ELECTRIC ROTARY WING AIRCRFTS. [3290] Field of invention relates to rotary wing aircrafts and the like. This invention relates to vertical propulsion turbine motors and generators combined including a digital glass cabin and manual navigation controllers consisting of a sphere or ball mounting in bearing in the stator casing and electrically connected with the flyby wire system. Helicopters and modern rotary wing aircraft and more particularly to helicopters with reduced blade length and increased speed and maneuverability with increased RPM. [3291] Combined propulsion and generator with linear rotors and perpendicular rotors. Helicopter in which in-plane Description of the prior art Sustainable and Zero emission helicopter with new means for navigating and power generating for electric flying vehicles. With wind turbines integrated in the duct and a steam turbine generator in a compressed machine casing electrically connected to the power supply. BACKGROUND OF THE INVENTION [3292] Conventional rotary wing aircraft are driven by combustion engines and are limited in application by rendering the aerial vehicles electric and digital with zero emission. Consisting rotary wing aircrafts ar helicopters and utility aerial vehicles, privet transport chopper, is a type of rotorcraft in which lift and thrust are supplied by propeller rotors. This allows the helicopter to take off and land vertically, to hover, and to fly forward, backward, and laterally. These attributes allow helicopters to be used in congested or isolated areas where fixed-wing aircraft and many forms of VTOL (Vertical Takeoff and Landing) aircraft cannot perform. The Electric aircraft is navigated by the main rotor and tail rotor and turbine engines and boosters comprising electric generators for power supply. [3293] Turbine rotor applicable generating thrust is applicable for airborne and flying objects, and tethered unmanned aircraft. Radio controlled and autonomous airplanes and drones having a physical link with the ground by means of satellite connection and radio transmitters, comprising A turbine rotor with at least one blade, Pitch adjustable mounted to the hub, rotor blade horizontal and vertical angle adjustable turbine rotor. Tilt able roto hub with swash mechanism and unit operable mounted with the disturbed drive shaft. Manual controller having a stick made on the upper Centre of the controller sphere and digital automated controllers. An example of application of the turbine machines for generating electric current and for propulsion of the aircraft. [3294] electric rotary wind aircrafts comprise an airframe or fuselage turbines, lading gears or amphibian with a single or dual main rotor system mounted concentric on a mast in a ball and socket joint tiltable and operable mounted rotor hub coupled with the swash actuator tilting mechanism coupled with swash bearing stator that is rotatable connected with the hub bearing mounts and bolted with the hub. [3295] The helicopter rotor is blade adjustable by means of a collective pitch mechanism or cyclic pitch are both applied for the digital helicopter and rotor hub mounted pitch system. The swash plates with a stationary member and rotating mechanisms titling angular with respect to the mast is adjustable in force and aft plane and in the lateral plane. The blade is connected members are operable connected to the plurality of rotor blades and control horn operable connected with the blade connecting member. With at least one hydraulic, pneumatic or electro mechanical actuator connected with the control horn. At least one actuator is operable connected to the swashplate assembly to the actuators. The rotor and airframe is suspended with a kinematic connection for stabilization of the airframe. The rotor head and blades include harmonic vibration. [3296] The helicopter airframe comprises the dual turbine rotor of figure 4. The dual turbines are mounted in the airframe vertical tubular duct with a lower output nozzle for navigation without the need of tilting the rotors or the duct in moving direction which is provided by the exhaust nozzle. The dual turbine rotors are mounted on a common stationary axis in axial direction. The shaft is mounted with three or more arms or beams serving as stationary intake and exhaust vanes wherein the center rings the axis ends is fixed in bearing and busing and looking nuts or Jesus nuts. The rotor rotates in the cylindrical cavity with a minimum spatial gap with respect to the inner cylindrical wall. Electric cables are ducted through one hallow support beam or rod at the shaft ends. Electrically connected with the power supply. [3297] The smaller turbine rotors are electromagnetically driven or by inductive electromotive forces. The motors reach a velocity of 3000rpm p/m in seconds which is at full throttle. By energizing the second motor the velocity is increased logarithmically wits is not a gain in speed but gain in propulsion force and compression. The vertical propelled craft is manurable and