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A typical helicopter has three flight control inputs: the cyclic stick, the collective lever, and the anti-torque pedals. [2] Depending on the complexity of the helicopter, the cyclic and collective may be linked together by a mixing unit , a mechanical or hydraulic device that combines the inputs from both and then sends along the "mixed ...
1. Non-rotating outer ring (blue). 2. Turning inner ring (silver). 3. Ball joint. 4. Control (pitch) preventing turning of outer ring. 5. Control (roll). 6. Linkages (silver) to the rotor blade. In aeronautics, a swashplate is a mechanical device that translates input via the helicopter flight controls into motion of the main rotor blades.
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
Pages in category "Helicopter components" The following 22 pages are in this category, out of 22 total. This list may not reflect recent changes. A. Apache Arrowhead; B.
The worldwide fleet of 190 AW101 helicopters had achieved in excess of 200,000 flight hours in Canada, UK, Italy, Denmark, Portugal, and Japan. [4] In June 2011, several former USN VH-71s, which are also based on the AW101, were purchased by Canada to be used as spare parts for the CH-149 fleet. [5]
A further 6 Mi-8T and 18 Mi-8MTV-1 helicopters were bought from ex-Warsaw Pact countries during the war, with 16 being used in active service, and remaining were used as source for spare parts. The remaining Mi-8Ts were retired from service in the Croatian Air Force after the war, while the Mi-8MTVs continued their service in 20th Transport ...
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 ...
The first Italian Navy production helicopter (MM81480) flew on 4 October 1999 and was officially presented to the press on 6 December 1999. Italy accepted delivery of the 21st AW101, configured for anti-submarine warfare, on 4 August 2009. [117] In total 22 AW101 helicopters have been delivered to the Italian Navy. [116]
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