FI (list display)

  • B64C27/00
  • Rotorcraft; Rotors peculiar thereto [1, 2006.01] HB CC 3D140
  • B64C27/02
  • .Gyroplanes HB CC 3D140
  • B64C27/04
  • .Helicopters HB CC 3D140
  • B64C27/06
  • ..with single rotor HB CC 3D140
  • B64C27/08
  • ..with two or more rotors HB CC 3D140
  • B64C27/10
  • ...arranged coaxially HB CC 3D140
  • B64C27/12
  • ..Rotor drives HB CC 3D140
  • B64C27/14
  • ...Direct drive between power plant and rotor hub HB CC 3D140
  • B64C27/16
  • ...Drive of rotors by means, e.g. propellers, mounted on rotor blades HB CC 3D140
  • B64C27/18
  • ....the means being jet-reaction apparatus HB CC 3D140
  • B64C27/20
  • .Rotorcraft characterised by having shrouded rotors, e.g. flying platforms HB CC 3D140
  • B64C27/22
  • .Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft HB CC 3D140
  • B64C27/24
  • ..with rotor blades fixed in flight to act as lifting surfaces HB CC 3D140
  • B64C27/26
  • ..characterised by provision of fixed wings HB CC 3D140
  • B64C27/28
  • ..with forward-propulsion propellers pivotable to act as lifting rotors HB CC 3D140
  • B64C27/30
  • ..with provision for reducing drag of inoperative rotor HB CC 3D140
  • B64C27/32
  • .Rotors [1, 2006.01] HB CC 3D140
  • B64C27/33
  • ..having flexing arms [3] HB CC 3D140
  • B64C27/35
  • ..having elastomeric joints [3] HB CC 3D140
  • B64C27/37
  • .. having articulated joints [3, 2006.01] HB CC 3D140
  • B64C27/39
  • ...with individually articulated blades, i.e. with flapping or drag hinges [3] HB CC 3D140
  • B64C27/41
  • ...with flapping hinge or universal joint, common to the blades [3] HB CC 3D140
  • B64C27/43
  • ....see-saw type, i.e. two-bladed rotor [3] HB CC 3D140
  • B64C27/45
  • ...with a feathering hinge only [3] HB CC 3D140
  • B64C27/46
  • ..Blades HB CC 3D140
  • B64C27/467
  • ...Aerodynamic features [6] HB CC 3D140
  • B64C27/473
  • ...Constructional features [6] HB CC 3D140
  • B64C27/48
  • ....Root attachment to rotor head HB CC 3D140
  • B64C27/50
  • ....Blades foldable to facilitate stowage of aircraft HB CC 3D140
  • B64C27/51
  • .Damping of blade movements [3] HB CC 3D140
  • B64C27/52
  • .Tilting of rotor bodily relative to fuselage (of see-saw type construction B64C 27/43) HB CC 3D140
  • B64C27/54
  • .Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement HB CC 3D140
  • B64C27/56
  • ..characterised by the control initiating means, e.g. manually actuated [1, 2006.01] HB CC 3D140
  • B64C27/57
  • ...automatic or condition responsive, e.g. responsive to rotor speed, torque or thrust [3] HB CC 3D140
  • B64C27/58
  • ..Transmitting means, e.g. interrelated with initiating means or means acting on blades (means acting on blades B64C 27/72) [1, 2006.01] HB CC 3D140
  • B64C27/59
  • ...mechanical [3] HB CC 3D140
  • B64C27/605
  • ....including swash plate, spider or cam mechanisms [3] HB CC 3D140
  • B64C27/615
  • ....including flaps mounted on blades [3] HB CC 3D140
  • B64C27/625
  • ....including rotating masses or servo rotors [3] HB CC 3D140
  • B64C27/635
  • ....specially for controlling lag-lead movements of blades [3] HB CC 3D140
  • B64C27/64
  • ...using fluid pressure, e.g. having fluid power amplification [3] HB CC 3D140
  • B64C27/68
  • ...using electrical energy, e.g. having electrical power amplification [3] HB CC 3D140
  • B64C27/72
  • ..Means acting on blades HB CC 3D140
  • B64C27/78
  • ..in association with pitch adjustment of blades of anti-torque rotor HB CC 3D140
  • B64C27/80
  • ..for differential adjustment of blade pitch between two or more lifting rotors HB CC 3D140
  • B64C27/82
  • .characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting-rotor torque or changing direction of rotorcraft HB CC 3D140
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