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  2. Disk loading - Wikipedia

    en.wikipedia.org/wiki/Disk_loading

    When a helicopter is being maneuvered, its disk loading changes. The higher the loading, the more power needed to maintain rotor speed. [3] A low disk loading is a direct indicator of high lift thrust efficiency. [4] Increasing the weight of a helicopter increases disk loading. For a given weight, a helicopter with shorter rotors will have ...

  3. Helicopter rotor - Wikipedia

    en.wikipedia.org/wiki/Helicopter_rotor

    This three-engined helicopter has a single large main rotor and smaller tail rotor. On a helicopter, the main rotor or rotor system is the combination of several rotary wings (rotor blades) with a control system, that generates the aerodynamic lift force that supports the weight of the helicopter, and the thrust that counteracts aerodynamic ...

  4. Eagle Helicycle - Wikipedia

    en.wikipedia.org/wiki/Eagle_Helicycle

    The Helicycle is a single-seat, semi-rigid two-bladed main rotor, helicopter powered by a Solar T62-32 engine. Manufactured by Helicycle Ventures LLC in Mesilla, New Mexico as a kit, the aircraft is intended to be assembled by the owner and is considered a homebuilt aircraft.

  5. EDM Aerotec CoAX 2D/2R - Wikipedia

    en.wikipedia.org/wiki/EDM_Aerotec_CoAX_2D/2R

    The CoAX 2D/2R was originally known as the FLIP 2 (Fly In Perfection) and is a derivative of the FLIP 1, a conventional helicopter with a main and tail rotor.[1]The CoAX 2D/2R was designed to comply with the European Class 6 microlight helicopter rules, including the category's maximum takeoff weight of 450 kg (992 lb).

  6. Coning (aerodynamics) - Wikipedia

    en.wikipedia.org/wiki/Coning_(aerodynamics)

    Coning is a phenomenon which affects helicopter rotor discs, where the blades describe a cone shape as they rotate. For a helicopter on the ground, as the blades rotate, they describe a horizontal disc due to centrifugal force. However, as the helicopter generates lift, the blades are pulled upwards into a cone shape. [1] [2] [3]

  7. Dynali H3 EasyFlyer - Wikipedia

    en.wikipedia.org/wiki/Dynali_H3_EasyFlyer

    The aircraft fuselage frame is made from welded stainless steel tubing. Its two-bladed rotor has a diameter of 7.14 m (23.4 ft) and a chord of 18.5 cm (7.3 in). With the Rotax 914 engine the aircraft has a typical empty weight of 290 kg (639 lb) and a gross weight of 600 kg (1,323 lb), giving a useful load of 310 kg (683 lb).

  8. Windspire Aeros - Wikipedia

    en.wikipedia.org/wiki/Windspire_Aeros

    The aircraft fuselage is made from a mix of aluminum and steel tubing. Its 22.0 ft (6.7 m) diameter two-bladed rotor has a chord of 8 in (20.3 cm) and employs a NACA 0012 airfoil. The drive train consists of a primary belt drive connected to a geared transmission built with Volkswagen gears and a belt-driven tail rotor drive. The tail rotor has ...

  9. Gyrodyne RON Rotorcycle - Wikipedia

    en.wikipedia.org/wiki/Gyrodyne_RON_Rotorcycle

    The Gyrodyne RON Rotorcycle (originally designated HOG) was a tiny, single-seat helicopter designed under contract for the United States Navy. [1] in the mid-1950s.It later was redesigned for a U.S. Marine Corps requirement for a small personal helicopter that would fulfill an array of roles, including observation, liaison, small unit tactical maneuvers, and which could be dropped to downed ...