Napier Javelin

{{short description|British air-cooled engine}}

{{Use dmy dates|date=December 2017}}

{{Use British English|date=December 2017}}

{{Infobox Aircraft Begin

|name=Javelin

|image= NapierJavelin.JPG

|caption=

}}{{Infobox Aircraft Engine

|type=Piston aero-engine

|manufacturer=D. Napier & Son

|first run=1932

|major applications=Martin-Baker M.B.1 (one aircraft only)
Percival Gull Four Mk IIA

}}

The Napier Javelin was a British six-cylinder inline air-cooled engine designed by Frank Halford and built by D. Napier & Son.Lumsden 2003, p.173. First flown in March 1934 in the prototype of the Percival Mew Gull racing aircraft, the engine was also used in the Spartan Arrow biplane and the Percival Gull.Lumsden 2003, p.174.

Development and design

In 1930 D. Napier & Son identified a market for light aircraft engines, noting that light aircraft cost much the same as their car and were being bought by much the same class of person. Frank Halford had been engaged as consultant designer and now began work on an air-cooled inverted six-cylinder design. Following a change of personnel, the engine was given the go-ahead in 1932, with aircraft manufacturer de Havilland identified as a likely customer.Charles Wilson and William Reader; Men and Machines: D. Napier & Son 1808-1958, Weidenfeld & Nicolson, 1958. pp. 132-3, 141, 145-6.

Unlike the later de Havilland Gipsy Six the poppet valves were operated by a single gear driven overhead camshaft.

The engine was first named the E97 and introduced to the market in 1932."Messrs. Napier Inaugurate a New Policy with a Six‐Cylinder Air‐Cooled Type", Aircraft Engineering and Aerospace Technology, Vol.4, No.8, 1 August 1932. pp. 210-212. However, none were sold, and, after slight modifications, it was reintroduced the next year as the Javelin.

Development continued but only a few were sold for experimental and prototype aircraft.

By 1935 Napier needed to refocus their efforts and, with Halford's broadly similar but more powerful de Havilland Gipsy Six now on the market, the Javelin was withdrawn.

Variants

=E.97=

:Initial version offered in 1932.

=Javelin I=

:First version bearing the Javelin name, producing {{cvt|150|hp|kW}}.

=Javelin III=

:A longer stroke and increased capacity version of {{cvt|160|hp|kW}}.

=Javelin IIIA=

:A Mark III with a starter motor, generator and other improvements for the Martin Baker MB.1.

Applications

Specifications (Javelin I)

{{pistonspecs|

|ref=Lumsden 2003, p.173.

|type=6-cylinder inverted inline air-cooled engine.

|bore=4.5 in (114.3 mm)

|stroke=5.25 in (133.35 mm)

|displacement=501 cu in (8.21 L)

|length=58.5 in (1486 mm)

|diameter=

|width=26 in (660.4 mm)

|height=31.5 in (800 mm)

|weight=410 lb (186 kg)

|valvetrain=Overhead cam poppet-valves

|supercharger=

|turbocharger=

|fuelsystem=Twin updraught carburettors

|fueltype=Petrol

|oilsystem=

|coolingsystem=Air-cooled

|power=150 hp (112 kW) at 2,000 rpm

|specpower=

|compression=5.3:1

|fuelcon=

|specfuelcon=

|oilcon=

|power/weight=0.365 hp/lb

|designer=

|reduction_gear=Direct drive, left hand tractor

|general_other=

|components_other=

|performance_other=

}}

See also

{{aircontent

|see also=

|related=

|similar aircraft=

|lists=

|similar engines=

}}

References

=Notes=

{{reflist}}

=Bibliography=

{{refbegin}}

  • Lumsden, Alec. British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing, 2003. {{ISBN|1-85310-294-6}}.

{{refend}}

{{Napierengines}}

Category:Aircraft air-cooled inline piston engines

Category:1930s aircraft piston engines

Category:Inverted aircraft piston engines

Javelin

Category:Straight-six engines