发明名称 |
Aircraft and propulsion system for an aircraft, and operating method |
摘要 |
The invention relates to a propulsion system for aircraft, especially for high-flying and long-distance flying unmanned aircraft, to the aircraft itself and to a method for controlling aircraft. Said propulsion system has a first jet turbine engine and a second jet turbine engine (22, 24). The invention also provides that the first jet turbine engine is a turbine engine (22) and the second jet turbine engine is an airscrew turbine engine (24). Said airscrew turbine engine (24) remains non-operational at least during the process for starting the aircraft (10).
|
申请公布号 |
US2004031880(A1) |
申请公布日期 |
2004.02.19 |
申请号 |
US20030275211 |
申请日期 |
2003.08.04 |
申请人 |
STEMME REINER;KAUFFMANN KONRAD |
发明人 |
STEMME REINER;KAUFFMANN KONRAD |
分类号 |
B64C39/02;B64D27/02;(IPC1-7):B64D27/00 |
主分类号 |
B64C39/02 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|