Curtiss C-6
From Wikipedia, the free encyclopedia
The Curtiss C-6 is a six-cylinder, water-cooled, inline aircraft engine.[1]
Design and development
The C-6 features an overhead cam and aluminum cylinder jackets. Further development as a V-12 engine was carried out resulting in the C-12 and CD-12 engines.
Variants
- 6-cylinder water-cooled in-line engine
Applications
- Curtiss Lark
- Curtiss Oriole
- Curtiss MF Seagull
- Laird C-6 Special
- Pitcairn PA-1 Fleetwing
- Pitcairn PA-2 Sesquiwing
- Travel Air 2000
- Waco 9
Engines on display
- The Museum of Flight in Seattle, Washington has a Curtiss C-6A on display.
- The Canada Aviation and Space Museum has a Curtiss C-6A mounted on its Curtiss MF Seagull.[2]
Specifications (C-6)
General characteristics
- Type: 6-cylinder water-cooled inline
- Dry weight: 420 lb
Components
- Valvetrain: Two intake and two exhaust valves per cylinder, pushrod-actuated
- Cooling system: Water-cooled
Performance
- Power output:
- 160 hp at 1,250 rpm[3]
- 161 hp at 1,760 rpm[4]
- Fuel consumption: .5 lbs per hp per hr
- Oil consumption: .016 lbs per hp per hr
- Power-to-weight ratio: 0.38 hp/lb
See also
- Related lists
References
- ↑ "Joe Gertler's Memaerolbilia". Retrieved 17 Feb 2011.
- ↑ "Curtiss Seagull". Retrieved 17 Feb 2011.
- ↑ "Curtiss Night Mail Plane". Flight. 1 November 1923.
- ↑ Glenn Dale Angle. Airplane engine encyclopedia: an alphabetically arranged compilation of all.
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