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  2. Rotorhead - Wikipedia

    en.wikipedia.org/wiki/Rotorhead

    The rotorhead is where the lift force from the rotor blades act. The rotorhead is connected to the main drive shaft via the Jesus nut, and houses several other components such as the swash plate, flight control linkages and fly-bars. [1] The rotor hub is also where the centre of gravity acts on the helicopter. The rotor head of a Sikorsky S-92

  3. Helicopter rotor - Wikipedia

    en.wikipedia.org/wiki/Helicopter_rotor

    Diagram of fully articulated main rotor head. Juan de la Cierva developed the fully articulating rotor for the autogyro. The basis of his design permitted successful helicopter development. In a fully articulated rotor system, each rotor blade is attached to the rotor hub through a series of hinges that let the blade move independently of the ...

  4. File:Fully articulated main rotor head.svg - Wikipedia

    en.wikipedia.org/wiki/File:Fully_articulated...

    English: Parts of fully articulated main rotor head of helicopters and the associated motions of the blades. Date: 7 September 2013, 08:43:27: Source:

  5. Sikorsky UH-60 Black Hawk - Wikipedia

    en.wikipedia.org/wiki/Sikorsky_UH-60_Black_Hawk

    The main rotor is fully articulated and has elastomeric bearings in the rotor head. The tail rotor is canted and features a rigid crossbeam. [27] The helicopter has a long, low profile shape to meet the Army's requirement for transporting aboard a C-130 Hercules, with some disassembly. [26]

  6. Helicopter - Wikipedia

    en.wikipedia.org/wiki/Helicopter

    At the top of the mast is the attachment point for the rotor blades called the hub. Main rotor systems are classified according to how the rotor blades are attached and move relative to the hub. There are three basic types: hingeless, fully articulated, and teetering; although some modern rotor systems use a combination of these. [citation needed]

  7. AgustaWestland AW109 - Wikipedia

    en.wikipedia.org/wiki/AgustaWestland_AW109

    The engines drive a fully articulated four-blade rotor system. [16] Over time, more advanced rotor blade designs have been progressively adopted for the AW109's main and tail rotors, such as composite materials being used to replace bonded metal, [ 17 ] these improvements have typically been made with the aim of reducing operating costs and ...

  8. Boeing Vertol YUH-61 - Wikipedia

    en.wikipedia.org/wiki/Boeing_Vertol_YUH-61

    This also resulted in the main rotor being mounted very close to the cabin roof. While Sikorsky chose a fully articulated rotor head with elastomeric bearings, Boeing Vertol chose a rigid main rotor design, based upon technology supplied by MBB , which was partnered with Boeing Vertol at the time. [ 5 ]

  9. Schweizer S300 - Wikipedia

    en.wikipedia.org/wiki/Schweizer_S300

    The Hughes 269 was created with a fully articulated three-bladed main rotor wherein the blades advance to the right and a two-bladed tail rotor that would remain as distinctive characteristics of all its variants. It also has shock absorber-damped, skid-type landing gear.

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