Design method of fault response generator for testbed of liquid propellant rocket engine

A liquid rocket, fault response technology, applied in instruments, calculations, special data processing applications, etc., can solve problems such as deviation from the maintenance needs of the test bench, inconsistent response methods for early symptoms, etc.

Inactive Publication Date: 2015-12-09
BEIJING INST OF AEROSPACE TESTING TECH
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Problems solved by technology

However, in practical applications, the response methods to different degrees of faults and their early symptoms are not uniform, and the control decisions after faults mostly rely on experience to determine the scope of control intervention and the maintenance level or maintenance interval of each component. There is a phenomenon that the task deviates from the actual maintenance needs of the test bench

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  • Design method of fault response generator for testbed of liquid propellant rocket engine
  • Design method of fault response generator for testbed of liquid propellant rocket engine
  • Design method of fault response generator for testbed of liquid propellant rocket engine

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Embodiment Construction

[0017] The present invention will be described in detail below with reference to the accompanying drawings and examples.

[0018] The present invention provides such as figure 1 The design method of a fault response generator for a liquid rocket engine test bench is shown, and the specific steps are as follows:

[0019] Step 1: Evaluate the fault degree of the historical test data of the liquid rocket engine, and obtain fault diagnosis information, fault prediction information and fault degree grade;

[0020] Based on the historical test data of the liquid rocket engine test bed, using the fault degree evaluation method, a mathematical model is established, the test data is processed and the degree of deviation from the normal state is determined, and the fault diagnosis information, fault prediction information and fault diagnosis information of the liquid rocket engine are obtained. level of degree. The fault degree evaluation methods include statistical analysis method, n...

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Abstract

The invention discloses a design method of a fault response generator for a testbed of a liquid propellant rocket engine. The design method comprises following steps of: firstly, evaluating fault degree of historical test data of the liquid propellant rocket engine in order to obtain fault diagnosis information, fault predication information and fault level; secondly, gathering fault level of an overall testing stage in order to obtain a level curve of fault level and setting up a fault level library; thirdly, setting up mappings of fault diagnosis information, fault predication information and the fault level library and obtaining a fault response decision model according to the fact that all levels of the fault level curve in the fault level library respectively correspond to maintenance levels obtained by historical maintenance conditions; and fourth, linking different fault intervention and control measures to different maintenance levels in order to finish the design of the fault response generator for the testbed of the liquid propellant rocket engine. The design method of the fault response generator for the testbed of the liquid propellant rocket engine has following beneficial effects: a maintenance scheme can be made in advance for solving different faults and symptoms in order to decrease maintenance blind spots; and service lifetime and reliability of a testing system can be prolonged and improved.

Description

technical field [0001] The invention relates to the technical field of aerospace fault diagnosis, in particular to a design method for a fault response generator of a liquid rocket engine test bench. Background technique [0002] At present, there are many researches on rocket engine fault diagnosis at home and abroad, but in terms of engine maintenance, the current methods are regular inspection, pre-test inspection and post-fault maintenance. Periodic maintenance is to carry out periodic maintenance and precision calibration according to the reliability index of each component of the system; however, there is nothing to do about the failures that occur during the maintenance period, and it is difficult to accurately locate the location and cause of the failure. The inspection before the test is to carry out the debugging and performance inspection of the key components, sub-systems and the whole system before the engine works, and test whether the work of each link is norm...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F17/50
Inventor 周磊朱子环段娜管理周文怡马军强蔡睿马鑫田源
Owner BEIJING INST OF AEROSPACE TESTING TECH
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