| Patents for B64C 27 - Rotorcraft; Rotors peculiar thereto (10,112) |
|---|
| 03/20/2008 | US20080067284 Personal Land And Air Vehicle |
| 03/19/2008 | EP1901153A1 Control system for unmanned 4-rotor-helicopter |
| 03/19/2008 | EP1900636A1 Marine propulsion and constructional details thereof |
| 03/18/2008 | US7344108 Landing assist apparatus interface bulkhead and method of installation |
| 03/13/2008 | US20080065278 Mechanical Flight Control Auxiliary Power Assist System |
| 03/13/2008 | DE202007016293U1 Flugobjekt mit Tandemrotoren Flying object with tandem rotors |
| 03/13/2008 | DE202006020255U1 Helikopter Helicopter |
| 03/13/2008 | DE202006020254U1 Helikopter Helicopter |
| 03/12/2008 | CN101140011A Tandem stack angular contact bearing for rotary wing aircraft |
| 03/06/2008 | US20080056903 LP turbine blade airfoil profile |
| 03/06/2008 | US20080056902 HP turbine blade airfoil profile |
| 03/06/2008 | US20080056901 Turbine exhaust strut airfoil and gas path profile |
| 03/06/2008 | US20080054121 Ducted fan VTOL vehicles |
| 03/05/2008 | EP1893486A2 Variable speed transmission for a rotary wing aircraft |
| 03/05/2008 | EP1893483A2 Rotor blade for a high speed rotary-wing aircraft |
| 03/05/2008 | EP1893482A2 Rotor drive and control system for a high speed rotary wing aircraft |
| 03/05/2008 | EP1893314A2 Helicopter |
| 03/05/2008 | CN101134506A Helicopter rotor control mechanism |
| 03/05/2008 | CN101134505A Helicopter equilibrating and steadying technique |
| 03/05/2008 | CN100372735C Proprotor blade with leading edge slot |
| 02/28/2008 | WO2008002475B1 Speed changing gearbox with dual path input |
| 02/28/2008 | US20080048065 Flying Device With Improved Movement on The Ground |
| 02/28/2008 | DE102006037900A1 Signal transmission arrangement for structural component, has signal or power transmission between signal generator and signal receiver, where structural component has coupling designed at signal generator |
| 02/28/2008 | CA2598714A1 Tungsten carbide enhanced bearing |
| 02/27/2008 | EP1282555A4 Multi-mode tiltrotor nacelle control system with integrated envelope protection |
| 02/27/2008 | CN201026991Y Unpiloted telecontrolled dish shaped aircraft |
| 02/27/2008 | CN101132966A Propulsion device |
| 02/27/2008 | CN101131123A Multifunctional air inlet of turbine engine |
| 02/27/2008 | CN100371218C Vertiplane using power to directly push rotary wing changing into stopping wing |
| 02/27/2008 | CN100371217C Umbrella with wing blades and circular track |
| 02/26/2008 | US7334755 Tandem rotor wing and tandem fixed wing aircraft |
| 02/21/2008 | WO2008022201A2 Composite-steel hybrid mast for rotorcraft |
| 02/21/2008 | WO2008020848A2 Rotary-wing aircraft torque coupling with pad bearings |
| 02/21/2008 | WO2008020683A1 Main rotor assembly for helicopter |
| 02/21/2008 | US20080044288 Rotor blade for a second phase of a compressor |
| 02/21/2008 | US20080044283 Elastomeric bearing with heatable shims |
| 02/21/2008 | CA2660845A1 Composite-steel hybrid mast for rotorcraft |
| 02/20/2008 | EP1888403A2 Rotor hub fairing system for a counter-rotating, coaxial rotor system |
| 02/20/2008 | EP1888402A2 Apparatus for generating horizontal forces in aerial vehicles and related method |
| 02/19/2008 | US7331765 Two-sweep rotary wing blade with limited taper ratio |
| 02/19/2008 | US7331235 Device for indicating a beat level |
| 02/14/2008 | DE102007020609A1 Helicopter has main rotor and auxiliary rotor that are connected to each other by a mechanical link such that swinging motion of auxiliary rotor controls the angle of incidence of one propeller blade of the main rotor |
| 02/14/2008 | DE102006036389A1 Trailing edge flaps or ailerons for aircraft wing have spanwise anisotropic rubber panels covering chord gaps |
| 02/07/2008 | US20080031734 Main shaft slide sleeve assembly for remote control helicopter |
| 02/07/2008 | DE102007016701A1 Helikopter mit horizontaler Steuerung Helicopter with horizontal control |
| 02/06/2008 | EP1884047A2 De-rotation system for counter-rotating, coaxial rotor hub shaft fairing |
| 02/06/2008 | EP1883578A2 Aircraft jet engine pylon suspension attachment |
| 02/06/2008 | EP1754031B1 Method of adjusting at least one faulty rotor of a rotorcraft |
| 02/06/2008 | CN101117156A Jetocopter |
| 02/06/2008 | CN100366873C Radial engine |
| 02/05/2008 | US7326435 Method of illuminating a rotary blade by application of a photoluminescent paint |
| 01/31/2008 | US20080023586 Tiltrotor aircraft drivelink |
