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:
Jan. 06, 2015

Filed:

Jun. 14, 2011
Applicants:

Oh-kyu Kwon, Incheon, KR;

Ji-hyuk Yang, Incheon, KR;

Sang Yong Lee, Incheon, KR;

Inventors:

Oh-Kyu Kwon, Incheon, KR;

Ji-Hyuk Yang, Incheon, KR;

Sang Yong Lee, Incheon, KR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G06F 17/00 (2006.01); G06F 19/00 (2011.01); G01M 15/12 (2006.01); G01M 15/14 (2006.01); G01H 17/00 (2006.01);
U.S. Cl.
CPC ...
G01M 15/14 (2013.01); G01H 17/00 (2013.01); G01M 15/12 (2013.01);
Abstract

A system for detecting and diagnosing a faultive state of an airplane engine, including: at least one vibration sensor attached to an airplane; a reference model database construction unit; and a fault detection and diagnosis unit which estimates a parameter of a model, obtains a test variable and a numerator coefficient value difference of a transfer function between the models, and the covariance of parameter estimation error, and diagnoses the faultive state and the faultive cause of the airplane engine. Accordingly, the present invention can determine the faultive state and the detective cause of the airplane engine using the vibration data of the airplane engine.


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