VERTICAL TAKE OFF AND LANDING VEHICLE
VERTICAL TAKE OFF AND LANDING VEHICLE
- Neue Suche nach: ROSS EDWIN ANTON
- Neue Suche nach: JOORE HANS
- Neue Suche nach: STEKELENBURG MICHAEL ALWIN WILLIAM
- Neue Suche nach: DINGEMANSE LOURENS JACOBUS
- Neue Suche nach: ROSS EDWIN ANTON
- Neue Suche nach: JOORE HANS
- Neue Suche nach: STEKELENBURG MICHAEL ALWIN WILLIAM
- Neue Suche nach: DINGEMANSE LOURENS JACOBUS
A flying vehicle (1) comprises: - a body (10) having a tail section (20); - a main rotor (100) having a rotation axis on top of the body; - a central thrust unit (200) arranged along the longitudinal axis of the vehicle, at a distance from the rotation axis of the main rotor; - a mounting support (40) on either side of the body; - a side thrust unit (400) mounted to each mounting support. The central thrust unit comprises a fan which provides air flow with a flow component perpendicular to a virtual vertical midplane of the vehicle. Each of said side thrust units comprises a fan which provides air flow with a flow component parallel to said virtual vertical midplane. At least one of said thrust units is provided with controllable air deflection means (420) to deflect the corresponding output air flow in a controllable manner.
飞行载具(1)，包括：机身(10)，该机身(10)具有尾部(20)；主旋翼(100)，该主旋翼(100)的旋转轴位于机身(10)的顶部；中央推力单元(200)，该中央推力单元(200)沿载具(1)的纵轴布置，与主旋翼(100)的旋转轴保持一定距离；位于机身任意侧的安装支撑件(40)；安装在每个安装支撑件(40)上侧推力单元(400)；中央推力单元包括风扇，该风扇提供至少一个垂直于载具虚拟垂直中平面的气流分量；每个侧推力单元包括风扇，该风扇提供至少一个平行于所述虚拟垂直中平面的气流分量的气流；推力单元中的至少一个设置有可控气流偏转装置(420)，所述可控气流偏转装置(420)以可控方式偏转相应的输出气流。
Dokumentinformationen
VERTICAL TAKE OFF AND LANDING VEHICLE
垂直起降载具
2021-10-15
Patent
Elektronische Ressource
Chinesisch
| IPC: | B64C AEROPLANES , Flugzeuge |