| 01/31/2008 | US20080023583 Composite anti-crash structure with lateral retention, for an aircraft |
| 01/31/2008 | US20080023582 Composite anti-crash structure with controlled buckling for an aircraft |
| 01/31/2008 | DE102006054467A1 Verfahren und Vorrichtung zur Zustandsüberwachung des Wälzlagers einer Taumelscheibe eines Drehflüglers Method and apparatus for monitoring the condition of the rolling bearing of a swash plate of a rotorcraft |
| 01/30/2008 | EP1882628A2 Method and device for status monitoring of the roller bearing of a swash plate of a rotorcraft |
| 01/29/2008 | US7324016 Navigational indicating system for rotary wing aircraft |
| 01/24/2008 | DE10258545B4 Verfahren und System zur Stabilisierung einer Translationsbewegungsgröße eines Flugkörpers Method and system for stabilizing a translational movement quantity of a missile |
| 01/23/2008 | CN101111429A Assembly for providing flexure to blade system |
| 01/23/2008 | CN101108654A Double-culvert one-seater vertically taking off and landing flyer |
| 01/17/2008 | WO2008006784A1 Aircraft engine attachment device comprising two thrust-reacting link rods that fit together transversely |
| 01/17/2008 | WO2007140362A3 Rotary wing aircraft rotary lead lag damper |
| 01/17/2008 | WO2007084234A3 Helicopter |
| 01/17/2008 | US20080014091 Frequency tailored thickness blade for a turbomachine wheel |
| 01/17/2008 | US20080014087 Tail rotor for remotely controlled toy helicopter |
| 01/17/2008 | CA2658149A1 Aircraft engine mount structure comprising two thrust links with transverse fitting |
| 01/16/2008 | EP1877930A2 Fly by wire static longitudinal stability compensator system |
| 01/16/2008 | EP1877307A2 Rotary wing aircraft |
| 01/16/2008 | CN101107164A Assembly for providing flexure to blade system |
| 01/16/2008 | CN101107163A 旋翼机传扭器 Rotorcraft transmission torque converter |
| 01/16/2008 | CN101107162A Wire strike system |
| 01/16/2008 | CN100361868C Second generation automobile helivehicle plane |
| 01/10/2008 | WO2008003455A1 Aircraft with a convertible flight system |
| 01/10/2008 | US20080008592 Method and apparatus for controlling tonal noise from subsonic axial fans |
| 01/10/2008 | US20080008587 Cyclical wave energy converter |
| 01/10/2008 | US20080006737 Aircraft |
| 01/09/2008 | EP1718526B1 Wire strike system |
| 01/03/2008 | WO2008002475A1 Speed changing gearbox with dual path input |
| 01/03/2008 | WO2008002338A2 Rotary fluid dynamic utility structure |
| 01/03/2008 | WO2008000203A1 Aircraft |
| 01/03/2008 | US20080003109 Component of variable thickness having residual compressive stresses therein, and method therefor |
| 01/03/2008 | US20080003106 Rotor apparatus and methods for vertical lift aircraft |
| 01/03/2008 | US20080003103 Vortex control for rotor blade devices |
| 01/03/2008 | DE102006030089B3 Helicopter rotor control device, has rotor shaft connected with rotor head, and wobble plates with respective rotary parts that are connected with rotor blade, where one plate is arranged around other plate |
| 12/27/2007 | WO2007147650A1 Controlled rotor brake |
| 12/27/2007 | WO2007147640A1 A flying aircraft supported by a birotor having dihedral blades |
| 12/27/2007 | WO2007075805A3 Retractable lifting blades for aircraft |
| 12/27/2007 | WO2005033544A3 Harmonic force generator for an active vibration control system |
| 12/27/2007 | US20070298663 Composite structural member having an integrated electrical circuit |
| 12/27/2007 | US20070295857 Emergency Device |
| 12/27/2007 | DE102006028671A1 Geregelte Rotorbremse Controlled brake rotor |
| 12/27/2007 | DE102006027599A1 Profile shaped aerodynamic effective component e.g. airplane wings, airplane control, rotor blade and rotor of wind energy plant, has double walled vane shell and composition is almost free from raw material |
| 12/26/2007 | EP1870332A1 Decoupled ducting for twin-engine reaction rotor drive |
| 12/26/2007 | CN101092168A Flapping wings helicopter with changeable giro wing |
| 12/26/2007 | CN101092167A Dished aircraft |
| 12/21/2007 | WO2005079200A3 Active force generation system for minimizing vibration in a rotating system |
| 12/21/2007 | CA2650535A1 Compliant structure design for varying surface contours |
| 12/20/2007 | US20070292273 Turbine blade with ceramic tip |
| 12/20/2007 | DE102006028167A1 Device e.g. wind energy plant, operating method, involves detecting characteristic values by sensors, and conducting fluid coming from pressure source outwards to medium surrounding lifting body |
| 12/19/2007 | CN101091055A A wind turbine blade equipped internally with collection means |