发明名称 |
Aircraft with vertical take-off and landing, has at least two propellers in aerofoil driven by gas stream from turbine air jet engine |
摘要 |
The aircraft ahs a turbine air jet engine fixed in the longitudinal axis of the aircraft. The engine generates thrust using a primary air jet. A secondary jet provides lift. The turbine air jet engine outputs a gas stream which drives a blower (propeller) by means of aerostatic or aerodynamic motors on its axes. The number of propellers in the aerofoil exceeds two.
|
申请公布号 |
DE19950723(A1) |
申请公布日期 |
2001.05.10 |
申请号 |
DE19991050723 |
申请日期 |
1999.10.19 |
申请人 |
BACH, JOACHIM |
发明人 |
BACH, JOACHIM |
分类号 |
B64C29/00;(IPC1-7):B64C29/00;B64C27/20 |
主分类号 |
B64C29/00 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|