公开(公告)号：US20220250739A1

公开(公告)日：2022-08-11

申请号：US17585735

申请日：2022-01-27

申请人： Airspace Experience Technologies, Inc.

发明人： Jon Rimanelli ,  Gregory Peterson

IPC分类号： B64C17/02 ,  B64C37/00 ,  B64C1/16 ,  B60F5/02 ,  B60F3/00

摘要： A modular aircraft includes a plurality of structural elements. The structural elements include a pod module assembly, a wing assembly, and a chassis module. The pod module assembly is configured to be selectively attached to and detached from at least one of the chassis module and the wing module when the aircraft is not in flight. The pod module assembly is configured to transport at least one of a passenger and cargo.

公开(公告)号：US20220144421A1

公开(公告)日：2022-05-12

申请号：US17520929

申请日：2021-11-08

申请人： Airspace Experience Technologies, Inc.

发明人： Jon Rimanelli ,  Qhase Lokhandwala

IPC分类号： B64C29/00 ,  B64D27/24 ,  B64C3/38 ,  B64D31/00 ,  B64C25/10

摘要： An electrically powered vertical takeoff and landing aircraft (EVTOL) includes a payload module, a plurality of electrical power sources. a wing, and a plurality of electric thrust generators. The wing is pivotally attached to the payload module and is configured to pivot about a pivot axis, relative to the payload module, to transition between vertical flight and horizontal flight. The electric thrust generators are operatively attached to the wing, where each one is operatively connected to a different electrical power source. The electric thrust generators operate to provide thrust to the aircraft in response to receiving electric power from the electrical power sources. The electric thrust generators pivot, with the wing, about the pivot axis, relative to the payload.