Tilt rotor flight control system pdf#

PROCEDE POUR TENDRE A OPTIMISER LE BRUIT EMIS PAR UN ROTOR AUXILIAIRE ET LES PERFORMANCES D'UN GIRAVION, ET UN GIRAVIONġ. SISTEMA DE SUSTENTACION PARA UNA AERONAVE CONVERTIBLE Y AERONAVE CONVERTIBLE QUE LO INCORPORA. Lift and flight control unit for an aircraft and aircraftĪuftriebseinheit für ein Fluggerät und Fluggerät Koaxial-Helikopter mit Gewichtskraftsteuerung Propeller device for producing fluid flow, and for use in drive unit for driving vehicle or vehicle model, has propeller, which is arranged coaxial to rotary axis, and is coupled to rotor by using power-transferring coupling Gondola propelling system for ship or windmill Method for control of rotary wing aircraft Means for controlling lateral movement of a helicopter Helicopter with counter-rotating coaxial rotors without cyclic variation of pitch, equipped with means for aerodynamic control of attitude and flight path SWASHPLATELESS COAXIAL ROTARY WING AIRCRAFT Swashplateless coaxial rotary wing aircraftĬoaxial counter-rotating unmanned helicopterĬoaxial Counter-Rotating Unmanned Helicopter TILTING COAXIAL ROTOR FOR A ROTARY WING AIRCRAFT YAW MOMENT SUPPLEMENT FOR DIRECTIONAL CONTROL Yaw moment supplement for directional control REDUNDANT HELICOPTER PITCH CHANGE BEARING Tilting coaxial rotor for a rotary wing aircraft UNMANNED COAXIAL ROTOR AERIAL VEHICLE FOR TRANSPORT OF HEAVY LOADS Gear-driven axial modulating mechanism for rotating shafts realizing a controllable pitch propeller/fan Reactionless free-spinning motor with dual propellers 210000003746 Feathers Anatomy 0.COAXIAL HELICOPTER AND CONTROL METHOD THEREOF.150000001875 compounds Chemical class 0.000 claims description 6.

230000010006 flight Effects 0.000 claims abstract description 75.

Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.) Filing date Publication date Priority to GB0400335.6 priority Critical Priority to GB0400335A priority patent/GB2409845A/en Application filed by Robert Graham Burrage filed Critical Robert Graham Burrage Priority to PCT/GB2004/005449 priority patent/WO2005066020A1/en Publication of US20070158494A1 publication Critical patent/US20070158494A1/en Application granted granted Critical Publication of US7584923B2 publication Critical patent/US7584923B2/en Status Active legal-status Critical Current Adjusted expiration legal-status Critical Links ( en Inventor Robert Graham Burrage Original Assignee Robert Graham Burrage Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.) Active, expires Application number US10/585,505 Other versions US20070158494A1

Tilt rotor flight control system pdf#

Google Patents US7584923B2 - Tilt-rotor aircraftĭownload PDF Info Publication number US7584923B2 US7584923B2 US10/585,505 US58550504A US7584923B2 US 7584923 B2 US7584923 B2 US 7584923B2 US 58550504 A US58550504 A US 58550504A US 7584923 B2 US7584923 B2 US 7584923B2 Authority US United States Prior art keywords aircraft rotors rotor lift flight Prior art date Legal status (The legal status is an assumption and is not a legal conclusion.