MAN Turbo 6022
| 6022 | |
|---|---|
 | |
| MTU 6022 engine on display at the Hubschraubermuseum Bückeburg | |
| Type | Turboshaft |
| National origin | Germany |
| Manufacturer | MAN Turbo/MTU |
| First run | 1962 |
| Major applications | MBB Bo 105 |
| Number built | 82 |
The MAN Turbo 6022 (also BMW 6022/MTU 6022) is a German gas turbine turboshaft engine for helicopter use. Designed in the early 1960s by BMW the engine powered the third prototype of the MBB Bo 105 on its maiden flight in December 1967.[1]
Variants
- 6022-A1
- Base variant. 162 kW (217 shp) at 6,000 rpm.
- 6022-A2
- 260 kW (350 shp) at 6,000 rpm. Powered the third prototype Bo 105. Passed 100 hour type test in 1968.
- 6022-A3
- 280 kW (375 shp) at 6,000 rpm. Production engines for Bo 105 with strengthened reduction gear.
Applications
- MBB Bo 105 (third prototype)
- Dornier Aerodyne
- Dornier Kiebitz
Engines on display
Specifications (6022-A3)
Data from Jane's.[2]
General characteristics
- Type: Turboshaft
- Length: 115 cm (45.3 in)
- Diameter: 54 cm (21.3 in)
- Dry weight: 90 kg (198 lb) (minus reduction gear and starter motor)
Components
- Compressor: Two-stage centrifugal
- Combustors: Single tube
- Turbine: Three-stage axial
- Fuel type: Jet fuel
Performance
- Maximum power output: 280 kW (375 shp)
- Overall pressure ratio: 6.4:1
- Air mass flow: 1.9 kg/s (4.2 lb/s)
- Specific fuel consumption: 424 g/kW h
- Power-to-weight ratio:
See also
Comparable engines
Related lists
References
 |
Wikimedia Commons has media related to MAN Turbo 6022. |
- Notes
- Bibliography
- MTU engine history (German language) - www.mtu.de
- Taylor, John W.R. Jane's All the World's Aircraft 1972-73., London, Sampson Low, Marston and Company Ltd, 1972. ISBN 0-354-00109-4.
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