Armstrong Siddeley Genet
| Genet | |
|---|---|
| File:ASGenet.JPG 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 is 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
[edit | edit source]Genet I
[edit | edit source]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
- Medwecki and Nowakowski M.N.5
- Saro Cutty Sark
- Southern Martlet
- Westland-Hill Pterodactyl
Genet II
[edit | edit source]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
[edit | edit source]Also 80 hp and with minor differences to the Mark I.
Engines on display
[edit | edit source]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)
[edit | edit source]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
[edit | edit source]Related development
Comparable engines
Related lists
References
[edit | edit source]Notes
[edit | edit source]Bibliography
[edit | edit source]- Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
- Lumsden, Alec. British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing, 2003. Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value)..
External links
[edit | edit source]
- Armstrong Siddeley Genet at the Australian National Aviation Museum
- Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).