Movatterモバイル変換


[0]ホーム

URL:


Jump to content
WikipediaThe Free Encyclopedia
Search

Kroeber M4

From Wikipedia, the free encyclopedia
1930s German two-stroke piston engine
M4 Köller
National originGermany
ManufacturerDr. Kroeber & Sohn G.m.b.H.
First run1930s
Major applicationsMöller Stomo 3,ITS-8

TheKroeber M4 Köller was a 2-stroke air-cooled horizontally opposed piston engine designed and built byDr. Kroeber & Sohn G.m.b.H. inGermany in the late 1930s. The M4 proved relatively popular, for powering the ultra-light aircraft and motor-gliders in vogue during the 1920s and 1930s.

Variants

[edit]
Kroeber M3 Köller
either a typo or a variant of the M4, (only reference is Cynk's Polish aircraft 1893-1939)[1]
Kroeber M4 Köller
Main production variant

Applications

[edit]

Data from AEHS: HOAE Kroeber[2]

Engines on display

[edit]

There are several M4 engines on display, but one of the best preserved and presented is at thePolish Aviation Museum inKraków.[3]

Specifications (M4)

[edit]

Data from Flugzeug-Typenbuch. Handbuch der deutschen Luftfahrt- und Zubehör-Industrie 1944,[4][5]

General characteristics

  • Type: 2-cylinder 2-stroke air-cooled horizontally-opposed
  • Bore: 75 mm (2.95 in)
  • Stroke: 72 mm (2.83 in)
  • Displacement: 0.634 L (38.69 cu in)
  • Length: 550 mm (21.7 in)
  • Width: 550 mm (21.7 in)
  • Height: 646 mm (25.4 in)
  • Dry weight: 27.8 kg (61 lb)

Components

  • Fuel system: 2x Meco S1/f carburetor
  • Fuel type: 1:25 SAE 50 oil / gasoline blend
  • Oil system: blended with fuel
  • Cooling system: air-cooled

Performance

  • Power output:
  • 18 PS (18 hp; 13 kW) at 2,700 rpm (30 minutes) at sea level
  • 16.6 PS (16 hp; 12 kW) at 2,650 rpm (max. continuous / cruise) at sea level
  • Specific power: 28.4 PS/L (0.46 hp/cu in; 20.89 kW/L)
  • Compression ratio: 6.2:1
  • Specific fuel consumption: 0.228 kg/PSh (0.510 lb/(hp⋅h); 0.310 kg/kWh) at max continuous
  • Oil consumption: 0.002–0.003 kg/PSh (0.004–0.007 lb/(hp⋅h); 0.003–0.004 kg/kWh) at max continuous
  • Power-to-weight ratio: 0.645 PS/kg (0.289 hp/lb; 0.474 kW/kg)
  • B.M.E.P.: 2.55 atm (2.58 bar; 37.5 psi)

References

[edit]
  1. ^Cynk, Jerzy B (1971).Polish aircraft 1893-1939. Putnam. p. 652.ISBN 0-370-00085-4.
  2. ^"Kroeber".www.enginehistory.org. AEHS. Retrieved5 February 2020.
  3. ^"Aircraft engine: Köller Kroeber M4". Polish Aviation Museum Kraków. Retrieved25 December 2023.
  4. ^Schneider, Helmut (Dipl.Ing.) (1944).Flugzeug-Typenbuch. Handbuch der deutschen Luftfahrt- und Zubehör-Industrie 1944 (in German) (Facsimile reprint 1986 ed.). Leipzig: Herm. Beyer Verlag. p. 417.ISBN 381120484X.{{cite book}}:ISBN / Date incompatibility (help)
  5. ^Grey, C.G.; Bridgman, Leonard, eds. (1938).Jane's All the World's Aircraft 1938. London: Sampson Low, Marston & company, ltd. p. 64d.
Retrieved from "https://en.wikipedia.org/w/index.php?title=Kroeber_M4&oldid=1321530652"
Categories:
Hidden categories:

[8]ページ先頭

©2009-2025 Movatter.jp