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:
Feb. 13, 2024

Filed:

Dec. 22, 2020
Applicant:

Bell Textron Inc., Fort Worth, TX (US);

Inventor:

Thomas Dewey Parsons, Fort Worth, TX (US);

Assignee:

Textron Innovations Inc., Providence, RI (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 9/20 (2006.01); F02C 7/262 (2006.01); F02C 7/057 (2006.01); F02C 7/26 (2006.01);
U.S. Cl.
CPC ...
F02C 9/20 (2013.01); F02C 7/057 (2013.01); F02C 7/26 (2013.01); F02C 7/262 (2013.01); F05D 2220/323 (2013.01); F05D 2260/85 (2013.01); F05D 2270/02 (2013.01); F05D 2270/09 (2013.01);
Abstract

Embodiments are directed to systems and methods for controlling an aircraft engine inlet comprises determining a required engine RPM for an engine in-flight restart based upon current aircraft parameters, detecting a command to initiate the engine in-flight restart, and managing a position of an engine inlet barrier to control a volume of air entering an engine intake, wherein the ram air causes an engine turbine to achieve the required engine RPM. The required engine RPM may be an N1 gas generator RPM. The engine inlet barrier may be a hinged door positioned within the engine inlet or a series of inlet variable guide vanes that are configured to rotate between a closed position and an opened position. The position of the engine inlet barrier may be controlled by a flight control computer or an engine control computer.


Find Patent Forward Citations

Loading…