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:
Jul. 15, 2025

Filed:

Dec. 16, 2022
Applicant:

Rtx Corporation, Farmington, CT (US);

Inventors:

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

Michael Winter, New Haven, CT (US);

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

Nathan Snape, Tolland, CT (US);

Alan H. Epstein, Lexington, MA (US);

Assignee:

RTX CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 13/08 (2006.01); B01D 45/08 (2006.01); B01D 53/00 (2006.01); B03C 1/28 (2006.01); B64D 13/06 (2006.01); B64D 27/12 (2006.01); B64D 33/08 (2006.01); F01D 15/00 (2006.01); F01D 25/12 (2006.01); F02C 6/08 (2006.01); F02C 7/141 (2006.01); F02C 7/143 (2006.01); F02C 7/16 (2006.01); F02C 7/18 (2006.01); F02C 9/18 (2006.01); F02K 3/06 (2006.01); F17C 7/02 (2006.01); F17C 7/04 (2006.01); F25B 9/14 (2006.01); F25J 1/00 (2006.01); F25J 3/04 (2006.01); B64D 37/32 (2006.01);
U.S. Cl.
CPC ...
B64D 13/08 (2013.01); B01D 45/08 (2013.01); B01D 53/002 (2013.01); B03C 1/288 (2013.01); B64D 13/06 (2013.01); B64D 27/12 (2013.01); B64D 33/08 (2013.01); F01D 15/00 (2013.01); F01D 25/12 (2013.01); F02C 6/08 (2013.01); F02C 7/141 (2013.01); F02C 7/143 (2013.01); F02C 7/16 (2013.01); F02C 7/185 (2013.01); F02C 9/18 (2013.01); F02K 3/06 (2013.01); F17C 7/02 (2013.01); F17C 7/04 (2013.01); F25B 9/14 (2013.01); F25J 1/0012 (2013.01); F25J 3/04254 (2013.01); F25J 3/04975 (2013.01); B64D 2013/0614 (2013.01); B64D 2013/0659 (2013.01); B64D 2013/0674 (2013.01); B64D 2013/0677 (2013.01); B64D 2013/0681 (2013.01); B64D 37/32 (2013.01); F05D 2220/323 (2013.01); F05D 2260/205 (2013.01); F05D 2260/211 (2013.01); F05D 2260/232 (2013.01); F05D 2260/60 (2013.01); F25J 2240/42 (2013.01); F25J 2240/80 (2013.01); F25J 2290/70 (2013.01);
Abstract

An engine-driven cryogenic cooling system for an aircraft includes a first air cycle machine, a second air cycle machine, and a means for condensing a chilled air stream into liquid air for an aircraft use. The first air cycle machine includes a plurality of components operably coupled to a gearbox of a gas turbine engine and configured to produce a cooling air stream based on a first engine bleed source of the gas turbine engine. The second air cycle machine is operable to output the chilled air stream at a cryogenic temperature based on a second engine bleed source cooled by the cooling air stream of the first air cycle machine.


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