Continental O-170
| A65/O-170 | |
|---|---|
| |
| Continental O-170 on display at the Wings Over the Rockies Air and Space Museum | |
| Type | Piston aero-engine |
| Manufacturer | Continental Motors |
The Continental O-170 engine is the collective military designation for a family of small aircraft engines, known under the company designation of A50, A65, A75 and A80. The line was designed and built by Continental Motors commencing in the 1940s. It was employed as the powerplant for civil and military light aircraft.[1]
The horizontally opposed, four-cylinder engines in this family are all identical in appearance, bore, stroke, dry weight and piston displacement. All feature a bottom-mounted updraft carburetor fuel delivery system. The higher power variants differ only in compression ratio and maximum allowable rpm, plus minor modifications. The lower power versions are fully convertible to the higher rated versions.[1]
Design and development
In all models of this family of engines the cylinder heads are of aluminum alloy, screwed and shrunk onto steel barrels. Spark plug inserts and intake valve seats are made from aluminum-bronze alloy, while the exhaust valve seats are steel. The engines all employ hydraulic tappets which operate in aluminum guides that are machined into the crankcase. The tappets are built from four parts, a cam follower body, cup, cylinder and piston and operate with clearances of 0.03 in (1 mm) to 0.11 in (3 mm). The pushrods are steel and feature pressed-in ball ends.[1]
Lubricating oil is delivered under pressure from the 4 US qt (4 L) oil sump to the drive bearings and the crankpins though the crankshaft. The cylinder walls and pistons are spray lubricated. Normal operating oil pressure is 35 psi, with minimum idle oil pressure 10 psi.[1]
Variants
- A50
- 50 hp (37 kW), Compression ratio 5.4:1, max rpm 1,900, fuel consumption at cruise 3.8 US gph[1]
- A50-1
- A50-2
- A50-3
- A50-4
- A50-5
- A50-6
- A50-7
- A65
- 65 hp (48 kW), Compression ratio 6.3:1, max rpm 2,300, fuel consumption at cruise 4.4 US gph. The exhaust valves have stellite faces. The pistons have three rings, although some early production A65s had four piston rings.[1][2]
- A65-1
- A65-2
- A65-3
- A65-4
- A65-5
- A65-6
- A65-7
- A65-8
- A65-8F
- A65-9:
- A65-85
- ?
- A75
- 75 hp (56 kW), Compression ratio 6.3:1, max rpm 2,600, fuel consumption at cruise 4.8 US gph. The exhaust valves have stellite faces and the connecting rods have a 0.125 in (3 mm) hole drilled in the rod cap to improve lubrication. The pistons have three rings and smaller piston pins.[1][2]
- A75-1
- A75-2
- A75-3
- A75-4
- A75-5
- A75-6
- A75-14
- A80
- 80 hp (60 kW), Compression ratio 7.55:1, max rpm 2,700, fuel consumption at cruise 5.2 US gph. The connecting rods have a 0.125 in (3 mm) hole drilled in the rod cap to improve lubrication. The pistons have five rings and smaller piston pins.[1]
- A80-1
- A80-2
- A80-3
- A80-4
- A80-5
- A80-6
- A80-8
- O-170
- Military designation for the A55, A65, A75, A80 family of engines.
- O-170-1
- O-170-3
- O-170-5
- O-170-7
Applications
- A50
- Aeronca KCA
- Aeronca 50C
- Aeronca 50TC
- Aeronca S50C[3]
- Luscombe 8[3]
- Piper J-3[3]
- Piper J-4[3]
- Porterfield CP50[3]
- Porterfield CP55[3]
- Taylorcraft BC[3]
- Taylorcraft BCS[3]
- A65
- Aeronca S65C
- Aeronca S65CA[3]
- Aeronca 65F
- Aeronca 65CA[3]
- Aeronca Champion
- Airdrome Fokker D-VIII
- Bearhawk LSA
- Christavia Mk I
- Circa Reproductions Nieuport
- Coupé-Aviation JC-01
- Ercoupe 415C[3]
- E & P Special
- Falconar F11 Sporty
- Fisher Celebrity
- Fisher Dakota Hawk
- Helmy Aerogypt[4]
- Henderson Little Bear
- Interstate SIA Cadet[3]
- Jameson RJJ-1 Gipsy Hawk
- Luscombe 8A[3]
- Piper J-3[3]
- Piper J-4A[3]
- Porterfield CP65[3]
- Rearwin Skyranger 165[3]
- Smith Miniplane[5]
- Stolp SA-900 V-Star
- Taylorcraft BCS
- Taylorcraft BCS12
- Taylorcraft 65[1][3]
- Tayorcraft BC
- Taylorcraft BC1265
- Taylorcraft BCT[1][3]
- Taylorcraft L-2
- Taylorcraft Tandem[3]
- Turner T-40
- Warner Revolution I
- Wolf W-11 Boredom Fighter
- A75
- Bearhawk LSA
- Culver LCA[3]
- Luscombe 8C
- Luscombe 8D[3]
- Piper J-4E[3]
- Piper J-5[3]
- Porterfield 75C[3]
- Rearwin Skyranger 175[3]
- Stinson HW75[3]
- A80
Specifications (O-170-3 or A-65-8)
Data from Continental Aircraft Engine Operator's Manual[2]
General characteristics
- Type: 4-cylinder air-cooled horizontally opposed aircraft piston engine
- Bore: 3.875 in (98 mm)
- Stroke: 3.625 in (92 mm)
- Displacement: 171 in³ (2.8 L)
- Length: 31 in (787 mm)
- Width: 31.5 in (800 mm)
- Height: 29 5/16 in (745 mm)
- Dry weight: 170 lb (77 kg)
Components
- Valvetrain: One intake and one exhaust valve per cylinder, pushrod-actuated.
- Fuel system: Updraft carburetor
- Fuel type: 80/87 octane avgas
- Oil system: Wet sump
- Cooling system: Air-cooled
Performance
- Power output: 65 hp (48 kW) at 2,300 rpm
- Specific power: 0.38 hp/in³ (17.1 kW/L)
- Compression ratio: 6.3:1
- Fuel consumption: 4.4 US gal/hr
- Oil consumption: maximum desirable 0.37 US quarts/hr
- Power-to-weight ratio: 0.38 hp/lb (0.62 kW/kg)
See also
Related lists
Notes
- ^ a b c d e f g h i j Christy (1983)
- ^ a b c Teledyne Continental Motors: Continental Aircraft Engine Operator's Manual, pages 4-5. Teledyne Continental Motors, FAA Approved December 1980. Continental Form No. X30012
- ^ a b c d e f g h i j k l m n o p q r s t u v w x y z aa Wooden props (2008). "Fahlin Propellers". Retrieved 2008-12-13.
- ^ Jackson (1974)
- ^ Plane & Pilot: 1978 Aircraft Directory, page 153. Werner & Werner, 1978. ISBN 0-918312-00-0
References
- Christy, Joe: Engines for Homebuilt Aircraft & Ultralights, pages 43–52. TAB Books, 1983. ISBN 0-8306-2347-7
- Donald, David (1995). American Warplanes of World War II. New York: Barnes & Noble Books. ISBN 0-7607-2274-9.
- Jackson, A.J. (1974). British Civil Aircraft since 1919 Volume 3. London: Putnam. ISBN 0-370-10014-X.
{{cite book}}: Cite has empty unknown parameter:|coauthors=(help) - Instruction Manual Continental Models A50, A65, A75 and A80 Aircraft Engines. Muskegon, Michigan: Continental Motors Corporation. 1944.