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Aircraft anti-insect system

Authors :
Spiro, Clifford Lawrence
Fric, Thomas Frank
Leon, Ross Michael
Publication Year :
1997
Publisher :
United States: NASA Center for Aerospace Information (CASI), 1997.

Abstract

Insect debris is removed from or prevented from adhering to insect impingement areas of an aircraft, particularly on an inlet cowl of an engine, by heating the area to 180.degree.-500.degree. C. An apparatus comprising a means to bring hot air from the aircraft engine to a plenum contiguous to the insect impingement area provides for the heating of the insect impingement areas to the required temperatures. The plenum can include at least one tube with a plurality of holes contained in a cavity within the inlet cowl. It can also include an envelope with a plurality of holes on its surface contained in a cavity within the inlet cowl.

Subjects

Subjects :
Aeronautics (General)

Details

Language :
English
Database :
NASA Technical Reports
Notes :
NAS3-26617
Publication Type :
Report
Accession number :
edsnas.20080004618
Document Type :
Report