umwelt-online: VBUF - Vorläufige Berechnungsmethode für den Umgebungslärm an Flugplätzen - VBUF-AzB

Flugzeugklasse S 5.3 - Ab

Datenblatt

n	(1) O_n [dB]	(2) R_n
1	89,0	1,0
2	93,0	1,0
3	93,5	1,0
4	92,0	1,0
5	89,0	1,0
6	85,5	1,0
7	78,5	1,0
8	70,0	1,0

s_o = 300 m

(3) P_F: Startpunkt

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
0	0	40	0
2.000	0	85	0
4.400	0	85	-
4.900	-	85	460
5.400	-2	-	-
8.100	-2	115	610
11.600	-2	135	830
σ' [m]	dZ/dσ' [dB/m]	dV/dσ' [s^-1]	dH/dσ'
> 11.600	0	0	0,117

Flugzeugklasse S 5.3 - An

Datenblatt

n	(1) O_n[dB]	(2) R_n
1	72,5	1,0
2	76,5	1,0
3	77,0	1,0
4	75,5	1,0
5	72,5	1,0
6	69,0	1,0
7	62,0	1,0
8	53,5	1,0

s_o = 300 m

(3) P_F: Landeschwelle

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
-300	0	68	0
7.400	0	72	-
X	-1	108	h_o
σ' [m]	dZ/dσ' [dB/m]	dV/dσ' [s^-1]	dH/dσ'
> x	0	0	0

X = h_o · cot w - 300

h_o Flughöhe nach Nr. 2.2.2.6 bzw. Nr. 2.2.3.5 VBUF-DES

w Gleitwinkel nach Nr. 2.2.2.3 bzw. Nr. 2.2.3.6 VBUF-DES

Flugzeugklasse S 6.1 - Ab

Datenblatt

n	(1) O_n[dB]	(2) R_n
1	87,5	1,0
2	91,0	1,0
3	89,0	1,0
4	87,5	1,0
5	84,5	1,0
6	81,5	1,0
7	78,5	1,0
8	69,0	1,0

s_o = 300 m

(3) P_F: Startpunkt

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
0	0	40	0
1.900	0	90	0
4.100	0	90	-
4.600	-	90	460
5.100	-2,5	-	-
8.300	-2,5	120	670
12.000	-2,5	135	1 030
σ' [m]	dZ/dσ' [dB/m]	dV/dσ' [s^-1]	dH/dσ'
> 12.000	0	0	0,135

Flugzeugklasse S 6.1 - An

Datenblatt

n	(1) O_n [dB]	(2) R_n
1	70,5	1,0
2	78,5	1,0
3	76,5	1,0
4	77,5	1,0
5	75,0	1,0
6	72,0	1,0
7	72,5	1,0
8	59,0	1,0

s_o = 300 m

(3) P_F: Landeschwelle

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
- 300	0	70	0
7.400	0	75	-
X	-1	108	h_o
σ' [m]	dZ/dσ' [dB/m]	dV/dσ' [s^-1]	dH/dσ'
> x	0	0	0

X = h_o · cot w - 300

h_o Flughöhe nach Nr. 2.2.2.6 bzw. Nr. 2.2.3.5 VBUF-DES

w Gleitwinkel nach Nr. 2.2.2.3 bzw. Nr. 2.2.3.6 VBUF-DES

Flugzeugklasse S 6.2 a) - Ab

Datenblatt

n	(1) O_n[dB]	(2) R_n
1	92,0	1,0
2	95,5	1,0
3	93,5	1,0
4	92,0	1,0
5	89,0	1,0
6	86,0	1,0
7	83,0	1,0
8	73,5	1,0

s_o = 300 m

(3) P_F: Startpunkt

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
0	0	40	0
1.500	0	85	0
3.400	0	85	-
3.900	-	85	460
4.400	-3	-	-
6.500	-3	110	650
11.000	-3	135	1.050
σ' [m]	dZ/dσ' [dB/m]	dV/dσ' [s^-1]	dH/dσ'
> 11.000	0	0	0,145

Flugzeugklasse S 6.2 b) - Ab

Datenblatt

n	(1) O_n[dB]	(2) R_n
1	92,0	1,0
2	95,5	1,0
3	93,5	1,0
4	92,0	1,0
5	89,0	1,0
6	86,0	1,0
7	83,0	1,0
8	73,5	1,0

s_o = 300 m

(3) P_F: Startpunkt

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
0	0	40	0
2.100	0	90	0
5.000	0	90	-
5.500	-	90	460
6.500	-3	-	-
9.600	-3	120	720
15.900	-3	140	1.200
σ' [m]	dZ/dσ' [dB/m]	dV/dσ' [s^-1]	dH/dσ'
> 15.900	0	0	0,107

Flugzeugklasse S 6.2 a/b) - An

Datenblatt

n	(1) O_n [dB]	(2) R_n
1	73,0	1,0
2	81,0	1,0
3	79,0	1,0
4	80,0	1,0
5	77,5	1,0
6	74,5	1,0
7	75,0	1,0
8	61,5	1,0

s_o = 300 m

(3) P_F: Landeschwelle

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
-300	0	73	0
7 400	0	77	-
X	-1	108	ho
σ' [m]	dZ/dσ' [dB/m]	dV/dσ' [s^-1]	dH/dσ'
> X	0	0	0

