Patents
Patents for B64C 27 - Rotorcraft; Rotors peculiar thereto (10,112)
06/2012
06/27/2012CN102514712A Vertical take-off and landing aircraft
06/27/2012CN102514711A Multi-rotor fuel-electric hybrid aircraft
06/27/2012CN101612990B Blade for reducing the drag movements of said blade and method for reducing such a drag movement
06/26/2012US8206113 Method and apparatus for converting marine wave energy by means of a difference in flow resistance form factors into electricity
06/26/2012US8206105 Method and device for controlling load reduction for a wind turbine rotor
06/26/2012US8205822 Active maple seed flyer
06/26/2012US8205821 Engine propulsion system and methods of assembling the same
06/21/2012WO2012081926A2 Long-endurance airplane using wind power energy
06/21/2012WO2012079100A2 Rotor blades of a gyrocopter
06/21/2012US20120156050 Detachable rotor blade fairing apparatus and method
06/21/2012US20120156049 Method and coating for protecting and repairing an airfoil surface
06/21/2012US20120153074 Electronic flight control system for an aircraft capable of hovering
06/21/2012US20120153073 Mission-adaptive rotor blade
06/21/2012US20120153072 Method of controlling and regulating the deflection angle of a tailplane in a hybrid helicopter
06/20/2012EP2465771A1 Blade for an anti-torque device of a helicopter
06/20/2012EP2464567A1 Tilt-rotor aircraft
06/20/2012EP2464566A2 Stabilized safety gyroplane
06/20/2012EP2334549B1 Blade for a turbomachine
06/20/2012CN202279232U Tail transmission shaft supporting arrangement
06/20/2012CN102501970A Band type damper and preparation method thereof
06/20/2012CN102501969A One-man flight vehicle capable of jetting at points of rotor blades
06/20/2012CN102501968A Ducted coaxial helicopter control mechanism
06/20/2012CN102501967A Multi-rotor aircraft
06/20/2012CN101501302B Rotor blade for a high speed rotary-wing aircraft
06/19/2012US8201772 Method for suppressing vibration and acoustic signature in a tiltrotor aircraft
06/19/2012US8201771 Helicopter rotor control system with individual blade control
06/15/2012CA2759763A1 Blade for helicopter anti-torque device
06/14/2012WO2012076705A2 Aircraft rotor comprising rotary wings
06/13/2012EP2462022A2 Rotor assembly for a rotorcraft
06/13/2012EP2234792B1 Helicopter blade mandrel with roller assembly and methods to make and use it
06/13/2012CN102490907A Airplane for aerial photography
06/13/2012CN102490900A Small individual aircraft with folding rotor wings
06/13/2012CN102490899A Composite rotor blade for unmanned helicopter and manufacturing method thereof
06/13/2012CN102490898A Coaxial dual-rotor helicopter
06/13/2012CN102490897A Multi-driving embedded rotor manned helicopter
06/13/2012CN102490896A Variable-torque four-rotor aircraft with large load capacity
06/13/2012CN101495368B Automatic dual rotor speed control for helicopters
06/12/2012US8197205 Swashplateless helicopter blade actuation system
06/12/2012US8196857 Variable ratio crank for a manual flight control linkage of a rotary wing aircraft
06/12/2012US8196856 Method for suppressing vibration in a tiltrotor aircraft
06/12/2012US8196855 Helicopter auxiliary anti-torque system
06/12/2012US8196854 Tilt rotor aircraft with tilting tail rotor—TT
06/12/2012DE202012002493U1 Hubschrauberheck Helicopter tail
06/12/2012CA2635672C Stiff-in-plane gimbaled tiltrotor hub
06/12/2012CA2585918C Drive installation for rotary-wing aircraft
06/07/2012WO2012075236A1 Frequency-dependent damper and rotary wing system
06/07/2012WO2012075022A2 Adjustable wind-resistance windmill with indicia
06/07/2012WO2012035025A3 Method for improving the flying characteristics of a multicopter in failure situations and multicopter with improved flying characteristics in failure situations
06/07/2012US20120141276 Frequency-dependent damper and rotary wing system
06/07/2012US20120138732 Helicopter with folding rotor arms
06/07/2012US20120138731 Rotorcraft structural element for reducing aerodynamic drag
06/07/2012US20120138730 Stabilized safety gyroplane
06/07/2012CA2772799A1 Apparatus for stringing a line underneath a cross member
06/06/2012EP2460720A1 Structural element of a rotorcraft for reducing aerodynamic drag
