Volume 2, Issue 1, 2011, Full Text - 5th International Conference on ...
Volume 2, Issue 1, 2011, Full Text - 5th International Conference on ...
Volume 2, Issue 1, 2011, Full Text - 5th International Conference on ...
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Sustainable C<strong>on</strong>structi<strong>on</strong> and Design <str<strong>on</strong>g>2011</str<strong>on</strong>g><br />
V. Secti<strong>on</strong> after the moment of take off;<br />
VI. Take off process in the air.<br />
The examinati<strong>on</strong> of secti<strong>on</strong>s after these happened separately. We used Fourier transformati<strong>on</strong> (FFT)<br />
examining the secti<strong>on</strong>s. Is a results of FFT we got vibrati<strong>on</strong> accelerati<strong>on</strong>-frequency values from the<br />
vibrati<strong>on</strong> accelerati<strong>on</strong>-time functi<strong>on</strong>s [5].<br />
This guaranteed for us that we could determined the repetiti<strong>on</strong> member (frequency) of load bel<strong>on</strong>ging to the<br />
characteristic accelerati<strong>on</strong> values. An example pricked out of Fourier transformati<strong>on</strong> can be seen in Figure<br />
6. The characteristic accelerati<strong>on</strong> values are marked in the Figure so, as an exposed value (A), as well as a<br />
characteristic secti<strong>on</strong> (B).<br />
14<br />
12<br />
10<br />
8<br />
Vibrati<strong>on</strong>-accelerati<strong>on</strong> in „z” directi<strong>on</strong> measured in the cabin<br />
Belső z irányítottságú gyorsulás<br />
d<br />
I. II. III. IV. V. VI.<br />
a [gyorsulás] [m/s 2 ]<br />
6<br />
4<br />
2<br />
0<br />
0<br />
-2<br />
5 10 15 20 25 30<br />
-4<br />
-6<br />
-8<br />
Time, t [idő] [s] t [s]<br />
Figure 5. Characteristic secti<strong>on</strong>s of vibrati<strong>on</strong>-accelerati<strong>on</strong> in „z” directi<strong>on</strong> in the functi<strong>on</strong> of<br />
time measured in the cabin<br />
Vibrati<strong>on</strong>-accelerati<strong>on</strong>, Rezgésgyorsulás, a a [m/s 2 ]<br />
2 ] Rezgésgyorsulás, Vibrati<strong>on</strong>-accelerati<strong>on</strong>, a [m/s a 2 [m/s ]<br />
2 ]<br />
10<br />
0<br />
-10<br />
0 2 4 6 8 10<br />
Idő, t [s]<br />
1.5<br />
1<br />
0.5<br />
0<br />
0 5 10 15 20 25 30 35 40 45 50<br />
Frekvencia, f [Hz]<br />
Figure 6. Time-functi<strong>on</strong> of accelerati<strong>on</strong> measured in the aircraft and FFT frequency<br />
spectrum, in the secti<strong>on</strong> of decelerating taxiing <strong>on</strong> the field, „z” directi<strong>on</strong><br />
It can be stated by knowing the results that the breakdown of the silent-bloc then happens so<strong>on</strong>er if the<br />
load is accompanied with much higher repetiti<strong>on</strong> number.<br />
Knowing this it can be established that fact the critical secti<strong>on</strong>s c<strong>on</strong>sidering the silent-bloc are the<br />
decelerating/accelerating taxiing <strong>on</strong> the ground (III., IV. secti<strong>on</strong>) and not the moments of landing as well as<br />
take off. The characteristic values of accelerati<strong>on</strong> and frequency of decelerating/accelerating taxiing <strong>on</strong> the<br />
ground had to be applied for the further examinati<strong>on</strong>s.<br />
102<br />
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