Flywheel mechanism for micro/nano-satellite

A micro-nano-satellite and flywheel technology, which is applied to aerospace vehicles, aircraft, motor vehicles, etc., can solve the problems of low development cost and the inability of traditional flywheels to meet mission requirements, etc.

Inactive Publication Date: 2016-05-04
HARBIN INST OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The development cycle of traditional flywheels is generally several months or even one year, while the overall development cycle of low-cost micro-n

Method used

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  • Flywheel mechanism for micro/nano-satellite
  • Flywheel mechanism for micro/nano-satellite
  • Flywheel mechanism for micro/nano-satellite

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specific Embodiment approach 1

[0012] Specific implementation mode one: combine Figure 1-Figure 5 Describe this embodiment mode, a kind of flywheel mechanism for micro-nano satellite described in this embodiment mode, it comprises motor support 1, shock pad 2, brushless motor 3, wheel body 4 and protective cover 5; Shock pad 2 is Rectangular frame, the through hole for installing the motor is processed on the rectangular frame, the shock pad 2 is installed on the motor bracket 1, the brushless motor 3 is installed on the motor bracket 1, the shock pad 2 is set on the brushless motor 3 and the motor Between the brackets 1 , the wheel body 4 is set on the output end of the brushless motor 3 rotating shaft, the protective cover 5 is installed on the motor bracket 1 , and the protective cover 5 is fastened on the outside of the wheel body 4 .

specific Embodiment approach 2

[0013] Specific implementation mode two: combination Figure 1-Figure 2 Describe this embodiment, a flywheel mechanism for micro-nano satellites described in this embodiment, the shock-absorbing pad 2 is a shock-absorbing pad made of natural rubber, and the shock-absorbing pad 2 is installed on the motor bracket 1 through silicon rubber Above, other structures are the same as those in the first embodiment.

specific Embodiment approach 3

[0014] Specific implementation mode three: combination Figure 1-Figure 2 Describe this embodiment, a flywheel mechanism for micro-nano satellites described in this embodiment, it also includes a plurality of first pan head screws 6 and a plurality of second pan head screws 7; the brushless motor 3 passes through a plurality of second pan head screws A pan head screw 6 is fixedly installed on the motor bracket 1, and the protective cover 5 is fixedly installed on the motor bracket 1 through a plurality of second pan head screws 7, and other structures are the same as in the first embodiment.

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Abstract

The invention discloses a flywheel mechanism for a micro/nano-satellite, relates to a flywheel mechanism and aims at solving the problem that the micro/nano-satellite in the prior art is not provided with a flywheel which is short in manufacturing period, simple in structure, low in cost and reliable in performance. The flywheel mechanism comprises a motor support, a damping cushion, a brushless motor, a wheel body and a protective cover, wherein the damping cushion is a rectangular frame body; a through hole for mounting the motor is formed in the rectangular frame body; the damping cushion is arranged on the motor support; the brushless motor is arranged on the motor support; the damping cushion is arranged between the brushless motor and the motor support; the output end of a rotating shaft of the brushless motor is sleeved by the wheel body; and the protective cover is arranged on the motor support and is buckled outside the wheel body. The flywheel mechanism is used for the fields of flight and spaceflight.

Description

technical field [0001] The invention relates to a flywheel mechanism, in particular to a flywheel mechanism for micro-nano satellites. Background technique [0002] The reaction moment flywheel is the main actuator of the satellite attitude control system. The flywheels of traditional satellites are produced and developed by professional aerospace agencies, which have the advantages of high reliability and stable performance, but the disadvantages of high cost and long development cycle. And it takes up a lot of satellite space, and the development cost is basically in the millions. At present, most of the flywheels used in spaceflight are developed by aerospace institutes, and their mass is relatively large, while the mass of ordinary nano-satellites is less than 20kg. The 100 kg satellite with practical functions plays an important role in the fields of scientific research, national defense and commercial use. The development cycle of traditional flywheels is generally s...

Claims

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Application Information

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IPC IPC(8): B64G1/28
CPCB64G1/283
Inventor 王峰郭金生陈雪芹张天赫吴凡苗悦王骋
Owner HARBIN INST OF TECH
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