CN206733978U - A kind of airplane wheel tyre remover - Google Patents
A kind of airplane wheel tyre remover Download PDFInfo
- Publication number
- CN206733978U CN206733978U CN201720498615.0U CN201720498615U CN206733978U CN 206733978 U CN206733978 U CN 206733978U CN 201720498615 U CN201720498615 U CN 201720498615U CN 206733978 U CN206733978 U CN 206733978U
- Authority
- CN
- China
- Prior art keywords
- wheel
- support body
- detacher
- aircraft
- frame
- 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.)
- Expired - Fee Related
Links
- 210000000078 claw Anatomy 0.000 claims description 40
- 238000003825 pressing Methods 0.000 claims description 38
- 238000009434 installation Methods 0.000 claims description 5
- 230000000903 blocking effect Effects 0.000 claims description 4
- 238000003466 welding Methods 0.000 claims description 3
- 238000012423 maintenance Methods 0.000 abstract description 5
- 238000013461 design Methods 0.000 abstract description 3
- 230000005540 biological transmission Effects 0.000 description 6
- 238000000034 method Methods 0.000 description 4
- 230000008569 process Effects 0.000 description 4
- 238000010586 diagram Methods 0.000 description 2
- 238000002360 preparation method Methods 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000008439 repair process Effects 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
- 238000013519 translation Methods 0.000 description 1
Landscapes
- Working Measures On Existing Buildindgs (AREA)
Abstract
The utility model proposes a kind of airplane wheel tyre remover, the support body (11) of universal wheel (1) is carried including a bottom, the top of the support body (11) is provided with four paws (12), the sidepiece of the support body (11) is hinged a rotating turret (13), the rotating turret (13) is hinged with a wheel carrier bracker (14), the bottom of the support body (11) of paw described in face (12) is provided with wheel and taken over a business (15), the wheel, which takes over a business (15) and by the hydraulic hand-pump (17) installed on the support body (11) manipulates the wheel and take over a business (15), to be moved up and down.Above-mentioned airplane wheel tyre remover of the present utility model is a kind of available for big airplane wheel and the universal airplane wheel tyre remover of flivver wheel, its is reasonable in design, in light weight, small volume, and versatility is good, it is readily transported, is the essential equipment of outfield aircraft maintenance.
Description
Technical Field
The utility model relates to a quick dismantlement and erection equipment that can be used to aircraft wheel tire, especially a general type aircraft wheel that can be used to big aircraft wheel and little aircraft wheel tears child ware open, in particular to aircraft wheel tears child ware open.
Background
The airplane wheel tire detacher is necessary equipment for the maintenance of an outfield airplane, and the main function of the airplane wheel tire detacher is to detach and replace severely worn rubber tires. When the old rubber tire is disassembled, the rubber tire and the wheel hub are adhered closely, the rubber tire and the wheel hub are peeled and fall off by certain external force, the wheel needs to be moved and turned in the disassembling and replacing process, and particularly for the wheel of a larger airplane, time and labor are wasted in the moving and turning process due to large volume and heavy weight.
The tire dismounting device used at present mainly carries out the carrying and the overturning of the airplane wheel in a mode of combining manpower and a hydraulic mechanism, and can only dismount and replace the airplane wheel with a certain diameter and thickness, so that the problems of complex structure, large size, heavy weight, poor universality and the like generally exist.
For example, CN 103101410 a discloses a tire remover for an aircraft wheel tire, which is suitable for the self-pressing type aircraft tire and the wheel hub, and the tire remover comprises a guide screw, a pressing cap and a snap ring, wherein the guide screw is installed between the inner holes; the part of the guide screw rod protruding out of the inner hole is provided with a clamping ring, and the clamping ring is guided by the guide screw rod and pressed to the end surface of the wheel rim; the compression cap is threaded from the upper end of the lead screw and is rotatable to apply an axial force to the snap ring along the lead screw. The tire remover disclosed by the prior art is difficult to move, the structural space is very unfavorable for loading, moving and overturning of tires, the requirement on the physical strength of personnel is high, and the labor intensity is high. CN 206030972U discloses a tire dismounting vehicle, which is suitable for rapid repair of a wheel type armored tire, and comprises a base, a lifting power frame arranged on the base, and a lifting frame arranged on the lifting power frame; the lifting power frame comprises a guide rail, a hydraulic cylinder, a transmission wheel and a transmission belt, the transmission belt is matched with the transmission wheel, one end of the transmission belt is connected to the lifting power frame, and the other end of the transmission belt is connected to the lifting frame; the lifting frame moves between the two guide rails along the guide rails, and the lower part of the lifting frame is provided with a tire supporting leg; the driving wheel is pushed through the hydraulic cylinder, the driving belt is driven to pull the lifting frame, and the lifting action of the lifting frame is realized. This prior art provides removal and raising and lowering functions, can alleviate maintenance personal's intensity of labour, but what this prior art provided is only the transportation and raising and lowering functions of wheel, will dismantle the wheel and still need other child equipment of tearing open to cooperate, and the required equipment is too many in the outfield maintenance, and the operation is complicated, and practicality and commonality are all not good.
