König SD 570
| König SD 570 | |
|---|---|
| Type | Two-stroke aircraft engine |
| National origin | Canada |
| Manufacturer | Compact Radial Engines |
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The König SD 570 is a four-cylinder, two-stroke, single ignition radial aircraft engine designed for powered paragliders, powered parachutes and single place ultralight trikes.[1][2]
The engine was originally designed and produced by Dieter König of Berlin, Germany. The design was sold to Zanzottera Technologies of Italy and then sold again, along with the rest of Zanzottera's two-stroke ultralight aircraft engine line to Compact Radial Engines of Surrey, British Columbia, Canada.[1][2]
Development
The SD 570 is an unusual four-cylinder radial engine that is very compact and light weight at only 19 kg (42 lb). The engine features single capacitor discharge ignition, a single Bing 49 diaphragm-type carburetor and rotary valve induction. It is currently offered without a reduction drive, although when Zanzottera built it an optional 1.75:1 cog belt reduction drive was available. Starting is electric starter only and a recoil starter is not an option.[1][2][3]
Earlier versions produced 28 hp (21 kW) at 4200 rpm with a slide-type carburetor and reduction drive. The current version is rated at 24 hp (18 kW) at 4200 rpm. Time between overhaul is rated as 300 hours.[1][2][3]
The SC 430 shares the same bore and stroke as the smaller three-cylinder König SC 430 radial engine.[2][3]
Variants
- Zanzottera SD 570
- Four-cylinder, two-stroke, single-ignition, radial aircraft engine producing 28 hp (21 kW) at 4200 rpm. Equipped with a slide-type carburetor and an optional reduction drive.[1][3]
- Compact Radial Engines SD 570
- Four-cylinder, two-stroke, single-ignition, radial aircraft engine producing 24 hp (18 kW) at 4200 rpm. Equipped with a Bing 49 diaphragm-type carburetor and no reduction drive.[2]
Applications
Specifications (CD 570)
Data from Compact Radial Engines[2]
General characteristics
- Type: Four-cylinder, radial two-stroke aircraft engine
- Bore: 66 mm (2.60 in)
- Stroke: 42 mm (1.65 in)
- Displacement: 579 cc (35.33 cu in)
- Dry weight: 19 kg (42 lb)
Components
- Valvetrain: rotary valve induction
- Oil system: premixed oil and fuel
- Cooling system: air-cooled
- Reduction gear: none
Performance
- Power output: 24 hp (18 kW) at 4200 rpm
See also
References
- ↑ 1.0 1.1 1.2 1.3 1.4 Cliche, Andre: Ultralight Aircraft Shopper's Guide 8th Edition, page G-6 Cybair Limited Publishing, 2001. ISBN 0-9680628-1-4
- ↑ 2.0 2.1 2.2 2.3 2.4 2.5 2.6 Compact Radial Engines Inc (2009). "SD-570, 4 cylinders 2 stroke; direct drive". Retrieved 2010-01-22.
- ↑ 3.0 3.1 3.2 3.3 Purdy, Don: AeroCrafter - Homebuilt Aircraft Sourcebook, page 73. BAI Communications. ISBN 0-9636409-4-1
External links
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