Designing an electro-impulse de-icing systemBasic principles and parameters for a system to deice aircraft with electromagnetic impulses are described. The physical basis for deicing by such impulses is explained, and the requirements involved in the electrodynamic design, structural dynamic design, and system design are discussed. Some manufacturing and testing problems and techniques are described.
Document ID
19860035202
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Zumwalt, G. W. (Wichita Univ. Wichita, KS, United States)
Friedberg, R. A. (Wichita State University KS, United States)