Curtiss O

Curtiss engine From Wikipedia, the free encyclopedia

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]

National originUnited States
First run1911
Quick facts Type, National origin ...
Curtiss Model "O" Aero Engine
Replica of a Curtiss Model "O" engine
TypeV-8 piston engine
National originUnited States
ManufacturerCurtiss Aeroplane and Motor Company
First run1911
Developed fromCurtiss L
Developed intoCurtiss OX
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Design and development

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 (two overhead valves, one rocker, one 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 featured separate operation of the inlet and exhaust valves[3] and a noticeably longer crankcase than the earlier Model L. Engine lubrication was also more advanced with an oil reservoir cast in the lower half of the crankcase from where a submerged rotary pump forced lubricating oil direct to all the bearings through a hollow crankshaft and camshaft. The connecting rods were also hollow allowing oil to be pumped directly to the wrist pin bearings and cylinder walls. Both fuel and lube oil consumption were low by contemporary standards.[4]

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

Source:[5]

Specifications

Data from Angle[1] and Aeronautics[4]

General characteristics

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
  • Fuel consumption: 4 U.S. gal (15 L) per hour
  • Oil consumption: 1 U.S. gal (4 L) per hour

See also

References

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