ADC Cirrus
| Cirrus | |
|---|---|
|   | |
| ADC Cirrus II at the Science Museum, London | |
| Type | Air-cooled 4-cylinder inline piston engine | 
| National origin | United Kingdom | 
| Manufacturer | Aircraft Disposal Company, Cirrus Aero-Engines Limited | 
| First run | 1925 | 
| Major applications |  de Havilland DH.60 Moth  Avro Avian  | 
| 
 | |
The ADC Cirrus and Cirrus-Hermes are British aero engines of the mid-1920s. Sometimes known as the Blackburn Cirrus,[1] examples remain airworthy today.
Design and development
ADC Cirrus engines were originally built by ADC Aircraft until Cirrus Aero Engines Limited was formed in 1927. The company became Cirrus-Hermes in 1931 when it was bought by the Cirrus-Hermes Engineering Company and later became the Cirrus Engine Section of Blackburn & General Aircraft Limited in 1934, and operated as a separate division until production ended in the post-World War II era.[2]
Cirrus's first product was the 90 hp (67 kW) Cirrus I, which passed its 50-hour type rating in 1925. It was the first air-cooled inline engine, a design by Frank Halford that proved extremely popular for light aircraft. The basic layout (using one cylinder bank of an ADC Airdisco V-8 engine)[3] was quickly copied by a number of other manufacturers. Later versions named the Cirrus II, and Cirrus III were produced each with slightly greater displacement, and power (Cirrus II - 85 hp, Cirrus III - 90 hp).
The next model line, Cirrus-Hermes I, II, and IV were produced ranging in power from 105 hp to 140 hp depending on type. The later Cirrus engines were designed to run inverted.[4]
Variants

- Cirrus I
 - (1925)
 - Cirrus II
 - (1926)
 - Cirrus III
 - (1929)
 - Cirrus IIIA
 - (1933)
 - Cirrus-Hermes I
 - (1929)
 - Cirrus-Hermes II
 - (1930)
 - Cirrus-Hermes IIB (inverted)
 - (1931)
 - Cirrus-Hermes IV
 - (1930)
 - Cirrus-Hermes IVA
 - (1929) Inverted engine
 

Applications
Cirrus
  | 
  | 
Cirrus-Hermes
  | 
  | 
 
  | 
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Engines on display

- A preserved ADC Cirrus II is on display at the Science Museum (London).
 - A Cirrus Hermes is on display at the EAA AirVenture Museum in Oshkosh, Wisconsin.
 
Specifications (Cirrus I)
Data from Lumsden.[2]
General characteristics
- Type: Inline, air-cooled, upright 4-cylinder piston engine
 - Bore: 4.13 in (105 mm)
 - Stroke: 5.12 in (130 mm)
 - Displacement: 274.36 cu in (4.5 L)
 - Length: 45.8 in (116.3 cm)
 - Width: 18.26 in (46.4 cm)
 - Height: 34.3 in (87.1 cm)
 - Dry weight: lb ( kg)
 
Components
- Valvetrain: 1 inlet and 1 exhaust valve per cylinder
 - Fuel system: 1 Claudel carburettor
 - Fuel type: 70 octane
 - Cooling system: air
 
Performance
- Power output: 60 hp ( kW)
 - Compression ratio: 4.7:1
 
See also
- Related development
 
- Comparable engines
 
- Related lists
 
References
Notes
- ↑ This name applies only to the revised range of Cirrus engines produced after 1934 by Blackburn, e.g. the Blackburn Cirrus Major.
 - 1 2 Lumsden 2003, p. 130.
 - ↑ Gunston 1989, p. 40.
 - ↑ Lumsden 2003, p.132.
 - ↑ Lumsden 2003, pp. 130-132.
 - ↑ Cirrus engines may not be the main powerplant for these aircraft types (test installations are included).
 - ↑ Wesselink 1982 p.80
 - ↑ Wesselink 1982 p.81
 
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.
 
- Wesselink, Theo; Postma, Thijs (1982). De Nederlandse vliegtuigen. Haarlem: Romem. ISBN 90 228 3792 0.
 
External links
| Wikimedia Commons has media related to Cirrus engines. | 
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