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.
Patent No.:
Date of Patent:
Aug. 21, 2018
Filed:
Apr. 01, 2014
Applicant:
The Boeing Company, Chicago, IL (US);
Inventors:
David W. Foutch, Seattle, WA (US);
Steve G. Mackin, Bellevue, WA (US);
Michael D. Bowman, Bellevue, WA (US);
Assignee:
The Boeing Company, Chicago, IL (US);
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 6/08 (2006.01); F02C 7/047 (2006.01); F02K 3/02 (2006.01); F02C 7/32 (2006.01); F02C 7/36 (2006.01); F02C 9/18 (2006.01); F02C 7/141 (2006.01); B64D 13/06 (2006.01);
U.S. Cl.
CPC ...
F02C 7/047 (2013.01); F02C 6/08 (2013.01); F02C 7/141 (2013.01); F02C 7/32 (2013.01); F02C 7/36 (2013.01); F02C 9/18 (2013.01); F02K 3/02 (2013.01); B64D 2013/0603 (2013.01); B64D 2013/0607 (2013.01); Y02T 50/671 (2013.01);
Abstract
Bleed air systems for use with aircraft and related methods are disclosed. An example apparatus includes a compressor having a compressor inlet and a compressor outlet. The compressor is to be driven by a drive shaft extending from an engine of an aircraft. The example apparatus also includes a first passageway to fluidly couple a first low-pressure bleed air port from the engine to the compressor inlet and a second passageway to fluidly couple the compressor outlet to a system of the aircraft.