X = h_o · cot w - 300

h_o Flughöhe nach Nr. 2.2.2.6 bzw. Nr. 2.2.3.5 VBUF-DES

w Gleitwinkel nach Nr. 2.2.2.3 bzw. Nr.2.2.3.6 VBUF-DES

Flugzeugklasse S 6.3 - Ab

Datenblatt

n	(1) O_n[dB]	(2) R_n
1	88,0	1,0
2	91,5	1,0
3	89,5	1,0
4	88,0	1,0
5	85,0	1,0
6	82,0	1,0
7	79,0	1,0
8	69,5	1,0

s_o = 300 m

(3) P_F: Startpunkt

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
0	0	40	0
2.800	0	90	0
7.200	0	90	-
7.700	-	90	460
8.200	-2	-	-
18.700	-2	140	700
σ' [m]	dZ/dσ' [dB/m]	dV/dσ' [s^-1]	dH/dσ'
> 18.700	0	0	0,075

Flugzeugklasse S 6.3 - An

Datenblatt

n	(1) O_n [dB]	(2) R_n
1	69,0	1,0
2	77,0	1,0
3	75,0	1,0
4	76,0	1,0
5	73,5	1,0
6	70,5	1,0
7	71,0	1,0
8	57,5	1,0

s_o = 300 m

(3) P_F: Landeschwelle

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
- 300	0	73	0
7.400	0	77	-
X	-1	108	ho
σ' [m]	dZ/dσ' [dB/m]	dV/dσ' [s^-1]	dH/dσ'
> x	0	0	0

X = h_o · cot w - 300

h_o Flughöhe nach Nr. 2.2.2.6 bzw. Nr. 2.2.3.5 VBUF-DES

w Gleitwinkel nach Nr. 2.2.2.3 bzw. Nr. 2.2.3.6 VBUF-DES

Flugzeugklasse S 7 a) - Ab

Datenblatt

n	(1) O_n [dB]	(2) R_n
1	95,5	1,0
2	99,0	1,0
3	97,0	1,0
4	95,5	1,0
5	92,5	1,0
6	89,5	1,0
7	86,5	1,0
8	77,0	1,0

s_o = 300 m

(3) P_F: Startpunkt

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
0	0	40	0
1.800	0	90	0
4.700	0	90	-
5.200	-	90	460
5.700	-4,5	-	-
15.300	-4,5	140	1.080
σ' [m]	dZ/dσ' [dB/m]	dV/dσ' [s^-1]	dH/dσ'
> 15.300	0	0	0,102

Flugzeugklasse S 7 b) - Ab

Datenblatt

n	(1) O_n[dB]	(2) R_n
1	95,5	1,0
2	99,0	1,0
3	97,0	1,0
4	95,5	1,0
5	92,5	1,0
6	89,5	1,0
7	86,5	1,0
8	77,0	1,0

s_o = 300 m

(3) P_F: Startpunkt

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
0	0	40	0
2.600	0	100	0
6.600	0	100	-
7.100	-	100	460
7.600	-4,5	-	-
21.300	-4,5	150	1.140
σ' [m]	dZ/dσ' [dB/m]	dV/dσ' [s^-1]	dH/dσ'
> 21.300	0	0	0,084

Flugzeugklasse S 7 a/b) - An

Datenblatt

n	(1) O_n[dB]	(2) R_n
1	73,5	1,0
2	81,5	1,0
3	79,5	1,0
4	80,5	1,0
5	78,0	1,0
6	75,0	1,0
7	75,5	1,0
8	62,0	1,0

s_o = 300 m

(3) P_F: Landeschwelle

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
- 300	0	73	0
7.400	0	77	-
X	-1	108	h_o
σ' [m]	dZ/dσ' [dB/m]	dV/dσ' [s^-1]	dH/dσ'
> X	0	0	0

X = h_o cotw-300

h_o Flughöhe nach Nr. 2.2.2.6 bzw. Nr. 2.2.3.5 VBUF-DES

w Gleitwinkel nach Nr. 2.2.2.3 bzw. Nr. 2.2.3.6 VBUF-DES

Flugzeugklasse H 1 - Ab/An

Datenblatt

n	(1) O_n[dB]	(2) R_n
1	77,0	1,4
2	73,0	1,4
3	76,0	1,4
4	76,0	1,4
5	71,0	1,4
6	65,0	1,4
7	57,0	1,4
8	55,0	1,4

s_o = 150 m

(3) P_F: Hubschrauberstart- und -landestelle

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
0	0	30	0
X	0	30	ho
σ' [m]	dZ/dσ' [dB/m]	dV/dσ' [s^-1]	dH/dσ'
> X	0	0	0

X = h_o / 0,2

h_o Höhenangabe nach Nr. 2.2.7.5, Nr. 2.2.8.5 bzw. Nr. 2.2.9.5 VBUF-DES

Flugzeugklasse H 2 - Ab/An

Datenblatt

n	(1) O_n[dB]	(2) R_n
1	87,0	1,4
2	83,0	1,4
3	86,0	1,4
4	86,0	1,4
5	81,0	1,4
6	75,0	1,4
7	67,0	1,4
8	65,0	1,4

s_o=150m

(3) P_F: Hubschrauberstart- und -landestelle

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
0	0	30	0
X	0	30	ho
σ' [m]	dZ/dσ' [dB/m]	dV/dσ' [s^-1]	dH/dσ'
> X	0	0	0

X = h_o / 0,2

h_o Höhenangabe nach Nr. 2.2.7.5, Nr. 2.2.8.5 bzw. Nr. 2.2.9.5 VBUF-DES

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