公开(公告)号：US20240253763A1

公开(公告)日：2024-08-01

申请号：US18101914

申请日：2023-01-26

申请人： JETZERO, INC.

发明人： John Vassberg ,  Blaine Rawdon

IPC分类号： B64C1/16 ,  B64C39/10 ,  B64D27/26 ,  B64D29/04 ,  B64F5/10

CPC分类号： B64C1/16 ,  B64C39/10 ,  B64D27/40 ,  B64D29/04 ,  B64F5/10

摘要： A system for providing favorable environment for propulsion system of a blended wing body aircraft, wherein the system comprises a blended wing body, wherein the blended wing body comprises a main body, wherein the main body comprises a main body shaping comprising an upper aft surface configured to provide a favorable environment for a propulsion system of the blended wing body aircraft, and the propulsion system mounted to the upper aft surface of the main body, wherein the propulsion system comprises one or more prime movers, and a nacelle covering the one or more prime movers.

公开(公告)号：US20240253781A1

公开(公告)日：2024-08-01

申请号：US18101836

申请日：2023-01-26

申请人： JETZERO, INC.

发明人： Blaine Rawdon

IPC分类号： B64C39/10 ,  B64C1/20 ,  B64C1/22 ,  B64D37/04

CPC分类号： B64C39/10 ,  B64D39/00 ,  B64C2039/105

摘要： Aspects relate to blended wing body aircraft having a passenger compartment. Blended wing body aircraft may include a freighter aircraft, a tanker aircraft, a passenger aircraft, or the like. Blended wing body aircraft may include an upper seating area, such as a passenger compartment, configured to accommodate passengers or personnel of aircraft without sacrificing space of a main region of a fuselage of the aircraft.

公开(公告)号：US20240253760A1

公开(公告)日：2024-08-01

申请号：US18101877

申请日：2023-01-26

申请人： JETZERO, Inc.

发明人： Blaine Rawdon

IPC分类号： B64C1/06 ,  B64C1/10 ,  B64C1/12 ,  B64C39/10

CPC分类号： B64C1/061 ,  B64C1/10 ,  B64C1/12 ,  B64C39/10 ,  B64C2039/105

摘要： An airframe of a blended wing body aircraft with a non-cylindrical pressure vessel and methods of manufacture. The airframe includes a plurality of longitudinal stiffeners running substantially parallel to a longitudinal axis of the airframe and extending from a top side of the airframe to a bottom side of the airframe. The airframe includes at least a laterally outermost bulkhead configured to resist a cabin pressure. The airframe includes a skin comprising an outer mold line of the airframe that is configured to attach to the plurality of longitudinal stiffeners at the top side of the airframe and the bottom side of the airframe. In some embodiments, the airframe may include an aft pressure bulkhead.