D-Motor LF39

D-Motor LF39
Type Piston aero engine
National origin Belgium
Manufacturer D-Motor
Developed from D-Motor LF26

The D-Motor LF39 is a lightweight liquid cooled side-valve four-stroke flat six 4 litre petrol aircraft engine, produced by D-Motor in Deerlijk, Belgium.[1] It is a derivative of the flat four D-Motor LF26.

Design

The LF39 produces 125 hp (93 kW) and has a dry weight of 74 kg (163 lb).[2] Just like its smaller sibling, the LF26, this direct-drive aero-engine is unusual in two respects: it is very oversquare with a bore:stroke ratio of 1.295:1, and it has a side-valve valvetrain. The designer determined that since maximum continuous power output was to be developed at only 2800 rpm, the extra weight and complexity of overhead valves would be superfluous, so the resulting engine is compact and lightweight. The engine uses fuel injection, so carburetor heat is unnecessary. Lubrication is by dry sump, with an external oil tank. Dual ignition is used, each cylinder having twin spark plugs sited between the valves and the piston crowns.

Unlike an engine which uses ohv to be capable of high revs, a feature of the slow-revving side-valve arrangement is that the engine does not suffer high frictional losses, so the power curve is virtually linear from 50 kW @ 1920rpm to 91.55 kW @ 3100rpm.[3] An inherent disadvantage of the side-valve design is the relatively inefficient shape of the combustion chamber; but there remains potential for squish to promote turbulence of the fuel/air mix, and the low rpm means that the flame front is able ignite all the fuel in each power stroke.[4][5]

In its page,"Concept and advantages of the D-motor", the company claims:

Development

With the aid of funding from the Belgian government,[7] the D-Motor LF39 was developed from the LF26. The company encountered problems with the casting of the flat-six cylinder block and there were further problems with the flywheel/alternator, but these were solved using a lighter flywheel with neodymium magnets.[1]

The 2014 expected price was 17800.[8]

In September 2014, EDM Aerotec announced the results of test flying the engine in their EDM Aerotec CoAX 2D/2R coaxial rotor helicopter, saying, "We are glad to present the 6 cylinder in action. After more than 100 hours testflying ... the coax helicopter equipped with the 6 cylinder... (proved) a perfect combination according to the test pilots." and added, "Another 6 cylinder has been installed in a test plane in Belgium".[9]

Applications

Specifications

Reference: D-Motor[11][12]

General characteristics

Components

Performance

See also


Comparable engines
Related lists

References

  1. 1 2 3 "Kapelstraat 198 8540 Deerlijk - Recent information". D-motor1.vpweb.be. Retrieved 2012-08-14.
  2. D-Motor publicity specification sheet, August 2014
  3. D-motor performance graph
  4. Speedex, Special cylinder heads, retrieved 3 March 2016
  5. Second Chance Garage. "Combustion Chambers (and a little engine theory)". secondchancegarage.com. Retrieved 3 March 2016.
  6. "D-motor dmotor LF26 LF39 ultralight engine concept advantages". d-motor.eu. Retrieved 3 March 2016.
  7. "Kapelstraat 198 8540 Deerlijk - News". D-motor1.vpweb.be. Retrieved 2012-05-10.
  8. D-Motor, Expected Price, retrieved 1 September 2014
  9. "D-motor update ultralight engine". D-Motor. Retrieved 8 December 2014.
  10. "Technische Daten". EDM Aerotec GmbH. Retrieved 8 December 2014.
  11. "LF26 specifications". D-motor. Retrieved 26 June 2012.
  12. D-Motor, LF39 Dimensions, retrieved 1 September 2014

External links

This article is issued from Wikipedia - version of the 5/1/2016. The text is available under the Creative Commons Attribution/Share Alike but additional terms may apply for the media files.