Figure 8-26.-Dynamic sensor pendulum positions: (A) Coordinated turn; (B) Slip; (C)Skid.
A pin in the housing fits into a slot in
the fluid gives a long-term sensing characteristic
the mechanism shell. This positions the mecha-
that makes the unit relatively insensitive to
nism to give proper alignment of the synchro
transient oscillations. The damping chamber also
rotor with the longitudinal axis of the aircraft
limits displacement of the pendulum to 10 degrees
when installed.
either side of the center position.
8-22
