11-09 | 安徽江淮汽车股份有限公司 | A kind of tire assembling support means |
Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH08197902A (en) * | 1995-01-23 | 1996-08-06 | Central Japan Railway Co | Fastening device for wheel set bearing nut |
| CN2806201Y (en) * | 2005-04-03 | 2006-08-16 | 宁波庆源机械有限公司 | Tire mounting/dismounting machine |
| CN201002486Y (en) * | 2007-01-19 | 2008-01-09 | 努尔多拉 | Loader-unloader for automobile tyre |
| CN202106812U (en) * | 2011-02-15 | 2012-01-11 | 中国人民解放军济南军区72465部队 | Disassembly and assembly vehicle for band tyre |
| CN102320218A (en) * | 2011-06-30 | 2012-01-18 | 武汉科技大学 | Fork-type disassembling device used for large tyre |
| US20120224940A1 (en) * | 2010-11-05 | 2012-09-06 | Dana Andrews | Automobile Wheel Changing Tool |
| CN203957747U (en) * | 2014-05-16 | 2014-11-26 | 宁波市镇海富达汽车配件厂 | Tyre disassembling devices |
| CN204322925U (en) * | 2014-12-03 | 2015-05-13 | 伊恩·道格拉斯·梅赛森 | Tire lifting device |
| CN204488862U (en) * | 2015-03-31 | 2015-07-22 | 东风汽车公司 | A kind of band draws the tyre fixing transport trolley of horse device |
| CN205112881U (en) * | 2015-10-20 | 2016-03-30 | 重庆光煦科技有限公司 | Aircraft tire dismouting auxiliary device |
-
2015
- 2015-10-20 CN CN201510684940.1A patent/CN105216561A/en active Pending
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH08197902A (en) * | 1995-01-23 | 1996-08-06 | Central Japan Railway Co | Fastening device for wheel set bearing nut |
| CN2806201Y (en) * | 2005-04-03 | 2006-08-16 | 宁波庆源机械有限公司 | Tire mounting/dismounting machine |
| CN201002486Y (en) * | 2007-01-19 | 2008-01-09 | 努尔多拉 | Loader-unloader for automobile tyre |
| US20120224940A1 (en) * | 2010-11-05 | 2012-09-06 | Dana Andrews | Automobile Wheel Changing Tool |
| CN202106812U (en) * | 2011-02-15 | 2012-01-11 | 中国人民解放军济南军区72465部队 | Disassembly and assembly vehicle for band tyre |
| CN102320218A (en) * | 2011-06-30 | 2012-01-18 | 武汉科技大学 | Fork-type disassembling device used for large tyre |
| CN203957747U (en) * | 2014-05-16 | 2014-11-26 | 宁波市镇海富达汽车配件厂 | Tyre disassembling devices |
| CN204322925U (en) * | 2014-12-03 | 2015-05-13 | 伊恩·道格拉斯·梅赛森 | Tire lifting device |
| CN204488862U (en) * | 2015-03-31 | 2015-07-22 | 东风汽车公司 | A kind of band draws the tyre fixing transport trolley of horse device |
| CN205112881U (en) * | 2015-10-20 | 2016-03-30 | 重庆光煦科技有限公司 | Aircraft tire dismouting auxiliary device |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106080031A (en) * | 2016-06-30 | 2016-11-09 | 安徽江淮汽车股份有限公司 | A kind of tire assembling support means |
| CN106080031B (en) * | 2016-06-30 | 2018-06-01 | 安徽江淮汽车集团股份有限公司 | A kind of tire assembles support device |
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Application publication date: 20160106 |