发明名称 |
ИМПУЛЬСНАЯ ДЕТОНАЦИОННАЯ СИСТЕМА ДЛЯ ГАЗОТУРБИННОГО ДВИГАТЕЛЯ И ГАХОТУРБИННЫЙ ДВИГАТЕЛЬ С ТАКОЙ СИСТЕМОЙ |
摘要 |
A pulse detonation system (12) for a gas turbine engine (10) includes a core engine (30). The pulse detonation system is downstream from the core engine and is configured to create a temperature rise and a pressure rise within the gas turbine engine and to increase engine thrust. The pulse detonation system comprises a multi-staged pulse detonation augmentor (60) that comprises a predetonator (48) operable with at least a first operating stage wherein a less-than-stoichiometric fuel-air mixture is provided to the predetonator. <IMAGE> |
申请公布号 |
RU2003136814(A) |
申请公布日期 |
2005.05.20 |
申请号 |
RU20030136814 |
申请日期 |
2003.12.19 |
申请人 |
ДЖЕНЕРАЛ ЭЛЕКТРИК КОМПАНИ (US) |
发明人 |
КОШОФФЕР Джон Майкл (US) |
分类号 |
F02C5/10;F02K1/00;F02K3/075;F02K3/08;F02K7/04;F02K7/06;F02K7/075;F23R7/00 |
主分类号 |
F02C5/10 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|