De Havilland Iris

Last updated

Iris
De Havilland Iris.JPG
de Havilland Iris
Type Piston aero engine
Manufacturer Iris Cars Ltd, Willesden
First run1909
Major applications de Havilland Biplane No. 1
de Havilland Biplane No. 2
Number built6

The de Havilland Iris was a British four-cylinder, liquid-cooled, horizontally opposed aero engine. Notable as the first aero engine to be designed by Geoffrey de Havilland it was produced in small numbers between 1909 and 1910 by Iris Cars Ltd of Willesden from which it took its name.

Contents

Design and development

By 1908 Geoffrey de Havilland had designed and built two motorcycle engines and was planning his first aircraft, the de Havilland Biplane No. 1. He had studied the engine used by the Wright brothers and believed that he could design a similar unit with an improved power-to-weight ratio. Whilst working as a designer for the Motor Omnibus Construction Company in London he produced drawings for his new engine over a period of three to four months and commissioned the Iris Cars Ltd, where his brother Ivon de Havilland had been the Chief Designer, to build it at a cost of £250. [1]

The design featured a horizontally opposed, four-cylinder layout with a single camshaft operating poppet valves through pushrods that were hollowed to save weight. The crankshaft was supported on ball bearings which allowed a simple 'splash' lubrication system to be used. Cooling was by water with the cylinders being encased in copper jackets. The engine ran adequately but was not placed into series production. A small order was received from the British Government for use in airships. [2]

1957 replica

In 1957 instructors and apprentices from the de Havilland Aircraft Company Technical School decided to construct a replica engine, almost 50 years after the original Iris was built. The Iris Motor Company had long since closed and its records, along with the original engine drawings, were destroyed by German bombing during World War II. Flight magazine had featured an article on the engine in May 1910 with a detailed technical description and line drawings. This information along with the original designer's memory were used to produce a new set of drawings and components. Several companies involved with the original engine assisted with new parts, Claudel-Hobson supplied the carburettor, Lodge Plugs Ltd the spark plugs and Simms Motor Units assisted with re-conditioning a magneto that had been borrowed from the London Science Museum. [3]

Connected to a lathe via a belt drive, the engine started at the first attempt in May 1961 and idled steadily at 2-300 rpm. It is reported that the engine was then displayed in the showroom of the de Havilland Engine Company at Leavesden. [3]

Applications

Iris-powered de Havilland Biplane No. 2 or RAF F.E.1 RAEF1.jpg
Iris-powered de Havilland Biplane No. 2 or RAF F.E.1

Specifications (Iris)

Data fromLumsden and Flight [4] [5]

General characteristics

Components

Performance

See also

Comparable engines

Related lists

Related Research Articles

<span class="mw-page-title-main">Bristol Jupiter</span> British nine-cylinder radial engine family

The Bristol Jupiter is a British nine-cylinder single-row piston radial engine that was built by the Bristol Aeroplane Company. Originally designed late in World War I and known as the Cosmos Jupiter, a lengthy series of upgrades and developments turned it into one of the finest engines of its era.

<span class="mw-page-title-main">Bristol Perseus</span> 1930s British piston aircraft engine

The Bristol Perseus was a British nine-cylinder, single-row, air-cooled radial aircraft engine produced by the Bristol Engine Company starting in 1932. It was the first production sleeve valve aero engine.

de Havilland Gipsy Major 1930s British piston aircraft engine

The de Havilland Gipsy Major or Gipsy IIIA is a four-cylinder, air-cooled, inverted inline engine used in a variety of light aircraft produced in the 1930s, including the famous Tiger Moth biplane. Many Gipsy Major engines still power vintage aircraft types.

The Cirrus and Hermes or Cirrus-Hermes are a series of British aero engines manufactured, under various changes of ownership, from the 1920s until the 1950s. The engines were all air-cooled, four-cylinder inline types, with earlier ones upright and later designs inverted.

<span class="mw-page-title-main">Rolls-Royce Condor</span>

The Rolls-Royce Condor aircraft piston engine was a larger version of the Rolls-Royce Eagle developing up to 675 horsepower. The engine first ran in 1918 and a total of 327 engines were recorded as being built.

<span class="mw-page-title-main">Armstrong Siddeley Jaguar</span> 1920s British piston aircraft engine

The Armstrong Siddeley Jaguar is an aircraft engine developed by Armstrong Siddeley. The Jaguar was a petrol-fuelled air-cooled 14-cylinder two-row radial engine design. The Jaguar III was first used in 1923, followed in 1925 by the Jaguar IV and in 1927 by the Jaguar VI. In 1925 the Jaguar became the first production aero engine incorporating a geared supercharger.

de Havilland Gipsy 1920s British piston aircraft engine

The de Havilland Gipsy is a British air-cooled four-cylinder in-line aircraft engine designed by Frank Halford in 1927 to replace the ADC Cirrus in the de Havilland DH.60 Moth light biplane. Initially developed as an upright 5 litre capacity engine, later versions were designed to run inverted with increased capacity and power.

