January, 2009
7
2.2 Turbine
It is a single shaft turbojet with an annular combustor. A single stage axial flow turbine drives
a single stage centrifugal compressor. The shaft is supported by 2 fuel/oil lubricated pre-
loaded angular contact bearings. The turbine speed is controlled by the amount of fuel
received from the fuel pump, which is controlled by the
I.C.S.
Turbine Specifications
Bee II
Rabbit
Cheetah
Rhino
Mammoth
Thrust Class
7 Kg (15.5 Lbs)
@
185,000 RPM
8.6 Kg (19 Lbs)
@
152,000 RPM
14 Kg (31 Lbs)
@
130,000 RPM
16.3 Kg (36 Lbs)
@
117,000 RPM
21.5 Kg (48 Lbs)
@
104,000 RPM
Full Throttle
Fuel
Consumption
0.24 Lt/min
(8.1 Oz/min)
0.31 Lt/min
(10.4 Oz/min)
0.47 Lt/min
(16 Oz/min)
0.52 Lt/min
(17.5 Oz/min)
0.70 Lt/min
(23 Oz/min)
R.P.M. range
55,000-185,000
40,000-152,000
35,000-130,000
30,000-117,000
28,000-104,000
E.G.T.
500°C - 700°C
(932 -1292°F)
500°C - 700°C
(932 -1292°F)
500°C - 700°C
(932 -1292°F)
500°C - 700°C
(932 -1292°F)
500°C - 700°C
(932 -1292°F)
Weight
0.880 Kg
(1.94 Lbs)
with starter
1.0 Kg
(2.2 Lbs) with
starter
1.360 Kg
(3 Lbs)
with starter
1.700 Kg
(3.75 Lbs)
with starter
2.240 Kg
(4.9 Lbs)
With starter
Diameter
82 mm
(3.228 inches)
91 mm
(3.582 inches)
102 mm
(4 inches)
111 mm
(4.37 inches)
124 mm
(4.881 inches)
Length
232 mm
(9.13 inches)
245 mm
(9.645 inches)
250 mm
(9.842 inches)
300 mm
(11.8 inches)
349 mm
(13.74 inches)
Содержание Rabbit
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