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词条 Hispano-Suiza 14AA
释义

  1. Variants

  2. Applications

  3. Specifications (14AA-04)

  4. See also

  5. References

name= 14AAimage = Hispano-Suiza 14AA.jpgcaption =
}}{{Infobox Aircraft Engine
type= Radial enginenational origin =manufacturer= Hispano-Suizafirst run= 1930smajor applications=number built =program cost =unit cost =developed from = Wright R-2600developed into =variants with their own articles =
}}

The Hispano-Suiza 14AA, also known as Type 79, was a fourteen-cylinder aircraft radial engine used in France during the late 1930s. As Hispano-Suiza lacked recent experience in developing radial engines, it was derived from the licensed Wright R-2600 engine.[1] Due to reliability problems, the engine was largely supplanted by the similar Gnome-Rhône 14N.

Not to be confused with the smaller Hispano-Suiza 14AB, which was derived from the smaller Wright Whirlwind series.

Variants

14AA-00

Direct drive LH rotation

14AA-01

Direct drive RH rotation as -00

14AA-02

0.625:1 reduction gear LH rotation

14AA-03

0.625:1 reduction gear RH rotation as -02

14AA-04

0.625:1 reduction gear LH rotation

14AA-05

0.625:1 reduction gear RH rotation as -04

14AA-06

Direct drive LH rotation

14AA-07

Direct drive RH rotation as -06

Applications

  • Amiot 341
  • LeO 45
  • Farman F.223
  • Latécoère 530
  • Latécoère 570
  • Koolhoven F.K.58
  • Potez 501
  • Romano R.120

Specifications (14AA-04)

'Note: - The 14AA-03 was identical except for the propeller shaft rotating in the opposite direction

{{pistonspecs|
|ref=[2]
|type=Fourteen-cylinder two-row supercharged air-cooled radial engine
|bore=155,6 mm (6.126 in)
|stroke=170 mm (6.693 in)
|displacement=45.257 l (2,761 in³)
|length=1,650 mm (64.96 in)
|diameter=1,260 mm (49.61 in)
|width=
|height=
|weight=640 kg (1,411 lb)
|valvetrain=Overhead valves
|supercharger=Single-speed centrifugal type supercharger, 10.0:1 reduction
|turbocharger=
|fuelsystem=Carburetor
|fueltype=85-87 octane rating gasoline
|oilsystem=
|coolingsystem=Air-cooled
|power=793 kW (1,063 hp) at 2,125 rpm for takeoff
|specpower=17.52 kW/l (0.39 hp/in³)
|compression=6.2:1
|fuelcon=
|specfuelcon=369 g/(kW•h) (0.61 lb/(hp•h))
|oilcon=12 g/(kW•h) (0.32 oz/(hp•h))
|power/weight=1.24 kW/kg (0.75 hp/lb)
|reduction_gear=1.58:1
}}

See also

{{aircontent
|see also=
|related=
|similar aircraft=
|lists=
  • List of aircraft engines

|similar engines=
}}

References

{{Commons category}}
1. ^Hartmann, Gérard, Hispano-Suiza. Les moteurs de tous les records
2. ^{{cite book|last=Tsygulev|title=Aviacionnye motory voennykh vozdushnykh sil inostrannykh gosudarstv (Авиационные моторы военных воздушных сил иностранных государств)|publisher=Gosudarstvennoe voennoe izdatelstvo Narkomata Oborony Soyuza SSR|location=Moscow|year=1939|url=http://base13.glasnet.ru/text/aviamotory/t.htm|deadurl=yes|archiveurl=https://web.archive.org/web/20090324160448/http://base13.glasnet.ru/text/aviamotory/t.htm|archivedate=2009-03-24|df=}}
{{Hispano-Suiza aeroengines}}

3 : Aircraft air-cooled radial piston engines|Aircraft piston engines 1930–1939|Hispano-Suiza aircraft engines

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