Patents for B64C 27 - Rotorcraft; Rotors peculiar thereto (10,112) |
---|
04/17/1996 | EP0600040B1 Bearingless main rotor assembly torque tube |
04/09/1996 | US5505589 For a rotary wing aircraft |
03/26/1996 | US5501434 Hybrid fluid and elastomer damper |
03/19/1996 | US5499903 For securing a helicopter snubber bearing |
03/14/1996 | WO1996002417A3 Apparatus and methods for fabricating a helicopter main rotor blade |
03/13/1996 | EP0700828A1 Method of controlling the resultant aerodynamic force produced by a propeller and a device for carrying out the said method |
03/13/1996 | EP0700510A1 Monitoring apparatus |
03/13/1996 | EP0700350A1 A flexbeam for a helicopter bearingless main rotor assembly |
03/12/1996 | US5498129 Counter-torque device with ducted tail rotor and ducted flow-straightening stator, for helicopters |
03/12/1996 | US5497960 Device for aircraft and aircraft provided with such a device |
03/07/1996 | WO1996006776A1 Fiber reinforced composite spar for a rotary wing aircraft and method of manufacture thereof |
03/07/1996 | WO1996006775A1 Method and apparatus for balancing helicopter rotor blades |
03/07/1996 | CA2198718A1 Method and apparatus for balancing helicopter rotor blades |
02/29/1996 | WO1996006006A1 Yaw control and stabilization system for helicopters |
02/29/1996 | WO1996006005A1 Model helicopter |
02/21/1996 | EP0696984A1 Airborne vehicule |
02/21/1996 | EP0696983A1 Ancillary aerodynamic structures for an unmanned aerial vehicle having ducted, coaxial counter-rotating rotors |
02/20/1996 | US5492448 Rotary blades |
02/15/1996 | WO1996004492A1 Fluid damping devices |
02/15/1996 | WO1996004125A1 Method and apparatus for forming airfoil structures |
02/06/1996 | US5489193 Antivibration supports for helicopter blades, and a helicopter rotor including such supports |
02/01/1996 | WO1996002417A2 Apparatus and methods for fabricating a helicopter main rotor blade |
02/01/1996 | WO1996002416A1 An eop scribe device |
02/01/1996 | CA2195077A1 An eop scribe device |
01/23/1996 | US5486096 Erosion resistant surface protection |
01/18/1996 | WO1996001503A1 Piezoelectric actuator |
01/18/1996 | DE4424720A1 System pressure actuated by=pass valve for servomotor |
01/11/1996 | WO1996000842A1 Erosion resistant surface protection |
01/11/1996 | DE4422987A1 Tilt rotor vertical take off aircraft |
01/10/1996 | CN1114831A Flight device |
01/10/1996 | CN1114623A Operation of a helicopter |
01/08/1996 | WO1996022914A1 Power transmission device for helicopter |
01/04/1996 | DE4423247A1 Single=bladed rotor with passive aerodynamic autonomous control |
01/03/1996 | EP0689990A1 Noise reduction device for rotorcraft |
01/03/1996 | EP0667283A4 Hybrid aircraft. |
01/03/1996 | EP0642441B1 Variable diameter rotor having an offset twist |
12/28/1995 | WO1995035455A1 Self-scavenging, hybrid lubrication subsystem |
12/28/1995 | WO1995035235A1 Aircraft rotor arrangement |
12/26/1995 | US5478204 Ducted fan and pitch controls for tail rotor of rotary wing aircraft |
12/26/1995 | US5478029 Rotorcraft blade-vortex interaction controller |
12/14/1995 | WO1995034029A1 Inertial velocity command system |
12/14/1995 | WO1995029842A3 Main rotor system for helicopters |
12/14/1995 | CA2191861A1 Inertial velocity command system |
12/13/1995 | EP0686554A1 Stator and composite stator blade for a counter-torque device consisting of a shrouded rotor and stator and their manufacturing method |
12/13/1995 | EP0595914B1 Adaptive control system input limiting |
12/12/1995 | US5475622 Method and apparatus for balancing helicopter rotor blades |
12/12/1995 | US5474424 Rotorcraft rotor head, which is rigid in drag and articulated in pitch and flapping |
12/07/1995 | WO1995032895A1 A stacked compound planetary gear train for an upgraded powertrain system for a helicopter |
12/05/1995 | US5472386 Stacked compound planetary gear train for an upgraded powertrain system for a helicopter |
12/05/1995 | US5472156 Air combat collective control head |
11/23/1995 | DE4417144A1 Aircraft buoyancy rotor with tangential drive |
11/22/1995 | CN1030303C Fuselage structure for helicopter |
11/16/1995 | WO1995030843A1 Hybrid fluid and elastomer damper |
