초록 ▼

An unmanned aerial vehicle (UAV) has a payload or body affixed at one end of an elongated airfoil. The entire airfoil/payload combination rotates about a center of mass to define a rotor disk. Thrust is provided by air-augmented rocket engine thrusting tangentially at a location remote from the payl

An unmanned aerial vehicle (UAV) has a payload or body affixed at one end of an elongated airfoil. The entire airfoil/payload combination rotates about a center of mass to define a rotor disk. Thrust is provided by air-augmented rocket engine thrusting tangentially at a location remote from the payload. A control system maintains knowledge of its environment, as by a camera, to produce directional control signals which actuate lift control means in synchronism with the rotational position of the vehicle. A deployable object may be carried. Protection of the stowed vehicle is provided by blister packaging.

대표청구항 ▼

1. A monocopter, said monocopter comprising: an airfoil with a body attached to a first end of the airfoil, the body including an exterior surface;a propulsion device associated with said airfoil for rotating said air foil and said body, for thereby defining a rotor disk;a controller for causing lif

1. A monocopter, said monocopter comprising: an airfoil with a body attached to a first end of the airfoil, the body including an exterior surface;a propulsion device associated with said airfoil for rotating said air foil and said body, for thereby defining a rotor disk;a controller for causing lift adjustment of said airfoil to tilt the rotor disk; anda holder for a deployable payload object, the holder including at least one fixed wall extending outwardly from the exterior surface of said body, said wall and said exterior surface of said body defining a cavity of the body, said cavity dimensioned to accommodate said deployable payload object. 2. A monocopter according to claim 1, wherein said holder further includes: a retainer for retaining said deployable payload object within said cavity during stowed operation, and for releasing said deployable payload object from said cavity for deployment. 3. A monocopter according to claim 2, wherein said retainer comprises a latch which withdraws to release said deployable payload object. 4. A monocopter according to claim 2, wherein said retainer comprises a lip on said at least one wall. 5. A monocopter according to claim 2, wherein said retainer comprises an electromagnet.