Turbine engine intake with gas mixer

Power plants – Combustion products used as motive fluid – Combined with regulation of power output feature

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Details

137 151, F02D 704

Patent

active

059138084

ABSTRACT:
An inlet gas mixing element for a gas turbine engine, comprising a gas intake duct 10, and downstream of the inlet duct a mixing element 22, the mixing element being so disposed in relation to the inside of the duct so as to rotate thereby urging the forced mixing of the air and other gases moving past the element 22 towards the face of the fan blades of the downstream engine compressor stage 16. The action of the mixing element serves to increase the mixing of new air and other possibly hotter gasses so as to reduce the temperature differential across the face of the engine compressor stages.

REFERENCES:
patent: 2726508 (1955-12-01), Halford et al.
patent: 3719428 (1973-03-01), Dettmering
patent: 3832086 (1974-08-01), Hull et al.

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