11/16/1995 | WO1995030575A1 An unmanned vtol ground surveillance vehicle |
11/16/1995 | CA2189854A1 An unmanned vtol ground surveillance vehicle |
11/09/1995 | WO1995030181A1 Turn coordination inhibit for rotary wing aircraft control system |
11/09/1995 | WO1995029842A2 Main rotor system for helicopters |
11/08/1995 | EP0680876A1 Anti-torque shrouded rotor with play-mounted blades |
11/08/1995 | EP0680875A1 Anti-torque device with shrouded rotor and straightening stator for helicopters |
11/08/1995 | EP0680874A1 Stator guide vane for anti-torque device with shrouded rotor and straightening stator for helicopters |
11/08/1995 | EP0680873A1 Anti-torque device with shrouded rotor and straightening stator and slanted guide vanes |
11/08/1995 | EP0680872A1 Anti-torque device with shrouded rotor and straightening stator and phase modulation of the rotor blades positions, for helicopters |
11/08/1995 | EP0680871A1 Anti-torque device with shrouded rotor and phase modulation of the rotor blades positions for helicopters |
11/08/1995 | EP0448711B1 Jam resistant ball screw actuator |
11/07/1995 | US5465212 Helicopter integrated fire and flight control having a pre-launch and post-launch maneuver director |
11/02/1995 | EP0535114B1 Linkage rod |
10/31/1995 | US5462409 Leading edge weight retention assembly for a helicopter rotor |
10/31/1995 | US5462408 Blade made of thermoplastic composite, in particular for ducted tail rotor of a helicopter, and its method of manufacture |
10/31/1995 | US5462137 Gyroplane rotor braking unit |
10/31/1995 | US5461796 Gunsight device for rotating-wing aircraft |
10/26/1995 | WO1995028761A2 A system for generating power and propulsive force or lift by use of an electrostatic motor |
10/25/1995 | EP0678448A1 Helicopter anti-torque and yaw control system |
10/24/1995 | US5460487 Pitch adjustment assembly for bearingless main rotors |
10/12/1995 | WO1995026904A1 Method of controlling the resultant aerodynamic force produced by a propeller and a device for carrying out the said method |
10/11/1995 | EP0676015A1 Tubular elastomer damper |
10/10/1995 | US5456341 Method and apparatus for actively adjusting and controlling a resonant mass-spring system |
10/03/1995 | US5454693 Blade made of thermoplastic composite, in particular for ducted tail rotor of a helicopter, and its method of manufacture with injection step |
10/03/1995 | US5454691 Flow-straightener vane for counter-torque device with ducted rotor and ducted flow-straightening stator, for helicopter |
10/03/1995 | US5454530 Canard rotor/wing |
10/03/1995 | US5454153 Adjustable assembly for use in the repair or replacement of a pitch change link or rod end of critical predetermined length |
09/21/1995 | WO1995025037A1 Airborne vehicule |
09/20/1995 | CN2207997Y Single helicopter |
09/19/1995 | US5451472 Multiple density sandwich structures and method of fabrication |
09/19/1995 | US5451015 Crashworthy composite aircraft structure with integral fuel tank |
09/14/1995 | WO1995024339A1 An expandable spar filler block device |
09/14/1995 | CA2184370A1 An expandable spar filler block device |
09/13/1995 | EP0670796A1 Rotor blade balance weight assembly. |
09/12/1995 | US5449152 Tubular elastomer damper |
08/30/1995 | EP0668829A1 Flight device. |
08/30/1995 | EP0668828A1 A pitch actuation system restraint device for a helicopter blade folding system. |
08/22/1995 | CA2028023C Rotary viscons-elastic return device, and drag damping, for a gyroplane rotor black, and rotor head containing same |
08/17/1995 | WO1995021765A1 An optical tracker system |
08/17/1995 | CA2182566A1 An optical tracker system |
08/16/1995 | EP0667283A1 Hybrid aircraft |
08/10/1995 | WO1995021327A1 Windmill blade |
08/09/1995 | EP0665795A1 Rotary wing comprising two coaxial rotors. |
08/09/1995 | EP0601123B1 Low speed model following velocity command system for rotary wing aircraft |
08/08/1995 | US5440193 Method and apparatus for structural, actuation and sensing in a desired direction |
08/01/1995 | US5437419 Rotorcraft blade-vortex interaction controller |
07/27/1995 | WO1995020104A1 Fabrication of aerodynamic profiles |