CN210211924U - Multifunctional aircraft tire decomposer - Google Patents

Multifunctional aircraft tire decomposer Download PDF

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Publication number
CN210211924U
CN210211924U CN201920926042.6U CN201920926042U CN210211924U CN 210211924 U CN210211924 U CN 210211924U CN 201920926042 U CN201920926042 U CN 201920926042U CN 210211924 U CN210211924 U CN 210211924U
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China
Prior art keywords
fixedly connected
decomposer
wall
support frame
shaped support
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CN201920926042.6U
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Chinese (zh)
Inventor
Minggang Zhang
张明刚
Yanbin Lyu
吕延宾
Binglong Shen
申炳龙
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Nantong Huaxia Airplane Engineering Technology Co Ltd
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Nantong Huaxia Airplane Engineering Technology Co Ltd
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Priority to CN201920926042.6U priority Critical patent/CN210211924U/en
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Abstract

The utility model discloses a multi-functional aircraft tire decomposer, including the decomposer shell, sliding connection has the workstation between the corresponding both sides of decomposer shell inner wall, electric telescopic handle's work end and the top fixed connection of workstation, rotate between the corresponding both sides of U-shaped support frame inner wall and be connected with the lead screw, the equal threaded connection in position of lead screw surface has the sliding block, the bottom fixedly connected with splint of sliding block, inner wall one side fixedly connected with pneumatic cylinder of decomposer shell, the work end fixedly connected with top dish of pneumatic cylinder, surface one side fixedly connected with electro-magnet of top dish. The utility model discloses reached automatic clamping and dismantled, the effect of avoiding dropping has realized the automation, and labour saving and time saving has reduced the hand labor volume, has improved work efficiency, avoids appearing the condition of accidental injury, and factor of safety is high, has improved performance.

