Discrete source distributed impact test device and method
A kind of impact test, distributed technology, applied in the direction of measuring device, impact test, aircraft component test, etc., can solve the problem of single impact source, unable to adjust the working attitude of the test piece arbitrarily, difficult to simulate the impact strength of aircraft against foreign objects, etc. Adjust flexible effects
Pending Publication Date: 2021-10-01
CHINA AIRPLANT STRENGTH RES INST
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Problems solved by technology
[0003] The existing ground simulation impact test method has a single impact source, and cannot simulate the continuous impact scene of birds in the air or multiple hailstones; in addition, the test pieces of the existing air cannon device are generally fixed, a
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Abstract
The invention belongs to the field of impact dynamics tests, and particularly relates to a discrete source distributed impact test device and method. The device comprises a gas tank, multiple gas guns, discrete sources, a to-be-tested piece and a multi-target velocimeter. The gas guns are connected with the gas tank through gas guide pipes, controllable air valves are arranged on the gas guns, and the controllable air valves are connected with the controller; the discrete sources are arranged in the gas guns; and the to-be-tested piece is located at the position matched with openings in the rear ends of the gas guns, and the to-be-tested piece is installed on a posture adjusting mechanism capable of achieving six-degree-of-freedom adjustment. The multi-target velocimeter is located between the gas guns and the to-be-tested piece. According to the invention, the impact test of multiple impact sources can be carried out at the same time, the multiple impact sources can be synchronously launched or asynchronously launched in time, and the impact points of multiple discrete sources can be adjusted in space, so that the spatial distribution of the impact of the discrete sources is realized, and the spatial attitude of an impacted test piece can be adjusted, so that flexible adjustment can be carried out according to the test purpose.
Description
technical field [0001] The application belongs to the field of impact dynamics test, in particular to a discrete source distributed impact test device and method. Background technique [0002] The important structural components of the aircraft, such as skin, windshield, radomes, etc., are often hit by birds, hail, etc., resulting in structural failure and damage, which seriously threatens the flight safety of the aircraft. Generally, the impact-sensitive surface of the aircraft needs to be verified by the ground simulation impact test. The air cannon is a commonly used ground simulation impact test device. Simulate the impact of foreign objects on important structural components of the aircraft. [0003] The existing ground simulation impact test method has a single impact source, and cannot simulate the continuous impact scene of birds in the air or multiple hailstones; in addition, the test pieces of the existing air cannon device are generally fixed, and different clips...
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IPC IPC(8): G01M7/08B64F5/60
CPCG01M7/08B64F5/60
Inventor 王计真刘小川王彬文白春玉郭军
Owner CHINA AIRPLANT STRENGTH RES INST
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