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Application filed by Александр Иванович Семенец, Владимир Петрович Маслов, Юрий Михайлович Родичев, Евгений Александрович Соловьев, Наталия Владимировна КачурfiledCriticalАлександр Иванович Семенец
Priority to UAU201208311UpriorityCriticalpatent/UA81525U/en
Publication of UA81525UpublicationCriticalpatent/UA81525U/en
A thermal electrical system for heating aircraft glass comprises glass panels comprising of a layer of transparent material applied to internal glass panels, a current-conductive bus supplying power to the transparent layer, a current censor and a power supply system which provides required temperature of heating. The device comprises two feedback channels for adjustment heating temperature and rate of temperature increase.
UAU201208311U2012-07-062012-07-06Thermal electrical system for heating aircraft glass
UA81525U
(en)