Wren 44 TurboProp Users Manual. Copyright Wren Turbines Ltd February 2008 Page 16
Performance
We have tested the turboprop unit in a variety of situations and loads. The main indicator of the
performance of the unit from the users point of view, is the rpm that can be achieved with a given
propeller load. Larger propellers and/or more blades produce higher torque figures but not always
the highest thrust figures.
We have listed the outputs for a range of propellers and the thrust produced for each combination
together with the calculated torque and shaft power figures. From these it should be possible for
the reader to gauge the ideal propeller combination for their aircraft.
The figures are reproduced in order of highest thrust first and are with gas generator at maximum
speed - 195,000rpm.
Propeller
Size
RPM
Static Thrust Torque
KW
HP
2-Bladed:
MENZ-S
610 x 200 (24” x 8”)
7110
167N
6.82Nm
5.08
6.81
MENZ-S
610 x 305 (24” x 12”)
5900
160N
7.06Nm
4.36
5.84
APC-N
430 x 305 (17” x 12”)
8900
95N
4.49Nm
4.18
5.60
3-Bladed:
Mejzlik
560 x 305 (22” x 12”)
6300
150N
8.52Nm
5.62
7.53
Mejzlik
510 x 305 (20” x 12”)
7020
135N
7.22Nm
5.31
7.12
MENZ-S
460 x 305 (18” x 12”)
7540
128N
5.47Nm
4.32
5.79
Note the high rpms achieved with the smaller propellers. It is most important that propellers
smaller than listed are not used or if they are the maximum rpm should be reduced on the engine,
to prevent the possibility of overstressing (the propeller). In all cases, follow the propeller
manufacturers recommendations for preparation and use.
NOTE
The maximum speed of the unit with
any
propeller should not exceed 9,000rpm on the ground.