Английская Википедия:Continental A40

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The Continental A40 engine is a carbureted four-cylinder, horizontally opposed, air-cooled aircraft engine that was developed especially for use in light aircraft by Continental Motors. It was produced between 1931 and 1941.[1][2][3]

Design and development

The Шаблон:Convert A40 was introduced in the depths of the Great Depression. At the time there were a number of small engines available but all suffered from either high cost, complexity, or low reliability. The A-40 addressed all those shortcomings and was instrumental in the production of light aircraft in the difficult economic constraints of the period. The A-40-4 introduced an increase in power to Шаблон:Convert. The engine later inspired the A-50 and subsequent engines.[1][2][4]

The A40 featured single ignition until the A-40-5 version, which introduced dual ignition. All engines in this family have a 5.2:1 compression ratio and were designed to run on fuel with a minimum octane rating of 73.[2][3]

The entire family of engines had its certification terminated on 1 November 1941. Engines produced before that date are still certified, but none can be produced after that date.[2][3]

Variants

A40
Single ignition, Шаблон:Convert at 2550 rpm, dry weight Шаблон:Convert[2]
A40-2
Single ignition, Шаблон:Convert at 2550 rpm, dry weight Шаблон:Convert[2]
A-40-3
Single ignition, Шаблон:Convert at 2550 rpm, dry weight Шаблон:Convert[2] Featured cadmium-nickel connecting rod bearings.[5]
A40-4
Single ignition, Шаблон:Convert at 2575 rpm, dry weight Шаблон:Convert,[2] Steel backed connecting rod inserts
A40-5
Dual ignition, Шаблон:Convert at 2575 rpm, dry weight Шаблон:Convert[3]

Applications

Файл:TaylorE-2CubC-GCGE.jpg
Taylor E-2 Cub showing its A-40 engine with the cylinders protruding through the cowling, Canada Aviation Museum.

Engines on display

Specifications (A40-5)

Шаблон:Pistonspecs

See also

Шаблон:Aircontent

References

Шаблон:Reflist

External links

Шаблон:Commons category

Шаблон:Continental aeroengines