In this article we are going to talk about Kinner C-5, a topic that has become very relevant in recent years/centuries. Kinner C-5 is a topic that has captured the attention of experts and people of all ages, due to its impact on various aspects of society. Throughout this article, we will thoroughly examine what Kinner C-5 is, its importance, evolution over time and its influence in different areas. Additionally, we will explore the different perspectives and opinions that exist about Kinner C-5, as well as the challenges and benefits it poses. Without a doubt, Kinner C-5 is a topic that concerns us all, and it is essential to understand it in its entirety to better understand the world in which we live.
| C-5 | |
|---|---|
| Type | Radial engine |
| Manufacturer | Kinner Airplane & Motor Corporation |
| Developed from | Kinner R-5 |
The Kinner C-5 was an American five cylinder radial engine for small general and sport aircraft of the 1930s.
Design and development
The C-5 was a development of the earlier R-5 with greater power and dimensions. The main change was the increase in cylinder bore from 128 mm (5.0 in) to 143 mm (5.625 in) and an increase in cylinder stroke from 140 mm (5.5 in) to 145 mm (5.75 in). This led to a corresponding increase in displacement from 8.85 liters (540 cu in) to 11.71 liters (715 cu in).
The U.S. military designation was R-720.
Applications
- Consolidated YPT-11B
- Kellett K-3
- Kinner P
- Stearman 6H Cloudboy
- Stearman YPT-9C
- Verville YPT-10D
- Waco OSO
- Waco OEC
- Waco ODC
- Waco OBF
- Waterman FlexWing
Specifications
Data from Jane’s All the World’s Aircraft 1938[1]
General characteristics
- Type: 5-cylinder air cooled radial
- Bore: 5.625 in (143 mm)
- Stroke: 5.75 in (145 mm)
- Displacement: 715 cu in (11.71 liters)
- Length: 34.8in (884 mm)
- Diameter: 50 in (1,270 mm)
- Dry weight: (dry) 420 lb (190 kg)
Components
- Valvetrain: 1 inlet and 1 exhaust valve per cylinder
- Fuel system: 1 Stromberg carburetor
- Fuel type: 73 octane
- Cooling system: Air
Performance
- Power output: maximum 245 hp at 2,200 rpm, cruise 210 hp at 1,900 rpm
- Compression ratio: 5.25:1
- Specific fuel consumption: 0.6 lb (273 gm) /hp/hr
- Oil consumption: 0.015 lb (7 gm) /hp/hr
See also
Related lists
References
- Grey, C.G. (1972). Jane’s All the World’s Aircraft 1938. London: David & Charles. pp. 88d. ISBN 0-7153-5734-4.
