Patents
Patents for B64C 27 - Rotorcraft; Rotors peculiar thereto (10,112)
10/2001
10/16/2001US6302356 Helicopter two stage main reduction gearbox
10/16/2001US6302229 Air cushion transport vehicle and method for controlling same
10/10/2001EP1140622A1 Variable diameter rotor blade actuation system
10/10/2001EP1140621A1 A drive system for a variable diameter tilt rotor
10/10/2001EP1140620A2 Method of providing a signal for controlling blade vortex interaction noise of a rotorcraft
10/10/2001EP1140619A1 Helicopter single-blade rotor
10/10/2001CN1072586C Operation of helicopter
10/09/2001US6299102 Aviation crash sensor
10/02/2001US6296444 Prop rotor hub
10/02/2001US6296378 Position light for aircraft
09/2001
09/27/2001US20010023907 Rotary blade of helicopter
09/27/2001DE10014899A1 Annular wing all-weather aircraft has drive-creating part fixed to horizontal axes connected to wing rings
09/26/2001EP1136719A1 Vibration damper, in particular for helicopter rotor
09/26/2001EP1136354A1 Vibration damper, in particular for an helicopter rotor
09/26/2001EP0910534B1 Helicopter rotor blade control device
09/26/2001CN1314287A Absorber of hozirontal rotary wing, particular for helicopter
09/25/2001US6295006 Flap angle measurement system for an active rotor control system
09/25/2001US6293492 Coaxial twin-rotor type helicopter
09/25/2001US6293491 Vertical take-off and landing aircraft
09/20/2001WO2001069058A2 Fluid loading system
09/20/2001US20010022418 Vibration damper, in particular for a helicopter rotor
09/20/2001DE10013385A1 Flying object, e.g. model spaceship, has drive mechanism out of sight, concealed by bodywork
09/19/2001CN1313226A Disk-shaped aircraft with wings
09/19/2001CN1313225A Aircraft with slant rotor
09/18/2001US6290171 Device for controlling a helicopter hybrid countertorque system
09/13/2001WO2001031229A3 Method and apparatus for adjusting lubricant temperature within a gearbox
09/12/2001CN2447293Y Helicopter with rotor guard
09/12/2001CN1312205A Spherical crown helicopter with single rotary wing and no tail paddle
09/11/2001US6287076 Rotor blade, in particular for helicopter antitorque tail rotor
09/11/2001US6286783 Aircraft with a fuselage substantially designed as an aerodynamic lifting body
09/11/2001US6286782 Apparatus and method for reducing vibrations of a structure particularly a helicopter
09/07/2001WO2001064512A1 Vertical takeoff aircraft
09/06/2001US20010019089 Aviation crash sensor
09/05/2001CN1070443C Stacked compound planetary gear for an upgrade powertrain system for a helicopter
09/04/2001US6283408 Anti-vibration suspension device having a torsion spring, for a helicopter
09/04/2001US6283406 Use of flow injection and extraction to control blade vortex interaction and high speed impulsive noise in helicopters
08/2001
08/30/2001WO2001062590A1 Method for determining a minimal set of rotor blade adjustments
08/30/2001DE10022819C1 Verfahren und Vorrichtung zur Vermeidung der Kolllision eines rotierenden Rotorblattes eines Drehflüglers mit Blattwirbeln Method and apparatus for preventing Kolllision a rotating rotor blade of a rotorcraft blade vortices
08/29/2001EP1127786A1 Rotary blade of helicopter
08/28/2001US6280141 Swash-plates system for control of the pitch of rotor blades with rotating plate driver
08/28/2001US6279704 Device for reducing the vibration generated on the structure of a rotary-wing aircraft
08/28/2001CA2010802C Roll vibration absorber
08/23/2001WO2001060692A1 Remote-controlled flying machine, in particular for surveillance or inspection
08/23/2001DE10007236A1 Verfahren zum Überwachen und Auswerten von Zustandsparametern A method for monitoring and evaluation of state parameters
08/21/2001US6276633 Convertible aircraft with tilting rotors
08/21/2001CA2080532C Multiblade rotor, namely for the anti-torque back propeller of an helicopter and fabrication process
08/21/2001CA2055469C Annular body aircraft
08/14/2001US6273681 Rotor blade flap driving apparatus
