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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]
| A40 | |
|---|---|
 | |
| Preserved Continental A40-5 (dual magneto, two spark plugs per cylinder) | |
| Type | Piston aero-engine |
| National origin | United States |
| Manufacturer | Teledyne Continental Motors |
| First run | 1931 |
| Major applications | Taylor E-2 Cub Piper J-2 Cub |
Design and development
The 37 hp (28 kW) 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 40 hp (30 kW). 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, 37 hp (28 kW) at 2550 rpm, dry weight 144 lb (65 kg)[2]
- A40-2
- Single ignition, 37 hp (28 kW) at 2550 rpm, dry weight 144 lb (65 kg)[2]
- A-40-3
- Single ignition, 37 hp (28 kW) at 2550 rpm, dry weight 144 lb (65 kg)[2] Featured cadmium-nickel connecting rod bearings.[5]
- A40-4
- Single ignition, 40 hp (30 kW) at 2575 rpm, dry weight 144 lb (65 kg),[2] Steel backed connecting rod inserts
- A40-5
- Dual ignition, 40 hp (30 kW) at 2575 rpm, dry weight 156 lb (71 kg)[3]
Applications
- Aeronca KC[6]
- Arup S-2
- Heath Parasol LNA-40
- Nicholson Junior KN-2
- Piper J-3 Cub[7][8]
- Porterfield CP-40 Zephyr[6]
- Rose Parakeet[6]
- Taylor E-2 Cub[1]
- Piper J-2 Cub[1]
- Taylorcraft A[6]
- Welch OW-5M[9]
Engines on display
Specifications (A40-5)
Data from Type Certificate Data Sheet 72,[2] Jane's 1938[10]
General characteristics
- Type: 4-cylinder air-cooled horizontally opposed aircraft piston engine
- Bore: 3.125 in (79.3 mm)
- Stroke: 3.75 in (95.3 mm)
- Displacement: 115 cu in (1.9 L)
- Length: 27.9375 in (710 mm)
- Width: 26.4375 in (672 mm)
- Height: 20.4375 in (519 mm)
- Dry weight: 154 lb (69.9 kg) dry with carburrettor and magnetos
Components
- Valvetrain: One intake and one exhaust side-valve per cylinder with a flathead valve design.
- Fuel system: CMC Stromberg NA-82 carburetor
- Fuel type: minimum 73 octane
- Cooling system: Air-cooled
Performance
- Power output: 40 hp (30 kW) at 2,575 rpm
- Specific power: 0.35 hp/(cu in) (15.3 kW/L)
- Compression ratio: 5.2:1
- Specific fuel consumption: 0.72 lb/(hp h) (0.439 kg/(kW h))
- Oil consumption: 0.025 lb/(hp h) (0.0153 kg/(kW h))
- Power-to-weight ratio: 0.28 hp/lb (0.45 kW/kg)
See also
Comparable engines
Related lists
References
- "Continental A-40". Old Rhinebeck Aerodrome. Retrieved 2011-09-26.
- Federal Aviation Administration (November 1941). "Approved Type Certificate 72" (PDF). Retrieved 2019-01-11.
- Federal Aviation Administration (November 1941). "Approved Type Certificate 174" (PDF). Retrieved 2019-01-11.
- Christy, Joe: Engines for Homebuilt Aircraft & Ultralights, pages 8-9. TAB Books, 1983. ISBN 0-8306-2347-7
- Sport Aviation. December 1959.
{{cite journal}}: Missing or empty|title=(help) - Wooden props (2008). "Fahlin Propellers". Archived from the original on 2013-12-28. Retrieved 2008-12-13.
- "ATC 660 data sheet" (PDF). Federal Aviation Administration. Retrieved 2011-09-27.
- "Aircraft Specification No. A-691" (PDF). Federal Aviation Administration. Retrieved 2011-09-27.
- "TC 637 data sheet" (PDF). Federal Aviation Administration. Retrieved 2011-09-26.
- Jane's All the World's Aircraft 1938. London: Sampson, Low & Martin company Limited. 1938.
External links
 |
Wikimedia Commons has media related to Continental A-40. |
- E-2 "Cub" Powerplant Instl - Holcomb's Aerodrome. The A-40, as installed in the Taylor E-2 Cub.
На других языках
[de] Continental A40
Der Continental A40 ist ein luftgekühlter Vierzylinderboxermotor des US-amerikanischen Herstellers Continental Motors, der speziell für den Einsatz in Leichtflugzeugen entwickelt wurde. Er wurde in den Jahren 1931 bis 1941 gebaut.[1]- [en] Continental A40
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