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KSP
I
ZV
1 2 3
4
3 N 1
24 V
230 V
?
max.
80 kg
Ë
G = FB [m] * FH [m] * X
D
G =
Flügelgewicht
X =
Füllungsgewicht
t
G =
Sash weight
X =
insert element weight
F
G =
Poids du vantail
X =
Poids garniture
G =
Vleugelgewicht
X =
Vullingsgewicht
I
G =
Peso anta
X =
Peso inserto
E
G =
Peso de la hoja
X =
Peso de relleno
G = Ciężar skrzydła
X = Masa wypełnienia
G = Вес створки
T
X = Вес наполнителя
24
I = 25 ... 65
FS
ZV
ZV/F =
I = 35 ... 55
I = 40 ... 50
FH
1 S + ZV
[mm]
1 S
2400
2300
Positionen nicht
2200
2100
2000
1900
verändern!
1800
1700
1600
1500
1400
1300
1200
1100
1000
X=
X=
900
50 kg/m
2
40 kg/m
800
X=
700
70 kg/m
2
600
500
400
300
FH
1 S + ZV
[mm]
1 S
2400
2300
2200
2100
2000
1900
1800
1700
1600
1500
1400
1300
1200
1100
1000
X=
900
50 kg/m
800
X=
700
2
70 kg/m
600
500
400
300
FH
1 S + ZV
[mm]
1 S
2400
2300
2200
2100
2000
1900
1800
1700
1600
1500
1400
1300
1200
1100
1000
900
800
X=
700
70 kg/m
2
600
500
400
300
2 S +
2 S + ZV
ZV <<>>
2 S
X=
20 kg/m
2
25 kg/m
2
X=
30 kg/m
2
2
2 S +
2 S + ZV
ZV <<>>
2 S
X=
20 kg/m
2
X=
25 kg/m
2
X=
30 kg/m
2
X=
2
2
40 kg/m
2 S +
2 S + ZV
ZV <<>>
2 S
X=
20 kg/m
2
X=
X=
30 kg/m
2
25 kg/m
2
X=
X=
50 kg/m
2
40 kg/m
2
ZV <<
ZV >>
G
FB
[mm]
ZV <<
ZV >>
G
FB
[mm]
ZV <<
ZV >>
G
FB
[mm]
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