Invention Grant
- Patent Title: Integrated heat exchangers for low fan pressure ratio geared turbofan
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Application No.: US15953791Application Date: 2018-04-16
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Publication No.: US10781772B2Publication Date: 2020-09-22
- Inventor: Gary D. Roberge
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: RAYTHEON TECHNOLOGIES CORPORATION
- Current Assignee: RAYTHEON TECHNOLOGIES CORPORATION
- Current Assignee Address: US CT Farmington
- Agency: Cantor Colburn LLP
- Main IPC: F02K3/115
- IPC: F02K3/115 ; F02K3/105 ; F02C7/06 ; F01D9/06 ; F02K3/06 ; F02C7/14 ; F02C7/18

Abstract:
An oil cooling system and method are provided for use with respect to a lubricated mechanical system within a bypass configured gas turbine engine. A surface cooler is fluidly linked to the lubricated mechanical system to receive oil from the lubricated mechanical system for cooling and reuse. In an embodiment, the surface cooler is mounted on an existing surface within the bypass airflow path of the bypass configured gas turbine engine to provide effective cooling while avoiding the introduction of additional aerodynamic disturbances in the bypass path. In an embodiment, the surface cooler is mounted on the fan casing or on a fan exit guide vane.
Public/Granted literature
- US20180238270A1 INTEGRATED HEAT EXCHANGERS FOR LOW FAN PRESSURE RATIO GEARED TURBOFAN Public/Granted day:2018-08-23
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