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Novel full aircraft high-strength irradiation test method

A test method and high-strength technology, applied in the direction of measuring devices, instruments, measuring electricity, etc., can solve the problems of limited operation of the test piece, poor repeatability of test results, and low test cost-effectiveness ratio, so as to reduce test costs and improve Effects of Test Efficiency

Active Publication Date: 2014-03-19
CHINESE AERONAUTICAL RADIO ELECTRONICS RES INST
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AI Technical Summary

Problems solved by technology

[0007] Aiming at the technical, economic and safety problems that are difficult to overcome in the high-intensity irradiation test of the existing aircraft, such as high cost of test stress, limited operation of the test piece, poor test result repeatability, and low cost-effectiveness ratio of the test , the purpose of the present invention is to provide a new type of high-intensity irradiation test method for the whole aircraft with strong operability, so that the test can be carried out in engineering, and the test efficiency can be improved and the cost can be reduced.

Method used

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Embodiment

[0035] When carrying out the substitution test of loop current injection on the aircraft surface, it is necessary to obtain the corresponding magnitude relationship between the irradiated field strength and the loop current injected into the surface, that is, the transfer function value, usually some data pairs. It is roughly divided into two steps: one is the low level coupling test LLCT (Low Level Coupling Test), and the other is the high level injection test HLIT (High Level Injection Test). The test process is as follows: in important areas such as the cockpit and equipment compartment of the aircraft, a number of 50-ohm wires are laid around the fuselage on the vertical axis, or obliquely around the fuselage in the front left (right) and rear right (left), firstly perform low-level irradiation, and measure The induced current in each surface loop is obtained, and the transfer function between the irradiated field strength and the induced current in the surface loop is obta...

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Abstract

The invention discloses a completely new full aircraft high-strength irradiation HIRF test method. Based on an electromagnetic effect produced to an aircraft by an external electromagnetic environment and response of functional performance of the aircraft to electromagnetic stress, the invention provides a method for determining equivalent effect and response produced by the aircraft to different external electromagnetic stresses; a plurality of wires surrounding the surface of the aircraft are used as a sensor to actually measure induction current of the current on the surface of a shell of the aircraft in a loop under a low-level irradiation field; then the induction current corresponding to a high-level irradiation field is extrapolated by using linear relation between high level and low level; an equivalent amount of the induction current obtained by the extrapolation is injected into the loop to produce the same surface induction current distribution as the irradiation field on the aircraft shell; and the aircraft is kept under the equivalent electromagnetic stress to finish high-strength irradiation test. In the method, the field is substituted by a path, and an electromagnetic irradiation coupling mode is substituted by an injection current coupling mode, so that the test efficiency is obviously increased, and the test expense is reduced.

Description

technical field [0001] The invention belongs to the field of electromagnetic compatibility test, and in particular relates to a new method for high-intensity irradiation test of the whole aircraft, that is, the loop current injection technology on the surface of the aircraft. Background technique [0002] In the predetermined external electromagnetic environment, the aircraft must be able to work normally with full performance. Therefore, it is required to carry out high-intensity electromagnetic radiation tests on the whole aircraft during the process of aircraft development and finalization to verify its compliance. But the current actual situation is that there are no engineering facilities that can fully carry out such tests. [0003] In the high-intensity irradiation test of the whole aircraft, the traditional test method is to uniformly irradiate the aircraft with the RF energy output by the broadband high-power amplifier HPA through the antenna in the form of free-sp...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01R31/00G01R33/00
Inventor 方愔李培侯典国
Owner CHINESE AERONAUTICAL RADIO ELECTRONICS RES INST
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