The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Nov. 08, 2022

Filed:

Jun. 13, 2019
Applicant:

Dalian University of Technology, Liaoning, CN;

Inventors:

Yanhua Ma, Liaoning, CN;

Xian Du, Liaoning, CN;

Rui Wang, Liaoning, CN;

Tongjian Liu, Liaoning, CN;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 9/00 (2006.01); G05B 23/02 (2006.01); B64D 31/00 (2006.01);
U.S. Cl.
CPC ...
F02C 9/00 (2013.01); B64D 31/00 (2013.01); G05B 23/0218 (2013.01); G05B 23/0286 (2013.01); F05D 2220/323 (2013.01); F05D 2270/46 (2013.01);
Abstract

A bumpless transfer fault tolerant control method for aero-engine under actuator fault is disclosed. For an aero-engine actuator fault, by adopting an undesired oscillation problem produced by an active fault tolerant control method based on a virtual actuator, in order to solve the shortage of the existing control method, a bumpless transfer active fault tolerant control design method for the aero-engine actuator fault is provided, which can guarantee that a control system of the reconfigured aero-engine not only has the same state and output as an original fault-free system without changing the structure and parameters of a controller, to achieve a desired control objective, and that a reconfigured system has a smooth transient state, that is, output parameters such as rotational speed, temperature and pressure do not produce the undesired transient characteristics such as overshoot or oscillation.


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