A windshield (10) of an aircraft (1) of the present invention includes a conductive member (21, 22, 23, 26, 27, 28) that is configured to generate heat when a current is supplied. The conductive member (21, 22, 23, 26, 27, 28) is oriented in a lateral direction (DH) that is a horizontal direction included in an in-plane direction of the windshield (10).
WINDSHIELD OF AIRCRAFT
2016-08-11
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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