Foreign particle separator system

Gas separation – Aircraft anti-ingestion means

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Details

60 3909P, 244 53B, B01D 3900

Patent

active

042656460

ABSTRACT:
A system of separating or removing foreign particles from the gaseous fluid flowing in the primary flow path of a gas turbine engine is provided wherein the particles are removed from the stream near the engine inlet and flow through a conduit to ejector means operative to effect a flow of a second stream of fluid in the conduit. Mixing means are provided for mixing the second stream of fluid with the gaseous fluid flowing in the primary flow path.

REFERENCES:
patent: 3348379 (1967-10-01), Wilde et al.
patent: 3362155 (1968-01-01), Driscoll
patent: 3766719 (1973-10-01), McAnally
patent: 3811254 (1974-05-01), Amelio
patent: 3832086 (1974-08-01), Hull et al.
patent: 4002024 (1977-01-01), Nye et al.
patent: 4175384 (1979-11-01), Wagenknecht

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