The present invention provides a windshield (10) of an aircraft, including a plurality of conductive members (21, 22, 23) that are disposed along an in-plane direction of the windshield (10), and are wire-connected together, wherein the plurality of conductive members (21, 22, 23) are heaters that generate heat when supplied with an alternating current, and the conductive members (21, 22, 23) are wire-connected such that induced currents induced in the respective conductive members (21, 22, 23) by a magnetic field in association with a lightning current are circulated between the conductive members (21, 22, 23).
WINDSHIELD OF AIRCRAFT
WINDSCHUTZSCHEIBE EINES FLUGZEUGS
PARE-BRISE D'AÉRONEF
2018-08-01
Patent
Electronic Resource
English
AIRCRAFT WINDSHIELD AND METHOD FOR SUSPENDING AIRCRAFT WINDSHIELD
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