Invention Grant
- Patent Title: Heat exchanger for a turbomachine and manufacturing thereof
-
Application No.: US17264636Application Date: 2019-07-30
-
Publication No.: US11754020B2Publication Date: 2023-09-12
- Inventor: Lancelot Guillou , Stéphane Louis Lucien Auberger
- Applicant: Safran Aircraft Engines
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: Christensen O'Connor Johnson Kindness PLLC
- Priority: FR 57152 2018.07.31
- International Application: PCT/FR2019/051871 2019.07.30
- International Announcement: WO2020/025895A 2020.02.06
- Date entered country: 2021-01-29
- Main IPC: F02K3/115
- IPC: F02K3/115 ; F01D25/12 ; F02C7/14 ; F28F1/02 ; F28F1/26

Abstract:
An annular heat exchanger for a turbomachine, is intended, for example, to be supported by an annular ferrule of a housing of the turbomachine, and includes an annular one-piece part having a first fluid circuit having at least one first conduit and at least one second conduit extending in an annular manner. The first conduit and the second conduit lead into a first cavity formed on a first circumferential end of said annular part, and the heat exchanger includes detachable sealing means which are applied to said first end and designed to allow a flow of fluid from the second conduit into the first cavity then into the first conduit.
Public/Granted literature
- US20210310443A1 HEAT EXCHANGER FOR A TURBOMACHINE AND MANUFACTURING THEREOF Public/Granted day:2021-10-07
Information query