Missile mounting vehicle traction mechanism
The technology of a traction mechanism and a bomb trailer, which is applied in the space field, can solve the problems of inability to control the direction of the handle, time-consuming and labor-intensive, poor reliability, etc., and achieves the effects of saving time and effort in disassembly and assembly, high versatility, and low cost.
Inactive Publication Date: 2021-04-13
北京航天飞腾装备技术有限责任公司
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- Application Information
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Problems solved by technology
[0002] Existing bomb vehicles need to turn and move frequently. At present, the combination of universal wheels and directional wheels is commonly used. However, the universal wheels are easy to break after a period of use, and the reliability is poor. In some cases, the handle Unable to control the direction, time-consuming and labor-intensive
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[0019] Exemplary embodiments of the present disclosure will be described in more detail below with reference to the accompanying drawings. Although exemplary embodiments of the present disclosure are shown in the drawings, it should be understood that the present disclosure may be embodied in various forms and should not be limited by the embodiments set forth herein. Rather, these embodiments are provided for more thorough understanding of the present disclosure and to fully convey the scope of the present disclosure to those skilled in the art. It should be noted that, in the case of no conflict, the embodiments of the present invention and the features in the embodiments can be combined with each other. The present invention will be described in detail below with reference to the accompanying drawings and examples.
[0020] figure 1 It is a structural schematic diagram of the traction mechanism of the bomb trailer provided by the embodiment of the present invention. like...
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The invention discloses a missile mounting vehicle traction mechanism which comprises a handle, a first steering block, a second steering block, a vehicle body, a first trundle, a second trundle, a steering control block, a first connecting shaft, a second connecting shaft, a connecting rod, a first bearing, a second bearing, a second connecting shaft, a third connecting shaft and a fourth connecting shaft. The handle is connected with the steering control block through a fourth connecting shaft; the steering control block is connected with the vehicle body through a third connecting shaft; the steering control block is connected with the connecting rod through a second connecting shaft; the connecting rod is connected with the first steering block through a first connecting shaft and connected with the second steering block through the second connecting shaft. One end of the first trundle penetrates through a first bearing arranged in the vehicle body and is connected with the first steering block; and one end of the second trundle penetrates through a second bearing arranged in the vehicle body and is connected with the second steering block. The missile mounting vehicle traction mechanism can conveniently, quickly and flexibly turn and advance, the operation efficiency is improved, and the application range is wide.
Description
technical field [0001] The invention belongs to the field of space technology, and in particular relates to a traction mechanism for a bomb trailer. Background technique [0002] Existing bomb vehicles need to turn and move frequently. At present, the combination of universal wheels and directional wheels is commonly used. However, the universal wheels are easy to break after a period of use, and the reliability is poor. In some cases, the handle Unable to control the direction, time-consuming and labor-intensive. Contents of the invention [0003] The technical problem solved by the present invention is to overcome the deficiencies of the prior art and provide a traction mechanism for the bomb trolley, which can make the trolley trolley turn and move conveniently, quickly and flexibly, improve the operating efficiency, and have a wide range of applications. [0004] The purpose of the present invention is achieved through the following technical solutions: a traction mec...
Claims
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IPC IPC(8): B60D1/00B60D1/14B64F1/36
CPCB60D1/00B60D1/14B64F1/36B60D2001/001
Inventor 赵安龙李淼华玉龙刘红艺荆宝坤谷文杰
Owner 北京航天飞腾装备技术有限责任公司