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Verner VM 133

The Verner VM 133 is a family of Czech two cylinder, horizontally opposed, four stroke aircraft engines, designed and built by Verner Motor of Šumperk.[1][2][3]

Verner VM 133
Verner VM 133MK
Type Aircraft engine
National origin Czech Republic
Manufacturer Verner Motor
Major applications Airflow Twinbee
Avid Catalina
SlipStream Genesis
Produced up until about 2013
Developed from Verner 1400

Design and development edit

The 133M is based on the earlier Verner 1400 and 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][4]

The engine was still advertised for sale on the company website in 2013, but by 2015 was no longer listed as available and it is likely that production has ended.[5]

Variants edit

VM 133M
Original model
VM 133MK
Improved model

Applications edit

Specifications (VM133 MK) edit

Data from Technical Data VM133 MK[2]

General characteristics

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
  • Oil system: oil class SH/SG 5
  • 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

See also edit

Related lists

References edit

  1. ^ a b c Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 22. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
  2. ^ a b c Verner Motor (n.d.). "TECHNICAL DATA VM133 MK". Retrieved 24 April 2012.
  3. ^ a b Central Florida Flyers (n.d.). "VM 133M". Retrieved 24 April 2012.
  4. ^ Zdeněk Klučka. . vernermotor.com. Archived from the original on 26 August 2013. Retrieved 30 June 2015.
  5. ^ . Internet Archive Wayback Machine. Retrieved 30 June 2015.
  6. ^ SlipStream, International (2009). . Archived from the original on 6 July 2011. Retrieved 24 April 2012.

External links edit

  • Official website

verner, family, czech, cylinder, horizontally, opposed, four, stroke, aircraft, engines, designed, built, verner, motor, Šumperk, mktype, aircraft, enginenational, origin, czech, republicmanufacturer, verner, motormajor, applications, airflow, twinbeeavid, cat. The Verner VM 133 is a family of Czech two cylinder horizontally opposed four stroke aircraft engines designed and built by Verner Motor of Sumperk 1 2 3 Verner VM 133Verner VM 133MKType Aircraft engineNational origin Czech RepublicManufacturer Verner MotorMajor applications Airflow TwinbeeAvid CatalinaSlipStream GenesisProduced up until about 2013Developed from Verner 1400 Contents 1 Design and development 2 Variants 3 Applications 4 Specifications VM133 MK 4 1 General characteristics 4 2 Components 4 3 Performance 5 See also 6 References 7 External linksDesign and development editThe 133M is based on the earlier Verner 1400 and 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 4 The engine was still advertised for sale on the company website in 2013 but by 2015 was no longer listed as available and it is likely that production has ended 5 Variants editVM 133M Original model VM 133MK Improved modelApplications editAirflow Twinbee 1 Airkraft Sunny Aquilair Swing Avid Catalina Flitzer Z 21 citation needed Rainbow Cheetah SlipStream Genesis 6 Specifications VM133 MK editData from Technical Data VM133 MK 2 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 Oil system oil class SH SG 5 Cooling system air cooled Reduction gear 2 1 or 2 29 1 oil filled gear boxPerformance 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 kgSee also editVerner JCV 360Related lists List of aircraft enginesReferences edit a b c Bayerl Robby Martin Berkemeier et al World Directory of Leisure Aviation 2011 12 page 22 WDLA UK Lancaster UK 2011 ISSN 1368 485X a b c Verner Motor n d TECHNICAL DATA VM133 MK Retrieved 24 April 2012 a b Central Florida Flyers n d VM 133M Retrieved 24 April 2012 ZdenA k KluATka Verner Motor Czech Republic ultralight aircraft LSA vernermotor com Archived from the original on 26 August 2013 Retrieved 30 June 2015 Verner Motor Internet Archive Wayback Machine Retrieved 30 June 2015 SlipStream International 2009 Revelation Powerplant Options Archived from the original on 6 July 2011 Retrieved 24 April 2012 External links editOfficial website Photo of the VM 133 Retrieved from https en wikipedia org w index php title Verner VM 133 amp oldid 1128743038, wikipedia, wiki, book, books, library,

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