Patent ID: 11932384
Assignee: WISK AERO LLC
Field: Transport (Mechanical engineering)
Classification: CPC B  G | IPC B  G

Claim 13:
14. An aircraft comprising:
a fuselage; and
a plurality of lift rotors disposed on a wing on each side of the fuselage, the plurality of lift rotors including a set of forward lift rotors provided forward of the wing and a set of aft lift rotors provided aft of the wing on each side of the fuselage,
wherein the set of forward lift rotors are coupled to the wing with a forward tilt,
wherein each lift rotor is oriented at a corresponding non-zero angle to a substantially horizontal plane of the aircraft, wherein the non-zero angle for at least two pairs of lift rotors on each side of the fuselage is such that the at least two pairs of lift rotors tilt toward the fuselage; and
wherein an outermost pair of lift rotors on each side of the fuselage is oriented at the non-zero angle relative to the substantially horizontal plane of the aircraft such that the outermost pair of lift rotors tilt outboard away from the fuselage.