ARGO AH-2.2

The Ultralight Helicopter

 

Multi‐purpose two‐seater ULTRA - light helicopter ARGO AH-2.2 is designed for comfortable, fast and safety travel

Helicopter ARGO AH-2.2 has the following advantages in its class:

 

  • Excellent controllability, flight stability, maneuverability, low vibrations and noise level due to an ideal design balance and a three‐blade rotor.
  • Efficient performance and aerodrome service independence due to use of А‐95 gasoline and small overall dimensions.
  • It is an innovative design for ultra-light helicopters.
  • It has enough space to carry up to 2 people
  • It will be powered by a modern light engine from ULPower , its run on standard automotive fuel.
  • It has a three bladed rotor, which guarantees incredible stability in flight, its shape gives a low aerodynamic drag.
  • Thanks to the modern four cylinder 150Hp aircrafts engine you can reach speeds up to 200 km/h.

 

The UL 350 iHPS engine characteristics

 

This powerful engine is developed for helicopters and gyrocopters and is equipped with a forced cooling system. While hovering, the natural airflow is insufficient to cool the cylinder heads.  So a fan driven by the crankshaft blows air through aluminium air boxes to maintain efficient cooling whatever the flight conditions. This forced cooling system has an integrated oil radiator.

 

 

Engine characteristics:

 

  • This powerful engine is developed for helicopters and gyrocopters and is equipped with a forced cooling system. While hoovering the natural airflow is not sufficient to cool down the cylinder heads. So a fan driven by the crankshaft, blows air along the aluminium air boxes.
  • Thanks to the modified camshaft and inlet collector the UL350IHPS generates up to 150HP at 3500 rpm. This forced cooling system has an integrated oil radiator.
  • 4 stroke, 4 cylinder, horizontally opposed
  • Dual (redundant) electronic spark ignition (variable timing)
  • Electronic multipoint fuel injection (pressure and temperature compensated)
  • Electronic RPM limiter
  • Direct propeller drive
  • 5 bearing crankshaft with surface hardening treatment and additional large thrust bearing (ball bearing type)
  • Single central camshaft
  • Push rods, tappets and OHV (hydraulic compensators have not been used)
  • Wet sump forced lubrication with integrated pressure regulator
  • Ram air cooled cylinders and cylinder heads
  • Integrated permanent magnet AC generator, external rectifier-regulator
  • Electric starter
  • Electric fuel pump and pressure regulator to eliminate vapor lock and facilitate starting even under adverse conditions.

 

ARGO Aero ... powering your dream to become reality

POLITYKA PLIKÓW COOKIES

Celier Aviation Sp. z o.o. która przekształciła sie w ARGO.Aero

Al. Katowicka, 11 05-830 Wolica/Warszawa, Polska

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VAT : 1231208563 | Regon: 142314725 KRS:0000355281

Sąd Rejonowy dla m.st. Warszawy XIV Wydział Gospodarczy

 

 

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