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).
Aircraft Electrical Ice Protection Systems
Aircraft Engineering and Aerospace Technology ; 40 , 7 ; 7-8
1968-07-01
2 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Aircraft electrical ice protection systems
Engineering Index Backfile | 1968
|Control Systems for Aircraft Electrical Ice Protection
Emerald Group Publishing | 1968
|PROTECTION OF ELECTRICAL SYSTEMS ON MILITARY AIRCRAFT
SAE Technical Papers | 1945
|TIBKAT | 1987
|SLUB | 1986
|