Patents
Patents for B64C 27 - Rotorcraft; Rotors peculiar thereto (10,112)
01/1984
01/24/1984US4427340 Soft inplane bearingless helicopter rotor
01/18/1984EP0098739A1 Improvements in or relating to link means
01/18/1984EP0098704A2 Helicopter rotors
01/17/1984CA1160612A1 Flying craft
01/11/1984EP0097885A2 Soft inplane bearingless helicopter rotor
01/10/1984US4425082 Composite hub for a helicopter rotor
12/1983
12/28/1983EP0097091A1 Vibration damper, in particular a frequency adapter for helicopter blades
12/27/1983US4422757 Apparatus and method for optical phasing of helicopter main rotor blades
12/20/1983US4421287 Helicopter cyclic stick midposition feel indicator
12/13/1983US4420808 Multi-axis force stick, self-trimmed aircraft flight control system
12/13/1983US4420134 Vibration isolator with crank driven inertia bar
12/13/1983CA1158622A1 Blade retention system
12/07/1983EP0095994A1 Helicopter power available to hover indicator
12/06/1983US4419398 Laminated stop of curved shape, particularly for the rotors of helicopters
12/06/1983US4419051 Twin tension/torsion beam rotor system
12/06/1983CA1158219A1 Multi-axis force stick, self-trimmed aircraft flight control system
11/1983
11/30/1983EP0095434A2 Super contingency aircraft engine control
11/22/1983US4416434 Blade section for rotating wings of an aircraft
11/09/1983EP0093684A2 Helicopter engine control with rotor speed decay anticipator
11/09/1983EP0022847B1 Desensitizing helicopter control response to inadvertent pilot input
11/01/1983US4412784 Monocoque type rotor blade
11/01/1983US4412664 Family of airfoil shapes for rotating blades
10/1983
10/26/1983EP0092500A2 Helicopter engine torque compensator
10/26/1983EP0092424A2 Method and apparatus for damping aircraft rotor drive
10/26/1983EP0091969A1 Rotor, in particular for rotorcraft
10/19/1983EP0091744A1 Helicopter transmission systems
10/13/1983WO1983003395A1 Aircraft without engine
10/04/1983US4407688 Method of making helicopter blade spars
10/04/1983US4407635 Aircraft propeller assembly with composite blades
10/04/1983US4407633 Helicopter rotor
10/04/1983US4407467 Tactical wire-cutter system for helicopters
10/04/1983US4407466 Jet nozzle rotary wing aircraft
09/1983
09/28/1983EP0089793A1 Helicopter rotors
09/28/1983EP0089381A1 Rotor for rotorcraft
09/20/1983US4405103 Hydraulically operated air borne rotor craft
09/20/1983US4405101 Vibration isolation system
09/20/1983US4404794 Turbo-generator for a rotary wing helicopter
09/14/1983EP0088247A1 Device operated by an explosive charge to free a loaded connection
09/13/1983US4403918 Hubless, hingeless and bearingless helicopter rotor system
09/13/1983US4403681 Three directional vibration isolator
09/13/1983CA1153810A1 Tested, dissimilar helicopter stability augmentation
08/1983
08/24/1983EP0086490A1 Twin tension/torsion beam rotor system
08/10/1983EP0085129A1 Rotor, particularly for rotary wing aircraft
08/10/1983EP0085128A1 Rotor, particularly for a rotary wing aircraft
08/10/1983EP0085127A1 Rotor, in particular for rotary wing aircraft, with fibre-reinforced plastic hub
08/02/1983CA1151130A1 Unmanned remotely piloted aircraft
07/1983
07/20/1983EP0027468B1 Blade fold restraint system
07/12/1983US4392781 High performance blade for helicopter rotor
07/05/1983CA1149360A1 Pylon mounting system for reducing helicopter vibration
06/1983
06/28/1983US4390148 Rotary wing device
06/21/1983US4389162 Rotor blade comprising a plurality of individual sections
06/14/1983US4387867 Flying craft
