Patents
Patents for B64C 27 - Rotorcraft; Rotors peculiar thereto (10,112)
06/2002
06/12/2002EP1212541A1 Hybrid ball bearing with oblique contact, and axial stop comprising same
06/11/2002US6402089 System for control of active system for vibration and noise reduction
06/11/2002US6402088 Passenger vehicle employing a circumferentially disposed rotatable thrust assembly
06/11/2002US6401398 Sealing arrangements
06/11/2002CA2038088C Link and bearing for rotary coupling
06/06/2002WO2002043947A1 Improved wavy composite structures
06/06/2002US20020066831 Lifting surface with active variable tip member and method for influencing lifting surface behavior therewith
06/05/2002EP1211173A2 Hybrid aircraft
06/05/2002EP1211172A2 Hybrid aircraft
06/05/2002CN1085973C Aircraft with fuselage substantially designed as aerodynamic filting body
06/04/2002US6398497 Blade lock system for variable diameter rotor systems
06/04/2002US6398496 Minimizing wind forces on helicopter blades
06/04/2002US6398159 Arial disk
05/2002
05/30/2002US20020065139 Aircraft, particularly a helicopter, transmission system
05/30/2002US20020063186 Actuator for an active transmission mount isolation system
05/29/2002EP1209546A1 Tracking device
05/29/2002EP1209076A2 Hybrid aircraft
05/29/2002EP0931227A4 Concentric face gear transmission assembly
05/28/2002US6394397 Lifting surface with active variable tip member and method for influencing lifting surface behavior therewith
05/28/2002US6394387 Rotor shaft support and drive arrangement
05/23/2002WO2001092823A3 Method, apparatus and computer program product for displaying terrain in rotary wing aircraft
05/23/2002US20020060268 Method and apparatus for improved vibration isolation
05/23/2002US20020060267 Unmanned mobile device
05/21/2002US6390413 Years two thousand of new safety helicopter
05/21/2002US6390412 Method and device for assisting the pilot in controlling the turboshaft power and/or rotor speed of heat-propelled helicopters
05/16/2002WO2002038442A2 Microfabricated translational stages for control of aerodynamic loading
05/16/2002US20020058810 As antiinflammatory agents
05/15/2002CN1084696C Blade profile for aircraft rotor and rotor comprising same
05/15/2002CN1084695C Composite tip cap assembly for a helicopter main rotor blade
05/08/2002EP0996570B1 Structural component having means for actively varying its stiffness to control vibrations
05/08/2002DE10052757A1 Rotorblatt-Steuerungsvorrichtung Rotor blade control device
05/07/2002US6382560 High speed vertical take-off and land aircraft
05/07/2002US6382558 Safety system for a helicopter
05/07/2002US6382556 VTOL airplane with only one tiltable prop-rotor
05/02/2002WO2002034620A1 Unpiloted rotor-driven aircraft
05/02/2002EP1201538A1 Rotor blade control device
05/02/2002EP0854821B1 Hybrid aircraft
05/02/2002DE10139686A1 Piezoelectric extension actuator for damping structural vibration uses stack of d33 piezoelements between output elements secured to structure
04/2002
04/30/2002USRE37673 Methods for fabricating a helicopter main rotor blade
04/30/2002US6378808 Device for releasing a parachute
04/30/2002US6378470 Rotary engine and helicopter application
04/25/2002US20020049518 Sterring control device for radio-controlled model helicopter
04/25/2002US20020047071 Lifting platform with energy recovery
04/23/2002US6375426 Protective edge members for composite flexures
04/23/2002CA2255602C Aerodyne with vertical take-off and landing
04/18/2002WO2002031378A1 Piezoelectric extension actuator
04/18/2002WO2001090694A3 Apparatus, method and computer program product for helicopter ground proximity warning system
04/18/2002WO2001090693A3 Apparatus, method and computer program product for helicopter enhanced ground proximity warning system
04/18/2002DE10046805A1 Control for near-ground craft or aircraft comprises packets of flap pairs equi-spaced round ring channel periphery and converged or diverged under servomotor control for aircraft maneuvers.
04/18/2002DE10034306A1 Aircraft rotor blade consists of several surface flaps circling round flight-normal drive axis and mechanically controlled in angle or rotation position to form lift profiles.
