Patents
Patents for B64C 27 - Rotorcraft; Rotors peculiar thereto (10,112)
06/2006
06/15/2006US20060124800 Powered aircraft including inflatable and rotatable bodies exhibiting a circular cross-section perpendicular to its rotation axis and in order to generate a lift force
06/14/2006EP1669547A2 Composite aerofoil
06/14/2006EP1343979B1 Rotor shaft support
06/14/2006DE102004058301A1 Rotorcraft has an active vibration isolation system, which has actively controlled load transmitting electro-magnetic vibration damper
06/13/2006US7059931 Reduced visibility rotorcraft and method of controlling flight of reduced visibility rotorcraft
06/13/2006US7059562 Vertical lift flying craft
06/08/2006US20060121818 Micro aerial vehicle
06/08/2006DE202006005862U1 Double rotor helicopter has contra rotating rotors driven by a differential and with a single swashplate control and without a tail rotor
06/07/2006EP1666355A1 Helicopter bvi noise reducing method and device
06/07/2006EP1663779A2 Braided spar for a rotor blade and method of manufacture thereof
06/07/2006EP1339601A4 Flap actuator system
06/07/2006EP1224116A4 Flap actuator system
06/07/2006CN1784338A Method and apparatus for preventing adverse effects of vortex ring state
06/06/2006CA2278315C Rotor head for rotary wing aircraft
06/01/2006US20060115360 Doppler radar sensing system for monitoring turbine generator components
06/01/2006US20060113426 Vtol vehicles
06/01/2006US20060113425 Vertical take-off and landing aircraft with adjustable center-of-gravity position
05/2006
05/31/2006EP1662166A1 Device for filtering vibrations between two parts and applications
05/31/2006CN2784310Y Screw propeller bracket of electric helicopter
05/30/2006US7052232 Method for determining the angle of a rotor blade pertaining to a wind energy installation
05/30/2006US7051979 Auxiliary fuel tank systems for aircraft and methods for their manufacture and use
05/30/2006US7051535 Turbine engine differential-pressure torque measurement system
05/25/2006US20060110256 Impeller and method using solid free form fabrication
05/25/2006US20060108474 Hollow assembly structure and fabrication method therefor
05/24/2006EP1659309A1 Vibration damping apparatus
05/24/2006EP1658222A2 Soft in-plane rotor hub
05/24/2006EP1658184A2 Dual spring rate damper
05/24/2006CN2782557Y Umbrella wing shape screw prepeller
05/23/2006US7047596 Structural bushing application for highly loaded composites lugs
05/23/2006CA2260960C Landing and take-off assembly for vertical take-off and landing and horizontal flight aircraft
05/18/2006US20060104816 Running wheel
05/18/2006US20060104815 Wind energy installation comprising a concentric gearbox generator arrangement
05/18/2006US20060104811 Device for optimizing and adjustment of steam balance hole area
05/18/2006US20060102777 Coaxial rotorcraft control system
05/18/2006US20060102776 Dual action inlet door and method for use thereof
05/17/2006EP1656294A1 Gyropter having increased safety
05/17/2006CN1774366A Rotor and gyrocopter with said rotor
05/17/2006CN1772561A Complex rotary wine/off-set rotary wine craft
05/16/2006US7044877 Two speed transmission with smooth power shift
05/11/2006WO2006048205A1 Rotational speed controlled helicopter
05/11/2006US20060097104 Method and a device for using a steerable tall fin to reduce the vibration generated on the fuselage of a helicopter
05/11/2006US20060097103 Method and apparatus for vehicle control using variable blade pitch
05/11/2006DE102005010336A1 Drehzahlgesteuerter Hubschrauber Speed-controlled helicopter
05/10/2006EP1655221A1 Individual blade control for a helicopter main rotor with additional separate collective blade control
05/10/2006EP1654110A1 Bearing structure
05/10/2006CN1771162A Non-articulated rotor and rotorcraft comprising a rotor of this type
05/09/2006US7040863 Variable pitch rotor blade for shrouded rotors, in particular helicopter rotors
05/04/2006WO2005100153A3 Method and device for minimising rotorcraft take-off and landing noise
05/04/2006US20060091258 Autonomous, back-packable computer-controlled breakaway unmanned aerial vehicle (UAV)
