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:
Sep. 29, 2020

Filed:

Jun. 01, 2016
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Michael J. Duffy, Prospect Park, PA (US);

Rene Woszidlo, St. Charles, MO (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 21/04 (2006.01); B64C 21/08 (2006.01); B64C 21/06 (2006.01); B62D 35/00 (2006.01); B63B 1/32 (2006.01); B63G 8/00 (2006.01); B64C 5/02 (2006.01); B64C 9/14 (2006.01); B64C 9/00 (2006.01);
U.S. Cl.
CPC ...
B64C 21/04 (2013.01); B62D 35/00 (2013.01); B63B 1/32 (2013.01); B63G 8/00 (2013.01); B64C 5/02 (2013.01); B64C 9/14 (2013.01); B64C 21/06 (2013.01); B64C 21/08 (2013.01); B60Y 2200/11 (2013.01); B60Y 2200/114 (2013.01); B60Y 2200/14 (2013.01); B60Y 2200/143 (2013.01); B60Y 2200/30 (2013.01); B60Y 2200/50 (2013.01); B64C 2009/005 (2013.01); B64C 2230/04 (2013.01); B64C 2230/06 (2013.01); Y02T 50/166 (2013.01);
Abstract

A method and apparatus for controlling an airflow. The method draws air through a group of inlets. The group of inlets is located in a group of locations on the vehicle such that the group of inlets actively controls the airflow relative to an aircraft when drawing the air. The method compresses the air drawn by the group of inlets in a group of air compressor units located in an aircraft structure to form pressurized air. Further, the method sends the pressurized air through a group of exit ports in the aircraft structure. The pressurized air flowing out of the group of exit ports actively controls the airflow for an aircraft, enabling an improved performance of the aircraft.


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