Zobrazeno 1 - 3
of 3
pro vyhledávání: '"B. Kh. Perel'shtein"'
Publikováno v:
Russian Aeronautics. 61:687-691
The approaches to integration of a high-pressure super-reaction turbine of an aircraft gas turbine engine and a gas-dynamic laser are considered.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4c3464fc390db7c9f59fa972653feb09
https://doi.org/10.3103/s1068799818040293
https://doi.org/10.3103/s1068799818040293
Publikováno v:
Russian Aeronautics. 60:474-477
We consider a turbofan engine (TFE), where the turbine rotor blades of the low pressure turbine (LPT) are micro-Laval nozzles. We demonstrated the possibility of integrating the super jet turbine and a jet nozzle as a single binary system for the pur
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6b9b8541ab7f114022d359b3b3935f83
https://doi.org/10.3103/s1068799817030230
https://doi.org/10.3103/s1068799817030230
Publikováno v:
Russian Aeronautics (Iz VUZ). 50:430-435
The air heat pump (HP) driven from GTP, created on the basis of aircraft GTE removed from service, is considered. The heat pump uses ambient air from negative (−40 °C) to positive (+15 °C) temperature values as a low-grade heat source and provide
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1c36cd6c51cfc5d668b21e05e72cb5c7
https://doi.org/10.3103/s1068799807040149
https://doi.org/10.3103/s1068799807040149