Mi-30 is a project of the Soviet multi-purpose tiltrotor developed by the M. L. Mil MVZ under the direction of M. N. Tishchenko in 1972 . Inside the design bureau, this design scheme had its own name " propeller ". The main task was to provide such parameters of speed and flight range that would exceed the similar parameters of helicopters . The Mi-30 tiltrotor was considered as a replacement for the Mi-8 multipurpose helicopter in the future.
| Mi-30 | |
|---|---|
Mi-30 model in transition flight mode | |
| Type of | Passenger and freight; military transport |
| Chief Designer | |
Content
Flight performance
As the power plant, it was supposed to use two TV3-117 engines located above the cargo compartment, which were supposed to actuate by means of a transmission two main rotors with a diameter of 11 m each. The estimated flight speed was to be 500 - 600 km / h, flight range - 800 km, take-off weight - 10.6 tons. The Mi-30 in the original design was intended for passenger and freight transportation of 19 passengers or 2 tons of cargo. [1] . Subsequently, the carrying capacity was increased to 3-5 tons, and passenger capacity up to 32 people [2] .
Military Modification
The military approved the development, but demanded that the propeller plane be equipped with a more powerful power plant with two D-136 engines. The estimated mass of such an apparatus increased to 30 tons [2] .
See also
- Bell v-22 osprey
- Bell xv-15
- Bell xv-3
Notes
- ↑ Mi-30 helicopter (inaccessible link) . Moscow Helicopter Plant named after M. L. Mil . Date of treatment April 13, 2012. Archived September 17, 2012.
- ↑ 1 2 Vadim Mikheev. and how are we? The “Vintoplan” project Mi-30 (15.2 Mb) (Russian) // Takeoff : National Aerospace Journal / Ed. A. Fomina. - M .: LLC Aeromedia. - Vol. 2006 . - No. 10 . - S. 18-19 . - ISSN 1819-1754 .
Links
Literature
- V.R. Mikheev. Moscow Helicopter Plant. M. L. Mil. 50 years. - M .: Favorite book, 1998.
- Shcherbakov V. The convertorplanes of the country of the Soviets // Brother: Monthly magazine of special forces. - M .: Vityaz-Bratishka LLC, 2012. - No. 11 . - S. 68-71 .