发明名称 |
Jumbo aircraft, in particular of high-wing monoplane design |
摘要 |
This invention relates to an improvement in a jumbo aircraft, in particular of high-wing monoplane design, with a fuselage and a retractable and steerable main landing gear and a device for high lift generation, the improvement comprising (a) a plurality of rows of landing gear units mounted along the aircraft fuselage and spread across a range extending predominantly in the longitudinal aircraft direction, the units forming the main landing gear, (b) the landing gear units being of the same design and identical dimensions, and (c) a device for switching-on the lift generating device at predetermined lift conditions together with setting and maintaining a longitudinal attitude of the aircraft or of its landing gear parallel to the taxiway and runway, whereby the take-off phase or the landing phase is performed using the method of direct lift control.
|
申请公布号 |
US4638962(A) |
申请公布日期 |
1987.01.27 |
申请号 |
US19800135548 |
申请日期 |
1980.03.31 |
申请人 |
DORNIER GMBH |
发明人 |
GUENTER, HEINZ;KRIECHBAUM, GERHARD;KROJER, HUBERT;MATECKI, RUDOLF;SPINTZYK, JOHANNES |
分类号 |
B64C25/10;(IPC1-7):B64C13/16;B64C25/04 |
主分类号 |
B64C25/10 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|