Invention Grant
- Patent Title: Reversible system for dissipating thermal power generated in a gas-turbine engine
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Application No.: US16302184Application Date: 2017-05-19
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Publication No.: US10794231B2Publication Date: 2020-10-06
- Inventor: Samer Maalouf
- Applicant: SAFRAN
- Applicant Address: FR Paris
- Assignee: SAFRAN
- Current Assignee: SAFRAN
- Current Assignee Address: FR Paris
- Agency: Oblon, McClelland, Maier & Neustadt, L.L.P.
- Priority: com.zzzhc.datahub.patent.etl.us.BibliographicData$PriorityClaim@570af58b
- International Application: PCT/FR2017/051223 WO 20170519
- International Announcement: WO2017/198965 WO 20171123
- Main IPC: F01K25/02
- IPC: F01K25/02 ; F01K15/00 ; F02C7/14 ; F02C7/141 ; F02C7/16 ; F02C7/18 ; F02C1/10

Abstract:
A reversible system for dissipating heat power generated in a gas turbine engine, the system including a condenser-forming first heat exchanger, an evaporator-forming second heat exchanger, a scroll compressor suitable for operating as a compressor when the temperature of the cold source is higher than a predefined threshold temperature and as a turbine when the temperature of the cold source is lower than the threshold temperature, an expander and a pump arranged in parallel, and a control valve arranged upstream from the expander and the pump and suitable for directing the refrigerant fluid to the expander when the temperature of the cold source is higher than the threshold temperature and to the pump when the temperature of the cold source is lower than the threshold temperature.
Public/Granted literature
- US20190277165A1 REVERSIBLE SYSTEM FOR DISSIPATING THERMAL POWER GENERATED IN A GAS-TURBINE ENGINE Public/Granted day:2019-09-12
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