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

Flugzeugklasse P 1.3 - Ab

Datenblatt

n	(1) O_n[dB]	(2) R_n
1	79,5	1,0
2	78,5	1,0
3	74,0	1,0
4	70,0	1,0
5	65,0	1,0
6	59,0	1,0
7	52,0	1,0
8	44,0	1,0

s_o = 300 m

(3) P_F: Startpunkt

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
0	0	18	0
250	0	36	0
X	0	36	h_o
X + 1.000	-8	43	h_o
σ' [m]	dZ/dσ' [dB/m]	dV/dσ' [s^-1]	dH/dσ'
> X + 1.000	0	0	0

X = h_o / 0,105 + 250

h_o Flughöhe nach Nr. 2.2.1.4 bzw. Nr. 2.2.3.5 VBUF-DES

Flugzeugklasse P 1.3 - An

Datenblatt

n	(1) O_n[dB]	(2) R_n
1	69,5	1,0
2	68,5	1,0
3	64,0	1,0
4	60,0	1,0
5	55,0	1,0
6	49,0	1,0
7	42,0	1,0
8	34,0	1,0

s_o = 300 m

(3) P_F: Landeschwelle

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
- 150	0	31	0
X - 1.000	0	31	-
X	2	43	h_o
σ' [m]	dZ/dσ' [dB/m]	dV/dσ' [s^-1]	dH/dσ'
> X	0	0	0

X = h_o · cot w - 150

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 P 1.4 - Ab

Datenblatt

n	(1) O_n[dB]	(2) R_n
1	84,5	1,0
2	83,0	1,0
3	81,0	1,0
4	78,5	1,0
5	73,5	1,0
6	67,5	1,0
7	60,5	1,0
8	52,5	1,0

s_o = 300 m

(3) P_F: Startpunkt

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
0	0	35	0
550	0	68	0
X	0	68	h_o
X + 1.000	-5	75	h_o
σ' [m]	dZ/dσ' [dB/m]	dV/dσ' [s^-1]	dH/dσ'
> X + 1000	0	0	0

X = h_o / 0,141 + 550

h_o Flughöhe nach Nr.2.2.1.4 bzw. Nr. 2.2.3.5 VBUF-DES

Flugzeugklasse P 1.4 - An

Datenblatt

n	(1) O_n[dB]	(2) R_n
1	77,5	1,0
2	76,0	1,0
3	74,0	1,0
4	71,5	1,0
5	66,5	1,0
6	60,5	1,0
7	53,5	1,0
8	45,5	1,0

s_o = 300 m

(3) P_F: Landeschwelle

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
- 300	0	51	0
X - 1 000	0	51	-
X	2	75	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 P 2.1 - Ab

Datenblatt

n	(1) O_n[dB]	(2) R_n
1	87,0	1,0
2	85,5	1,0
3	81,5	1,0
4	77,0	1,0
5	73,5	1,0
6	69,5	1,0
7	69,5	1,0
8	64,5	1,0

s_o = 300 m

(3) P_F: Startpunkt

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
0	0	35	0
900	0	70	0
3.800	0	70	-
4.300	-	70	310
4.800	-2	70	340
σ' [m]	dZ/dσ' [dB/m]	dV/dσ' [s^-1]	dH/dσ'
> 4.800	0	0	0,06

Flugzeugklasse P 2.1 - An

Datenblatt

n	(1) On [dB]	(2) R_n
1	77,5	1,0
2	72,0	1,0
3	73,5	1,0
4	74,5	1,0
5	71,0	1,0
6	69,5	1,0
7	71,5	1,0
8	60,5	1,0

s_o=300m

(3) P_F: Landeschwelle

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
- 300	0	60	0
X - 1 000	0	60	-
X	5	70	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 P 2.2 - Ab

