FUNCTIONAL TESTING APPARATUS OF AN AIRCRAFT HYDRAULIC SYSTEM, CAPABLE OF PERFORMING FUNCTIONAL TESTS FOR A HYDRAULIC SYSTEM AND AN ATTACHED DEVICE REGARDLESS OF AIRCRAFT FLIGHT CONDITIONS AND TRIAL CONDITIONS

摘要

PURPOSE: A functional testing apparatus of an aircraft hydraulic system is provided to check integrity of a hydraulic system before or after the operation of an aircraft which is capable of being checked during a trial operation and a normal flight.;CONSTITUTION: A functional testing apparatus (100) of an aircraft hydraulic system comprises a first connection unit, a second connection unit, and a test point. The first connection unit is electrically connected to components of the aircraft hydraulic system and an attached device (10) of the aircraft hydraulic system. The second connection unit is electrically connected to with an aircraft testing system (20). The test point is electrically connected to the first connection unit and the second connection unit; monitors an electrical signal to the first connection unit and the second electrical unit; and applies a signal, which is input by an operator, to the second connection unit.;COPYRIGHT KIPO 2013;[Reference numerals] (10) Hydraulic system and attached devices; (100) Functional testing apparatus for an aircraft hydraulic system; (20) Aircraft testing system