2km fiber optic cable drum
3km fiber optic cable drum
5km fiber optic cable drum
10km fiber optic cable drum
Size: 101.6mm (diameter) *274mm
O Ca p s t e m ical f at i e b r e i r s al: A pe B c S ifications: 0.5 mm
W Ou e t i l g e h t n t: 6 oz 0 z 0 l g ( e: A 2k lu m m ) inum alloy nozzle, carbon tube 5cm
Size: 101.6mm (diameter) *274mm
Case material: ABS
W Op e t ig ic h a t l f : 8 ib 0 e 0 r s g ( p 3 e k c m if ) ications: 0.5mm
Outlet nozzle: Aluminum alloy nozzle, carbon tubé 5cm
S C i a z s e e m : 10 a 1 t . e 6 r m ia m ( l:AB d S iameter) *351 mm
W Op e t ig ic h a t l f : 1 ib 2 e 5 r s 0g ( pe 5 c k i m fic ) ations: 0.5mm
Outlet nozzle: Aluminum alloy nozzle, carbon tubé 5cm
Size: 142mm (diameter) * 404mm
Case material: carbon fiber
W Op e t ig ic h a t l f :2 i 4 b 5 e 0 r s g ( pe 1 c 0 i k f m ica ) tions: 0.5 mm
Outlet nozzle: Aluminum alloy nozzle, carbon tube 5cm
Optical fiber interface:Fiber Channelinterface
Optical fiber type:single-mode -Single-fiber
Data interface:GH1.25
Video format:NTSC/PAL/SECAM
Data direction:bidirectional
Data format:TTL/S.BUS
Speed:0 to 1Mbps
Wavelength single mode:1310(9/125μm)+1550
Transmission distance:single mode fiber O~20km
Tips
CRYSTAL LINK GBD
1,Fiber optic cable tube disk installation, fiber optic disk outlet nozzle should be as far
away from the propeller as possible, but additional attention should be paid to the
balance point of the center of gravity of the aircraft.
2,Fiber optic cable tube disk installation should be based on the aircraft's tilt angle,
the mounting bracket should be reserved for a certain tilt angle (as shown in the
figure).The mounting angle should be close to the tilt angle, so that the fiber optic cable
tube disk out let angleis a horizontal position.
3,Fiber optic cable tube winding uses spe cial glue,the first 200 meters of distance is the -
glue application area,in this area the flight speed ofthe aircraft should be controlled at
30km/h or 8m/s or less, to avoid high speed flight in the area with the glue.
4,Maximum flight speed of the aircraft should be controlled within 120km/h.
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