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:
Apr. 25, 2023

Filed:

Oct. 01, 2021
Applicant:

Aurora Flight Sciences Corporation, a Subsidiary of the Boeing Company, Manassas, VA (US);

Inventor:

Francesco Giannini, Falls Church, VA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 21/08 (2006.01); B64C 29/00 (2006.01); B64C 21/02 (2006.01); B64C 9/00 (2006.01); B64D 35/04 (2006.01); B64D 29/02 (2006.01);
U.S. Cl.
CPC ...
B64C 21/08 (2013.01); B64C 9/00 (2013.01); B64C 21/025 (2013.01); B64C 29/0033 (2013.01); B64D 29/02 (2013.01); B64D 35/04 (2013.01);
Abstract

An aircraft and a control system for the aircraft includes a tilt-wing defining an inlet configured to receive air and an outlet in fluid communication with the inlet such that the outlet is configured to expel the air. The control system includes a high-lift device coupled to at least one of a leading edge, and a trailing edge of the tilt-wing. The high-lift device is movable relative to the tilt-wing. The control system includes a compressor in fluid communication with the inlet and the outlet. The compressor is configured to increase pressure of the air that is expelled out of the outlet. The outlet directs the pressurized air toward at least one of the high-lift device and a center section of the tilt-wing to maintain attachment of airflow across the tilt-wing. A method of operating the control system of the aircraft occurs to maintain attachment of airflow across the tilt-wing.


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