Rotax 185
| 185 | |
|---|---|
| File:Rotax185LazairEngine (cropped).png Rotax 185 with Lazair aircraft mount and muffler installed | |
| Type | Piston aero-engine |
| National origin | Austria |
| Manufacturer | Rotax |
| Major applications | Ultraflight Lazair |
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The Rotax 185 is a 9 hp (7 kW), single cylinder, two-stroke, direct drive, industrial engine, built by Rotax of Austria for use in fire fighting water pumps that has also been adapted as an aircraft engine for use in ultralight aircraft.[1]
Development
[edit | edit source]The Rotax 185 was designed as a fire-fighting pump, but the rights to the design were sold by Rotax to the Wildfire Group who use the engine in their Mark 3 High Pressure Centrifugal Fire Pump.[2]
Due to its design purpose as a water pump engine it proved reliable enough for use on ultralight aircraft,[3][4] and was adopted as an engine for the twin-engine Ultraflight Lazair ultralight aircraft - as a replacement for the 5.5 hp (4 kW) Pioneer chainsaw engines used on the early Series I. The 185 provides enough power to allow the Lazair to be flown on floats.
In the Lazair application the 185 was used to drive two propellers stacked together in biplane configuration. This was not done for aerodynamic reasons but rather because the Lazair manufacturer had ample quantities of the nylon propellers on hand for its earlier engines and stacking them was more cost efficient than scrapping them and buying new propellers.[5]
Applications
[edit | edit source]
- Lazair
- Wildfire Mark-3 High Pressure Centrifugal Fire Pump
Specifications (185)
[edit | edit source]Data from Rotax 185 Engine Data[6]
General characteristics
- Type: two-stroke air-cooled engine
- Bore: 2.441 in (62 mm)
- Stroke: 2.4 in (61 mm)
- Displacement: 185 cc (11.29 cu in)
Components
- Valvetrain: piston ports
- Fuel system: Tillotson pneumatic pump carburettor
- Fuel type: regular autofuel
- Oil system: premixed in the fuel at 40:1
- Cooling system: free air
- Reduction gear: Custom made belt drive reduction units have been employed
Performance
- Power output: 9 hp (7 kW) at 5000 rpm
- Fuel consumption: 4 L/hr (1 US gph)
References
[edit | edit source]- ^ Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
- ^ Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).[permanent dead link]
- ^ Hunt, Adam & Ruth Merkis-Hunt: Skeletal Remains, pages 64-70. Kitplanes Magazine, September 2000.
- ^ Cliche, Andre: Ultralight Aircraft Shopper's Guide 8th Edition, page E-21. Cybair Limited Publishing, 2001. Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
- ^ Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
- ^ Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
