Invention Grant
- Patent Title: Compressor core inner diameter cooling
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Application No.: US14967518Application Date: 2015-12-14
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Publication No.: US10330010B2Publication Date: 2019-06-25
- Inventor: Gabriel L. Suciu , Brian D. Merry , Jesse M. Chandler , William K. Ackermann , Matthew R. Feulner , Om P. Sharma
- 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: F02C7/18
- IPC: F02C7/18 ; F02C7/143 ; F02C9/18 ; F02C3/04 ; F02K3/06 ; F01D5/08 ; F04D29/58

Abstract:
A compressor section for use in a gas turbine engine comprises a compressor rotor having a hub and a plurality of blades extending radially outwardly from the hub and an outer housing surrounding an outer periphery of the blades. A tap taps air at a radially outer first location, passing the tapped air through a heat exchanger, and returning the tapped air to an outlet at a second location which is radially inward of the first location, to provide cooling air adjacent to the hub. A gas turbine engine is also disclosed.
Public/Granted literature
- US20170167384A1 COMPRESSOR CORE INNER DIAMETER COOLING Public/Granted day:2017-06-15
Information query
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