Direct Effects Protection-Chapter 5Protection of an aircraft and each of its various systems against the direct effects of lightning were analyzed. Components located in different sections of the aircraft were individually examined since they are likely to experience different degrees of susceptibility to lightning, and may be vulnerable to different components of the lightning flash. The basic steps to be followed in establishing lightning protection were presented by discussing the varieties of arc entry and current flow-through damage. The lightning-strike zones and lightning current environments are established, since environmental conditions in the zones are those under which specific protective measures must perform. Airworthiness regulations which apply to lightning protection are cited.
Document ID
19780003086
Acquisition Source
Glenn Research Center
Document Type
Book Chapter
Authors
Franklin A Fisher (General Electric (United States) Boston, Massachusetts, United States)
J Anderson Plumer (General Electric (United States) Boston, Massachusetts, United States)