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Spatial reconfigurable truss type arresting mechanism and its arresting method

A capture mechanism and truss-type technology, applied in the field of spatially reconfigurable truss-type capture mechanisms, can solve the problems of poor adaptability of captured objects, inability to dock and expand, and small capture space, and achieve easy technical implementation and deployment. The effect of technology promotion and rich material resources

Active Publication Date: 2021-07-20
HARBIN INST OF TECH
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  • Abstract
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In view of this, the present invention aims to propose a space reconfigurable truss-type capture mechanism and its capture method, which solves the problem that the existing space capture device has complex structure, heavy mass, small capture space, and adaptability to captured objects. Problems of poor performance and inability to connect and expand

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  • Spatial reconfigurable truss type arresting mechanism and its arresting method
  • Spatial reconfigurable truss type arresting mechanism and its arresting method
  • Spatial reconfigurable truss type arresting mechanism and its arresting method

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Embodiment Construction

[0055] 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.

[0056] The present invention will be described in detail below with reference to the accompanying drawings and examples.

[0057] Such as Figure 1-Figure 9 As shown, a spatially reconfigurable truss-type capture mechanism includes a base 1 and two reconfigurable truss-type capture fingers, and each reconfigurable truss-type capture finger includes a docking plug truss unit 4, One docking interface truss unit 2, several modular expandable truss units 3 and several linear drive devices 5, and one docking plug truss unit 4 for each reconfigurable truss type grabbing finger, several modular expandable trusses The unit 5 and a docking interface truss unit 2 are connected in sequence, and a linear drive device 5 is connected between two adjacent truss units of each reconfigurable truss-type catching finger;

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Abstract

The invention provides a spatially reconfigurable truss-type capture mechanism and a capture method thereof. The capture mechanism includes a base and two reconfigurable truss-type capture fingers, and each reconfigurable truss-type capture finger has Consists of a butt plug truss unit, a dock interface truss unit, several modular expandable truss units and a number of linear drives, one butt plug truss unit for each reconfigurable truss-type grabbing finger, several modular expandable truss units and A docking interface truss unit is connected in sequence, and a linear drive device is connected between two adjacent truss units of each reconfigurable truss type grabbing finger. The present invention can realize the docking or separation between the grasping finger and the base, and the docking and separation between the two fingers. According to the different requirements of the grasping task, the two fingers can be selected to cooperate to capture or the two fingers can be docked to form an extended finger. Complete capture; docking extension, simple structure, light weight, large capture space, good adaptability to capture objects.

Description

technical field [0001] The invention belongs to the technical field of space robots, and in particular relates to a space reconfigurable truss type capture mechanism and a capture method thereof. Background technique [0002] With the development of aerospace technology, the frequency of space exploration activities has increased year by year, and more and more spacecraft are performing tasks in orbit. However, due to its own failure, exhaustion of fuel or collision, the orbiting spacecraft will fail and become space junk, threatening the safety of other spacecraft and astronauts. The use of on-orbit capture devices to capture and reuse failed spacecraft is of great significance to extend the service life of spacecraft, reduce costs and maintain the safety of the space environment. Therefore, from a long-term development perspective, the capture device for on-orbit service will become an indispensable application technology in my country's future space exploration. [0003...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64G4/00
CPCB64G4/00B64G2004/005
Inventor 乔尚岭肖洪杨帆郭宏伟李兵刘荣强邓宗全
Owner HARBIN INST OF TECH
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