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Electric Heating System for Aircraft Applications
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English
Abstract
The adaptation of a 3-phase, alternating current, automotive modified to produce a-c energies of sufficient magnitude as to provide cabin heating for light commercial aircraft is described.
Such a system is primarily intended to provide a high degree of reliability, along with the ability to provide continuous controllable heat for long durations. Aircraft heat power sources of this type can be easily constructed, readily installed, and offers simplicity of design for uncompromising safety.
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Authors
Topic
Citation
Riff, J., "Electric Heating System for Aircraft Applications," SAE Technical Paper 720329, 1972, https://doi.org/10.4271/720329.Also In
References
- Nelson Roger E. “Evaluating of Motorola Alternator for Windshield Heating.” Sierracin Report RO-71-12
- Cherry James R. “Electrical Quick Heat: Concept and Application.” Paper 710033 SAE Automotive Engineering Detroit January 1971