Patents
Patents for B64C 27 - Rotorcraft; Rotors peculiar thereto (10,112)
05/2004
05/11/2004US6732973 Stabilizer for a propeller related vehicle
05/06/2004WO2003039950A9 Propellers, propeller stabilizers, and propeller related vehicles
05/06/2004WO2003024790A9 Optimum speed tilt rotor
05/06/2004US20040084818 Fluid-elastomeric damper assembly including internal pumping mechanism
05/04/2004US6729839 Toroidal and compound vortex attractor
05/04/2004US6729576 Composite tail cone assembly
05/04/2004US6729139 Engine control system
04/2004
04/28/2004EP1412245A1 Helicopter main rotor blade balance weight retention assembly
04/22/2004WO1994016238A3 Coupling device for drive shaft segments
04/22/2004US20040075018 Unmanned helicopter, takeoff method of unmanned helicopter, and landing method of unmanned helicopter
04/22/2004US20040075017 Control of an aircraft as a thrust-vectored pendulum in vertical, horizontal and all flight transitional modes thereof
04/21/2004EP1244873B1 Use of a butt joint for rotor blades
04/15/2004US20040070311 Piezoelectric extension actuator
04/15/2004US20040069901 Aircraft and hybrid with magnetic airfoil suspension and drive
04/15/2004US20040069145 Vortex vacuum cleaner nozzle with means to prevent plume formation
04/15/2004DE10306417A1 Aircraft position measurement device, especially for use with remotely controlled helicopters, forms part of an aircraft stability system and has an optoelectronic system for measuring the displacement of ground structures
04/14/2004EP1407965A1 Unmanned helicopter, takeoff method for unmanned helicopter, and landing method for an unmanned helicopter
04/13/2004US6719830 Toroidal vortex vacuum cleaner centrifugal dust separator
04/13/2004CA2082187C Gyroplane rotor braking unit
04/08/2004DE20122107U1 Propulsion assembly for model helicopters has horizontal turbine permitting turbine flow direction as in conventional helicopters
04/07/2004CN2609836Y Vertical/short distance take-off and landing aircraft
04/06/2004US6717333 Piezoelectric actuating device for controlling the flaps on the rotor blade of a helicopter
04/06/2004US6715992 Helicopter blade and method of manufacture
04/06/2004US6715711 Hub-protecting cap for a helicopter tail rotor
04/01/2004WO2004027434A1 Measuring and stabilising system for machine-controllable vehicles
04/01/2004WO2004026689A1 Torsionally de-coupled engine mount system
04/01/2004WO2003106259A3 Controlable rotorcraft using a pendulum
04/01/2004WO2002064425A9 Coaxial helicopter with one cyclic pitch control rotor
04/01/2004DE10258545A1 Aircraft position measurement device, especially for use with remotely controlled helicopters, forms part of an aircraft stability system and has an optoelectronic system for measuring the displacement of ground structures
03/2004
03/31/2004EP1403180A2 External airbag protection system for helicopters
03/30/2004US6712313 Constant velocity drive rotary-wing aircraft rotor with torque splitting differential
03/30/2004CA2272413C Hovering aircraft
03/25/2004WO2004024558A2 Fixed wing aircraft having powered rotor vtol capability with rotor blades stowable during horizontal flight
03/25/2004US20040056154 VTOL personal aircraft
03/25/2004US20040056145 Method for retrofitting an inertia reel access door to an ejection seat
03/25/2004US20040056144 Dual-flight mode tandem rotor wing
03/23/2004US6708921 Composite flapping flexure
03/23/2004US6708920 Air vehicle
03/18/2004WO2004022424A2 Retractable lifting blades for aircraft
03/18/2004WO2002098732A3 Vehicles particularly useful as vtol vehicles
03/11/2004WO2003086858A8 Method for producing a lift and a horizontal thrust
03/11/2004DE20314042U1 Model helicopter with swashplate mounted not on rotor shaft but in ring-shaped guide via guide webs
03/10/2004EP1395489A2 Anti-torque and yaw-control system for a rotary-wing aircraft
03/10/2004EP1395488A1 Rotor system vibration absorber
03/10/2004EP1224489B1 Helicopter-borne radar system
03/04/2004WO2003059735A3 Micro-rotocraft surveillance system
03/04/2004WO2002071388A3 System for control of active system for vibration and noise reduction
03/04/2004US20040042901 Extreme mu rotor
03/03/2004EP1392987A1 Vibration damping device
03/02/2004US6698685 Circular vertical take off and landing aircraft