Description

Multifunctional aircraft tire decomposer
Technical Field
The utility model relates to a tire decomposes technical field, specifically is a multi-functional airborne vehicle tire decomposes machine.
Background
The tire is a circular ring-shaped elastic rubber product which is assembled on various vehicles or machines and rolls with ground contact, the tire is used for lightening and absorbing the vibration and impact force of the automobile during running, preventing parts of the automobile from being severely vibrated and damaged early, adapting to the high-speed performance of the vehicle and reducing the noise during running, ensuring the running safety, the operation stability, the comfort and the energy-saving economy, the airplane is a common vehicle and is favored by people due to high speed, the airplane has to be strictly inspected before taking off due to the particularity of the flight route of the airplane, the tire is one of the most important parts of the airplane as the most foundation, the inspection of the tire is particularly important, and once the abrasion of the tire of the airplane is found, the tire needs to be decomposed and replaced by new tire rubber so as to be combined into a new airplane tire. At present, the tire decomposer that has now on the market is complicated in structure, uses inconveniently, needs a large amount of workman's work, has increased workman's the amount of labour, wastes time and energy, and work efficiency, wheel hub from the tire ejecting back in addition can directly drop, the potential safety hazard that exists causes the workman injured easily, factor of safety is low, has reduced performance.
SUMMERY OF THE UTILITY MODEL
The utility model provides a not enough to prior art, the utility model provides a multi-functional aircraft tire decomposes machine has solved the structure complicacy, uses inconveniently, needs a large amount of workman's work, has increased workman's the amount of labour, wastes time and energy, and work efficiency, wheel hub in the follow tire ejecting back in addition can directly drop, and the potential safety hazard that exists causes the workman injured easily, and factor of safety is low, has reduced the problem of performance.
In order to achieve the above purpose, the utility model discloses a following technical scheme realizes: a multifunctional aircraft tire decomposer comprises a decomposer shell, a workbench is connected between two corresponding sides of the inner wall of the decomposer shell in a sliding manner, electric telescopic rods are fixedly connected at corresponding positions of the top of the inner wall of the decomposer shell, the working ends of the electric telescopic rods are fixedly connected with the top of the workbench, a U-shaped support frame is fixedly connected with the top of the inner wall of the decomposer shell, the opening of the U-shaped support frame is downward, a screw rod is rotatably connected between two corresponding sides of the inner wall of the U-shaped support frame, sliding blocks are connected with the corresponding positions of the surface of the screw rod in a threaded manner, the tops of the sliding blocks are connected with the top of the inner wall of the U-shaped support frame in a sliding manner, a clamping plate is fixedly connected with the bottom of the sliding block, the working end of the hydraulic cylinder is fixedly connected with a top disc, and one side of the surface of the top disc is fixedly connected with an electromagnet.
One end of the screw rod penetrates through the inner wall of the U-shaped support frame and extends to the outside of the U-shaped support frame, a servo motor is fixedly connected to one side of the top of the inner wall of the shell of the decomposition machine, and an output shaft of the servo motor is fixedly connected with one end of the screw rod, which extends to the U-shaped support frame, through a coupler.
Preferably, an arc fixing concave surface is formed in one side of the surface of the clamping plate, and the friction convex points are fixedly connected to the surface of the clamping plate and located inside the arc fixing concave surface.
The disassembly machine comprises a disassembly machine shell, a screw rod, a limiting block, a base and a disassembly machine shell, wherein the screw rod is fixedly connected with the base in the corresponding position on the surface of the screw rod, and the base is fixedly connected with the disassembly machine shell in the corresponding position on the bottom of the disassembly machine shell.
The inner wall of the U-shaped support frame is provided with a sliding groove matched with the sliding block.
Preferably, the thread directions of the corresponding positions on the surface of the screw rod are opposite.
Advantageous effects
The utility model provides a multi-functional aircraft tire decomposes machine. The method has the following beneficial effects:
1. the utility model discloses a sliding connection has the workstation between the corresponding both sides of decomposition shell inner wall, electric telescopic handle's work end and the top fixed connection of workstation, the inner wall top fixedly connected with U-shaped support frame of decomposition shell, it is connected with the lead screw to rotate between the corresponding both sides of U-shaped support frame inner wall, the equal threaded connection in position of lead screw surface corresponding has the sliding block, the top of sliding block and the inner wall top sliding connection of U-shaped support frame, the bottom fixedly connected with splint of sliding block, the effect of self-holding dismantlement has been reached, and is rational in infrastructure simple, high durability and convenient use, the automation has been realized, time saving and labor saving, the amount of labor is reduced, and the work.
2. The utility model discloses a decomposition shell's inner wall one side fixedly connected with pneumatic cylinder, the working end fixedly connected with of pneumatic cylinder pushes up the dish, pushes up the surperficial one side fixedly connected with electro-magnet of dish, has reached the effect of avoiding dropping, and is rational in infrastructure simple, and convenient to use, wheel hub can not drop after ejecting, avoids appearing the condition of accidental injury, and factor of safety is high, has improved performance.
Drawings
Fig. 1 is a schematic structural view of the present invention;
fig. 2 is a top view of the interior of the present invention;
fig. 3 is a partially enlarged view of a portion a in fig. 1.
In the figure:
1. a decomposer housing; 2. a work table; 3. an electric telescopic rod; 4. a U-shaped support frame; 5. a screw rod; 6. a slider; 7. a splint; 8. positioning the concave surface; 9. a hydraulic cylinder; 10. a top tray; 11. an electromagnet; 12. a servo motor; 13. a circular arc fixing concave surface; 14. rubbing the salient points; 15. a limiting block; 16. a base.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Please refer to fig. 1-3, the utility model provides a multi-functional aircraft tire decomposer, including decomposer shell 1, sliding connection has workstation 2 between the corresponding both sides of decomposer shell 1 inner wall, the sliding tray with workstation 2 looks adaptation is all seted up to the corresponding both sides of decomposer shell 1 inner wall, the equal fixedly connected with electric telescopic handle 3 in position that decomposes 1 inner wall top is corresponding, the top fixed connection of electric telescopic handle 3's working end and workstation 2, the inner wall top fixedly connected with U-shaped support frame 4 of decomposer shell 1, the opening of U-shaped support frame 4 is down, it is connected with lead screw 5 to rotate between the corresponding both sides of U-shaped support frame 4 inner wall, the corresponding position screw thread direction in lead screw 5 surface is opposite, convenient clamp.
The equal threaded connection in 5 surperficial corresponding positions of lead screw has sliding block 6, the sliding tray with 6 looks adaptations of sliding block is seted up at the inner wall top of U-shaped support frame 4, the top of sliding block 6 and the inner wall top sliding connection of U-shaped support frame 4, the bottom fixedly connected with splint 7 of sliding block 6, location concave surface 8 has been seted up to the top central point of workstation 2.
The inner wall one side fixedly connected with pneumatic cylinder 9 of decomposition machine shell 1, the working end fixedly connected with of pneumatic cylinder 9 pushes up dish 10, the surperficial one side fixedly connected with electro-magnet 11 of pushing up dish 10, electro-magnet 11 holds wheel hub, avoids dropping the accidental injury others, has improved the security performance.
The one end of lead screw 5 runs through the inner wall of U-shaped support frame 4 and extends to its outside, inner wall top one side fixedly connected with servo motor 12 of decomposition shell 1, servo motor 12's output shaft passes through the shaft coupling and extends to the one end fixed connection of U-shaped support frame 4 with lead screw 5, the fixed concave surface 13 of circular arc has been seted up to surface one side of splint 7, the surface of splint 7 and the inside fixedly connected with friction bump 14 that is located the fixed concave surface 13 of circular arc, friction bump 14 increases frictional force, avoids appearing the phenomenon of skidding, improves clamping efficiency.
The corresponding positions on the surface of the screw rod 5 are fixedly connected with limit blocks 15, and the corresponding positions on the bottom of the decomposer shell 1 are fixedly connected with bases 16.
The utility model discloses a theory of operation does: firstly, starting an electric telescopic rod 3 to work, driving a workbench 2 to move downwards by a working end of the electric telescopic rod 3 until the workbench moves to the lowest position, stopping the electric telescopic rod 3 at the moment, rolling a tire to be decomposed to the position of a positioning concave surface 8 at the top of the workbench 2 at the moment, starting the electric telescopic rod 3 at the moment, slowly lifting the workbench 2, stopping the electric telescopic rod 3 when the workbench reaches a specified height, starting a servo motor 12 to work, driving a screw rod 5 by an output shaft of the servo motor 12 through a coupler so as to drive a sliding block 6, driving a clamping plate 7 to clamp the tire, starting a hydraulic cylinder 9 at the moment, driving a top disc 10 and an electromagnet 11 by the working end of the hydraulic cylinder 9, stopping the hydraulic cylinder 9 when the electromagnet 11 is close to the surface of a wheel hub, immediately powering on the electromagnet 11, sucking the wheel hub by magnetic force at the moment, the hydraulic cylinder 9 is started again, the wheel hub is ejected out through the top disc 10, the tire and the wheel hub are disassembled, the electromagnet 11 is powered off by a worker at the moment, the wheel hub is taken down, the top disc 10 and the electromagnet 11 are contracted through the hydraulic cylinder 9 at the moment, the tire is loosened through the reverse rotation of the servo motor 12, the workbench 2 is moved to the lowest position through the electric telescopic rod 3, and the tire can be taken out.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation. The use of the phrase "comprising one of the elements does not exclude the presence of other like elements in the process, method, article, or apparatus that comprises the element.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims (6)