04/17/2002EP1196696A2 Rotor with a split rotor blade
04/17/2002EP1196226A1 Electrical remote-control and remote-power flying saucer
04/17/2002CN1082922C Optimized composite flexbeam for helicopter tail rotors
04/17/2002CN1082921C Optimized composite flexbeam for helicopter rotors
04/16/2002US6371681 Anti-rotation clip
04/16/2002US6371415 Aerodynamic component with a leading edge flap
04/16/2002US6371408 Helicopter tail rotor authority altitude compensator
04/11/2002WO2002028710A1 Elastomeric bearing
04/10/2002EP1042707B1 Compensation for rotorcraft pitch axis control saturation
04/10/2002CN1343579A Multifunctional miniature car
04/09/2002US6367736 Convertiplane
04/04/2002WO2002027210A1 Method and apparatus for improved vibration isolation
04/04/2002WO2001089926A3 Power lever tactile cueing system
04/04/2002US20020039620 A brass coated metallic wire for use as a reinforcing component in an elastomeric article, such as a motor vehicle tire.
04/04/2002DE10043929A1 Rotor blade control flap drive system control method by modifying control parameter if static friction occurs
04/03/2002EP1193168A2 Unmanned mobile device
04/02/2002US6364615 Blade for the rotary wings of an aircraft
04/02/2002US6364611 Helicopter power transmitting apparatus
04/02/2002US6364249 Engine integrated with rotary wing aircraft transmission
03/2002
03/28/2002WO2002024526A1 Variable edge rotor blade
03/28/2002US20020036119 Device for lubricating a power gearbox with a variable orientation, particularly for a convertible tilt-rotor aircraft
03/28/2002DE10046247A1 Aircraft e.g. tilt rotor aircraft, has position light that is provided on wing tip along with pivoting reflector
03/27/2002EP1191259A1 Lubrication device of a variable orientable power transmission especially for convertible plane with tilt rotors
03/27/2002EP0740746B1 Vibration isolation system
03/27/2002CN1341534A Equipment and method for manufacturing main rotor blade of helicopter
03/26/2002US6361279 Blade profile for aircraft rotor and rotor comprising same
03/26/2002US6361278 Coupling membrane for a helicopter rotor head
03/21/2002WO2002023125A1 Method, apparatus and computer program product for helicopter tail strike warning
03/21/2002CA2320025A1 Position light for aircraft
03/14/2002US20020030956 Power switching device in an electrical power distribution system on board a helicopter
03/14/2002US20020030607 Method, apparatus and computer program product for helicopter tail strike warning
03/14/2002US20020030136 Years two thousand of new safety helicopter
03/13/2002EP1185456A1 Device for simultaneously interlocking a plurality of actuators
03/12/2002US6355339 Mechanically secured foam core reinforcement
03/12/2002US6354536 Rotor hub mounted actuator for controlling a blade on a rotorcraft
03/12/2002CA2042532C Spar-to-hub joint for a flexbeam helicopter rotor
03/07/2002US20020028332 Wavy composite tubular structures
03/05/2002US6352220 Helicopter tail boom with venting for alleviation and control of tail boom aerodynamic loads and method thereof
02/2002
02/28/2002DE10026018A1 Kipp- bzw. Drehpositionierungsmittel Tilting and rotational positioning means
02/26/2002US6349903 Control surface for an aircraft
02/21/2002US20020021965 Rotor blade having a control flap
02/21/2002US20020021964 Tilt and swivel positioning device
02/21/2002US20020020296 Toroidal vortex vacuum cleaner with alternative collection apparatus
02/21/2002US20020020035 Toroidal vortex bagless vacuum cleaner
02/14/2002WO2002012063A1 Rotor hub mounted actuator for controlling a blade on a rotorcraft
02/14/2002US20020018716 Helicopter in-flight rotor tracking system, method, and smart actuator therefor
02/14/2002US20020017591 Drive unit for a model helicopter
02/14/2002CA2421853A1 Rotor hub mounted actuator for controlling a blade on a rotorcraft
02/13/2002CN1335248A Helicopter with driving rotary wings
02/12/2002US6345792 Actuating device with at least three stable positions
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