The invention discloses an
airplane porthole component performance test
system comprising an industrial control computer, a
programmable logic controller, an
airplane porthole component test device, and an air source. The industrial
personal computer is used for being connected with the
programmable logic controller, transmitting a pulse
signal of controlling the
airplane porthole component test device, and receiving a current
signal, processed by the
programmable logic controller, of the airplane porthole component test device. The programmable logic controller is used for receiving a pulse
signal whereby the industrial control computer controls the airplane porthole component test device, and receiving and
processing the current signal from the airplane porthole component test device. The air source is used for providing the airplane porthole component test device with air. The airplane porthole component performance test
system is capable of effectively simulating flight
temperature and pressure parameters of an airplane, is capable of truly indicating the
physical performance of airplane porthole glass during actual operation and the influence of component
assembly upon the performance of the airplane porthole glass, is also capable of automatically intercepting and storing
test data in performance test process into the industrial
personal computer, and has an extensible test function.