Aircraft Electrical Ice Protection Systems

descriptionPublicationkeyboard_double_arrow_right Article 01 Jul 1968 English Publisher:EmeraldJournal:Aircraft Engineering and Aerospace Technology, volume 40, pages 7-8 (issn: 0002-2667,

Copyright policy )

Authors: R.A. Foster;

doi: 10.1108/eb034393

Aircraft Electrical Ice Protection Systems

- Summary
- Metrics

Abstract

THERMAL protection from the effects of ice built up can be achieved by means of anti‐icing or de icing. Most aircraft structures are de‐iced since this consumes considerably less power, but in some cases it is essential that the surface be anti‐iced, (e.g. engine intakes, where ice ingestion to the engine is unacceptable and any formation of ice must therefore be prevented).

Impact byBIP!

	selected citations These citations are derived from selected sources. This is an alternative to the "Influence" indicator, which also reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).	1
	popularity This indicator reflects the "current" impact/attention (the "hype") of an article in the research community at large, based on the underlying citation network.	Average
	influence This indicator reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).	Average
	impulse This indicator reflects the initial momentum of an article directly after its publication, based on the underlying citation network.	Average