A propulsion system (14,16) including a gas turbine engine (20) and a nacelle (18) surrounding a portion of the gas turbine engine. The propulsion system further includes a heat exchanger (36), which is arranged within a strut (24) connecting the gas turbine engine and the nacelle, adapted to cool fluid from the gas turbine engine.
HEAT EXCHANGER FOR A GAS TURBINE ENGINE PROPULSION SYSTEM
WÄRMETAUSCHER FÜR EIN GASTURBINENMOTORANTRIEBSSYSTEM
ÉCHANGEUR DE CHALEUR POUR UN SYSTÈME DE PROPULSION DE MOTEUR À TURBINE À GAZ
2020-04-08
Patent
Electronic Resource
English
IPC: | F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES |
HEAT EXCHANGER FOR A GAS TURBINE ENGINE PROPULSION SYSTEM
European Patent Office | 2021
|Heat exchanger for a gas turbine engine propulsion system
European Patent Office | 2020
|HEAT EXCHANGER ASSEMBLY FOR A GAS TURBINE ENGINE PROPULSION SYSTEM
European Patent Office | 2018
|Heat exchanger assembly for a gas turbine engine propulsion system
European Patent Office | 2019
|