Armstrong Siddeley Genet
| Genet | |
|---|---|
 | |
| Preserved Armstrong Siddeley Genet at the Shuttleworth Collection | |
| Type | Radial engine |
| National origin | United Kingdom |
| Manufacturer | Armstrong Siddeley |
| First run | 1926 |
| Developed into | Armstrong Siddeley Genet Major |
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. Following the company tradition with a slight deviation the engine was named after the Genet, a catlike animal of the same order but different family.[1]
Variants and applications
Genet I
Genet I producing 65 hp.
- Avro 618 Ten
- Avro Avian prototype
- Blackburn Bluebird I
- BFW M.23
- Cierva autogyros. C.9 and C.10
- Drzewiecki JD-2
- Fleet Fawn
- Junkers A50 Junior
- Saro Cutty Sark
- Southern Martlet
- Westland-Hill Pterodactyl
Genet II
The Genet II produced 80 hp due to an increased compression ratio of 5.25:1.[2]
- ANEC IV
- Avro Avian
- Blackburn Bluebird II
- Cierva C.19 autogyro
- Darmstadt D-18
- de Havilland DH.60 Moth
- Fairchild 21
- Klemm Kl 25
- Nicholas-Beazley NB-8G
- Parnall Imp
- Robinson Redwing II
- Southern Martlet
- Westland Widgeon
Genet IIA
Also 80 hp and with minor differences to the Mark I.
Engines on display
Two preserved Armstrong Siddeley Genets are on static display at the Shuttleworth Collection, Old Warden, Bedfordshire.
A preserved Genet is on display at the Australian National Aviation Museum, Moorabbin, Victoria, Australia
There is a restored Genet at the New England Air Museum, Bradley Int'l Airport, Windsor Locks, CT.
A Genet is on display at the Aviation Heritage Museum (Western Australia).[3]
Specifications (Genet I)
Data from Lumsden.[4]
General characteristics
- 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)
- Dry weight: 168 lb (76 kg)
Components
- Valvetrain: Overhead poppet valves
- Cooling system: Air-cooled
- Reduction gear: Direct drive, Left hand tractor
Performance
- Power output: 65 hp at 1,800 rpm
- Compression ratio: 5.2:1
- Power-to-weight ratio: 0.38 hp/lb
See also
- Related development
- Comparable engines
- Related lists
References
Notes
- ↑ Sanderson, Living Mammals of The World, NY, c.1967
- ↑ Lumsden 2003, p.69.
- ↑ http://www.raafawa.org.au/museum/engines
- ↑ Lumsden 2003, p.68
Bibliography
- Gunston, Bill (1986). World Encyclopedia of Aero Engines. Wellingborough: Patrick Stephens. p. 18. ISBN 0-7509-4479-X.
- Lumsden, Alec. British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing, 2003. ISBN 1-85310-294-6.
External links
 |
Wikimedia Commons has media related to Armstrong Siddeley Genet. |
- Armstrong Siddeley Genet at the Australian National Aviation Museum
- "Armstrong Siddeley Genet.". Flight. No. 26 August 1926. pp. 531–2.