02/2004
02/26/2004US20040038768 Pivoting power transmission unit with load transfer via the casing
02/26/2004US20040037701 Helicopter rotor hub, and rotor featuring such a hub
02/26/2004US20040035978 System for controlling the torsional stability of the drivetrain of a machine, in particular of a helicopter
02/26/2004DE20318278U1 Dynamo for supplying electric equipment fastened on or integrated in a wheel or rotor generates electric power with a permanent magnet
02/25/2004EP1390259A2 Ducted fan vehicles particularly useful as vtol aircraft
02/25/2004EP1175339B1 Flap angle measurement system for an active rotor control system
02/24/2004US6696477 Heterocyclo substituted hydroxamic acid derivatives as cyclooxygenase-2 and 5-lipoxygenase inhibitors
02/24/2004US6695583 Snubber-vibration damper system for a bearingless main rotor
02/24/2004US6695264 Power lever tactile cueing system
02/24/2004US6695254 Rotary-wing aircraft rotor with constant velocity drive
02/24/2004US6695253 Method and apparatus for folding/unfolding the blades of a rotary-wing aircraft rotor
02/24/2004US6695106 Method and apparatus for improved vibration isolation
02/19/2004WO2004014726A1 Composite tail cone assembly for a helicopter
02/19/2004WO2003095268A3 Retrofitting ejection seat with inertia reel access door
02/19/2004US20040031879 Composite tail cone assembly
02/17/2004US6693548 Structural monitoring system for helicopter rotor components
02/17/2004US6691830 Device for lubricating a power gearbox with a variable orientation, particularly for a convertible tilt-rotor aircraft
02/12/2004WO2004012993A1 Vtol vehicles
02/12/2004WO2003018342A3 Compact vibration cancellation device
02/12/2004US20040026564 Method and apparatus for folding/unfolding the blades of a rotary-wing aircraft rotor
02/12/2004DE4413447B4 Verfahren und Vorrichtung zum aktiven Einstellen und Steuern eines resonanten Masse-Feder-Systems Method and apparatus for actively adjusting and controlling a resonant mass-spring system
02/10/2004US6689225 Toroidal vortex vacuum cleaner with alternative collection apparatus
02/10/2004US6688767 Self-aligning dynamic hinge sleeve
02/10/2004US6687951 Toroidal vortex bagless vacuum cleaner
02/05/2004WO2001069058A3 Fluid loading system
02/04/2004EP1385738A1 Composite rotor blade and method of manufacture
02/04/2004EP1185456B1 Device for simultaneously interlocking a plurality of actuators
02/04/2004CN1472113A Helicopper
02/03/2004CA2093701C Single rotor helicopter with mixed anti-torque and method to counter act single rotor induced torque
01/2004
01/29/2004WO2004009723A2 Low light level illumination for rotating objects
01/29/2004US20040018089 Vortex attractor
01/29/2004DE10211510B4 Steuergewicht am Rotorblatt des Heckrotors eines Hubschraubers zur Einstellung des Propellermoments Control weight on the rotor blade tail rotor of a helicopter for adjusting the propeller torque
01/28/2004EP1384896A2 Method and apparatus for modulating airfoil lift
01/28/2004EP1384662A1 Vtol micro-aircraft
01/28/2004EP1383680A1 Dual trunnion hub-to-mast assembly
01/22/2004WO2004007282A2 A rotary-wing aircraft having horizontal stabilizer
01/22/2004US20040013524 Method for determining the angle of a rotor blade pertaining to a wind energy installation
01/22/2004CA2493087A1 Rotary-wing aircraft
01/21/2004EP1382527A1 Tilting power transmission box with load transfer through the housing
01/21/2004EP1175338B1 Actuation system for an active rotor control system
01/21/2004CN2600337Y Propeller helicopter driven by air injection
01/20/2004US6680554 Aircraft, particularly a helicopter, transmission system
01/15/2004US20040007645 Rotary-wing aircraft
01/15/2004US20040007644 Rotor craft
01/15/2004US20040007080 Fuselage pitot-static tube
01/14/2004EP1212541B1 Hybrid ball bearing with oblique contact, and axial stop comprising same
01/13/2004US6677683 System for supplying power to ROSAR transponders, including transmitting and receiving antennas for ROSAR devices
01/13/2004US6676526 Coupling anti-flail cup
01/13/2004US6676377 Device for simultaneously interlocking a plurality of actuators
01/13/2004US6676074 Dual piston drag damper for rotary-wing aircraft rotor
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