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:
May. 06, 2025
Filed:
Mar. 10, 2022
Applicant:
Rtx Corporation, Farmington, CT (US);
Inventor:
Michael Winter, New Haven, CT (US);
Assignee:
RTX CORPORATION, Farmington, CT (US);
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 13/08 (2005.12); B01D 45/08 (2005.12); B01D 53/00 (2005.12); B03C 1/28 (2005.12); B64D 13/06 (2005.12); B64D 27/12 (2005.12); B64D 33/08 (2005.12); B64D 37/32 (2005.12); F01D 15/00 (2005.12); F01D 25/12 (2005.12); F02C 6/08 (2005.12); F02C 7/141 (2005.12); F02C 7/143 (2005.12); F02C 7/16 (2005.12); F02C 7/18 (2005.12); F02C 9/18 (2005.12); F02K 3/06 (2005.12); F17C 7/02 (2005.12); F17C 7/04 (2005.12); F25B 9/14 (2005.12); F25J 3/04 (2005.12);
U.S. Cl.
CPC ...
B64D 13/08 (2012.12); B01D 45/08 (2012.12); B01D 53/002 (2012.12); B03C 1/288 (2012.12); B64D 13/06 (2012.12); B64D 27/12 (2012.12); B64D 33/08 (2012.12); F01D 15/00 (2012.12); F01D 25/12 (2012.12); F02C 6/08 (2012.12); F02C 7/141 (2012.12); F02C 7/143 (2012.12); F02C 7/16 (2012.12); F02C 7/185 (2012.12); F02C 9/18 (2012.12); F02K 3/06 (2012.12); F17C 7/02 (2012.12); F17C 7/04 (2012.12); F25B 9/14 (2012.12); F25J 3/04254 (2012.12); F25J 3/04975 (2012.12); B64D 2013/0614 (2012.12); B64D 2013/0659 (2012.12); B64D 2013/0674 (2012.12); B64D 2013/0677 (2012.12); B64D 2013/0681 (2012.12); B64D 37/32 (2012.12); F05D 2220/323 (2012.12); F05D 2260/205 (2012.12); F05D 2260/211 (2012.12); F05D 2260/232 (2012.12); F05D 2260/60 (2012.12); F25J 2240/42 (2012.12); F25J 2240/80 (2012.12); F25J 2290/70 (2012.12);
Abstract
A system for an aircraft includes an engine bleed source of a gas turbine engine. The system also includes a means for chilling an engine bleed air flow from the engine bleed source to produce a chilled working fluid. The system further includes a means for providing the chilled working fluid for an aircraft use.