<span class="mw-page-title-main">Blackburn Cirrus Major</span> 1930s British piston aircraft engine

The Blackburn Cirrus Major is a British, inline-four aircraft engine that was developed in the late 1930s.

<span class="mw-page-title-main">Siddeley Tiger</span> 1920s British piston aircraft engine

The Siddeley Tiger was an unsuccessful British aero engine developed shortly after the end of World War I by Siddeley-Deasy. Problems encountered during flight testing caused the project to be cancelled.

<span class="mw-page-title-main">ABC Dragonfly</span>

The ABC Dragonfly was a British radial engine developed towards the end of the First World War. It was expected to deliver excellent performance for the time and was ordered in very large numbers. It proved, however, to be extremely unreliable and was abandoned when its faults were unable to be corrected.

<span class="mw-page-title-main">ADC Cirrus</span> 1920s British piston aircraft engine

The ADC Cirrus is a series of British aero engines manufactured using surplus Renault parts by the Aircraft Disposal Company (ADC) in the 1920s.

<span class="mw-page-title-main">Napier Cub</span> 1910s British aircraft piston engine

The Napier Cub was an unusual and very large experimental 1,000 horsepower (750 kW) 16-cylinder 'X' pattern liquid-cooled aero engine built by the British engine company D. Napier & Son. The Cub was the only Napier 'X' engine design. First flown on 15 December 1922 in an Avro Aldershot biplane bomber aircraft, the only other application was in the Blackburn Cubaroo. Only six engines of this type were ordered and produced.

<span class="mw-page-title-main">Napier Javelin</span> British air-cooled engine

The Napier Javelin was a British six-cylinder inline air-cooled engine designed by Frank Halford and built by D. Napier & Son. 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.

<span class="mw-page-title-main">ABC Scorpion</span> 1920s British piston aircraft engine

The ABC Scorpion is a 30 hp (22 kW) two-cylinder aero engine designed by British engineer Granville Bradshaw for use in light aircraft. The engine was built by ABC Motors Limited and first ran in 1921.

<span class="mw-page-title-main">ADC Airdisco</span> 1920s British piston aircraft engine

The ADC Airdisco is a British V-8 aero engine that first ran in 1925.

The ADC Nimbus was a British inline aero engine that first ran in 1926. The Nimbus was developed from the Siddeley Puma aero engine by Frank Halford of the Aircraft Disposal Company, the goal was to develop the Puma to produce its intended power output which Halford eventually achieved. The Nimbus was further developed into an air-cooled version known as the ADC Airsix which did not enter production and was not flown.

The Blackburn Cirrus Midget was a British four-cylinder, inverted, inline air-cooled aero engine designed and built in 1937 by the Cirrus Engine Section of Blackburn Aircraft Limited. Little is known of its development and use, its sole aircraft application being reported as the Chilton D.W.1 although it is possible that this did not transpire.

The de Havilland Ghost was a British V-8 aero engine that first ran in 1928.

<span class="mw-page-title-main">Beardmore 160 hp</span>

The Beardmore 160 hp is a British six-cylinder, water-cooled aero engine that first ran in 1916, it was built by Arrol-Johnston and Crossley Motors for William Beardmore and Company as a development of the Beardmore 120 hp, itself a licensed-built version of the Austro-Daimler 6.

<span class="mw-page-title-main">Green D.4</span> Engine

The Green D.4 was a four-cylinder watercooled inline piston engine produced by the Green Engine Co in the UK in 1909. It produced about 60 hp (45 kW) and played an important role in the development of British aviation before World War I.

References

Notes

  1. McKay 2010, p. 16.
  2. McKay 2010, p. 17.
  3. 1 2 McKay 2010, pp. 18 - 19.
  4. Lumsden 2003, p. 136.
  5. Gough 1956, p. 166.

Bibliography

  • Gough, Edward. A. The first D.H. engine. Flight, 27 July 1956.
  • Lumsden, Alec. British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing, 2003. ISBN   1-85310-294-6.
  • McKay, Stuart. The Moth - Magazine of the de Havilland Moth Club, No. 150. de Havilland Moth Club Ltd. Berkhamsted, Hertfordshire. June 2010.