The Curtiss O was a 75 hp (56 kW) water-cooled V-8 aero-engine, which was the basis of the commercially successful Curtiss OX series of engines.[1][2]
| Curtiss Model "O" Aero Engine | |
|---|---|
| |
| Replica of a Curtiss Model "O" engine | |
| Type | V-8 piston engine |
| National origin | United States |
| Manufacturer | Curtiss Aeroplane and Motor Company |
| First run | 1912 |
| Developed from | Curtiss L |
| Developed into | Curtiss OX |
Design and development edit
In 1909 Glenn Curtiss won the inaugural Gordon Bennett Trophy flying a Curtiss racing biplane powered by a V8 engine featuring a cross-flow OHV configuration (2 overhead valves, 1 rocker, 1 push-pull rod per cylinder). At that time most of Curtiss’s competitors were using less-efficient suction intake valves.[2]
Curtiss continued the development of their V8 OHV engines with demand for higher power outputs being driven by the US Navy’s requirement for seaplanes. By 1912 Curtiss V8’s were developing 75 hp at 1,100 rpm and were known as the Model O.[2]
The Model O was further developed to achieve 90 hp[2] at 1,200 rpm at which time it was designated as the Curtiss Model OX.[1][2] Curtiss OX production started in 1913 and it became the first mass produced American aero engine series. The most successful engine in the series was the Curtiss OX-5 which powered many early American aircraft including the Curtiss Jenny, the standard trainer used by American and Canadian forces during World War One.[1]
Applications edit
Source:[3]
- Curtiss Model E-8-75 Amphibious Aircraft
- Curtiss Model F Flying Boat. 1912 prototypes and 1913 models fitted with Curtiss "O“ engine.
- Curtiss Model G Tractor Biplane. Two aircraft completed for the US signal corps. 1st aircraft (No.21) fitted with 75 hp Curtiss O engine driving a 3 blade propeller through a chain speed reduction system. 2nd aircraft (No 22) fitted with a 90 hp direct drive Curtiss OX engine.
Specifications edit
General characteristics
- Type: 8-cylinder water-cooled Vee piston engine
- Bore: 4 in (102 mm)
- Stroke: 5 in (127 mm)
- Displacement: 503 in³ (8.2 L)
Components
- Valvetrain: One intake and one exhaust valve per cylinder, pushrod-actuated
- Cooling system: Water-cooled
Performance
- Power output: 75 hp (56 kW) at 1,100 rpm
References edit
- ^ a b c Angle, Glenn D. (1921). Airplane Engine Encyclopedia. Dayton, Ohio: The Otterbein Press.
- ^ a b c d e Rinek, Larry (1994). "Glenn H. Curtiss: An Early American Innovator in Aviation and Motorcycle Engines". SAE Transactions. 103: 927–945. Retrieved 31 Dec 2022.
- ^ Bowers, Peter M (1979). "Curtiss Companies and Accomplishments, 1909-14". Curiss Aircraft 1907-1947. Putnam. ISBN 0370100298.