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. 09, 2021

Filed:

Nov. 28, 2017
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Joseph Brent Staubach, Colchester, CT (US);

Nathan Snape, Tolland, CT (US);

Frederick M. Schwarz, Glastonbury, CT (US);

Charles E. Lents, Amston, CT (US);

Michael K. Ikeda, West Hartford, CT (US);

Assignee:

Raytheon Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 9/18 (2006.01); F02C 7/18 (2006.01); B64D 33/02 (2006.01); B64D 13/00 (2006.01); F02C 7/14 (2006.01); F02C 7/32 (2006.01); F02C 7/224 (2006.01); F02C 3/04 (2006.01); F02C 7/22 (2006.01); B64D 13/06 (2006.01);
U.S. Cl.
CPC ...
F02C 9/18 (2013.01); B64D 13/00 (2013.01); B64D 33/02 (2013.01); F02C 7/14 (2013.01); F02C 7/18 (2013.01); F02C 7/185 (2013.01); F02C 7/224 (2013.01); F02C 7/32 (2013.01); B64D 2013/0618 (2013.01); B64D 2013/0648 (2013.01); B64D 2033/024 (2013.01); F02C 3/04 (2013.01); F02C 7/22 (2013.01); F05D 2220/323 (2013.01); F05D 2220/62 (2013.01); F05D 2220/76 (2013.01); F05D 2240/35 (2013.01); F05D 2260/213 (2013.01);
Abstract

A lower pressure tap is connected to a first heat exchanger to be cooled by cooling air, and then to a selection valve. The selection valve selectively delivers the lower pressure tap air to a boost compressor. The lower pressure tap air downstream of the boost compressor is connected to cool the at least one turbine. The selection valve also selectively delivers a portion of the lower pressure tap air across a first cooling turbine, and to a line associated with an air delivery system for a cabin on an associated aircraft. A portion of the air downstream of the first cooling turbine is connected to a second cooling turbine, and air downstream of the second cooling turbine is connected for use in a cold loop A method of operating an air supply system is also disclosed.


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