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A Fault Tolerance Method for Full Authority Control System of Turbofan Engine

A turbofan engine and full-authority control technology, which is applied in the direction of machines/engines, mechanical equipment, gas turbine devices, etc., can solve the problem of no fault-tolerant method and achieve the effect of improving work reliability

Active Publication Date: 2017-09-29
AECC SHENYANG ENGINE RES INST
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

In the aforementioned aircraft with redundant engine control systems, there is not yet a method for fault tolerance

Method used

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  • A Fault Tolerance Method for Full Authority Control System of Turbofan Engine

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Embodiment Construction

[0046] In order to make the objectives, technical solutions and advantages of the present invention clearer, the technical solutions in the embodiments of the present invention will be described in more detail below in conjunction with the drawings in the embodiments of the present invention. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are some, but not all, embodiments of the invention. The embodiments described below by referring to the figures are exemplary and are intended to explain the present invention and should not be construed as limiting the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention. Embodiments of the present invention will be described in detail below ...

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Abstract

The invention discloses a fault-tolerant method for a full authority control system of a turbofan engine. The fault-tolerant method for the full authority control system of the turbofan engine includes the following steps that (1) the full authority electronic-control control system receives signals transmitted by all sensors on the turbofan engine; (2) whether the signals transmitted by the sensors break down or not is judged, the steps are stopped if the signals transmitted by the sensors do not break down, and the next step is executed if the signals transmitted by the sensors break down; (3) the types of faults occurring in the step (2) are judged; and (4) a fault-tolerant solution method used when the types of faults stored in the full authority electronic-control control system occur are called, and the fault-tolerant solution method is executed. According to the fault-tolerant method for the full authority control system of the turbofan engine, when the faults of the sensor signals such as the rotating speed and the temperature occur in the control system, recombination and optimizing of a control system structure and a control system plan are achieved, and the working reliability of the control system is greatly improved.

Description

technical field [0001] The invention relates to the technical field of turbofan engine control, in particular to a fault-tolerant method for a full-authority control system of a turbofan engine and a fault-tolerant system for a full-authority control system of a turbofan engine. Background technique [0002] Fault-tolerant control technology means that when some components fail and the original control plan cannot be realized, the control system automatically adjusts the control plan and control structure to ensure that the engine can still complete the engine safely according to the original performance or a slight decrease in performance. A technique for a given control task. Using the powerful calculation ability, logical judgment ability and decision-making ability of modern computers, good results have been achieved in improving engine reliability and maintainability. Due to the limited comprehensive parameters of the original mechanical-hydraulic control system, no ma...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F02C9/00
CPCF02C9/00
Inventor 刘永泉荣莉张千一方政柳阳
Owner AECC SHENYANG ENGINE RES INST