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Optimization method for electromagnetic compatibility fault repair by adopting electromagnetic compatibility test over-standard strategy

An electromagnetic compatibility and optimization method technology, which is applied in the direction of measuring electricity, measuring devices, and measuring electrical variables, etc., can solve the problems of inability to determine the priority relationship of airborne equipment rectification sequence, time-consuming work, repetition and cost increase, and the failure of helicopters to be finalized on time mass production etc.

Inactive Publication Date: 2013-04-17
BEIHANG UNIV
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  • Application Information

AI Technical Summary

Problems solved by technology

However, there is currently no reasonable and feasible EMC fault repair method, and it is impossible to determine the priority relationship of the rectification sequence of airborne equipment that has EMC interference faults, which often makes EMC rectification work time-consuming, repetitive and costly, and even causes the helicopter to fail to be finalized on time. , mass production

Method used

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  • Optimization method for electromagnetic compatibility fault repair by adopting electromagnetic compatibility test over-standard strategy
  • Optimization method for electromagnetic compatibility fault repair by adopting electromagnetic compatibility test over-standard strategy
  • Optimization method for electromagnetic compatibility fault repair by adopting electromagnetic compatibility test over-standard strategy

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Embodiment

[0208] It is set that five airborne equipment will cause electromagnetic compatibility interference to the electromagnetic compatibility of the whole machine. The test curves of the five airborne equipment are obtained from the CE102, CS114, RE102, and RS103 electromagnetic compatibility tests in GJB151A and GJB152A, combined with electromagnetic vulnerability Weight Quantification processing and data processing are carried out on the exceeding part, and the weight of conduction emission index, conduction sensitivity index weight, radiation emission index weight and radiation sensitivity index weight are obtained. At the same time, according to the national military standard GJB72A-2002 "Electromagnetic Interference and Electromagnetic Compatibility Terminology" Section 2.1.56, the provisions of the key categories of subsystems and equipment, the weight of the electromagnetic compatibility classification index is obtained. Combining the weight of conduction emission index, cond...

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Abstract

The invention discloses an optimization method for electromagnetic compatibility fault repair by adopting electromagnetic compatibility test over-standard strategies. In the method, a conducted emission curve, a conducted susceptibility curve, a radiated emission curve and a radiated susceptibility curve are used and are respectively compared with requirements of national military standards to obtain over-standard areas; according to electromagnetic vulnerability weights of different frequency ranges, an area weighted integration method is adopted to quantify the over-standard areas to obtain respective weights; and finally the respective weights are introduced to obtain electromagnetic compatibility weight expected values of helicopter-borne equipment. By virtue of index quantification and weight allocation, the electromagnetic compatibility interference faults of the helicopter-borne equipment are associated with the electromagnetic compatibility of the entire helicopter, factors such as electromagnetic compatibility conducted emission, conducted susceptibility, radiated emission, radiated susceptibility and electromagnetic compatibility classification of all helicopter-borne equipment are comprehensively considered, the index quantification and the corresponding weight allocation are conducted to obtain degrees of influence of the electromagnetic compatibility interference faults of the helicopter-borne equipment on the electromagnetic compatibility of the entire helicopter are obtained, the priorities of the repair sequences of the electromagnetic compatibility interference faults of the helicopter-borne equipment are determined and a basis is provided for determining sequences for electromagnetic compatibility rectification.

Description

technical field [0001] The invention relates to a helicopter electromagnetic compatibility rectification and optimization method, specifically referring to an optimization method for repairing the electromagnetic compatibility failure of the helicopter by using the electromagnetic compatibility test exceeding the standard strategy in the environment where electromagnetic compatibility interference occurs in multiple airborne equipment method. Background technique [0002] With the continuous development of science and technology, modern helicopters adopt a large number of high-tech, automation and digitalization are getting higher and higher, and the electronic system of the helicopter has undergone great changes. There are many on-board electronic devices used in the whole machine, and the working frequency band is wider. High transmit power, high receive sensitivity, serious overlapping of transmit and receive frequency bands, and complex electromagnetic coupling hinge rel...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01R31/00
Inventor 贾云峰马超胡修吴亮魏嘉利马新超苏东林
Owner BEIHANG UNIV
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