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

Claim 13:
14. The aeronautical apparatus of claim 13, wherein:
the first landing element is one of a first landing foot and a first wheel having an axis of rotation parallel to the transverse axis;
the second landing element is one of a second landing foot and a second wheel having an axis of rotation parallel to the transverse axis;
the axis of rotation of the first propeller motor changes in response to rotation of the first thrust-angle motor;
the axis of rotation of the second propeller motor changes in response to rotation of the second thrust-angle motor;
the axis of rotation of the third propeller motor changes in response to rotation of the third thrust-angle motor; and
the axis of rotation of the fourth propeller motor changes in response to rotation of the fourth thrust-angle motor.