Datenblatt

n	(1) O_n[dB]	(2) R_n
1	94,5	1,0
2	93,0	1,0
3	89,0	1,0
4	84,5	1,0
5	81,0	1,0
6	77,0	1,0
7	77,0	1,0
8	72,0	1,0

s_o = 300 m

(3) P_F: Startpunkt

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
0	0	35	0
900	0	70	0
3.800	0	70	-
4.300	-	70	310
4.800	-2	70	340
σ' [m]	dZ/dσ' [dB/m]	dV/dσ' [s^-1]	dH/dσ'
> 4.800	0	0	0.06

Flugzeugklasse P 2.2 - An

Datenblatt

n	(1) O_n [dB]	(2) R_n
1	77,5	1,0
2	72,0	1,0
3	73,5	1,0
4	74,5	1,0
5	71,0	1,0
6	69,5	1,0
7	71,5	1,0
8	60,5	1,0

s_o = 300 m

(3) P_F: Landeschwelle

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
- 300	0	60	0
X - 1.000	0	60	-
X	5	70	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 1.0 - Ab

Datenblatt

n	(1) O_n[dB]	(2) R_n
1	82,0	1,0
2	85,5	1,0
3	83,5	1,0
4	82,0	1,0
5	79,0	1,0
6	76,0	1,0
7	73,0	1,0
8	63,5	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
1.100	0	75	0
5.100	0	75	-
5.600	-	75	460
6.100	-1	-	-
10.400	-1	110	650
15.000	-1	135	1.000
σ' [m]	dZ/dσ' [dB/m]	dV/dσ' [s^-1]	dH/dσ'
> 15.000	0	0	0,126

Flugzeugklasse S 1.0 - An

Datenblatt

n	(1) O_n[dB]	(2) R_n
1	68,0	1,0
2	76,0	1,0
3	74,0	1,0
4	75,0	1,0
5	72,5	1,0
6	69,5	1,0
7	70,0	1,0
8	56,5	1,0

s_o=300m

(3) P_F: Landeschwelle

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
- 300	0	65	0
7.400	0	65	-
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 1.1 - Ab

Datenblatt

n	(1) O_n[dB]	(2) R_n
1	94,0	1,2
2	100,5	1,2
3	100,5	1,2
4	98,5	1,2
5	95,5	1,1
6	91,5	1,0
7	87,5	1,0
8	72,0	1,0

s_o - 300 m

(3) P_F: Startpunkt

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
0	3	40	0
1.300	0	80	0
3.600	0	80	-
4.100	-	80	460
4.600	-3	80	-
7.800	-3	80	920
18.800	-3	135	1.283
σ' [m]	dZ/dσ' [dB/m]	dV/dσ' [s^-1]	dH/dσ'
> 18.800	0	0	0,033

Flugzeugklasse S 1.1 - An

Datenblatt

n	(1) O_n[dB]	(2) R_n
1	76,0	1,2
2	78,5	1,2
3	80,0	1,2
4	78,0	1,2
5	75,5	1,1
6	77,0	1,0
7	77,5	1,0
8	65,0	1,0

s_o = 300 m

(3) P_F: Landeschwelle

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
-300	0	67	0
7.400	0	67	-
8.400	-2	82	-
X	-2	98	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 1.2 - Ab

Datenblatt

n	(1) O_n[dB]	(2) R_n
1	94,0	1,2
2	100,5	1,2
3	100,5	1,2
4	98,5	1,2
5	95,5	1,1
6	91,5	1,0
7	87,5	1,0
8	72,0	1,0

s_o = 300 m

(3) P_F: Startpunkt

σ' [m]	(4) Z [dB]	(5) V [m/s]	(6) H [m]
0	3	40	0
1.400	0	80	0
3.100	0	80	-
3.600	-	80	460
4.100	-3	80	-
6.700	-3	80	920
12.300	-3	135	1120
σ' [m]	dZ/dσ' [dB/m]	dV/dσ' [s^-1]	dH/dσ'
> 12.300	0	0	0,13

Flugzeugklasse S 1.2 - An

Datenblatt

n	(1) O_n[dB]	(2) R_n
1	75,5	1,2
2	78,0	1,2
3	79,5