Invention Application
- Patent Title: METHOD AND SYSTEM FOR COOLING AIRCRAFT ENGINE FLUID
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Application No.: US14937266Application Date: 2015-11-10
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Publication No.: US20170130606A1Publication Date: 2017-05-11
- Inventor: Daniel Alan Niergarth , Brandon Wayne Miller , Kyle Robert Snow , Christopher James Kroger
- Applicant: General Electric Company
- Main IPC: F01D25/12
- IPC: F01D25/12 ; F04D29/32 ; F01D25/24 ; F01D25/20 ; F01D25/16

Abstract:
A self-contained lubrication fluid circulation system for use with a gas turbine engine defining a core air flowpath includes a sump configured to collect lubrication fluid and a heat source coupled in fluid communication with the sump and configured to transfer heat to the lubrication fluid. The system also includes a heat sink positioned within the sump and coupled in fluid communication with the heat source. A lubrication fluid conduit of the system is configured to channel the lubrication fluid between the heat source and the heat sink, wherein the lubrication fluid conduit is positioned entirely within the sump.
Public/Granted literature
- US10539076B2 Self-contained lubrication cooling system with heat exchanger integrated with sump Public/Granted day:2020-01-21
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