articulated rotor

articulated rotor
несущий винт с шарнирно закреплёнными лопастями

Englsh-Russian aviation and space dictionary. - M.: Military publishing house USSR Ministry of Defence. . 1974.

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  • articulated rotor — A rotor in which the individual blades are free to flap (i.e., move up and down), drag (i.e., move back and forth in the plane of rotation), and change their pitch angle independently. This is done by mounting the blades on flapping and drag… …   Aviation dictionary

  • fully articulated rotor — A rotor with three or more blades in which the individual blades are free to flap (move up and down), drag (move back and forth in the plane of rotation), and change their pitch angle as they rotate around the disc. This is done by mounting the… …   Aviation dictionary

  • rotor system types — There are three types of rotors: rigid, semirigid, and fully articulated. In a rigid rotor, the blades are free to change pitch but otherwise are made as rigid as possible. The blades of rigid rotor have no hinges that allow them to flap or drag …   Aviation dictionary

  • Helicopter rotor — This article is about helicopter main rotor systems. For antitorque control, see tail rotor. Helicopter rotor The rotor head of a Sikorsky S 92 A helicopter main rotor or rotor system is a type of fan that is used to generate both the aerodynamic …   Wikipedia

  • door-hinge rotor — Articulated blades on flapping hinges visually resembling a door hinge …   Aviation dictionary

  • Helicopter — For other uses, see Helicopter (disambiguation). Helicopter An LAPD Bell 206 …   Wikipedia

  • TH-55 Osage — Infobox Aircraft name = TH 55 Osage Hughes 269 caption = Hughes TH 55 Osage type=Light utility and trainer helicopter manufacturer= Hughes Helicopters designer= first flight= October 1956 introduced= retired= status= primary user= United States… …   Wikipedia

  • Juan de la Cierva — This name uses Spanish naming customs; the first or paternal family name is De la Cierva and the second or maternal family name is Codorníu. Juan de la Cierva …   Wikipedia

  • Transverse flow effect — is an aerodynamic effect encountered when the helicopter moves (typically forward) through the air.In a hover, the air above the rotor disk is being pulled down from above and is equally distributed around the rotor disk. The air is descending… …   Wikipedia

  • Cierva C.8 — C.8 Role experimental autogyro Manufacturer Cierva Designer Juan de la Cierva First flight 1926 Number built 6 The Cierva C.8 was an experimental autogyro built by Juan de la Cierva in England in 1926 in a …   Wikipedia

  • Air & Space 18A — Infobox Aircraft name=Air Space 18A caption= type=Autogyro manufacturer=Air and Space Manufacturing, Inc. developer=Raymond E. Umbaugh designer=Gilbert Devore first flight=1964 introduced=1965 retired= status=Out of production primary user= more… …   Wikipedia


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