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:
Apr. 19, 2022
Filed:
Jun. 30, 2020
Applicant:
GE Aviation Systems Llc, Grand Rapids, MI (US);
Inventors:
Dominique Patrick Sautron, Chicago, IL (US);
Julian Alexander Opificius, Elk River, MN (US);
Assignee:
GE Aviation Systems LLC, Grand Rapids, MI (US);
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 13/00 (2006.01); B64D 13/06 (2006.01); F02C 6/08 (2006.01); B64D 13/02 (2006.01); B64D 15/00 (2006.01); F02C 9/18 (2006.01);
U.S. Cl.
CPC ...
B64D 13/06 (2013.01); B64D 13/02 (2013.01); B64D 15/00 (2013.01); F02C 6/08 (2013.01); F02C 9/18 (2013.01); B64D 2013/0607 (2013.01); B64D 2013/0618 (2013.01); B64D 2013/0648 (2013.01); F05D 2220/323 (2013.01); Y02T 50/50 (2013.01);
Abstract
An aircraft includes an environmental control system having a bleed air inlet, a gas turbine engine having a low pressure bleed air supply and a high pressure bleed air supply, and a turbo air cycle machine. The turbo air cycle machine includes a compressor fluidly coupled to the low pressure bleed air supply, as well as a turbine fluidly coupled to at least one of the low pressure bleed air supply or the high pressure bleed air supply.