| 词条 | Turbomeca Bastan | ||||||||||||||
| 释义 |
The Turbomeca Bastan was a turboprop engine developed in France in 1957. Early models developed 650 shp (485 kW), but by 1965 this had been increased to 1,048 shp (780 kW) with the Bastan VII. Flight tests of some Bastan models were carried out using a Lockheed Constellation flying test bed. The engine's principal applications were the Aérospatiale N 262 (Nord 262) and Nord 260 airliners. The Bastan was also developed into the Turbomeca Aubisque turbofan. Applications
Variants
Specifications (Bastan VIC){{jetspecs|ref=Janes's All The World's Aircraft 1965-66.[3] |type=Turboprop |length=2,034 mm (80.1 in) |diameter=685 mm (26.97 in) width, 775.5 mm (30.53 in) |weight=212 kg (467 lb) |compressor=Single-stage axial compressor followed by single-stage centrifugal compressor |combustion=Direct flow annular type |turbine=Three-stage axial flow |fueltype= |oilsystem= |power=794 kW (1,065 ehp) |thrust= |compression=5.83:1 |bypass= |aircon= |turbinetemp= |fuelcon= |specfuelcon= 352 g/kWh (0.578 lb/eshp hr) |power/weight=3.7 kW/kg (2.3 lb/ehp) |thrust/weight= }} See also{{aircontent|see also= |related=
|similar aircraft= |lists=
|similar engines= }} References1. ^1 {{cite book|last=Taylor|first=John W.R. FRHistS. ARAeS|title=Jane's All the World's Aircraft 1962-63|year=1962|publisher=Sampson, Low, Marston & Co Ltd|location=London}} 2. ^1 2 3 {{cite book |last=Wilkinson |first=Paul H. |title=Aircraft engines of the World 1970 |year=1970 |publisher=Paul H. Wilkinson |location=Washington D.C. |edition=21st |page= |pages=184-185}} 3. ^Taylor 1965, pp. 461–462.
2 : Turbomeca aircraft engines|Turboprop engines 1950–1959 |
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