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A separation and delivery centrifugal gravity compensation device and method

A technology of gravity compensation and separation point, applied in the field of mechanical design and aerospace engineering, to achieve the effect of reducing cost, large volume and many equipment

Active Publication Date: 2021-04-13
CHINA ACAD OF AEROSPACE AERODYNAMICS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The technical problem solved by the present invention is: to overcome the defects of the prior art, to make the rotational movement of the model generate centrifugal acceleration, to compensate the problem of insufficient line displacement caused by the insufficient acceleration of the model movement, and to provide a separation and delivery centrifugal gravity compensation technology and method

Method used

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  • A separation and delivery centrifugal gravity compensation device and method
  • A separation and delivery centrifugal gravity compensation device and method
  • A separation and delivery centrifugal gravity compensation device and method

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Embodiment Construction

[0031] The present invention will be further described below in conjunction with the accompanying drawings.

[0032] see Figure 1 ~ Figure 3 As shown, the centrifugal gravity compensation device provided by the present invention includes a rotating table 1, a rotating arm 2, a rotating counterweight 5, and a rotating rod 3; the rotating table 1 is vertically fixed on the ground, and the top of the rotating table 1 is provided with a motor. The rotating arm 2 is perpendicular to and fixed on the motor shaft, and the motor shaft drives the rotating arm 2 to rotate around the rotating table 1; one end of the rotating rod 3 is sleeved in the rotating arm 2, and the other end extends along the rotating arm 2 to the outside of the rotating arm 2, and the end Used to fix the tested carrier model 4, the tested carrier model 4 is equipped with a separation model 11, and the installation attitude of the carrier model 4 can be adjusted to ensure that the separation direction of the sepa...

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PUM

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Abstract

The invention relates to a centrifugal gravity compensation device for separation and delivery. The device includes a rotating table, a rotating arm, a rotating counterweight, and a rotating rod; the rotating table is vertically fixed on the ground; On the top of the rotating shaft of the rotating table motor, the rotating arm driven by the motor rotating shaft can rotate around the rotating table; one end of the rotating rod is sleeved in the rotating arm, and the other end extends along the rotating arm to the outside of the rotating arm, and the end is used to fix the loader model under test. A separation model is installed on the carrier model under test, and the installation attitude of the carrier model can be adjusted to ensure that the separation direction of the separation model is the direction of the extension line of the rotating rod; the rotating arm and the rotating rod rotate around the rotating table, and the centrifugal force generates separation acceleration. When the carrier model under test rotates to the separation point, release the separation model.

Description

technical field [0001] The invention relates to mechanical design and wind tunnel test, in particular to a technology and method for centrifugal gravity compensation of separation and delivery, belonging to the fields of mechanical design and aerospace engineering. Background technique [0002] The aircraft model wind tunnel test plays an important role in the initial stage of aircraft development. A major feature of the wind tunnel test is that various parameters of the real aircraft are similarly scaled, and the test is carried out on the scaled model. The data obtained from the test are reversed by the similar scale formula. All kinds of aerodynamic parameters of the real aircraft can be obtained through directional calculation. In the wind tunnel free flight model test, the size of the model is often much smaller than that of the real aircraft. In practice, it is often necessary to scale down a real missile several meters long into a test model of the size of a ballpoint...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01M9/08
CPCG01M9/08
Inventor 薛飞董垒鲁伟蒋增辉
Owner CHINA ACAD OF AEROSPACE AERODYNAMICS
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