Lobed mixer/inverter

Power plants – Reaction motor – Air passage bypasses combustion chamber

Patent

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Details

60264, 181220, F02K 140

Patent

active

043029345

ABSTRACT:
A fairing added to the upstream end of the lobe of conventional lobed mixers or inverters for a gas turbine engine redirects the boundary layer so as to improve engine performance.

REFERENCES:
patent: 3861140 (1975-01-01), Krabacher
patent: 4117671 (1978-10-01), Neal et al.
patent: 4149375 (1979-04-01), Wynosky et al.

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