SUMMERY OF THE UTILITY MODEL
The to-be-solved technical problem of the utility model is to provide an aircraft wheel detacher to reduce or avoid the aforementioned problem.
For solving the technical problem, the utility model provides an aircraft wheel child ware of tearing open for aircraft wheel tire's dismantlement and installation, wherein, aircraft wheel child ware of tearing open includes that a lower part has the support body of universal wheel, four pressure claws are installed on the upper portion of support body, a rotating turret of lateral part hinge of support body, the rotating turret articulates there is a wheel bracket, just right press the claw the wheel top dish is installed to the lower part of support body, the wheel top dish passes through manual hydraulic pump manipulation of installation on the support body the wheel top dish reciprocates.
Preferably, the upper part of the frame body is provided with a cross-shaped pressing claw sliding beam for installing the pressing claw, and the cross-shaped pressing claw sliding beam is formed by welding a circular tube, a vertical plate with a rectangular hole and a support ring.
Preferably, the pressing claw can slide along the round pipe and can rotate to be horizontal at the rectangular hole and be fixed.
Preferably, the turret has a vertical pivot axis for moving the wheel carriage horizontally into and out of the frame.
Preferably, the rotating frame has a horizontal rotating shaft which can rotate the wheel bracket to a vertical direction after the wheel bracket is horizontally moved out of the frame body.
Preferably, two wheel blocking rods are arranged on the wheel bracket.
Preferably, the manual hydraulic pump has a detachable hydraulic rod, and the hydraulic rod is detachably mounted on the frame body.
Preferably, the airplane wheel tyre detacher further comprises a detachable traction rod, and the traction rod is detachably placed on the frame body.
The utility model discloses a child ware is torn open to aircraft wheel is a general type aircraft wheel that can be used to big aircraft wheel and little aircraft wheel and tears child ware open, and its structural design is reasonable, light in weight, small, and the commonality is good, and the transportation of being convenient for is the equipment that outfield's aircraft maintenance is indispensable.
Drawings
The drawings are only intended to illustrate and explain the present invention and do not limit the scope of the invention. Wherein,
fig. 1 is a schematic structural view showing an unused state of an aircraft wheel detacher according to an embodiment of the present invention;
FIG. 2 is a schematic view of the aircraft wheel detacher shown in FIG. 1 being placed into a small wheel ready for disassembly;
FIG. 3 is a schematic illustration of the aircraft wheel detacher of FIG. 1 deployed in preparation for loading a large wheel;
fig. 4 is a schematic view showing the airplane wheel detacher of fig. 3 in a state of being loaded with a large wheel.
Detailed Description
In order to clearly understand the technical features, objects, and effects of the present invention, embodiments of the present invention will be described with reference to the accompanying drawings. Wherein like parts are given like reference numerals.
The application provides an aircraft wheel tire remover, the structural schematic diagram of which is shown in fig. 1-4, wherein fig. 1 shows the structural schematic diagram of the aircraft wheel tire remover in an unused state according to a specific embodiment of the present invention; FIG. 2 is a schematic view of the aircraft wheel detacher shown in FIG. 1 being placed into a small wheel ready for disassembly; FIG. 3 is a schematic illustration of the aircraft wheel detacher of FIG. 1 deployed in preparation for loading a large wheel; fig. 4 is a schematic view showing the airplane wheel detacher of fig. 3 in a state of being loaded with a large wheel.
