avia.wikisort.org - Engine 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 .
1950s French turboprop aircraft engine
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.
A Bastan under test, mounted above a Lockheed Constellation in 1977
Applications
Variants
Bastan IV [1]
Bastan VI [1]
Bastan VIA1[2]
Bastan VIB1[2]
Bastan VIB2 [2]
Bastan VIC
Bastan VIC1 [3]
Bastan VII [3]
Bastan 16 [3]
Bastafan [3]
Bi-Bastan IV A paired Bastan IV developed for French-modified Sikorsky S-58 helicopters. De-rated to 1,119 kW (1,500 hp) [2]
Specifications (Bastan VIC)
Data from Janes's All The World's Aircraft 1965-66. [4]
General characteristics
Type: Turboprop
Length: 2,034 mm (80.1 in)
Diameter: 685 mm (26.97 in) width, 775.5 mm (30.53 in)
Dry weight: 212 kg (467 lb)
Components
Compressor: Single-stage axial compressor followed by single-stage centrifugal compressor
Combustors: Direct flow annular type
Turbine: Three-stage axial flow
Maximum power output: 794 kW (1,065 ehp)
Overall pressure ratio: 5.83:1
Specific fuel consumption: 352 g/kWh (0.578 lb/eshp hr)
Power-to-weight ratio: 3.7 kW/kg (2.3 lb/ehp)
See also
Related development
Related lists
References
Taylor, John W.R. FRHistS. ARAeS (1962). Jane's All the World's Aircraft 1962-63 . London: Sampson, Low, Marston & Co Ltd. Wilkinson, Paul H. (1964). Aircraft engines of the World 1964-65 (20th ed.). Washington D.C.: Paul H. Wilkinson. pp. 166–167. Wilkinson, Paul H. (1970). Aircraft engines of the World 1970 (23rd ed.). Washington D.C.: Paul H. Wilkinson. pp. 184–185. Taylor 1965, pp. 461–462.
Gunston, Bill (1986). World Encyclopedia of Aero Engines . Wellingborough: Patrick Stephens. p. 164.
Taylor, John W. R. (1965). Jane's All The World's Aircraft 1965-66 . London: Samson Low, Marston.
На других языках - [en] Turbomeca Bastan [fr] Turbomeca Bastan Le Turbomeca Bastan était un turbopropulseur développé en France en 1957. Les premiers modèles développaient 650 ch (485 kW), mais vers 1965 cette puissance fut portée à 1 048 ch (780 kW) avec le Bastan VII. [it] Turbomeca Bastan Il Turbomeca Bastan era un motore aeronautico turboelica prodotto dall'azienda francese Turbomeca dal 1957.
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