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Mil V-12 at the Central Air Force Museum. Design studies for a giant helicopter were started at the Mil OKB in 1959, receiving official sanction in 1961 by the GKAT (Gosudarstvenny Komitet po Aviatsionnoy Tekhnike - State Committee on Aircraft Technology) instructing Mil to develop a helicopter capable of lifting 20 to 25 tonnes (22 to 28 short tons).
In 2015, the joint project with Russian Helicopters grew to 38.2 t (84,000 lb), with a seven blade main rotor and a 5,700 m (18,700 ft) ceiling. In 2016, Avic took control, leaving Russian Helicopters as a supplier, presumably of the transmission. In 2018, maximum weight grew again to 42 t (93,000 lb). [1]
That weight exceeded the maximum payload of 9.1 tonnes (20,000 lb) at an altitude of 2,600 metres (8,500 ft) of the U.S. military's Sikorsky CH-53E. [ 4 ] The Mi-26 was located through Skylink Aviation in Toronto , which had connections with a Russian company called Sportsflite that operated three civilian Mi-26 versions called "Heavycopters".
The XH-17 was a heavy-lift rotorcraft that was designed to lift loads in excess of 15 metric tons. To speed construction, parts of the XH-17 were scavenged from other aircraft. The front wheels came from a North American B-25 Mitchell and the rear wheels from a Douglas C-54 Skymaster.
The Sikorsky CH-54 Tarhe is an American twin-engine heavy-lift helicopter designed by Sikorsky Aircraft for the United States Army.It is named after Tarhe, an 18th-century chief of the Wyandot Indian tribe whose nickname was "The Crane". [2]
The Harbin Z-20 (Chinese: 直-20) is a Chinese medium-lift utility helicopter produced by the Harbin Aircraft Industry Group (HAIG). It was first flown on 23 December 2013 and has a maximum takeoff weight in the range of 10 tonnes (22,000 lb).
At 302 feet (92 m) long, it would classify as the largest helicopter in the world, and would be capable of flying up to 800 miles (1,300 km) without a load. [4] The craft would use helium to provide enough lift to carry its own weight , and would use four helicopter rotors to lift the load and to propel the aircraft. [ 3 ]
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).