Verner 133M
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The Verner 133M, often called the VM 133M, is a Czech two cylinder, horizontally-opposed, four stroke aircraft engine, designed and built by Verner Motor of Šumperk.[1][2][3]
Design and development
The 133M uses a 12 volt 1000W electric starter and has a 12 volt 160W generator. It runs on 95 octane automobile fuel or 100LL Avgas. The recommended time between overhauls is 1000 hours.[1][2][3]
Applications
Specifications (133M)
Data from Manufacturer and Central Florida Flyers[2][3]
General characteristics
- Type: twin cylinder, horizontally-opposed, four-stroke aircraft engine
- Bore: 97 mm (3.82 in)
- Stroke: 90 mm (3.54 in)
- Displacement: 1,329 cc (81.1 cu in)
- Length: 617 mm (24.29 in)
- Width: 736 mm (28.98 in)
- Height: 456 mm (17.95 in)
- Dry weight: 61 kg (134 lb)
Components
- Fuel system: Two Bing 64 carburetors pressurized by a Pierburg 7.20971.63 fuel pump
- Fuel type: 95 octane auto fuel or 100LL Avgas
- Cooling system: air-cooled
- Reduction gear: 2:1 or 2.29:1 oil-filled gear box
Performance
- Power output: 63 kW (84 hp) at 5500 rpm for three minutes, 51 kW (68 hp) at 4200 rpm continuous
- Compression ratio: 9.8:1
- Fuel consumption: 11 litres (2.4 imp gal; 2.9 US gal) per hour at cruise settings
- Power-to-weight ratio: 1.03 kW/kg
References
- ↑ 1.0 1.1 1.2 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 22. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
- ↑ 2.0 2.1 2.2 Verner Motor (undated). "VM 133M". Retrieved 24 April 2012.
- ↑ 3.0 3.1 3.2 Central Florida Flyers (undated). "VM 133M". Retrieved 24 April 2012.
- ↑ SlipStream, International (2009). "Revelation Powerplant Options". Archived from the original on 6 July 2011. Retrieved 24 April 2012.
External links
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