Five-freedom active control magnetic suspension free rolling system

An active control and magnetic levitation technology, applied in aerodynamic tests, measuring devices, instruments, etc., can solve problems affecting the accuracy and reliability of test results, reduce axial detection signal errors, improve control accuracy, eliminate Effects of contact and interference

Inactive Publication Date: 2008-08-20
BEIHANG UNIV
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  • Abstract
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AI Technical Summary

Problems solved by technology

The rotor of the general free rock system is supported by mechanical bearings. Due to the friction of the mechanical bearings, the rotor is not completely free to move during the rotation process, but is restricted by the mechanical bearings, which affects the accuracy and credibility of the test results. Spend

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  • Five-freedom active control magnetic suspension free rolling system
  • Five-freedom active control magnetic suspension free rolling system
  • Five-freedom active control magnetic suspension free rolling system

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Embodiment Construction

[0021] Such as figure 1 As shown, the present invention is mainly composed of a magnetic suspension stator system and a magnetic suspension rotor system, wherein the magnetic suspension stator system is mainly composed of a first self-locking threaded ring 2, a second self-locking threaded ring 26, a third self-locking threaded ring 28, a fixing nut 29, Upper protective bearing sleeve 3, lower protective bearing sleeve 25, first radial displacement sensor 5, second radial displacement sensor 11, third radial displacement sensor 15, fourth radial displacement sensor 17, fifth radial displacement sensor 21. Upper axial displacement sensor 12, lower axial displacement sensor 22, upper radial magnetic bearing 9 stator, middle radial magnetic bearing 16 stator, lower radial magnetic bearing 19 stator, axial magnetic bearing 27 stator, front section of strut 8. The rear section of the pole 34, the cover plate 33, the tension bolt 35, the electromagnetic clutch assembly 30, the coupl...

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Abstract

A five-freedom active control magnetic suspension free rock system is mainly composed of a magnetic suspension stator system and a magnetic suspension rotor system. The magnetic suspension stator system is mainly composed of a support rod front segment, a support rod back segment, a cover plate, a rotary encoder, a shaft coupling, an electromagnetic clutch component, a tightening bolt, a fixed thread ring, a small self-locking thread ring, a large self-locking thread ring, an axial magnetic bearing stator, a radial magnetic bearing stator, an axial displacement sensor and a radial displacement sensor; and the magnetic suspension rotor system is mainly composed of a locating joint, a principal axis, a protecting bearing, a radial magnetic bearing rotor, an axial magnetic bearing rotor, an axial sensor detecting ring and a radial sensor detecting ring. The invention adopts a magnetic suspension support mode and greatly reduces the mechanical friction, leads to that the plane model can better analog the real aero flight of the plane and the precision of plane wind tunnel test is greatly increased.

Description

technical field [0001] The invention relates to a five-degree-of-freedom active control magnetic levitation free rock system, which can be used in aircraft wind tunnel tests, and can analyze a series of aircraft swing, vibration, whirl, rotation, subsonic flight, sonic flight, supersonic flight, far supersonic flight, etc. The test makes the aircraft model better simulate the real air flight of the aircraft. Background technique [0002] Today's research on aircraft flying in the air is mainly to analyze various flight conditions of the aircraft in the air, such as air body flipping, wing flutter, wing rocking, high angle of attack takeoff and landing of the aircraft, and subsonic speed of the aircraft. Fly, fly at the speed of sound, fly at the speed of sound, fly far beyond the speed of sound. These studies have brought great inconvenience to the experiments. The free rock system was born according to the principle of the relative air motion of the aircraft in the air. ...

Claims

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Application Information

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IPC IPC(8): G01M9/02
Inventor 房建成刘强韩邦成王曦孙津济刘刚韩辅君
Owner BEIHANG UNIV
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