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  2. Threaded insert - Wikipedia

    en.wikipedia.org/wiki/Threaded_insert

    TIME-SERT insert. A threaded insert, also known as a threaded bushing, is a fastener element that is inserted into an object to add a threaded hole. [1] They may be used to repair a stripped threaded hole, provide a durable threaded hole in a soft material, place a thread on a material too thin to accept it, mold or cast threads into a work piece thereby eliminating a machining operation, or ...

  3. Helical - Wikipedia

    en.wikipedia.org/wiki/Helical

    Helical may refer to: . Helix, the mathematical concept for the shape; Helical engine, a proposed spacecraft propulsion drive; Helical spring, a coilspring; Helical plc, a British property company, once a maker of steel bar stock

  4. Heli-Sport CH77 Ranabot - Wikipedia

    en.wikipedia.org/wiki/Heli-Sport_CH77_Ranabot

    The CH77 Ranabot was designed to comply with the European Class 6 microlight helicopter rules. It features a single main rotor and tail rotor, a single-seat, a two-seats-in side-by-side configuration enclosed cockpit, skid landing gear and an EPA Power-modified four-cylinder, liquid and air-cooled, four stroke 130 hp (97 kW) Rotax 914 engine.

  5. MD Helicopters MD Explorer - Wikipedia

    en.wikipedia.org/wiki/MD_Helicopters_MD_Explorer

    The design has a rotorless tail. The MD Helicopters MD Explorer is a twin engined utility helicopter; it is equipped with a fully-articulated five-bladed main rotor system as well as bearingless composite flexbeams and rotor hub.

  6. MBB Bo 105 - Wikipedia

    en.wikipedia.org/wiki/MBB_Bo_105

    The Messerschmitt-Bölkow-Blohm Bo 105 is a light, twin-engine, multi-purpose helicopter developed by Bölkow of Ottobrunn, West Germany.It was the first light twin-engine helicopter in the world, and the first rotorcraft that could perform aerobatic maneuvers such as inverted loops.

  7. NHIndustries NH90 - Wikipedia

    en.wikipedia.org/wiki/NHIndustries_NH90

    Data from AgustaWestland, Airbus Helicopters, The International Directory of Military Aircraft, 2002/2003 General characteristics Crew: 2 flight crew + loadmaster / sensor operator Capacity: 20 seated troops; or 12 medevac stretchers; or 2 NATO pallets; or 4,200 kg (9,259 lb) external slung load Length: 16.13 m (52 ft 11 in) Empty weight: 6,400 kg (14,110 lb) Max takeoff weight: 10,600 kg ...