A system (10) includes a primary heat exchanger (14) with a first passage connected to a hot fluid source (11), a second passage connected to the first passage, and a third passage connected to the second passage and an outlet line. A compressor inlet is connected to the outlet line. A secondary heat exchanger (38) is connected to a compressor outlet. First and second turbines (44,46) are connected to an outlet of the secondary heat exchanger. A first load heat exchanger (50) is connected to the first turbine. A second load heat exchanger (52) is between the second turbine and a system outlet (54). A first valve (22) connects the hot fluid source to the second and third passages. A second valve (24) connects the first and second passages with the outlet line. A third valve (56) is between the secondary heat exchanger and the second turbine. A fourth valve (58) is between the first load heat exchanger and the system outlet.
FLEXIBLE TURBINE ARRANGEMENT AIR CYCLE MACHINE WITH ADAPTIVE HEAT EXCHANGER
LUFTKREISLAUFMASCHINE MIT FLEXIBLER TURBINENANORDNUNG MIT ADAPTIVEM WÄRMETAUSCHER
MACHINE À CYCLE D'AIR D'AGENCEMENT DE TURBINE FLEXIBLE DOTÉ D'UN ÉCHANGEUR DE CHALEUR ADAPTATIF
01.05.2024
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
FLEXIBLE TURBINE ARRANGEMENT AIR CYCLE MACHINE WITH ADAPTIVE HEAT EXCHANGER
Europäisches Patentamt | 2022
|Flexible turbine arrangement air cycle machine with adaptive heat exchanger
Europäisches Patentamt | 2022
|