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Detachable cabin aircraft

阅读：243发布：2021-03-14

专利汇可以提供Detachable cabin aircraft专利检索，专利查询，专利分析的服务。并且A delta-wing air craft comprises a main wing and a pilot''s cabin section forwardly of the main wing, the pilot''s section being detachable from the main wing and including a pair of auxiliary wings pivotably mounted about a vertical axis of the aircraft. The auxiliary wings form the apex of the delta-wing in the attached position of the cabin section, and are pivotable to a deployed position when the cabin section is detached to provide a glider wing surface for the detached cabin section.，下面是Detachable cabin aircraft专利的具体信息内容。

权利要求

1. An aircraft comprising a main delta-wing section and a pilot''s cabin section forwardly of the main delta-wing section, said pilot''s cabin section being detachable from the main deltawing section and including a pair of auxiliary wings substantially coplanar with the main delta-wing section and pivotably mounted about a vertical axis of the aircraft, said auxiliary wings being pivoted from a retracted position when the cabin section is attached to the main delta-wing section, to a deployed position when the cabin section is detached from the main delta-wing section, said auxiliary wings in the retracted position being pivoted rearwardly and forming the apex and leading edge of the main delta-wing section, said auxiliary wings in the deployed position being pivoted forwardly and providing an increased glider wing surface for the detached cabin section.

2. An aircraft according to claim 1, wherein said auxiliary wings each includes two sections pivotably mounted to each other about a vertical axis of the aircraft to form foldable inner and outer sections, the outer sections being movable from a retracted position at cruising speeds to a deployed position at lower speeds or at the time the cabin is detached from the aircraft, and the inner sections being movable from a retracted position at cruising or lower speeds to a deployed position at the time the cabin is detached from the aircraft.

3. An aircraft according to claim 1, wherein said aircraft includes a further pair of auxiliary wings carried by and pivotably mounted to the main delta-wing from a retracted position at cruising speeds to a deployed position at lower speeds.

4. An aircraft according to claim 1, wherein said detachable cabin section includes a parachute for stabilizing same when detached from the aircraft.

5. An aircraft according to claim 1, wherein said detachable cabin section further includes a rocket to provide power for reclimbing.

6. An aircraft according to claim 1, wherein said detachable cabin section further includes a rudder for direction control.

7. An aircraft according to claim 1, wherein said detachable cabin section further includes a tail foldable against the cabin section when attached to the aircraft.

8. An aircraft according to claim 1, wherein said detachable cabin section further includes pivotable front elevators for longitudinal control.

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