Two engine versions are available to meet the widest range of installation requirements. Both horizontal and vertical axis installation are possible.
The GAS418S has a very compact size. It is thus to fit it into very small fuselages, helping to keep the overall weight low. Specific power is very high, going up to 2.31 hp/kg in the horizontal version. Peak power at sea level is 180hp @5800RPM.
The GAS418S relies on a single stage centrifugal supercharger, which is driven mechanically to increase its performance at high altitude.
Medium-high altitude performance of the mechanical supercharger are better than the turbocharger ones. The lower air density modifies the expansion ratio of the turbine, limiting the overall boosting capability due to anticipated turbine over speed.
Fuel injection and ignition are completely electronic and ECU controlled, making the engine run at its best under a wide range of ambient conditions.
All parts used inside the engine are manufactured in Italy or in countries of the European Union. The engine is completely designed and assembled in house at Flygas, based in the Italian motor valley.
GAS418S engine runs with the standard 98 octane number automotive gasoline.
On the market, there are not pistons engines intended for Ultralight Experimentals Aircrafts that use Centrifugal Superchargers and double (redundant) Fuel Supply Plant.
Flygas offers that kind of engine, made up from a GREAT Rotax 912 ULS standard engine equipped with Flygas innovative technical solutions.
Today all electronic fuel injection engines use a fuel pressure of 3 bar (10 times higher than 0.3 bar-4.5 PSI respect carburetor engines).
In the event of an emergency landing, with possible impact on the ground and trees, all E.F.I. engines still maintain the fuel supply line which is close to the engine at a pressure of 3 bar (45PSI), despite the pump of the fuel is turned off. This significantly increases the risk of fire, even in the event of a limited impact!
Since 2007 Flygas has been the only company in the world to create a redundant fuel supply system (injection and carburetors)
that allows you to quickly switch from injection to carburetors, discharging the high pressure of 3 bar (necessary for injection) down to 0.3 bar (required by carburetors)! Therefore, even in the event of a minor impact, the fuel spill following a break will be 10 times less than any other fuel injection system on the market today.
Flygas is the only firm in the world today that produces a Mechanical Fuel Pump for Rotax 912 Turbo or Supercharged engine.
Mechanical fuel pump and carburetors will allow your engine to work 100%, even in case of a 12 Volt power failure!
We supply the engine (Rotax 912 ULS New) completely assembled, bench tested and equipped with the following Flygas kits:
The “Fly-Safe” Electronic Fuel Injection system by Flygas stands as a parallel unit to the Carburetors.
At any time, the pilot can rapidly change from E.F.I. back to Carburetors and vice versa simply pushing or pulling the Flygas “K.E.D.” (Knob Exchange Device) on the cockpit.
In case of any malfunction with the E.F.I. the pilot can quickly change back to Carburetors, restoring engine operation and restarting it in two second!
This is also particularly useful in any unlikely case of emergency landing.
In order to reduce the risk of fire due to a heavy ground impact, you can discharge the high-level fuel pressure (3 bar -45 psi) of the E.F.I. to the low-level fuel pressure (0.3 bar – 4.5 psi) of Carburetors.
Turbochargers are very often used to boost power of combustion engines, but they have some limits:
All E.F.I. engines use an electrical pump to supply fuel flow, but this comes with some issue:
Increased reliability and safety, while saving electrical power
Flygas Mechanical Fuel Pump is driven directly from the crank-shaft and is installed on the engine flywheel, in a protected position in the event of an emergency landing.
It ensures a constant fuel flow at 3 bar pressure, while having a very light weight (only 680 grams: just basically the same weight as an electrical Pierburg fuel pump, complete with wires and switches.)
It replaces one of the two electric fuel pumps normally installed on a Rotax 912 and is configured as the “primary” fuel pump, leaving the residual electric pump as ”secondary”.
Remember: all aircraft and racing engines have always been equipped with mechanical fuel pumps, and they still are today!
• Engine Model: “GAS418HA”, 4stroke, Gasoline
• Displacement: 1.800 c.c. (110 c.inch.) – N°cyl. 4, Opposed,
(2 valves per cyl.)
• Bore \ stroke: 92mm\ 68mm (3,6 inch. \2,7 inch.)
• Maximum power: 132Kw (180hp) @ 5.800 RPM
• Alimentation supply: Centrifugal Supercharger single stage mechanical gears drived
• Ignition: Double spark-plugs, (different options to control its)
• Cooling: Water, forced circulation
• Lubrication: Dry or wet sump
• Alternator: 14 vdc, 32 Amph (secondary alternator could be supply)
• Ignition / Injection: [Redundant E.F.I.] or [E.F.I. + Carburattors (Flygas Patented kit)]
• Starting: Electric engine starter with sprug-clutch
• Reduction Gear Propeller: Gearbox with shock absorber: [2.18: 1] – [2.20:1] – [2.33:1]
• Fuel type: Gasoline “Normal green”
• Power/weight ratio: 2.3 Hp/kg!!
• Weight: 78 Kg (172 Lb. included Starter Motor, Alternator, Inj., Air Filter)
• Overall Dimensions: width 664mm (26.Inch.), height 449mm (17,5 Inch.)
• Depth from the propeller flange: 584mm (23 Inch.)
GAS 252 is engine for ultralight airplane and trike. The two cylinders boxer weight only 57 kg (125 pound) develops a power of 70.7hp (52kw) and has a very low fuel consumption in cruise speed, only 7,5 lt\hr (1.98 Gal\hr) @4500rpm.
Fuel consumption will vary depending on the installation