1. A multifunctional aircraft tire decomposer comprises a decomposer shell (1), and is characterized in that a workbench (2) is connected between two corresponding sides of the inner wall of the decomposer shell (1) in a sliding manner, electric telescopic rods (3) are fixedly connected to corresponding positions of the top of the inner wall of the decomposer shell (1), the working ends of the electric telescopic rods (3) are fixedly connected with the top of the workbench (2), a U-shaped support frame (4) is fixedly connected to the top of the inner wall of the decomposer shell (1), an opening of the U-shaped support frame (4) faces downwards, a screw rod (5) is rotatably connected between two corresponding sides of the inner wall of the U-shaped support frame (4), sliding blocks (6) are connected to corresponding positions of the surface of the screw rod (5) in a threaded manner, and the top of the inner wall of the U-shaped support frame (4) is, the bottom fixedly connected with splint (7) of sliding block (6), location concave surface (8) have been seted up to the top central point of workstation (2), inner wall one side fixedly connected with pneumatic cylinder (9) of decomposition shell (1), the working end fixedly connected with top dish (10) of pneumatic cylinder (9), surface one side fixedly connected with electro-magnet (11) of top dish (10).
2. The multifunctional aircraft tire decomposer according to claim 1, wherein one end of the screw rod (5) penetrates through the inner wall of the U-shaped support frame (4) and extends to the outside of the U-shaped support frame, a servo motor (12) is fixedly connected to one side of the top of the inner wall of the decomposer shell (1), and an output shaft of the servo motor (12) is fixedly connected with one end of the screw rod (5) extending to the U-shaped support frame (4) through a coupler.
3. The multifunctional aircraft tire disassembling machine according to claim 1, wherein an arc fixing concave surface (13) is formed on one side of the surface of the clamping plate (7), and a friction convex point (14) is fixedly connected to the surface of the clamping plate (7) and located inside the arc fixing concave surface (13).
4. The multifunctional aircraft tire decomposer according to claim 1, wherein a limiting block (15) is fixedly connected to a corresponding position on the surface of the screw rod (5), and a base (16) is fixedly connected to a corresponding position on the bottom of the decomposer shell (1).
5. The multifunctional aircraft tire decomposer according to claim 1, wherein sliding grooves matched with the workbench (2) are formed in two corresponding sides of the inner wall of the decomposer shell (1), and sliding grooves matched with the sliding blocks (6) are formed in the top of the inner wall of the U-shaped support frame (4).
6. Multifunctional aircraft tire deconsolidation machine according to claim 1, characterized in that the corresponding positions of the surface of said screw (5) are opposite in thread direction.
CN201920926042.6U 2019-06-19 2019-06-19 Multifunctional aircraft tire decomposer Active CN210211924U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201920926042.6U CN210211924U (en) 2019-06-19 2019-06-19 Multifunctional aircraft tire decomposer

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201920926042.6U CN210211924U (en) 2019-06-19 2019-06-19 Multifunctional aircraft tire decomposer

Publications (1)

Publication Number Publication Date
CN210211924U true CN210211924U (en) 2020-03-31

Family

ID=69932805

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201920926042.6U Active CN210211924U (en) 2019-06-19 2019-06-19 Multifunctional aircraft tire decomposer

Country Status (1)

Country Link
CN (1) CN210211924U (en)

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