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Aircraft anti-insect system
- 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 :
- Aeronautics (General)
Subjects
Details
- Language :
- English
- Database :
- NASA Technical Reports
- Notes :
- NAS3-26617
- Publication Type :
- Report
- Accession number :
- edsnas.20080004618
- Document Type :
- Report