DG Flugzeugbau DG-1000T Посібник з ремонту - Сторінка 16
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Part
Fuselage centre
section from
wing leading edge up
to 130mm (5,1 in.)
behind rear wing
suspension
Fuselage tail boom
Exterior skin
Core
Inner skin
Engine bay DG-1000T
Side walls
Rear engine bay
bulkhead
UD-tapes beside the
engine bay cut out
Fuselage shell
between engine bay
walls additionally
Engine bay DG-1000M
Side walls
Rear engine bay
bulkhead
UD-tapes beside the
engine bay cut out
Fuselage shell
between engine bay
walls additionally
Caution: There are several other reinforcements in the fuselage-fin
intersection and near the top of the fin and at the engine bay components.
Issued December 2010
Copyright DG Flugzeugbau GmbH - any copy or publishing prohibited
Repair manual DG-1000
overlap b
fabric type, etc.
(cm)
(in.) d= + 45°
l= 0°, 90°
from outside to inside
8
3.15 1x92110 d
1x92145 l
1x92125 d
3x92140 d
1x92145 l
from outside to inside
3.5
1.38 1x92110 d
1x92145 l
1x92125 d
/
/
Tubuscore B6 6mm thick
3.5
1.38 1x92140 d
1x92145 l
2 each 0.8
1x205g/m² carbonfibre d inside and
each
outside
2,5
1,0
1x245g/m² carbonfibre d inside and
each
each
outside
10
4.0 4 CFRP-UD-tapes 300 g/m² 7.5 cm
wide
2 each 0.8
1x205g/m² carbonfibre d inside and
each
outside
2 each 0.8
2x205g/m² carbonfibre d inside and
each
1x205g/m² outside
2,5
1,0
2x245g/m² carbonfibre d inside and
each
each
outside
25
10
10 CFRP-UD-tapes 300 g/m² 7.5
cm wide
2 each 0.8
1x205g/m² carbonfibre d inside and
each
outside
6.3