Invention Grant
- Patent Title: Oil cooling system for aircraft engine
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Application No.: US17350250Application Date: 2021-06-17
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Publication No.: US11591964B2Publication Date: 2023-02-28
- Inventor: Andrew Walz , Ritchie Domingo
- Applicant: PRATT & WHITNEY CANADA CORP.
- Applicant Address: CA Longueuil
- Assignee: PRATT & WHITNEY CANADA CORP.
- Current Assignee: PRATT & WHITNEY CANADA CORP.
- Current Assignee Address: CA Longueuil
- Agency: Norton Rose Fulbright Canada LLP
- Main IPC: F02C7/14
- IPC: F02C7/14 ; F02C7/06

Abstract:
An oil cooling system for an aircraft engine, a bypass valve and an associate method of cooling aircraft engine oil are provided. The oil cooling system includes a heat exchanger having an inlet and an outlet. The inlet is in fluid communication with a first oil conduit to receive a first oil flow from the first oil conduit. The heat exchanger facilitates heat transfer from the first oil flow to another fluid. A flow restrictor defining a constriction is operatively disposed to restrict the first oil flow through the heat exchanger. A second oil conduit receives the first oil flow from the heat exchanger. A bypass oil passage provides fluid communication between the first oil conduit and the second oil conduit to allow a second oil flow received from the first oil conduit to flow to the second oil conduit and bypass the heat exchanger.
Public/Granted literature
- US20220403779A1 OIL COOLING SYSTEM FOR AIRCRAFT ENGINE Public/Granted day:2022-12-22
Information query
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