Invention Grant
- Patent Title: Complex air supply system for gas turbine engine and associated aircraft
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Application No.: US15823639Application Date: 2017-11-28
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Publication No.: US10914242B2Publication Date: 2021-02-09
- Inventor: Joseph Brent Staubach , Nathan Snape , Frederick M. Schwarz , Charles E. Lents , Michael K. Ikeda
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Farmington
- Agency: Carlson, Gaskey & Olds, P.C.
- Main IPC: F02C9/18
- IPC: F02C9/18 ; F02C7/18 ; B64D33/02 ; B64D13/00 ; F02C7/14 ; F02C7/32 ; F02C7/224 ; F02C3/04 ; F02C7/22 ; B64D13/06

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.
Public/Granted literature
- US20190162121A1 COMPLEX AIR SUPPLY SYSTEM FOR GAS TURBINE ENGINE AND ASSOCIATED AIRCRAFT Public/Granted day:2019-05-30
Information query
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