Patents
Patents for B64C 27 - Rotorcraft; Rotors peculiar thereto (10,112)
09/2006
09/07/2006US20060196992 Cycloidal hybrid advanced surface effects vehicle
09/06/2006EP1592613A4 Anti-torque and yaw-control system for a rotary-wing aircraft
09/06/2006EP1590240B1 Deformable aerodynamic profile
09/06/2006EP1395489A4 Anti-torque and yaw-control system for a rotary-wing aircraft
09/06/2006CN1829596A Bearing structure
09/06/2006CN1827474A A device for locking a structure for securing a blade to the hub of a rotocraft rotor
09/05/2006US7101246 Reduced visibility rotorcraft and method of controlling flight of reduced visibility rotorcraft
09/05/2006US7100866 Control system for a flying vehicle
09/05/2006US7100468 Split torque gearbox
08/2006
08/31/2006US20060193727 Drilling element for a bearingless rotor
08/31/2006US20060192047 Double ducted hovering air-vehicle
08/30/2006EP1695907A1 Device for locking the mounting structure of a blade to the hub of a rotorcraft rotor
08/30/2006EP1543253A4 Piezoelectric liquid inertia vibration eliminator
08/30/2006CN1824576A Vertiplane using power to directly push rotary wing changing into stopping wing
08/30/2006CN1824575A Centrifugal type wind wheel aeroplane
08/30/2006CN1272084C Remote controllable aerobat
08/29/2006US7097427 Helicopter main rotor blade balance weight retention assembly
08/29/2006CA2195078C Apparatus and methods for fabricating a helicopter main rotor blade
08/24/2006US20060186269 Adaptive compliant wing and rotor system
08/24/2006US20060186263 Rotor, rotorcraft comprising a rotor of this type and method for adjusting the blade angle of a rotor
08/24/2006US20060186262 Rotorcraft control system with stepped mixing linkage
08/24/2006DE102005007129A1 Arrangement for controlling of rotor blades of helicopter has controlled actuator, for collective and cyclic adjustment of blade setting angle of rotor blades, which are mechanically forcibly coupled among themselves
08/23/2006CN1821611A An antivibration device having rotary flyweights and an epicyclic geartrain
08/22/2006US7093788 Rotating flying wing aircraft and control system
08/17/2006WO2006086147A2 Assembly for providing flexure to blade system
08/17/2006US20060182633 Turbine blade
08/17/2006US20060182631 Lifting stage
08/17/2006DE19500539B4 Bremsvorrichtung für Hubschrauber-Rotoren Braking apparatus for helicopter rotors
08/17/2006DE102004051625B4 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
08/17/2006CA2596322A1 Assembly for providing flexure to blade system
08/16/2006EP1689638A2 Tailboom-stabilized vtol aircraft
08/15/2006US7090550 Propeller with variable geometry and method for varying geometry of a propeller
08/15/2006US7090164 Method for producing a lift and a horizontal thrust
08/10/2006WO2006083259A1 Segmented rotor blade trim tab
08/10/2006WO2005069788A3 Split torque gearbox
08/09/2006EP1613534B1 Rotor and gyrocopter with said rotor
08/09/2006CN1814341A Helicopter screw propeller operating device
08/03/2006WO2006081181A2 Assembly for providing flexure to blade system
08/03/2006US20060169835 Method and apparatus for manufacturing a helicopter rotor fairing, and a fairing obtained thereby
08/03/2006US20060169834 Compound helicopter with combined wings and landing struts
08/03/2006DE202006005841U1 Self-locking rotor blade disc for helicopter model, has aligned recesses and raised parts on opposing disc surfaces
08/02/2006EP1686057A2 Compound helicopter with combined wings and landing struts
08/02/2006CN1810577A Method and apparatus for manufacturing a helicopter rotor fairing, and a fairing obtained thereby
08/01/2006US7085655 Method and device for detecting defects of at least one rotary wing aircraft rotor
08/01/2006US7083383 Segmented rotor blade trim tab
08/01/2006US7083142 Compact co-axial rotor system for a rotary wing aircraft and a control system thereof
08/01/2006CA2254464C Magnetic particle damper apparatus
07/2006
07/27/2006WO2005121598A3 Small-size traction drive transmission system for use in microturbine-powered aircraft
07/27/2006US20060165527 Assembly for providing flexure to blade system
07/27/2006US20060163432 Multi-servicing and retractable bridge for an operational ground support system
