Invention Grant
- Patent Title: Gas turbine engine heat exchanger system
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Application No.: US14104299Application Date: 2013-12-12
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Publication No.: US09915202B2Publication Date: 2018-03-13
- Inventor: Eric S. Donovan , Daniel J. Vonderwell , Craig Heathco
- Applicant: Rolls-Royce North American Technologies, Inc.
- Applicant Address: US IN Indianapolis
- Assignee: Rolls-Royce North American Technologies, Inc.
- Current Assignee: Rolls-Royce North American Technologies, Inc.
- Current Assignee Address: US IN Indianapolis
- Agency: Fishman Stewart PLLC
- Main IPC: F02C7/05
- IPC: F02C7/05 ; F02C7/052 ; F02C7/12

Abstract:
An apparatus includes a gas turbine engine and a heat transfer system. The gas turbine engine includes an inlet particle separator that separates inlet air into scavenge air and clean air. A scavenge air path conveys the scavenge air from the inlet particle separator to the heat transfer system. A heat exchange fluid path conveys a heat exchange fluid to the heat transfer system and a cooled heat exchange fluid away from the heat transfer system. The heat transfer system is configured to transfer heat from the heat exchange fluid path to the scavenge air path to cool the heat exchange fluid.
Public/Granted literature
- US20140356125A1 GAS TURBINE ENGINE HEAT EXCHANGER SYSTEM Public/Granted day:2014-12-04
Information query
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