Patent ID: 11964756
Assignee: AERHART, LLC
Field: Transport (Mechanical engineering)
Classification: CPC B  G | IPC B  G

Claim 0:
1. An aeronautical apparatus, comprising:
a fuselage having a longitudinal axis and a transverse axis;
a first wing coupled to a right side of the fuselage;
a second wing coupled to a left side of the fuselage;
first and second thrust-angle motors having an axis of rotation parallel to the transverse axis of the fuselage with the first and second thrust-angle motors coupled to a tip of the first and second wings, respectively;
a first assembly coupled to the first thrust-angle motor; and
a second assembly coupled to the second thrust-angle motor, wherein:
the first assembly comprises: a first propeller motor with a first propeller coupled thereto and a first landing element;
the second assembly comprises: a second propeller motor with a second propeller coupled thereto and a second landing element;
the axis of rotation of the first propeller motor changes in response to rotation of the first thrust-angle motor; and
the axis of rotation of the second propeller motor changes in response to rotation of the second thrust-angle motor.