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FM 1-506 Fundamentals of Aircraft Power Plants ... - Survival Books

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WWW.SURVIVALEBOOKS.COM<strong>FM</strong> 1-<strong>506</strong>Fail-safe to high power. By placing theschedule high, the torque motor is designed toreduce the schedule to the desired level when itis energized. Because loss <strong>of</strong> torque motor currentcauses the schedule to return to thehighest level, this provides failure protection toa high power. A schedule that is biased high dueto electrical failure does not cause power limiting.In the event <strong>of</strong> an electrical system failure,it can be manually retarded to a more desirablelevel using the PAS. With all engine protectionfunctions in the HMU, no engine damage orstall can occur during or following any loss <strong>of</strong>electrical signal to the torque motor.<strong>Power</strong> available with one engine out. Theschedule is placed high enough that, in the event<strong>of</strong> failure <strong>of</strong> one engine, the remaining engine’sgas generator can increase power enough (automaticcontingency power) to carry the load atthe given LDS (collective pitch) setting.Without this arrangement <strong>of</strong> schedules, a singleenginefailure could not be compensated for bythe remaining engine and would result in a significantloss <strong>of</strong> available power.Electrical Control Unit OperationThe ECU, powered from an engine-mounted alternator(Figures 4-21, 4-22)—4-20

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