- Armstrong Siddeley Genet
The
Armstrong Siddeley Genet was a five-cylinder, air-cooled, radial engine for aircraft use built in the UK, first run in 1926. It developed 80 hp at 2,200 rpm in its final form and was a popular light aircraft powerplant.Variants and applications
Genet I
Genet I producing 65 hp.
*Avro 618 Ten
* Avro Avian prototype
* Blackburn Bluebird I
* Ciervaautogyro s. C.9 and C.10
*Drzewiecki JD-2
*Fleet Fawn
*Junkers A50 Junior
*Saro Cutty Sark
*Westland-Hill Pterodactyl Genet II
The Genet II produced 80 hp due to an increased compression ratio of 5.25:1. [Lumsden 2003, p.69.]
*ANEC IV
*Avro Avian
* Blackburn Bluebird II
*Cierva C.19 autogyro
*de Havilland DH.60 Moth
*Klemm Kl 25
*Parnall Imp
* Robinson Redwing I
*Southern Martlet
*Westland Widgeon Genet IIA
Also 80 hp and with minor differences to the Mark I.
* Robinson Redwing IIpecifications (Genet I)
pistonspecs
ref= [Lumsden 2003, p.68]
type=5-cylinder single-row radial
bore= 4 in (101.6 mm)
stroke= 4 in (101.6 mm)
displacement= 251.43 cu in (4.1 L)
length=28.5 in (724 mm)
diameter=34 in (863.6 mm)
width=
height=
weight=168 lb (76 kg)
valvetrain=Overhead poppet valves
supercharger=
turbocharger=
fuelsystem=
fueltype=
oilsystem=
coolingsystem=Air cooled
power=65 hp at 1,800 rpm
specpower=
compression=5.2:1
fuelcon=
specfuelcon=
oilcon=
power/weight=0.38 hp/lbdesigner=
reduction_gear=Direct drive, Left hand tractorgeneral_other=
components_other=
performance_other=ee also
Aeroenginecontent
related=
*Armstrong Siddeley Genet Major similar aircraft=
lists=
*List of aircraft engines References
Notes
Bibliography
*
* Lumsden, Alec. "British Piston Engines and their Aircraft". Marlborough, Wiltshire: Airlife Publishing, 2003. ISBN 1-85310-294-6.External links
* [http://www.aarg.com.au/GenetEngine.htm Armstong Siddeley Genet at the Australian National Aviation Museum]
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