What is Armstrong Siddeley Jaguar?

Information about Armstrong Siddeley Jaguar

The Armstrong Siddeley Jaguar was an aero engine developed by Armstrong Siddeley. The jaguar was a petrol-fuelled aircooled 14-cylinder double radial engine design. The Jaguar III was first used in 1923, followed in 1924 by the Jaguar IV and 1926 by the Jaguar VI.

Specifications (Armstrong Siddeley Jaguar)

General characteristics
  • Type: 14 cylinder twin-row air cooled radial engine
  • Bore: 127mm (5 in)
  • Stroke: 140mm (5.5 in)
  • Displacement: 24.7 Liters (1,512 cu in)
  • Dry weight: 354kg (780lb)

Components

Performance

Applications

See also

External links


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Armstrong Siddeley was a British engineering group that operated during the first half of the 20th century. It was formed in 1919 and is best known for the production of luxury motor cars and aircraft engines.
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Gasoline or petrol is a petroleum-derived liquid mixture consisting mostly of aliphatic hydrocarbons and enhanced with aromatic hydrocarbons toluene, benzene or iso-octane to increase octane ratings, primarily used as fuel in internal combustion engines.
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1923 1924 1925 1926

19th Century · 20th century · 21st century
1890s 1900s 1910s 1920s 1930s 1940s 1950s
1920 1921 1922 1923
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For other meanings, see supercharger (disambiguation)


A supercharger (blower) is an air compressor that forces more air and more oxygen to the combustion chamber(s) of an internal combustion engine than achievable with ambient atmospheric
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In engineering, specific power, also known as power per unit mass or power density, refers to the amount of power delivered by an energy source, divided by some measure of the source's size or mass.
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Type airliner
Manufacturer Armstrong Whitworth
Maiden flight March 1926
Primary user Imperial Airways
Number built 7
For the 1950s transport, see Armstrong Whitworth AW.

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Type Army Cooperation Aircraft
Manufacturer Armstrong Whitworth
Maiden flight 1925
Introduced 1927
Retired 1935
Primary users Royal Air Force
Royal Canadian Air Force

Produced 1927 - 1933
Number built
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Type Fighter
Manufacturer Sir W.G. Armstrong Whitworth Aircraft Limited
Designed by F.M. Green
Maiden flight 1919 (Siddeley-Deasy S.R.2 Siskin), 1921
Introduced 1923
Retired 1932
Primary users Royal Air Force
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Type Fighter
Manufacturer Fairey
Maiden flight November 1922
Introduced 1923
Retired 1934
Primary user Fleet Air Arm
Produced 1923-1926
Number built 196

The Fairey Flycatcher
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Type Fighter
Manufacturer Gloster Aircraft Company
Designed by H.P.Folland
Maiden flight 1923
Introduced 1923
Retired RAF 1928, RNZAF 1938
Status extinct
Primary users Royal Air Force
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Type Airliner
Manufacturer Handley Page
Maiden flight 1919
Introduced 1921
Retired 1934
Primary users SABENA
Imperial Airways
Number built 25
Variants Handley Page Hyderabad The
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Type Army Cooperation Aircraft
Manufacturer Vickers
Maiden flight 1925
Introduced 1928
Retired 1940
Primary users Bolivia
Irish Air Corps
Number built 15

The Vickers Vespa
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List of aircraft engines:

Piston engines

Two- and four-stroke rotary, radial, inline.

A to E

ABC Motors
  • ABC Scorpion
  • ABC Wasp
Aeronca
  • Aeronca E-113
Aerosport-Rockwell

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aircraft is a vehicle which is able to fly through the air (or through any other atmosphere). All the human activity which surrounds aircraft is called aviation. (Most rocket vehicles are not aircraft because they are not supported by the surrounding air).
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Armstrong Siddeley was a British engineering group that operated during the first half of the 20th century. It was formed in 1919 and is best known for the production of luxury motor cars and aircraft engines.
..... Read more.
Armstrong-Siddeley Cheetah is a British air-cooled aircraft radial engine.

Development

The basic design of the Cheetah remained unchanged since its introduction in 1919.
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The Armstrong Siddeley Genet was a five-cylinder, air-cooled, radial engine for aircraft use built in the UK, first run in 1928. It developed 88 hp at 2,200 rpm and was a popular light airplane type.

Specifications

  • Bore: 101.

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The Armstrong Siddeley Leopard was an aero engine developed by Armstrong Siddeley.

Specifications (Armstrong Siddeley Leopard)

General characteristics
  • Type: 14 cylinder twin-row air cooled radial engine
  • Bore: 152mm (6 in)
  • Stroke:


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The Armstrong-Siddeley Lynx was an aero engine developed by Armstrong Siddeley. Testing began in 1923 and by 1939 6,000 had been produced. In Italy Alfa Romeo built license version of this engine named as Alfa Romeo Lynx (200 hp).
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The Armstrong Siddeley Mongoose was an aero engine developed by Armstrong Siddeley. Developed in the 1920s it was a radial engine used in the Hawker Tomtit trainer and Parnall Peto.
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The Armstrong Siddeley Nimbus was a piston aero-engine developed by Armstrong Siddeley.

See also

  • List of aircraft engines


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The Armstrong Siddeley Panther was an aero engine developed by Armstrong Siddeley.

Specifications (Armstrong Siddeley Panther VII)

General characteristics
  • Type: 14 cylinder twin-row air cooled radial engine
  • Bore: 155mm (5.


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Siddeley Puma was a British aero engine developed towards the end of World War I and produced by Siddeley-Deasy. The first engines left the production lines of Siddeley-Deasy in Coventry in August 1917 and the production continued until December 1918.
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The Armstrong-Siddeley Serval was an aero engine developed by Armstrong Siddeley.

Development

The Serval was a ten-cylinder, single-row, air-cooled radial piston engine.
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The Armstrong Siddeley Tiger was a 14-cylinder air cooled radial engine of the 1930-40's. It started life as the Armstong Siddeley Jaguar Major but was renamed as the Tiger.
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The Armstrong-Siddeley Adder was an early British turbojet engine developed by the Armstrong Siddeley company and first run in November 1948.

The Adder, a pure-jet derivative of the Armstrong Siddeley Mamba, was originally developed as an expendable engine to power the
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Sapphire was a turbojet engine produced by Armstrong Siddeley in the 1950s. It was the ultimate development of work that had started as the Metrovick F.2 in 1940, evolving into an advanced axial flow design with an annular combustion chamber that developed over 11,000 lbf
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Viper was a turbojet engine developed and produced by Armstrong Siddeley and then by its successor companies Bristol-Siddeley and Rolls-Royce Limited. It entered service in 1953.
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