Aircraft anti-insect system

Aeronautics and astronautics – Aircraft structure – Fuselage and body construction

Patent

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Details

244134F, 244130, 60 39092, 60 39093, B64C 138, B64D 1504

Patent

active

056830629

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.

REFERENCES:
patent: 2747365 (1956-05-01), Rainbow
patent: 3057154 (1962-10-01), Sherlaw et al.
patent: 3933327 (1976-01-01), Cook et al.
patent: 4482114 (1984-11-01), Gupta et al.
patent: 4674714 (1987-06-01), Cole et al.
patent: 5011098 (1991-04-01), McLaren et al.
patent: 5088277 (1992-02-01), Schulze

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