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   New Italian Helicopter
This Page was created
November 28th, 1998

The prototype of the  helicopter pictured below flew for the first time in September of 1998. Even though it takes a long time to go through all the necessary tests and licensing process, the project looks very promising. The designed of this revolutionary craft is a Italian engineer named Vladimiro Lidak.

This craft is one of the first "light" helicopters in the world powered by two separate piston engines, which obviously substantially increases its reliability and safety.

Mr. Lidak designed his helicopter to be equipped with two aeronautical four-stroke engines with the capability of flying with a reduced performance even with a single engine. The engines, 68 hp each, are completely independent, each one with its own electrical system and fuel system. The TBO (time between overhauls) is 1,000 hours.

The electronic fuel injection of this power plant guarantees a correct fuel mixing in all all meteorological conditions and  altitude, leading to reduced fuel consumption, less pollution as well as avoiding anomalies such as the formation of ice on the carburetors.

The fields of application of a light helicopter which, thanks to the twin engine, will be permitted to fly over large towns, are much more than those of traditional single engine helicopters. Keep in mind that the solution of the double engine is normally adopted in helicopters whose price is of the order of millions of dollars.

This helicopter is also equipped with a one-blade rotor. According to his developer, the use of the one-blade rotor eliminates various problems (and related costs) such as the periodic blade tracking, produces a better aerodynamic performance and better balancing during flight, thus reducing the vibrations and noise. The single blade is counterbalanced by a
counterweight.

A third important new feature of this helicopter is the transmission system to the tail rotor which is realized with a hydrostatic transmission. This eliminates the tail rotor variable pitch, all the devices from the control pedal to the tail for the pitch adjustment and, above all, the propeller shaft with its bevel gear box. All these innovations lead to a remarkable
constructive simplification and a reduction in friction losses. It is considered a highly reliable solution.

This two-seat two-engine one-blade helicopter could change the growth perspectives of the market of light helicopters in the world because it is not only is a credible candidate to catch an important share in its world market but also promises to enlarge the size of the market itself.
 


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