05/04/2006DE102004063205B3 Aircraft for transporting persons, has rotors/propellers with sheathings, which enable independent drive movement of aircraft on land according to function of wheel rims based on direct power transmission from aircraft to land
05/04/2006DE102004053001A1 Individual blade control for helicopter rotor has means for mechanical transmission of exclusively collective control movements from non-rotating system into rotating system, with control movements superimposed on actuators
05/04/2006DE102004051625A1 Verfahren zur Pilotenunterstützung bei Landungen von Helicoptern im Sichtflug unter Brown-Out oder White-Out Bedingungen A method for pilot support for landings of helicopters in visual flight under brownout or whiteout conditions
05/03/2006EP1653593A2 Dual output electromechanical motor
05/03/2006CN2776844Y Heavy load unmanned vertical flight
05/03/2006CN2776504Y Operating device of vertiplane screw propeller
05/03/2006CN1254297C Coaxile reverse rotating type radio controlled vertiplane
05/02/2006US7037072 Rotor head for a rotary-wing aircraft
04/2006
04/26/2006EP1428046B1 Combined loas and lidar system
04/26/2006EP1056640B1 Optimum speed rotor
04/26/2006CN1762765A Novel helicopter
04/26/2006CN1762764A Rotor type air dropping/ descending device capable of storing energy
04/25/2006US7032860 Emergency anti-torque thruster system
04/25/2006US7032859 Counter rotating ducted fan having a permanent magnet drive
04/20/2006WO2006041287A1 Personal land and air vehicle
04/20/2006US20060083619 Dual counterweight balancing system
04/20/2006US20060083615 Pitch drive system for a wind turbine
04/20/2006US20060083611 Butt connection for hollow profile members
04/20/2006CA2582250A1 Personal land and air vehicle
04/19/2006CN2772962Y Special aerobat with circular wing
04/19/2006CN1761536A Anti-vibratory device with rotary compensation weights
04/18/2006US7028954 Microfabricated translational stages for control of aerodynamic loading
04/18/2006US7028949 Landing assist probe mounting system
04/13/2006DE19962989B4 Rotorblatt für Windenergieanlagen Rotor blades for wind turbines
04/13/2006DE19638695B4 Modularer Schwingungskraftgenerator und Verfahren zu dessen Betrieb Modular vibratory force generator and method for operating the
04/12/2006EP1645505A2 Unmanned helicopter, takeoff method of unmanned helicopter, and landing method of unmanned helicopter
04/12/2006EP1644242A2 Rotor blade tip section
04/12/2006EP1511671A4 Control of an aircraft as a thrust-vectored pendulum in vertical, horizontal and all flight transitional modes thereof
04/12/2006CN1250889C Vibration damping device
04/06/2006WO2006036467A2 Polymeric fan
04/06/2006US20060073022 Frequency tailored thickness blade for a turbomachine wheel
04/06/2006US20060073018 Fan
04/06/2006US20060071817 Tactile cueing system and method for aiding a helicopter pilot in making landings
04/06/2006US20060071121 Gimbal system
04/06/2006DE102005012744A1 Vertical take-off and landing aircraft used as a type of helicopter in the military comprises devices for shifting the center of gravity of the aircraft within a plane running normal to the rotary axis
04/04/2006US7021897 Blade pitch control disk device for a rotorcraft rotor
03/2006
03/30/2006WO2006032900A1 Rotorcraft
03/30/2006US20060067829 Backswept titanium turbocharger compressor wheel
03/30/2006US20060067828 Wind turbine rotor blade with in-plane sweep and devices using same, and method for making same
03/30/2006US20060067824 Turbocharger with titanium component
03/30/2006US20060067823 Helicopter rotor
03/30/2006US20060067822 Pitch lock and lag positioner for a rotor blade folding system
03/30/2006CA2623367A1 Rotorcraft
03/29/2006EP1640266A1 Helicopter rotor with a vibration damping device
03/29/2006CN2767323Y Float bowl type loop umbrella one-seater aerobat
03/29/2006CN2767322Y Circular wing aerobat
03/29/2006CN1751964A Anti torque device used for single rotor vertiplane tail
03/28/2006US7017857 Active vibration control system
03/28/2006CA2520778A1 Helicopter rotor
03/28/2006CA2496385C Rotor and aircraft passively stable in hover
03/23/2006WO2006030213A1 Wing tip devices
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