VERTICAL TAKE-OFF AND LANDING (VTOL) AIRCRAFT

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VERTICAL TAKE-OFF AND LANDING (VTOL) AIRCRAFT

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MELO ADILSON / CASTELLI ALBERTO DEI / ZARONI FABIO / CURSINO FELIPE NAHIME / VIANNA FERNANDO RODRIGUES / SILVA FLAVIA RENATA DANTAS ALVES / CARVALHO GERALDO / RODRIGUES IGOR MIRANDA / GRAVES JULIO CESAR / JUNIOR LUIZ ANTONIO MADEIRA / ... [more]

Abstract

The invention relates to a vertical takeoff and landing (VTOL) aircraft. The VTOL aircraft, especially electric VTOL (e-VTOL) aircraft include a fuselage (which may include a pair of ground-engaging skids) defining a longitudinal axis of the aircraft, forward and aft pairs of port and starboard aerodynamic wings extending laterally outwardly from the fuselage and forward and aft pairs of port andstarboard rotor pods each being in substantial alignment with the longitudinal axis of the fuselage. In specific embodiments, each of the forward and aft pairs of port and starboard rotor pods comprises a forward and aft pair of rotor assemblies.

本发明涉及垂直起降(VTOL)飞机。垂直起降(VTOL)飞机、特别是电动VTOL(e‑VTOL)飞机包括机身(该机身可包括一对地面接合滑轨)，该机身限定了飞机的纵向轴线；前对左舷和右舷空气动力学机翼以及后对左舷和右舷空气动力学机翼，这些空气动力学机翼从机身侧向向外延伸；以及前对左舷和右舷旋翼吊舱以及后对左舷和右舷旋翼吊舱，每个旋翼吊舱均与机身的纵向轴线基本对齐。在特定实施例中，前对左舷和右舷旋翼吊舱和后对左舷和右舷旋翼吊舱中的每个旋翼吊舱均包括前后一对旋翼组件。

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Title :

VERTICAL TAKE-OFF AND LANDING (VTOL) AIRCRAFT

Additional title:

垂直起降(VTOL)飞机

Contributors:

MELO ADILSON (author) / CASTELLI ALBERTO DEI (author) / ZARONI FABIO (author) / CURSINO FELIPE NAHIME (author) / VIANNA FERNANDO RODRIGUES (author) / SILVA FLAVIA RENATA DANTAS ALVES (author) / CARVALHO GERALDO (author) / RODRIGUES IGOR MIRANDA (author) / GRAVES JULIO CESAR (author) / JUNIOR LUIZ ANTONIO MADEIRA (author)

Publication date :

2020-11-10

Type of media :

Patent

Type of material :

Electronic Resource

Language :

Chinese

Classification :

IPC:

B64C AEROPLANES , Flugzeuge