The invention relates to the technical field of aircraft
lightning protection tests, and discloses an aircraft
lightning indirect effect and HIRF conduction
sensitivity test device and method, and the device comprises a
device under test (EUT), an accompanying monitoring device, an auxiliary device, an HIRF injection probe, a
lightning injection probe, a monitoring probe, a lightning
signal isolator, and an HIRF conduction test
system. The invention discloses a lightning indirect effect test
system and a digital
oscilloscope. Aiming at the problem of
electromagnetic environment potential safety hazards caused by independent evidence obtaining and independent rectification of civil aircraft
thunder and lightning and HIRF airworthiness,
thunder and lightning indirect effect and HIRF conduction sensitivity tests can be simultaneously carried out on an aircraft electronic and electrical
system, the
thunder and lightning and HIRF comprehensive protection performance of the aircraft electronic and electrical system is verified, and the potential safety hazards of the
electromagnetic environment are effectively reduced. The thunder and lightning indirect effect and HIRF conduction
sensitivity test device is simple in construction and easy for
engineering realization, and can also be used for thunder and lightning and HIRF protection performance
verification tests of other aircrafts.