Green E.6

Last updated

E.6
Green E.6.JPG
Preserved Green E.6 on display at the Fleet Air Arm Museum
Type Piston aero engine
Manufacturer Green Engine Co Ltd
First runDecember 1911
Number built42

The Green E.6 was a British six-cylinder, water-cooled aero engine that first ran in 1911, [1] it was designed by Gustavus Green and built by the Green Engine Co and Mirlees, Bickerton & Day of Stockport between August 1914 and December 1918.

Aircraft engine Engine designed for use in powered aircraft

An aircraft engine is a component of the propulsion system for an aircraft that generates mechanical power. Aircraft engines are almost always either lightweight piston engines or gas turbines, except for small multicopter UAVs which are almost always electric aircraft.

Gustavus Green was a British engineer who made significant contributions to the design of early aircraft engines.

The Green Engine Co was a British engine company founded by Gustavus Green in Bexhill to sell engines of his design. He flourished especially as a designer of aeroplane engines during the first two decades of the 20th century. The engines were actually manufactured by the Aster Engineering Company.

Contents

Applications

Sopwith Bat Boat

The Sopwith Bat Boats were British flying boats designed and built from 1912 to 1914. A single-engined pusher biplane, the Bat Boat was the first successful flying boat and amphibious aircraft built in the United Kingdom, with examples used by the Royal Navy and by Greece and Germany.

The Sopwith Three-seater was a British aircraft designed and built prior to the start of the First World War. One of the first aircraft built by the Sopwith Aviation Company, it was operated by both the Royal Naval Air Service (RNAS) and the Royal Flying Corps (RFC), being used briefly over Belgium by the RNAS following the start of the War.

Sopwith 1913 Circuit of Britain floatplane

The Sopwith 1913 Circuit of Britain Biplane was a British floatplane built by Sopwith to take part in the 1913 Daily Mail Circuit of Britain Air race. The only entrant to start, it had to be withdrawn after a landing accident two-thirds of the way through the race.

Engines on display

A preserved Green E.6 engine is on public display at the Fleet Air Arm Museum, RNAS Yeovilton.

Fleet Air Arm Museum naval aviation museum in England

The Fleet Air Arm Museum is devoted to the history of British naval aviation. It has an extensive collection of military and civilian aircraft, aero engines, models of aircraft and Royal Navy ships, and paintings and drawings related to naval aviation. It is located on RNAS Yeovilton airfield, and the museum has viewing areas where visitors can watch military aircraft take off and land. It is located 7 miles (11 km) north of Yeovil, and 40 miles (64 km) south of Bristol.

RNAS Yeovilton (HMS Heron) airfield of the Royal Navy, sited a few miles north of Yeovil, Somerset in the UK

Royal Naval Air Station Yeovilton, or RNAS Yeovilton, is an airfield of the Royal Navy and British Army, sited a few miles north of Yeovil, Somerset. It is one of two active Fleet Air Arm bases and is currently home to the Royal Navy Wildcat HMA2 and Army Air Corps Wildcat AH1 helicopters as well as the Royal Navy's Commando Helicopter Force Merlin HCi3/3A/4 and Wildcat AH1 helicopters.

Specifications (E.6)

Data fromLumsden [2]

General characteristics

Components

Valvetrain mechanical system that controls operation of the valves in an internal combustion engine

A valvetrain or valve train is a mechanical system that controls operation of the valves in an internal combustion engine, whereby a sequence of components transmits motion throughout the assembly.

Overhead camshaft valvetrain configuration

Overhead camshaft, commonly abbreviated to OHC, is a valvetrain configuration which places the camshaft of an internal combustion engine of the reciprocating type within the cylinder heads and drives the valves or lifters in a more direct manner compared with overhead valves (OHV) and pushrods.

An octane rating, or octane number, is a standard measure of the performance of an engine or aviation fuel. The higher the octane number, the more compression the fuel can withstand before detonating (igniting). In broad terms, fuels with a higher octane rating are used in high performance gasoline engines that require higher compression ratios. In contrast, fuels with lower octane numbers are ideal for diesel engines, because diesel engines do not compress the fuel, but rather compress only air and then inject fuel into the air which was heated by compression. Gasoline engines rely on ignition of air and fuel compressed together as a mixture, which is ignited at the end of the compression stroke using spark plugs. Therefore, high compressibility of the fuel matters mainly for gasoline engines. Use of gasoline with lower octane numbers may lead to the problem of engine knocking.

Performance

Power density is the amount of power per unit volume.

Power-to-weight ratio is a calculation commonly applied to engines and mobile power sources to enable the comparison of one unit or design to another. Power-to-weight ratio is a measurement of actual performance of any engine or power source. It is also used as a measurement of performance of a vehicle as a whole, with the engine's power output being divided by the weight of the vehicle, to give a metric that is independent of the vehicle's size. Power-to-weight is often quoted by manufacturers at the peak value, but the actual value may vary in use and variations will affect performance.

See also

Comparable engines

Related lists

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Green C.4

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The Clerget 11Eb was an 11-cylinder rotary aircraft engine of the World War I era designed by Pierre Clerget. Powering Sopwith types it was nominally rated at 200 horsepower (150 kW).

The Clerget 7Z was a seven-cylinder rotary aircraft engine of the World War I era designed by Pierre Clerget. First appearing in 1911 it was nominally rated at 80 horsepower (60 kW). 347 examples were jointly built in Britain by Gordon Watney & Co Ltd of Weybridge and Gwynnes Limited of Hammersmith.

References

Notes

  1. Gunston 1986, p. 74.
  2. Lumsden 2003, p. 156.

Bibliography

  • Gunston, Bill. World Encyclopaedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN   1-85260-163-9
  • Lumsden, Alec. British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing, 2003. ISBN   1-85310-294-6.
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