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Document |
Document Title |
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7252265 |
Microaircraft and cellular phone equipped with microaircraft
An aircraft which is attachable to, for example, a cellular phone. The aircraft is provided with at least four rotors actuated with compressed fluid or by ring-shaped electric motors.
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6869042 |
System for airborne launch of an aircraft from a larger carrier aircraft
A system for launching, refuelling and recovering in flight an aircraft ( 10 ) such as an unmanned aerial vehicle (UAV) from a larger carrier aircraft ( 16 ) comprising a holder ( 22 ) on the...
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6793172 |
Lightweight remotely controlled aircraft
An aircraft which is designed for remote controlled slow flight, indoor or in a small outdoor yard or field. The aerial lifting body is defined by a series of lightweight planar or thin airfoil...
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6615165 |
Cable connections between an unmanned aircraft and a detachable data handling module
A power and communications connection arrangement for a miniature, unmanned aircraft having data handling capability. The aircraft has a microprocessor for managing flight control, a GPS receiver,...
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6488232 |
Single passenger aircraft
Disclosed is a single passenger aircraft configured to vertically take-off and land. An airframe is configured to support the passenger in an upright position during take-off and landing and during...
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5303695 |
Human free-flight launcher
A human free-flight launcher including a seat positioned within a tetrahedral frame and supported therein by elasticized cords which, upon retraction of the seat within the interior of the...
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4704732 |
Method of suspending a platform for communications and observation kept at high altitude by atmospheric molecular momentum transfer
The instant invention comprises a method for freely suspending without any solid material support, a platform in an atmosphere by atmospheric-particle-momentum transfer having opposite surface...
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4634080 |
Parafoil vertical lift mechanism
The invention is an improved method and device for utilizing the principles of lift achieved through the dynamic physics of the airfoil. In the case of the present invention, the airfoil utilized...
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4498645 |
Wingless aircraft with ducted variable pitch airfoils
A wingless aircraft having a power channel with two parallel ducts afixed to the top of the fuselage. A jet engine or other drive mechanism is positioned within each duct. No air flow is permitted...
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3773278 |
AERIAL BUOY FOR POSITION LOCATING
An aerial buoy including a frusto-conically shaped member, a tubular member extending coaxially therewith and upwardly therefrom, and a longitudinally extending support tube extending downwardly...
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3580528 |
MANEUVERING UNIT
A hand-held device for propelling an individual through space wherein pressurized fluid is selectively and individually discharged from oppositely directed coplanar nozzles in response to movement...
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3559922 |
FLYING PLATFORM CONSTRUCTION
A flying platform type of helicopter. A generally vertical, nonrotating main shaft has the platform affixed to its upper end and a landing gear attached to its lower end. A rotor member is...
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3490721 |
GRAVITY STABILIZED FLYING VEHICLE
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3474987 |
HELICOPTER DEVICE
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3273824 |
Single passenger aircraft
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3138350 |
Ducted fan aircraft and engine
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3098625 |
Rocket motor and control system
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3021095 |
Propulsion unit
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2920841 |
Helicopter with body attaching means
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2824711 |
Vehicle for testing control systems at supersonic speeds
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D114533 |
Title is not available
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3820743 |
Title is not available
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