06/06/2012EP2460647A1 Production of parts reinforced with composite materials with a single crossing line
06/06/2012EP2459442A2 Method and apparatus for pressure adaptive morphing structure
06/06/2012EP2007623B1 Rotor apparatus and methods for vertical lift aircraft
06/06/2012DE202012002513U1 Spezielles Framedesign für Multikopter mit freiem Kamerablickfeld nach oben Special frame design for Multikopter with free camera field of view to the top
06/06/2012CN202264885U 碟形飞行器 Flying
06/06/2012CN202264884U 太阳能飞碟装置 Solar UFO unit
06/06/2012CN101643116B Tiltrotor controlled by double-propeller vertical duct
06/05/2012US8192159 Rigid rotor assembly for folding helicopter blades
06/02/2012CA2759909A1 Aerofoil
05/2012
05/31/2012US20120136533 Helicopter vibration control system and circular force generation systems for canceling vibrations
05/31/2012US20120134741 Rotary wing aircraft rod end and method of making a helicopter vehicle rod end with a precocked orientation
05/31/2012US20120133136 Adjustable wind-resistance windmill with indicia
05/30/2012EP2457830A1 Blade to rotor hub joint
05/30/2012EP2457829A2 High Performance Low Noise Helicopter Blade Aerodynamic Design
05/30/2012EP2457828A2 High Performance Low Noise Helicopter Blade Aerodynamic Design
05/30/2012EP2457827A2 High Performance Low Noise Helicopter Blade Aerodynamic Design
05/30/2012EP2457826A2 Method for controlling a buoyancy system for an aircraft and buoyancy system implementing said method, and aircraft
05/30/2012CN202244098U Typhoon-resistant fixing device for helicopter
05/30/2012CN202244082U Shimmy damper for rotor wing of helicopter
05/30/2012CN202244081U Synchronous locking and unlocking device for flapping motion of wing
05/30/2012CN202244080U Ground effect aircraft
05/30/2012CN202244079U Power arm spindle driving device and helicopter formed by same
05/30/2012CN202244078U Multi-rotary-wing unmanned aircraft
05/30/2012CN102481975A Differential pitch control to optimize co-rotating stacked rotor performance
05/30/2012CN101263053B Engine assembly for aircraft comprising an engine as well as a device for assembling said engine
05/30/2012CN101219710B Power transmitting system for helicopter, having magnetic damper
05/29/2012US8186957 Fan propeller, in particular for motor vehicles
05/29/2012US8186629 Method and a device for optimizing the operation of propulsive propellers disposed on either side of a rotorcraft fuselage
05/29/2012US8186615 Rotor head of remotely-controlled helicopter and remotely-controlled helicopter
05/24/2012WO2011144692A3 Hybrid drive and energy system for aircraft
05/24/2012DE102010051848A1 Luftfahrzeug mit integrierter Arbeitsbühne Aircraft with integrated Platform
05/23/2012EP2455285A1 Shock absorbing structure
05/23/2012EP2454153A1 A multi-ratio rotorcraft drive system and a method of changing gear ratios thereof
05/23/2012EP2004483B1 Aircraft having the characteristic of hovering flight, fast forward flight, gliding flight, short take off, short landing, vertical take off and vertical landing
05/23/2012CN202226057U Rotatable aerofoil airplane with variable flight mode
05/23/2012CN102470922A 多传动比旋翼飞行器驱动系统以及改变其齿轮传动比的方法 Multi-rotor drive gear ratio system and change the way their gear ratios
05/23/2012CN102464107A 消除直升机机翼抖震和提升飞行速度的新理论和方法 Eliminate bouncing helicopter wings and upgrading new theories and methods of flying speed
05/23/2012CN101965217B Acrobatic rotary-wing toy helicopter
05/23/2012CN101559832B Fast hybrid helicopter with large range
05/23/2012CN101549754B A composite rotating fixed-wing aircraft and its design method
05/23/2012CN101525050B Gyroplane blade provided with spar surrounded by fasteners and construction method of spar
05/23/2012CN101456451B Rotorcraft blade, rotorcraft rotor equipped with said blade and method of manufacturing this blade
05/22/2012US8182233 Component with a damping filler
05/22/2012US8181901 Fast hybrid helicopter with long range and proportional drive to the rotor and the propeller
05/22/2012US8181755 Dual spring rate damper
05/18/2012WO2012064345A1 Propulsive anti-torque nozzle system with rotating thrust director for a rotorcraft
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