Technical data

Table of optimal speed at setting the blades from the smallest, which is 12 degrees, to the
biggest, which is 22 degrees. Engine with the reductor at 1:1.27./Rotax 912,914/ is assumed.
It is obvious that due to the output of the engine it is not possible to accomplish for all setting
sof all revolutions. The table introduces the speeds in km per hour in the slopes.
Revolutions of the engine Setting of the airscrew blades in degrees
12 17 22
3500 78 110 141
3600 80 113 145
3700 83 116 149
3800 85 119 153
3900 87 122 157
4000 89 125 161
4100 92 128 165
4200 94 132 169
4300 96 135 173
4400 98 138 177
4500 101 141 181
4600 103 144 186
4700 105 147 190
4800 107 150 194
4900 110 154 198
5000 112 157 202
5100 114 160 206
5200 116 163 210
5300 119 166 214
5400 121 169 218
5500 123 172 222
The effectiveness of airscrew work optimisation is not enough to ensure the flight with relatively
low consumption. Also the engine with exact effectiveness and its consumption is not increasing
with the revolutions in linear way, but it is increasing slightly progressively. / it mostly grows
between 3.500 and 5.500 revolutions /. We recommend to go through information in the
operating handbook of the engine, which is a part of the delivery. Also, there are introduced all
dependencies of the output of the engine on height of the flight and temperature of the air.
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