Invention Grant
- Patent Title: Intercooled compressor for a gas turbine engine
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Application No.: US14677539Application Date: 2015-04-02
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Publication No.: US09611744B2Publication Date: 2017-04-04
- Inventor: Jack R. Taylor
- Applicant: Betty Jean Taylor
- Agency: Hasse & Nesbitt LLC
- Agent Daniel F. Nesbitt
- Main IPC: F04D29/58
- IPC: F04D29/58 ; F01D5/18 ; F04D29/54

Abstract:
A multi-stage intercooled compressor for a gas turbine engine, including multiple stages of rotating blades and cooling stator vanes, a cooling stator vane including an outer wall that defines an internal coolant fluid passage and has a length along a centerline from a leading edge to a trailing edge of the outer wall, and an internal flow divider wall disposed within the internal passage and extending along the centerline to divide the internal coolant fluid passage into an inflow pathway and an outflow pathway.
Public/Granted literature
- US20160010498A1 Intercooled Compressor for a Gas Turbine Engine Public/Granted day:2016-01-14
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