CapExcellent
10th Sep 2009, 05:05
Hello,
I'm doing some research regarding how the WOW (weight-on-wheel(s)) sensor actually works, it's conncetion/correlation with the NWS (nose-wheel-steering) system.
1. WOW: Does it close the sensing loop by a "simple" contact, proximity sensor or
something more sophisticated (light-sensitive measurement like the one
used in CNC technology)?
2. NWS: Nothing is impossible in aviation, therefore: If the WOW sensor on the
nosewheel would be malfunction, would that mean that the crew has no
means of directional control at slower airspeeds (lets assume below
50knots, rudder inputs become less responsive) except for differential power?
And taking everything into consideration, would a worn out drag/shock strut affect the WOW sensing IN THE SAME MANNER as a bouncing airplane where the WOW system initally delays (sec./fraction of a second) an output signal to assure that the airplane is actually on the ground? Basically, once the plane decelerates and load is reduced on the nosewheel the WOW system would open the loop again rendering the NWS inop! What if the pilot has applied full rudder, with a "closed" WOW signal leading to max NWS rudder "mode" deflection and suddenly the WOW loop opens and the airplane goes left/right? :} Could this happen?
Hope it all makes sense and I would really appreciate any constructive input!:ok:
Cheers,
CE
PS: If it is of any help, I am referring more onto turboprop airplanes such as Atr, Dash, Embraer, Dornier etc.
I'm doing some research regarding how the WOW (weight-on-wheel(s)) sensor actually works, it's conncetion/correlation with the NWS (nose-wheel-steering) system.
1. WOW: Does it close the sensing loop by a "simple" contact, proximity sensor or
something more sophisticated (light-sensitive measurement like the one
used in CNC technology)?
2. NWS: Nothing is impossible in aviation, therefore: If the WOW sensor on the
nosewheel would be malfunction, would that mean that the crew has no
means of directional control at slower airspeeds (lets assume below
50knots, rudder inputs become less responsive) except for differential power?
And taking everything into consideration, would a worn out drag/shock strut affect the WOW sensing IN THE SAME MANNER as a bouncing airplane where the WOW system initally delays (sec./fraction of a second) an output signal to assure that the airplane is actually on the ground? Basically, once the plane decelerates and load is reduced on the nosewheel the WOW system would open the loop again rendering the NWS inop! What if the pilot has applied full rudder, with a "closed" WOW signal leading to max NWS rudder "mode" deflection and suddenly the WOW loop opens and the airplane goes left/right? :} Could this happen?
Hope it all makes sense and I would really appreciate any constructive input!:ok:
Cheers,
CE
PS: If it is of any help, I am referring more onto turboprop airplanes such as Atr, Dash, Embraer, Dornier etc.