Referring to fig. 1-4, the tire remover for airplane wheels of the present application can be used for removing and installing tires of airplane wheels, and particularly relates to a general tire remover for airplane wheels of an airplane which can be used for wheels of a large airplane and wheels of a small airplane, the general tire remover for airplane wheels of an airplane comprises a frame body 11 with a universal wheel 1 at the lower part, four pressing claws 12 are installed at the upper part of the frame body 11, a rotating frame 13 is hinged to the side part of the frame body 11, a wheel bracket 14 is hinged to the rotating frame 13, and an airplane wheel top disk 15 is installed at the lower part of the frame body 11 opposite to the pressing claws 12 (the airplane wheel top disk 15 is partially blocked by the wheel bracket 14 in fig. 1, and the airplane wheel top disk 15 is completely blocked by the airplane wheels in fig. 2), and the airplane wheel top disk 15 is operated to move up and down. To prevent the wheel hub surface from being scratched, in a preferred example, the wheel top disk 15 surface is provided with a rubber pad.
The frame 11 is shown as a generally portal structure, and the aircraft wheel tires can be placed inside the portal structure of the frame 11 for mounting and dismounting operations, as shown in fig. 2, for example, which shows a small wheel to be mounted and dismounted inside the frame 11.
The basic working characteristics of the aircraft wheel tire remover of the application are:
for a small lightweight wheel (as shown in fig. 2), the wheel bracket 14 can be removed from the frame body 11 by using the rotating frame 13, the wheel is manually placed on the wheel top disk 15 in the frame body 11, the pressing claw 12 is then deflected downward to be aligned with the wheel, the wheel top disk 15 is moved upward by operating the manual hydraulic pump 17, the edge of the wheel is made to abut against the pressing claw 12 upward, the rubber part of the wheel is deformed by the pressure of the pressing claw 12, the connecting structure of the rim part is removed, then the wheel top disk 15 is lowered to turn the wheel upside down, and the tire can be removed by abutting the rubber part again by the pressing claw 12. The tire removal step can be referred to the prior art cited in the background, and the process is related to the specific structure of the airplane wheel, which is not the scope of the present application, and is not described in detail herein.
For large wheels with large weight, as shown in fig. 3-4, it is difficult to place the large wheels on the wheel top disk 15 in the frame body 11 by manpower, and the operation of turning the wheels is very difficult, the present application designs the wheel carriage 14 specifically, the wheel carriage 14 is removed from the frame body 11 by the rotating frame 13 (rotated from the state shown in fig. 1 to the state shown in fig. 2 in which the frame body 11 is without wheels as shown in fig. 2), and then the wheel carriage 14 is rotated to the vertical state (the state shown in fig. 3), the wheels are then rolled vertically onto the wheel carriage 14 (as shown in fig. 4), and then the wheel carriage 14 and wheels are rotated to a horizontal position (back to a position similar to fig. 2 with wheels on the wheel carriage 14), and the wheel carriage 14 and wheels are rotated into the frame 11 (back to a position similar to fig. 1 with wheels on the wheel carriage 14). The operation is similar to the small wheel dismantling step, the pressing claw 12 is deflected downwards to align the wheel, the wheel top disc 15 moves upwards through a hole in the middle of the wheel bracket 14 by operating the manual hydraulic pump 17, the wheel top disc 15 is made to move upwards against the wheel, the edge of the wheel is made to upwards abut against the pressing claw 12, the rubber part of the wheel is deformed by the pressure of the pressing claw 12, the connecting structure of the wheel rim part is dismantled, the wheel top disc 15 is lowered to enable the wheel to move out of the frame body 11 by the wheel bracket 14, the wheel bracket 14 is rotated to the vertical state, the wheel is pushed down to be overturned by one hundred and eighty degrees and pushed onto the wheel bracket 14 again, the wheel bracket 14 and the overturned wheel are rotated into the frame body 11 again, and the rubber part is abutted by the pressing claw 12 again, so that the tire can be dismantled.
Can see through the description of above-mentioned operating characteristics, the utility model discloses an aircraft wheel child ware of tearing open is a general type aircraft wheel child ware of tearing open that can be used to big aircraft wheel and little aircraft wheel, and its structure contains mobilizable universal wheel, has the wheel bracket of accessible rotating turret operation moreover, utilizes the wheel bracket can remove and upset aircraft wheel, and the removal and the upset work of big aircraft wheel have been accomplished through the roll of wheel, upset and translation, and whole process only needs alone can accomplish fast, has saved manpower and time, has improved the efficiency of tearing open, installation.
