Invention Grant
- Patent Title: Heat exchanger system for an aircraft turbomachine
-
Application No.: US15117904Application Date: 2015-02-10
-
Publication No.: US10677165B2Publication Date: 2020-06-09
- Inventor: Amandine Roche
- Applicant: Safran Power Units
- Applicant Address: FR Toulouse
- Assignee: SAFRAN POWER UNITS
- Current Assignee: SAFRAN POWER UNITS
- Current Assignee Address: FR Toulouse
- Agency: Pearne & Gordon LLP
- Priority: com.zzzhc.datahub.patent.etl.us.BibliographicData$PriorityClaim@1f0c0642
- International Application: PCT/FR2015/050316 WO 20150210
- International Announcement: WO2015/121576 WO 20150820
- Main IPC: F02C7/18
- IPC: F02C7/18 ; F02C7/047 ; F02C7/04 ; F02C7/055

Abstract:
A heat exchange system in a turbomachine that comprises a plurality of members and equipment to be cooled and/or lubricated, the heat exchange system includes a fluid circuit for cooling and/or lubricating the equipment, the heat exchange system being configured to bring the fluid circuit in thermal contact with a fluid, wherein the heat exchange system further includes an open work structure which is in thermal contact with at least one hot section of the fluid circuit and through which the fluid passes.
Public/Granted literature
- US20160369699A1 HEAT EXCHANGER SYSTEM Public/Granted day:2016-12-22
Information query
IPC分类: