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:
Mar. 15, 2022

Filed:

May. 26, 2017
Applicant:

Sikorsky Aircraft Corporation, Stratford, CT (US);

Inventors:

Christopher A. Thornberg, Newtown, CT (US);

Glen A. Knaust, Palm City, FL (US);

Derek H. Geiger, Wilton, CT (US);

Assignee:

Sikorsky Aircraft Corporation, Stratford, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G05D 1/00 (2006.01); B64C 13/50 (2006.01); B64F 5/60 (2017.01); B64D 43/00 (2006.01); B64D 45/00 (2006.01); G05D 1/10 (2006.01);
U.S. Cl.
CPC ...
G05D 1/0061 (2013.01); B64C 13/503 (2013.01); B64C 13/506 (2018.01); B64D 43/00 (2013.01); B64D 45/00 (2013.01); B64F 5/60 (2017.01); G05D 1/0066 (2013.01); G05D 1/101 (2013.01); B64D 2045/0085 (2013.01);
Abstract

A method for providing adaptive control to a fly-by-wire aircraft includes measuring via at least one first sensor a characteristic of at least one component of the aircraft and measuring via at least one second sensor a state of the aircraft. Using the characteristic of at least one component and the state of the aircraft, a determination of at least one of an actual damage and remaining life of the at least one component is made. The operational envelope of the aircraft is adapted based on the at least one of actual damage and remaining life of the at least one component. Adapting the operational envelope includes adjusting an outer boundary thereof to prohibit operation exceeding a safe operation threshold and generating an intermediate boundary of the operational envelope. Operation of the aircraft within the intermediate boundaries minimizes further damage accrual of the at least one component.


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