Combustion apparatus

Power plants – Combustion products used as motive fluid – Combustion products generator

Patent

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Details

60751, F23R 346

Patent

active

043154050

ABSTRACT:
The airflow into a gas turbine engine combustion chamber e.g. through the primary air inlet and the dilution air inlets is directionally controlled by airflow directing inserts located in the air inlets. The inserts preferably comprise an open-ended cellular honeycomb structure.

REFERENCES:
patent: 2882681 (1959-04-01), Hudson et al.
patent: 2916878 (1959-12-01), Wirt
patent: 3726087 (1973-04-01), Bryce

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