The IAP offers many advantages over conventional
central hydraulic systems:
Survivability - The IAP can be remotely
located on the aircraft, connected to the aircraft electric power
supply and control system through small, easily redundant power
cables, and electrical, fiber optic or mechanical control signal
cables. This eliminates long hydraulic lines and the associated
weight of lines, fittings and hydraulic fluid, and reduces the sources
of potential fluid leakage to a minimum.
Reliability - Since the IAP is
a self-contained system it is not subject to secondary failure from
shared contaminated hydraulic fluid.
Efficiency - The pump is servo
controlled, developing only the pressure and flow necessary to work
against the static load and to respond to position commands. In
addition, pump output flows directly to the actuator, eliminating
the need for high-flow servo control valves and their associated
high-pressure drop, weight, volume and impact or system reliability.
Long Life - The pump develops
only the minimum pressure needed. The pump’s high-pressure components
are not continuously subjected to max pressure. This minimizes power
unit fatigue.
Consistency - As a constant-speed
and flow reversible unit, the IAP elimantes continuous stop-start-reverse
cycles. |