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A Vibration Suppression Method of Wind Tunnel Strut Based on Time Delay Compensation

A time-delay and wind-tunnel technology, applied in the field of wind-tunnel tests, can solve problems such as system instability, and achieve the effects of eliminating the influence of time-delay, good flexibility, and wide adjustable angle range

Active Publication Date: 2019-02-01
DALIAN UNIV OF TECH
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  • Abstract
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  • Claims
  • Application Information

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Problems solved by technology

The time lag of the acceleration sensor and the piezoelectric actuator excitation signal is obtained through the hammering method and Lissajous graph analysis, and the time lag compensation phase shift algorithm and the linear-quadratic-Gaussian control algorithm (linear-quadratic-Gaussian control, hereinafter referred to as The controller combined with LQG) solves the problem of system instability caused by phase lag in the signal transmission process to a certain extent, and can ensure the closed-loop stability of the system

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  • A Vibration Suppression Method of Wind Tunnel Strut Based on Time Delay Compensation
  • A Vibration Suppression Method of Wind Tunnel Strut Based on Time Delay Compensation
  • A Vibration Suppression Method of Wind Tunnel Strut Based on Time Delay Compensation

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Embodiment Construction

[0051] The specific embodiments of the present invention will be described in detail below in conjunction with the technical solutions and accompanying drawings.

[0052] The present invention adopts the vibration signal of the Lance ULT 2008 / V type acceleration sensor measurement system, the range is 10g, and the sensitivity is 500mv / g; the ds1103 type controller produced by dSPACE Company is used as the realization platform of the control algorithm; The PZD700A dual-channel power amplifier and the 20VS12 piezoelectric ceramic actuator of Xinming Company output reverse force and torque to suppress vibration; the following is the specific process of the wind tunnel strut vibration suppression method based on time-delay compensation in the wind tunnel test :

[0053] Step 1 Build a wind tunnel strut vibration suppression system based on time-delay compensation

[0054] Such as figure 1 As shown, the acceleration sensor 1 is installed on the aircraft model 8 as required, and t...

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Abstract

The invention discloses a wind tunnel strut vibration restraining method based on time delay compensation belonging to the technical field of wind tunnel test, and particularly relates to a wind tunnel strut vibration restraining method based on time delay compensation. Modal test is carried out on a cantilever beam system of a strut wind tunnel model through a hammering method to get a frequency response function of the system. A state feedback gain matrix is calculated using an LQR algorithm, and all states of an estimation system using a Kalman filter are output according to observation. The phase difference between acceleration sensor and piezoelectric actuator excitation signals in vibration control is analyzed using Lissajous figures, a phase shift algorithm is programmed in a controller to compensate the time delay, and finally, active vibration control is realized. The method can eliminate the influence of time delay, and has high flexibility and a large adjustable angle range. The problem that model vibration affects the safety of the system due to time delay in the existing wind tunnel ground experiment is solved. The method is of high adjustability, and is suitable for actual measurement in wind tunnel ground experiment.

Description

technical field [0001] The invention belongs to the technical field of wind tunnel tests, and in particular relates to a method for suppressing vibration of wind tunnel struts based on time-delay compensation. Background technique [0002] The wind tunnel test is based on the principle of relativity of motion, fixing the model or object of the aircraft in the artificial environment on the ground, artificially creating airflow to simulate various complex flight states in the air, and obtaining experimental data. important part of production. [0003] In wind tunnel experiments, the wind tunnel model generally adopts the tail support method. The tail of the model is connected to the force measuring balance and the support rod, and the tail of the support rod is fixed on the machete. The wind tunnel model-balance-support rod system forms a typical cantilever beam structure. This kind of support method has little influence on the flow field around the model, but because the le...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01M9/00G01M9/08
CPCG01M9/00G01M9/08
Inventor 刘巍姜雨丰张家昆袁晓晶刘惟肖鲁继文周孟德刘昱王世红贾振元
Owner DALIAN UNIV OF TECH
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