|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||F02C-006/00 F02G-001/00 F02G-003/00|
|미국특허분류(USC)||060/039.15; 060/039.163; 060/791; 060/039.17|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 4 인용 특허 : 27|
A convertible gas turbine propulsion system operates in multiple output modes. The convertible gas turbine propulsion system comprises a gas generator, a first power turbine, a secondary propulsion system and an exhaust duct. The gas generator is configured to produce exhaust gas. The first power turbine is aligned with the gas generator to receive the exhaust gas. The secondary propulsion system is in series with the gas generator and the first power turbine. The exhaust duct coaxially extends from the first power turbine to the secondary propulsion sys...
1. A convertible gas turbine propulsion system operable in multiple output modes, the propulsion system comprising: a gas generator for producing exhaust gas;a gas generator turbine driven by the exhaust gas;a first power turbine aligned in series with the gas generator turbine to receive the exhaust gas;a primary propulsion system coupled to the first power turbine and configured to produce thrust in a first axial direction;a secondary propulsion system in series with the gas generator turbine and the first power turbine, such that the propulsion system...