Invention Grant
- Patent Title: Turbine stage cooling
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Application No.: US14728991Application Date: 2015-06-02
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Publication No.: US10018360B2Publication Date: 2018-07-10
- Inventor: Gabriel L Suciu , Brian D Merry , James D Hill
- 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: F02C6/08
- IPC: F02C6/08 ; F23R3/10 ; F02C3/04 ; F01D5/08 ; F01D9/06 ; F01D25/12 ; F02C7/18

Abstract:
A turbine injection system for a gas turbine engine includes a first end operable to receive air from a heat exchanger, a second end operable to distribute mixed cooling air to a turbine stage, an opening downstream of said first end and a mixing plenum downstream of said first end and said opening. The opening provides a direct fluid pathway into said turbine injection system.
Public/Granted literature
- US20150354822A1 TURBINE STAGE COOLING Public/Granted day:2015-12-10
Information query
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