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Austro-Daimler 6

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Austro-Daimler
A 1912 Austro-Daimler 6 on display at thePorsche Museum
Type 6-cyl. water-cooled in-line piston engine
National origin Austria
Manufacturer Austro-Daimler
First run 1910
Variants Beardmore 120 hp

TheAustro-Daimler 6was a series ofAustriansix-cylinderwater-cooledinlineaero enginesfirst produced in 1910 by theAustro-Daimlercompany.

Design and development

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The first Austro-Daimler six-cylinder engine was designed byDr-Ing Ferdinand Porscheto be an aircraft engine from the outset. Of high quality manufacture, the Austro-Daimler was modestly rated at relatively low rpm, which gave the engine family a reputation for robustness and reliability.[1]

Features of the Austro-Daimler included welded steel water jackets (originally copper), seven main bearings and large diameter inclined inlet and exhaust valves opened by dual action push-pull rods and closed by spring pressure.[1]

Thesingle-overhead cam(SOHC) valvetrain of later engines was driven from the crankshaft through the usual vertically-oriented shaft as the contemporaryMercedes D.IIIwas, but the Austro-Daimler had its vertical camshaft drive system mounted at the front of the engine instead, and not the usual aft-end placement of other Central Powers straight-six SOHC liquid-cooled aircraft powerplants, like the Mercedes and BMW designs.

The Austro-Daimler inspired many imitators such as theMercedes D.II,Benz Bz.IVandHiero 6.Limited availability of the Austro-Daimler engines forced some aircraft manufacturers to substitute Mercedes (the German Daimler company) engines in their aircraft, due to greater availability.[1]From 1913, the 90 and 120 hp models were produced under license in Scotland byWilliam Beardmore and Company.TheBeardmore 120 hpwent on to power many British military aircraft duringWW1.[2]

Variants

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Data from:[1]

Austro-Daimler 90 hp 6-cyl.
The original low capacity version developing 90 hp (67.11 kW), introduced in 1910.
Austro-Daimler 120 hp 6-cyl.
Up-rated with a capacity of 13.9 L (848.23 cu in), from 130 mm (5.12 in) bore and 175 mm (6.89 in) stroke, developing 120 hp (89.48 kW) at 1,200 rpm, introduced in 1911.
Austro-Daimler 160 hp 6-cyl.
developing 160 hp (119.31 kW), introduced in 1913.
Austro-Daimler 185 hp 6-cyl.
developing 185 hp (137.95 kW), introduced in 1916.
Austro-Daimler 200 hp 6-cyl.
Up-rated with a capacity of 15.03 L (917.19 cu in), from 135 mm (5.31 in) bore and 175 mm (6.89 in), developing 200 hp (149.14 kW) at 1,350 rpm, introduced in December 1916.[3]
Austro-Daimler 210 hp 6-cyl.
210 hp (156.60 kW), introduced in late 1917.
Austro-Daimler 225 hp 6-cyl.
developing 225 hp (167.78 kW), introduced in 1918.

Applications

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Specifications (Austro-Daimler 200 hp)

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A 147 kW (197 hp) Austro-Daimler fitted to anAviatik (Berg) D.I,on display at theVienna Technical Museum

Data from[5]

General characteristics

  • Type:6-cylinder liquid-cooled inline engine
  • Bore:135 mm (5.31 in)
  • Stroke:175 mm (6.89 in)
  • Displacement:15.0 L (915.48 cu in)
  • Length:1,724 mm (67.875 in)
  • Width:568 mm (22.375 in)
  • Height:1,149 mm (45.25 in)
  • Dry weight:330.4 kg (728.5 lb)

Components

  • Fuel system:One duplex Austro-Daimler carburetor

Performance

See also

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Comparable engines

Related lists

Footnotes

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  1. ^abcdGunston 2006
  2. ^Lumsden, Alec (2002).British Piston Engines and their Aircraft.Airlife Publishing. pp. 80–81.ISBN1853102946.
  3. ^Grey 1969
  4. ^Jane 1969,p. 18
  5. ^Angle, Glenn D. (1921).Airplane Engine Encyclopedia.Dayton, Ohio: The Otterbein Press. pp. 64–67.

References

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  • Angelucci, Enzo (1980).The Rand McNally Encyclopedia of Military Aircraft 1914–1980.p. 102.
  • Grey, C. G. (1969) [1919].Jane's All the World's Aircraft 1919.David & Charles Publishing Ltd. pp. 1b–145b.ISBN0-7153-4647-4.