In one embodiment, the upper portion of the frame body 11 is provided with a cross-shaped pressing claw sliding beam 2 for installing the pressing claw 12, and the cross-shaped pressing claw sliding beam 2 is formed by welding a circular tube 21, a vertical plate 23 of a rectangular hole 22 and a supporting ring 24. The four pressing claws 12 are symmetrically distributed in a ring shape, and the pressing claws 12 can slide along the circular tube 21 and can rotate to be horizontal and fixed at the rectangular holes 22. In the embodiment shown in the figures, the top of the pressing claw 12 is provided with an opening 28, and when the pressing claw 12 is clamped on both sides of the vertical plate 23 by the opening 28, the pressing claw 12 cannot rotate to the horizontal state, which is favorable for resisting the rubber part of the wheel. When the wheel needs to be moved into the frame body 11, the pressing claw 12 needs to be rotated to a horizontal state to make room, and at this time, the pressing claw 12 can be moved to a position where the rectangular hole 22 is located along the circular tube 21, and the pressing claw 12 can be rotated to a horizontal state without being blocked by the vertical plate 23, and then the pressing claw 12 can be fixed by a pin or other structures. The figure shows a specific embodiment of fixing the pressing claw 12, namely, a notch 29 is arranged on the upper edge of the pressing claw 12, after the pressing claw 12 moves to the horizontal state, the pressing claw 12 is moved transversely along the round pipe 21, and the notch 29 on the pressing claw 12 can be used for being clamped on the vertical plate 23 at the edge of the rectangular hole 22, so that the pressing claw 12 can be fixed to prevent the pressing claw 12 from rotating downwards to block the placement of the wheel.
With respect to the rotation of the wheel carriage 14, it is necessary to use a rotating frame 13, the specific structure of which is shown in fig. 2, and the rotating frame 13 has a vertical rotating shaft 131 for horizontally moving the wheel carriage 14 into and out of the frame body 11. In addition, the rotating frame 13 has a horizontal rotating shaft 132 that allows the wheel carriage 14 to rotate to a vertical direction after being horizontally moved out of the frame body 11. Besides, after the wheel bracket 14 is horizontally moved out of the frame body 11, the rotating frame 13 can be fixed by matching pins and pin holes, so that the wheel bracket 14 is prevented from horizontally and vertically rotating, and the wheel is conveniently placed.
In addition, as shown in fig. 4, two wheel blocking levers 141 are installed on the wheel bracket 14 to block the wheels when the wheels are vertically placed, and the wheel blocking levers 141 have a simple structure, so that the structural weight can be reduced.
In addition, as can be seen from the figures, the manual hydraulic pump 17 of the present application may further include a detachable hydraulic rod 171, and the hydraulic rod 171 is detachably mounted on the frame body 11 (as shown in fig. 1).
Further, the airplane wheel tyre detacher further comprises a detachable traction rod 16, and the traction rod 16 is detachably arranged on the frame body 11.
In addition, a hand push handle 19 can be further arranged on the frame body 11, the hand push handle 19 is suitable for being pushed by manpower to realize movement in a short distance, the traction rod 16 is suitable for being pulled by a motor and meets the requirement of long-distance motor traction, and the traction rod 16 can be detached and fixed on the inner side of the frame body 11, so that the use and storage are convenient, and the volume during transportation is reduced.
It is to be understood by those skilled in the art that while the present invention has been described in terms of several embodiments, it is not intended that each embodiment cover a separate embodiment. The description is given for clearness of understanding only, and it is to be understood that all matters in the embodiments are to be interpreted as including all technical equivalents which are encompassed by the claims.
The above description is only exemplary of the present invention, and is not intended to limit the scope of the present invention. Any equivalent changes, modifications and combinations that may be made by those skilled in the art without departing from the spirit and principles of the invention should be considered within the scope of the invention.
Claims (8)
1. The utility model provides an aircraft wheel tire breaker for aircraft wheel tire's dismantlement and installation, its characterized in that, aircraft wheel tire breaker includes that a lower part has support body (11) of universal wheel (1), four pressure claws (12) are installed on the upper portion of support body (11), a swivel mount (13) is articulated to the lateral part of support body (11), swivel mount (13) articulate has a wheel bracket (14), just right press claw (12) wheel top dish (15) is installed to the lower part of support body (11), wheel top dish (15) pass through manual hydraulic pump (17) the manipulation of installation on support body (11) wheel top dish (15) reciprocate.
2. The airplane wheel tire detacher as claimed in claim 1, wherein the upper part of the frame body (11) is provided with a cross-shaped pressing claw sliding beam (2) for installing the pressing claw (12), and the cross-shaped pressing claw sliding beam (2) is formed by welding a circular tube (21), a vertical plate (23) of a rectangular hole (22) and a supporting ring (24).