07/27/2006US20060163424 AeroStreamer Flight Kit
07/27/2006DE10053134B4 Neuartiges Auftriebssystem für schuberzeugende Rotoren New type of lift system for thrust generating rotors
07/26/2006EP1682408A1 High ratio, reduced size epicyclic gear transmission for rotary wing aircraft with improved safety and noise reduction
07/26/2006EP1627158A4 Torque dividing gear drive system and method of driving an output gear
07/26/2006EP1512625B1 Autocopter, land motor vehicle which can be converted into an airmobile
07/26/2006CN1807923A Device for filtering vibrations between two parts and applications
07/26/2006CN1807185A Articulated type double-rotor flying robot
07/26/2006CN1807184A Tail rudder operated rotor flying robot
07/20/2006WO2006076743A1 Control system for a flying vehicle
07/20/2006WO2006075096A1 Device for orientation of the rotor head for helicopters
07/20/2006US20060157616 Tandem powered power tilting aircraft - JA
07/20/2006US20060157615 Control system for a flying vehicle
07/20/2006US20060157614 Wing for a compound helicopter
07/20/2006DE202006008024U1 Aufbau einer Serverhalterung für ferngesteuerte Hubschrauber Building a Server support for remote helicopter
07/19/2006EP1616114A4 Load sharing gear for high torque, split-path transmissions
07/18/2006US7077358 Helicopter with torque-correcting thruster device
07/13/2006US20060153685 Layer structure and method for producing such a layer structure
07/13/2006US20060153684 Methods and apparatus for assembling rotatable machines
07/13/2006US20060151665 Torsionally de-coupled engine mount system
07/13/2006US20060151272 Piezoelectric liquid inertia vibration eliminator
07/13/2006DE10241608B4 VTLO-Fluggerät mit zentrisch gelagertem Doppelrotor VTLO-flight device with centrally stored double rotor
07/12/2006CN1801582A A two-outlet electromechanical motor
07/11/2006US7074003 Helicopter moving device
07/06/2006WO2006069575A1 A wind turbine blade equipped internally with collection means
07/06/2006US20060147309 Blade pin alignment and positioning system for installation of helicopter rotor blades
07/06/2006US20060147306 Vibration reduction system for a wind turbine
07/06/2006US20060144994 Homeostatic flying hovercraft
07/06/2006DE102004061977A1 Klein-Flugkörper Small missile
07/05/2006EP1676775A1 Method and device of fabrication of an helicopter rotor housing
07/05/2006CN1798686A Crashworthiness structure and method
07/04/2006US7070151 In orbit space transportation and recovery system
07/04/2006US7070145 Tailboom-stabilized VTOL aircraft
06/2006
06/29/2006WO2006068507A1 Wire strike system
06/29/2006WO2006066561A1 Flying device with improved maneuverability on the ground
06/29/2006US20060140764 Wind turbine control having a lidar wind speed measurement apparatus
06/29/2006US20060140760 Active flow modifications on wind turbine blades
06/29/2006US20060138277 Steering aid system for altitude and horizontal speed, perpendicular to the vertical of an aircraft and aircraft equipped therewith
06/29/2006CA2557205A1 Wire strike system
06/28/2006EP1674819A1 Drone
06/28/2006CN2790906Y Rotatable two-rotary-wing light aircraft
06/27/2006US7068210 Low-cost position-adaptive UAV radar design with state-of-the-art cots technology
06/22/2006US20060135302 Anti-vibratory device with rotary compensation weights
06/22/2006US20060133940 Fatigue-resistant components and method therefor
06/22/2006US20060130780 Radial engine
06/22/2006DE102004060687A1 Rotor blade, for helicopter main and tail rotors, is a laminated fiber compound material with unidirectional glass fibers in a diameter of less than or equal to9 microns in bundles embedded in a matrix
06/22/2006DE102004004480A1 Electric power unit for driving coaxial shafts of rotary mechanisms, e.g. helicopter propeller, has electric motors with hollow shafts, where each stator and rotor is provided with independent power supply line over respective collector
06/21/2006EP1616111A4 Snubber
06/21/2006CN2789130Y Propeller thrust ring wing aerobat
06/20/2006US7063289 Helicopter tail section
06/15/2006US20060127222 Method for producing a rotor blade, a corresponding rotor blade and a wind power plant
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