06/08/1983EP0080920A1 Rotor for rotor craft with articulated joints incorporated in the blade root
06/07/1983US4387432 Pulsed aircraft actuator
06/07/1983US4386989 Method for producing a bendable and twistable element and such an element produced thereby
06/07/1983US4386748 Aircraft with counterrotating members
06/01/1983EP0080292A1 Helicopter rotors
05/1983
05/24/1983US4385355 Automatic outer loop centering of aircraft inner loop
05/18/1983EP0078915A2 Twisted structural construction element and device for working progression planes
05/11/1983EP0023909B1 Tail rotor control cable-pylon fold accommodation
05/03/1983US4382283 Helicopter attitude and airspeed acquisition and retention system
05/03/1983US4381902 Helicopter tail rotor of the elastomerically-mounted composite flexbeam type
05/03/1983CA1145734A1 Helicopter blade with a tip having a selected combination of sweep, taper, and anhedral to improve hover efficiency
05/03/1983CA1145569A1 Turbogenerator for helicopter rotor
04/1983
04/20/1983EP0077132A1 Improvements in and relating to a torsion link
04/12/1983US4379678 Individual blade control
04/06/1983EP0075877A2 Nonlinear vibration absorber
03/1983
03/30/1983EP0075407A1 Helicopter rotor
03/22/1983CA1143354A1 Helicopter blade with a tip having a selected combination of sweep, taper, and anhedral to improve hover efficiency
03/15/1983US4376979 Updated lock-positioning of foldable helicopter blades
03/08/1983US4375940 Rotor shaft with internal controls for helicopters
03/01/1983CA1142155A1 Inplane nodalization system
02/1983
02/22/1983CA1141738A1 Rotary wing rotor blade profile
02/15/1983US4373862 Rotor blade shaft integrity monitoring system
02/09/1983EP0070973A1 Servo control valve, in particular for a hydraulic servocontrolled airplane
02/08/1983US4372431 Six axis vibration isolation system
02/01/1983US4371938 Automatic airspeed engage/disengage
02/01/1983US4371314 Air jet helicopter rotor hub and air distribution system
01/1983
01/20/1983WO1983000118A1 Method of manufacturing a preform from fiber reinforced composite material
01/19/1983EP0069815A1 Device and procedure for measuring and checking the deviation in the wake of helicopter blades
01/18/1983US4369019 Helicopter rotor comprising elastomer joints
01/18/1983US4369018 Rotor head structure with stacked connecting elements, especially for a helicopter
01/12/1983EP0069455A1 Connecting element and helicopter rotor incorporating same
01/11/1983US4368006 Droop stop for fully articulated rotor
01/05/1983EP0068677A1 Transmission systems
01/04/1983US4367063 Pitch control mechanism for coaxial helicopter steering
12/1982
12/29/1982EP0067952A1 Rotor wherein the blade is joined to the rotor head by a root section which is flexible in torsion, flap and lead-lag
12/28/1982US4365936 Laminated elastomeric bearing unit
12/28/1982US4365771 Inplane nodalization system
12/28/1982US4365770 Fixed position variable frequency pendular-type vibration absorber
12/28/1982CA1138343A1 Rotor for operation in a flow medium
12/27/1982EP0059735A4 Hybrid composite structures.
12/22/1982EP0067548A1 Vibration suppressor
12/15/1982EP0067097A1 Tip for a rotor craft blade
12/07/1982US4362588 Method of fabricating a ducted blanket for a rotor spar
12/07/1982US4362281 Pylon mounting system for reducing helicopter vibration
12/07/1982US4362085 Flight control system
11/1982
11/30/1982US4361415 Rotary-wing aircraft rotor having a compact articulated hub
11/23/1982US4360337 Damping device for a helicopter rotor blade
11/10/1982EP0064346A1 Helicopters
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