公开(公告)号：US5056737A

公开(公告)日：1991-10-15

申请号：US499809

申请日：1990-03-27

Applicant: Douglas R. Taylor

Inventor： Douglas R. Taylor

IPC: B64C25/66 ,  B64C29/02 ,  B64C39/02 ,  B64F1/12

CPC classification number: B64C25/66 ,  B64C29/02 ,  B64C39/024 ,  B64F1/12 ,  B64C2201/048 ,  B64C2201/088 ,  B64C2201/104 ,  B64C2201/165 ,  B64C2201/167

Abstract: A vertical take-off and landing aircraft is configured so as to provide, when landing tail-first with its fuselage (1) in a generally vertical attitude, a touchdown area (21) at the tail of the aircraft at a position offset from a line extending along the length of the fuselage through the centre of gravity (23) of the aircraft such that after the touchdown area contacts a landing surface the aircraft topples under the action of gravity to bring an undercarriage (11, 13) of the aircraft into contact with the landing surface, thereby to attain a stable landed position.

Abstract translation: 垂直起飞和着陆飞机被配置为当其以机身（1）以大致垂直的姿态着陆尾部时，提供在飞行器尾部处的偏移的位置处的触地区域（21） 沿着机身的长度通过飞行器的重心（23）延伸，使得在着陆区域接触着陆表面之后，飞行器在重力作用下俯仰，使飞机的起落架（11,13）进入 与着陆面接触，从而达到稳定的着陆位置。

公开(公告)号：US3703998A

公开(公告)日：1972-11-28

申请号：US3703998D

申请日：1970-12-28

Applicant: TELEDYNE RYAN AERONAUTICAL CO

Inventor： GIRARD PETER F

IPC: B64C1/00 ,  B64C39/02 ,  B64C1/28 ,  B64C3/56

CPC classification number: B64C39/024 ,  B64C1/00 ,  B64C2001/0045 ,  B64C2201/048 ,  B64C2201/102 ,  B64C2201/121 ,  B64C2201/146 ,  B64C2201/162 ,  B64C2201/167

Abstract: A drone type aircraft having a telescopic fuselage and folding aerodynamic surfaces to facilitate installation in a limited capacity bomb bay or storage compartment of a launch aircraft. Prior to launch, the drone is lowered from the aircraft on a supporting frame, the aerodynamic surfaces are extended, and the nose section of the fuselage is extended. The added fuselage capacity is used as fuel tankage, which is filled from the launch aircraft to increase the operating range of the drone.

Abstract translation: 具有伸缩机身和折叠空气动力学表面的无人机型飞机，以便于安装在发射飞机的有限容量的炸弹舱或储藏室中。 在发射之前，无人机在支架上从飞机上下降，空气动力学表面延伸，机身的鼻部延伸。 增加的机身容量用作燃油箱，由发射机充满，以增加无人机的运行范围。

公开(公告)号：US3302908A

公开(公告)日：1967-02-07

申请号：US42180164

申请日：1964-12-29

Applicant: NORD AVIATION

Inventor： MICHEL LAZAREFF

IPC: B64C29/00 ,  B64C29/02 ,  B64C39/06

CPC classification number: B64C39/024 ,  B64C29/0091 ,  B64C29/02 ,  B64C39/062 ,  B64C2201/027 ,  B64C2201/048 ,  B64C2201/088 ,  B64C2201/108 ,  B64C2201/146 ,  B64C2201/162