08/14/2001CA2076599C Method and device for filtering out vibrational excitations between two parts, especially between the rotor and the fuselage of an helicopter
08/08/2001EP0794896A4 Tail rotor authority control for a helicopter
08/07/2001US6270038 Unmanned aerial vehicle with counter-rotating ducted rotors and shrouded pusher-prop
08/02/2001US20010010348 Actuating device with at least three stable positions
08/02/2001US20010010345 Method of improving the crashworthiness of an aircraft
08/01/2001EP1120340A2 Method of improving the crashworthiness of an aircraft
07/2001
07/31/2001US6267331 Airfoil with dynamic stall control by oscillatory forcing
07/29/2001CA2331107A1 Method of improving the crashworthiness of an aircraft
07/26/2001WO2001053150A1 Aircraft with rotary wings
07/26/2001DE10001159A1 Vibration insulator for helicopter; has two force conduction points connected by insulator that generates dynamic counter oscillations, which are transmitted by spring system
07/26/2001CA2397626A1 Aircraft with rotary wings
07/25/2001CN1305423A Rotor or propeller with blade folding and pitch control devices
07/24/2001US6263936 Technique for making fiber composite object
07/19/2001DE10037540A1 Technik zum Herstellen eines Faserverbundgegenstandes Technique for manufacturing a fiber composite article
07/18/2001EP1115614A1 Fluid damper including flexible damping plate
07/18/2001CN2439400Y Helicopter with wings
07/17/2001US6260809 Ovate loop for rotary-wing blades
07/17/2001US6260796 Multi-thrustered hover craft
07/10/2001US6257529 Servo actuator apparatus and aircraft control apparatus
07/05/2001WO2001048378A1 Butt joint for hollow profiles
07/05/2001WO2001002742A3 Rotor with a split rotor blade
07/05/2001US20010006207 Control surface for an aircraft
07/05/2001DE19962989A1 Stossverbindung für Hohlprofile Butt joint for hollow sections
07/05/2001DE19961071A1 Kupplungsmembran Coupling membrane
07/04/2001CN2437594Y Annular-wing helicopter
07/03/2001US6254504 Power transmission apparatus for helicopter
06/2001
06/28/2001DE19958058A1 Drive unit for model helicopter comprises turbine drive with gearbox arranged on inlet side
06/27/2001CN1300676A Helicopter-type vehicle with cyclone gyro for space and land
06/21/2001US20010004440 Coupling membrane for a helicopter rotor head
06/19/2001US6247670 Active flaperon assembly
06/19/2001CA2083904C Multi blade rotor with variable blade pitch for aft anti-torque of an helicopter
06/19/2001CA2072810C Process and device for the reduction of divergent type oscillations of the fuselage of an helicopter
06/14/2001WO2001026948A3 Microwave blade tracker
06/13/2001CN2434226Y Active rotary wing helicopter
06/13/2001CN2434225Y Rotary wing helicopter
06/13/2001CN1067027C Composite cuff structure for helicopter rotors
06/13/2001CN1067026C Axisymmetric elastomeric bearing assembly for helicopter rotors
06/12/2001US6244537 Apparatus for operating a wing in three modes and system of use
06/07/2001WO2001040052A1 Aircraft rotor and aircraft
06/06/2001EP1104389A1 Method for reducing blade-vortex interaction noise generated by a rotary wing
05/2001
05/30/2001EP1103461A1 Improvements in or relating to sealing arrangements
05/30/2001EP1102614A1 Model helicopter
05/30/2001CN1296902A Vertical-lift unit for helicopter
05/30/2001CN1066371C 轴相位控制机构 Axis phase control mechanism
05/23/2001DE19944124C1 Entlüftungsventil mit Be- und Entlüftungskanal für ein Tankgefäß eines Hubschraubers Vent valve with ventilation duct for a tank vessel of a helicopter
05/23/2001CN1066114C Apparatus and method for fabricating helicopter main rotor blade
05/22/2001US6234751 Oscillating air jets for reducing HSI noise
05/22/2001US6234422 Uniblade air rotor and flight and covercraft vehicles with its
05/22/2001CA1341239C Pale a faible signature radar
05/21/2001CA2315524A1 Personal hoverplane having four tiltmotors
05/17/2001WO2001034466A1 Helicopter with highly stable and highly manoeuvrable pendular piloting system
05/17/2001DE19945791C1 Hubschraubergetragene Radaranlage Helicopter-borne radar system
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