3. An aircraft wheel detacher as claimed in claim 2, characterised in that said presser foot (12) is slidable along said circular tube (21) and rotatable to horizontal and fixed at said rectangular hole (22).
4. An aircraft wheel detacher as claimed in claim 1, characterised in that said turret (13) has a vertical pivot (131) allowing said wheel carriage (14) to move horizontally in and out of said frame (11).
5. An aircraft wheel detacher as claimed in claim 1, characterised in that said turret (13) has a horizontal axis of rotation (132) allowing said wheel carrier (14) to rotate to a vertical orientation after being moved horizontally out of said frame (11).
6. An aircraft wheel detacher as claimed in claim 1, characterised in that two wheel blocking levers (141) are mounted on said wheel carriage (14).
7. An aircraft wheel detacher as claimed in claim 1, characterised in that said manual hydraulic pump (17) has a detachable hydraulic rod (171), said hydraulic rod (171) being removably mounted on said frame (11).
8. An aircraft wheel detacher as claimed in claim 1, further comprising a detachable drawbar (16), said drawbar (16) being detachably mounted on said frame (11).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720498615.0U CN206733978U (en) | 2017-05-08 | 2017-05-08 | A kind of airplane wheel tyre remover |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720498615.0U CN206733978U (en) | 2017-05-08 | 2017-05-08 | A kind of airplane wheel tyre remover |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206733978U true CN206733978U (en) | 2017-12-12 |
Family
ID=60562872
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720498615.0U Expired - Fee Related CN206733978U (en) | 2017-05-08 | 2017-05-08 | A kind of airplane wheel tyre remover |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206733978U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111823792A (en) * | 2020-08-07 | 2020-10-27 | 山东银宝轮胎集团有限公司 | Clamping device for tire |
| CN116118402A (en) * | 2022-12-13 | 2023-05-16 | 贵阳华丰航空科技有限公司 | Airplane wheel unloader |
-
2017
- 2017-05-08 CN CN201720498615.0U patent/CN206733978U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111823792A (en) * | 2020-08-07 | 2020-10-27 | 山东银宝轮胎集团有限公司 | Clamping device for tire |
| CN116118402A (en) * | 2022-12-13 | 2023-05-16 | 贵阳华丰航空科技有限公司 | Airplane wheel unloader |
| CN116118402B (en) * | 2022-12-13 | 2024-07-23 | 贵阳华丰航空科技有限公司 | Airplane wheel unloader |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106926650B (en) | A kind of vertical tyre disassembling devices | |
| CN107856482B (en) | Tyre disassembling machine | |
| CN206733978U (en) | A kind of airplane wheel tyre remover | |
| CN110444853B (en) | Replacement type antenna rod of emergency communication vehicle | |
| CN106103214A (en) | Automobile batteries clamping device | |
| CN105522878A (en) | Vehicle-mounted movable tire disassembling and assembling machine | |
| WO2022222669A1 (en) | Vertical tire disassembly/assembly robot | |
| CN206870768U (en) | A kind of vertical tyre disassembling devices | |
| CN206733976U (en) | A kind of collapsible tyre remover | |
| CN111169238A (en) | Tire removing equipment based on vertical simple assembly and use method | |
| CN109050181B (en) | Tire dismounting device and method | |
| US20230211636A1 (en) | Combined Tire-Disassembling Device And Horizontal Tire Changer | |
| CN109291734B (en) | Foldable tyre dismounting device | |
| CN209756663U (en) | Tire burst emergency protection device mounting tool based on rim | |
| CN209553229U (en) | Movable supporting rod vehicle | |
| CN210911883U (en) | Tire replacing device for automobile repair | |
| CN219969324U (en) | Unmanned aerial vehicle wheel tear child device open | |
| CN216783187U (en) | Tire lifting frame of tire dismounting machine | |
| CN217774370U (en) | Folding anticollision auxiliary device of sealing-tape machine | |
| CN221341078U (en) | General device of dragging of aircraft maintenance ladder frame | |
| CN116118402B (en) | Airplane wheel unloader | |
| CN212921007U (en) | Loading and unloading device for wheel | |
| CN218929105U (en) | Semi-automatic dismounting device for tyre body of automobile tyre | |
| CN219651398U (en) | Hydraulic general type airplane wheel disassembly and assembly device | |
| CN213413878U (en) | Aviation tire dismouting car |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20171212 Termination date: 20180508 |