Bristol Cherub

Clash Royale CLAN TAG#URR8PPP
| Cherub | |
|---|---|
| Preserved Bristol Cherub engine | |
| Type | Piston aircraft engine |
| Manufacturer | Bristol Aeroplane Company |
| First run | 1923 |
Major applications | Bristol Brownie Hawker Cygnet |
The Bristol Cherub is a British two-cylinder, air-cooled, aircraft engine designed and built by the Bristol Aeroplane Company. Introduced in 1923 it was a popular engine for ultralight and small aircraft in the 1930s.[1]
Contents
1 Variants
2 Applications
3 Survivors
4 Engines on display
5 Specifications (Cherub III)
5.1 General characteristics
5.2 Components
5.3 Performance
6 See also
7 References
7.1 Notes
7.2 Bibliography
8 External links
Variants
- Cherub I
- Initial direct drive version introduced in 1923. Bore and stroke of 3.35 by 3.8 inches (85 mm × 97 mm) for a displacement of 67 cu in (1.095 L). 32 horsepower (24 kW) at 2,500 rpm.[2]
- Cherub II
- Geared down (2:1) version of the Cherub I.
- Cherub III
- An improved and slightly larger (1.228 L) direct drive version introduced in 1925.
Applications
Cherub-powered Short Satellite
- Avia BH-2
- Avro Avis
- Beardmore Wee Bee
- Bristol Brownie
- Cranwell CLA.2
- Cranwell CLA.3
- Cranwell CLA.4
- Dart Pup
- Everson Evo III
- Granger Archaeopteryx
- Halton Mayfly
- Halton Minus
- Hawker Cygnet
- Messerschmitt M17
- Meyers Midget
Mignet HM.14 Pou-du-Ciel- Parnall Pixie
- Pander-DB two Pices
- Powell Racer
- RAE Scarab
- RAE Hurricane
- Short Cockle
- Short Satellite
- Supermarine Sparrow
- Vickers Vagabond
- Westland Woodpigeon
- Westland-Hill Pterodactyl
Survivors
An airworthy Messerschmitt M17 replica is owned and operated by the EADS Heritage Flight at Manching and is powered by an original Bristol Cherub III.[3]
Engines on display
A preserved Bristol Cherub is on static display at the Shuttleworth Collection, Old Warden, Bedfordshire.
Specifications (Cherub III)
Data from Lumsden.[4]
General characteristics
Type: 2-cylinder air-cooled, horizontally opposed, left-hand tractor
Bore: 3.54 in (90 mm)
Stroke: 3.8 in (96.5 mm)
Displacement: 75 in³ (1.228 L)
Width: 25.6 in (650 mm)
Dry weight: 98 lb (39.5 kg)
Components
Valvetrain: Overhead valve
Oil system: Dry sump
Cooling system: Air-cooled
Performance
Power output: 36 hp (24 kW) at 3,200 rpm
Compression ratio: 5.75:1
Fuel consumption: 2.5 imp. gallons per hour
Power-to-weight ratio: 0.36 hp/lb
See also
Comparable engines
- ABC Scorpion
- Aeronca E-113
- Armstrong Siddeley Ounce
- Walter Atom
Related lists
- List of aircraft engines
References
Notes
^ Guttery 1969, p.80.
^ Lumsden 2003, p.101.
^ EADS - Messerschmitt M17 Retrieved: 9 August 2009
^ Lumsden 2003, p.102.
Bibliography
.mw-parser-output .refbeginfont-size:90%;margin-bottom:0.5em.mw-parser-output .refbegin-hanging-indents>ullist-style-type:none;margin-left:0.mw-parser-output .refbegin-hanging-indents>ul>li,.mw-parser-output .refbegin-hanging-indents>dl>ddmargin-left:0;padding-left:3.2em;text-indent:-3.2em;list-style:none.mw-parser-output .refbegin-100font-size:100%
- Guttery, T.E. The Shuttleworth Collection. London: Wm. Carling & Co, 1969. .mw-parser-output cite.citationfont-style:inherit.mw-parser-output qquotes:"""""""'""'".mw-parser-output code.cs1-codecolor:inherit;background:inherit;border:inherit;padding:inherit.mw-parser-output .cs1-lock-free abackground:url("//upload.wikimedia.org/wikipedia/commons/thumb/6/65/Lock-green.svg/9px-Lock-green.svg.png")no-repeat;background-position:right .1em center.mw-parser-output .cs1-lock-limited a,.mw-parser-output .cs1-lock-registration abackground:url("//upload.wikimedia.org/wikipedia/commons/thumb/d/d6/Lock-gray-alt-2.svg/9px-Lock-gray-alt-2.svg.png")no-repeat;background-position:right .1em center.mw-parser-output .cs1-lock-subscription abackground:url("//upload.wikimedia.org/wikipedia/commons/thumb/a/aa/Lock-red-alt-2.svg/9px-Lock-red-alt-2.svg.png")no-repeat;background-position:right .1em center.mw-parser-output .cs1-subscription,.mw-parser-output .cs1-registrationcolor:#555.mw-parser-output .cs1-subscription span,.mw-parser-output .cs1-registration spanborder-bottom:1px dotted;cursor:help.mw-parser-output .cs1-hidden-errordisplay:none;font-size:100%.mw-parser-output .cs1-visible-errorfont-size:100%.mw-parser-output .cs1-subscription,.mw-parser-output .cs1-registration,.mw-parser-output .cs1-formatfont-size:95%.mw-parser-output .cs1-kern-left,.mw-parser-output .cs1-kern-wl-leftpadding-left:0.2em.mw-parser-output .cs1-kern-right,.mw-parser-output .cs1-kern-wl-rightpadding-right:0.2em
ISBN 0-901319-01-5 - 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 Bristol Cherub. |
- The Bristol Cherub - Flight, March 1923