Vertical-lift and horizontal flight aircraft

作者: Howard J. Carver

DOI:

关键词: Ground effect (aerodynamics)Adverse yawLift (soaring)Aerospace engineeringPropulsionEngineeringDragDissymmetry of liftThrustCyclic stress

摘要: A vertical-lift and horizontal flight aircraft, which can be operated in a mode, as soon ground clearance is made. And, because of its unique design very stable flight, light, has low drag resistance factor versatile the configurations that made from basic platform. The aircraft primarily disk shaped with body center surrounded by lift assembly housing, an outer surface propulsion thrust unit mounted aft central compartment. housing parallel contains inner drive ring, attached blades, facing inward toward compartment outward surface. Electromagnetic motors power each ring. assemblies are composed ring; ring guide-way electromagnetic motors. rings counter-rotate to alleviate any possible torque effect. Each controlled independently, synchronized achieve positive directional control. As rotate, blades move through air create lift. pitch fixed or variable. Once airborne forward motion attained, moving over provides for flight. An electric control mechanism will synchronize speed two counter-rotating purposes. This allow maintain steady course. Flight flaps direction aircraft.

参考文章(11)
Leonard W Grayson, Disc shaped aircraft ,(1955)
Gennady Ploshkin, Disc-shaped submersible aircraft ,(1995)
Alberto Kling, Rotor means for an aircraft ,(1976)
James P. Cycon, Christopher W. DeWitt, Mark Winfield Scott, Unmanned aerial vehicle with counter-rotating ducted rotors and shrouded pusher-prop ,(2000)
Raymond Jefferson, Rotary wing aircraft ,(1978)
Francis A Norman, Vertical lift aircraft ,(1967)