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The Blackburn Cirrus Minor is a British four-cylinder, inverted, in-line air-cooled aero-engine that was designed and built by the Cirrus Engine Section of Blackburn Aircraft Limited in the late 1930s.

Cirrus Minor
Blackburn Cirrus Minor 2A
Type Air-cooled 4-cylinder inline piston engine
National origin United Kingdom
Manufacturer Blackburn Aircraft
First run 1937

Design and development


The Cirrus Minor started life as a clean-sheet replacement for the original Cirrus and Hermes series of light aircraft engines. Design was led by Technical Director C. S. Napier, son of Montague Napier, and was already under way when in 1934 Cirrus-Hermes Engineering was taken over by the Blackburn Aeroplane & Motor Company and moved to Brough in Yorkshire.[1][2]

Napier remained Technical Director and, while he completed the development and initial sales of the Cirrus Minor and its larger stablemate the Cirrus Major, Blackburn kept Cirrus Hermes Engineering as a separate company (though without the hyphen in its name).[2]

Although completely new designs, they were of generally similar layout to the previous inverted engines, being air-cooled inverted four-cylinder inline designs. Like the others the Minor had a robust steel five-bearing crankshaft, but unlike them the long studs bolting the cylinder heads to the crank housing were replaced by short studs and flanges at each end of the cylinder barrels. Light alloy was used for the cylinder heads and con rods, while the valve gear was adopted with little change from the Hermes IV. The Claudel-Hobson down-draught carburetter featured independent altitude control, and the dual-redundant magnetos were of B.T.H. S.G.4/2 type.[1]

The Cirrus Minor was introduced in 1935. Two years later, Cirrus Hermes Engineering lost its identity as a separate company and was adopted as an operating division of its parent company, which by then had become Blackburn Aircraft.

The Minor was known for excellent reliability, and had a major "win" when it was selected to power the RAF's Taylorcraft Auster observation aircraft. The RAF's version had several modifications, known as the Series I. Although externally identical, the Series II engine was redesigned to operate on 77 octane fuel, as opposed to the original's 70, increasing power to 100 hp (75 kW).


Applications



Engines on display



Specifications (Cirrus Minor I)


Data from Lumsden [4]

General characteristics

Components

Performance


See also


Related development

Comparable engines

Related lists


References



Notes


  1. "A New Small Engine", Flight, 28 February 1935, pp.218-9.
  2. "The 'Cirrus Major'", Flight, 13 June 1935. Supplement.
  3. RAF Museum Cosford - Blackburn Cirrus II www.rafmuseum.org.uk Retrieved:1 January 2014
  4. Lumsden 2003, p. 90.

Bibliography





На других языках


[de] Blackburn Cirrus Minor

Der Blackburn Cirrus Minor war ein Kolbenflugmotor des britischen Herstellers Blackburn Aircraft für die allgemeine Luftfahrt. Abgeleitet war der Motor vom A.D.C. Cirrus, der von der Vorgängerfirma Cirrus Engines Ltd. ab 1925 produziert worden war. Diese hatte den Vierzylinder-OHV-Motor erstmals 1933 vorgestellt, zunächst mit einer Bohrung von 95 mm und einem Hub von 127 mm. Noch im selben Jahr wurde die Serienfertigung aufgenommen. Blackburn übernahm 1934 Cirrus Engines Ltd. und führte den Serienbau des Motors weiter. Er fand anschließend in mehreren Ausführungen breite Verwendung. 1937 wurde die Verdichtung erhöht und damit die Leistung entsprechend gesteigert.
- [en] Blackburn Cirrus Minor

[ru] Blackburn Cirrus Minor

Blackburn Cirrus Minor — британский поршневой авиационный двигатель воздушного охлаждения, разработанный и производившийся в конце 1930-х годов компанией Blackburn Aircraft.



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