fast because of the smaller turbine rotor with larger blade surface and rotational speed. All these factors multiplied with the digital screens and navigational controls and horizontal propulsion tube and electric generator. And types of turbine rotors in this application, with horizontal boosters and steam discharge boosters etc. With aerodynamic oval flattened fuselage and round oval top and sloped sides toward the lower bottom, having a flattened outer bottom with one or a pair of stabilizing fins minimum extending lower delta shaped wings. [3298] The propulsion system consists of many sorts of rotors and flow along the rotor and nacelle. Horizontal and vertical propulsion turbines obtained by the linear rotors with axial flow, cross axial-flow and combined. Horizontal and vertical propulsion turbines without tilting the turbine engine. [3299] Flying crafts are made with retractable and foldable rotors and tires. Helicopter with manual folding rotor blades for reducing the blade surface and parking multiple helicopters adjacent. Folding the plurality of blades in a group along the tail boom. The blade connecting mechanism such as a knuckle joint or universal joint mounted with the hub and shaft operable in a guiding ring in which the blade holder is movable by sliding the blade holder with the blade toward the tail. AMPHIBIAN ROATARY WING CRAFT. [3300] The invention related to a smaller type rotary amphibian wing aircraft for at least one person and maximum two persons. The electric rotary wing aircraft is designed to remain operable by the turbine motors and electric generating turbines and their motors. The craft can ride on three or four wheels on the road and extends the rotary wings and lift airborne and flying. The craft can take of vertically while parked stationary. The craft comprises retractable and extendable wings. PRIOR ART. [3301] The craft comprises a fuselage which is a molded and inflated unibody with an upper aluminum or titanium beam suspension structure whereon the fuselage is tiltable suspended with the alloy beams supported on the rotary wing and wheel side arms. The arms are slightly bend outward with the aerodynamics of the fuselage where the wheel and the inner rotor is vertically leveled by the welded connection with the arms. At least one ball and socket joint from suspending the fuselage or Universal connection that permits the fuselage to remain balanced when swung to the left or right. Whereby the tilting sensor contributes to the stability of the cabin with linear actuators. [3302] The alloy frame and transversal bar whereon the cabin is suspended. which is a thin fuselage of at least 70 cm wideness with a flat bottom and oval front and top cover. The fuselage comprises a cabin with two seats in a row, pilot controls. Cabin entrance by the front longitudinal upward opening window. The window comprises integrated digital screens and tinted glasses. The beck of the second seat is closed by a inner cabin wall where after the closed machine chamber is located wherein a steam turbine is fixed mounted including the power supply, water tank, and rechargeable means. [3303] The lower body comprises a flat rectangular duct of 50 centimeters wide and 10 centimeters in Hight. The duct travels through the fuselage from the nose till the tail through the machine room connected with the steam turbine that is bolted in the machine chamber in a compressed casing and connected with the duct for discharging gas in the duct and through the exhaust nozzle. [3304] The ducts comprise horizontal demi circular return blade chamber wherein the return blade chamber horizontal turbine rotors are operable suspended with the rotor axis rotatable through the bearing walls with the rotor axis extending from the side casing. The outer duct solid body is arranged with the electric motors and generators. The extended shaft comprises an magnet assembly in the stator casing and a stator armature opposing the magnet assembly. The motor can be made on both axial sides. With the rotor pushblades projecting in the duct with a minimum spatial gap with the surrounding wall. [3305] The horizontal turbine mounted duct provides electric current and propulsion. ROTARY WINGS AND WHEELS. [3306] The vehicle wheels and the pair of rotary wings are retracted and deployed separately while lift of from stationary mode or driven mode. When driving, the wheels and the rotary wings are only apart for take off and landing and are retracted together functioning for propulsion and navigation. When flying the tires and wheel provides navigation. The craft comprises two broad back wheels with motorcycle inflatable tires and with a front wheel reduced of size in diameter providing flyby-wire navigation when the vehicle is driven. [3307] The rear wheels are the size of motor cycle wheels whiteout the spoke frame and hub. In the round inner cavity of the magnetism driven wheels with tires, the rotors are seated inside the inner circular cavity. And locked together in the outer arm.