旋回する回転翼及び収容される回転翼羽根を有する空気力学的に効率の良い軽量の垂直離着陸航空機

Title:

旋回する回転翼及び収容される回転翼羽根を有する空気力学的に効率の良い軽量の垂直離着陸航空機

Document Type and Number:

Japanese Patent JP6878555

Kind Code:

B2

Abstract:

An aerial vehicle adapted for vertical takeoff and landing using a set of wing mounted thrust producing elements and a set of tail mounted rotors for takeoff and landing. An aerial vehicle which is adapted to vertical takeoff with the rotors in a rotated, take-off attitude then transitions to a horizontal flight path, with the rotors rotated to a typical horizontal configuration. The aerial vehicle uses different configurations of its wing mounted rotors and propellers to reduce drag in all flight modes.

Inventors:

Joe Ben Bivert
Alex stall

Application Number:

JP2019213745A

Publication Date:

May 26, 2021

Filing Date:

November 26, 2019

Export Citation:

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