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Szekely SR-3
From Wikipedia, the free encyclopedia
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Szekely aircraft engines were three-cylinder radial engines built in Holland, Michigan in the 1920s and 30s. They were used to power small aircraft such as the Rearwin Junior, Taylor H-2 and American Eagle Eaglet. Often criticized for reliability issues and design flaws, many were replaced with better engines in their original airframes. Few examples still exist but a museum quality example is on display in the Holland Museum in Holland, Michigan.
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Variants
Data from:Jane's all the World's Aircraft 1931[1]
- SR-3 O
- Overhead valve combustion chamber, compression ratio 4.6:1, 45 hp (34 kW) at 1,750 rpm.
- SR-3 L
- Side-valve combustion chamber, compression ratio 5:1, 30 hp (22 kW) at 1,750 rpm.
Applications
Specifications (SR-3 Model O)
Data from American Engine Specifications,[2] Jane's all the World's Aircraft 1938,[3] Jane's all the World's Aircraft 1931[1]
General characteristics
- Type: Three-cylinder radial engine
- Bore: 4+1⁄8 in (105 mm)
- Stroke: 4+3⁄4 in (121 mm)
- Displacement: 191 cu in (3.13 L)
- Length: 25 in (635 mm) overall
- Diameter: 36 in (914 mm) (Model L 30 in (760 mm))
- Dry weight: 147 lb (67 kg)
Components
- Valvetrain: one camshaft per cylinder: pushrod-operated overhead inlet outlet valves, one each per cylinder; (Model L valves directly operated by tappets.)
- Fuel system: Stromberg NA-S3 Carburetor or Zenith equivalent
- Cooling system: Air-cooled
- Bosch FU6/3 or Scintilla magnetoes
Performance
- Power output: 45 hp (34 kW) at 1,750 rpm
- Specific fuel consumption: 0.60 lb/(hp·h) [0.365 kg/(kW·h)]
- Oil consumption: 0.16 lb/(hp·h)
See also
Comparable engines
Related lists
References
External links
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