Noise reducing connection assembly for aircraft turbine housings

Acoustics – Sound-modifying means – Muffler – fluid conducting type

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181198, 181200, 181213, 181285, 181292, 23926513, 23926517, 23926519, B64D 3302, F02K 1100

Patent

active

061231703

ABSTRACT:
In an aircraft turbine, an assembly consisting of an air inlet structure, a air blower housing (22) and a connecting part (36), is fitted in such a way as to reduce noise including in the junction area between the structure and the housing. The connecting part (36) is fastened onto a rear section (20'), not provided with a honeycomb core, of the internal wall (20) of the air inlet structure. A honeycomb structure (44) is fitted inside the air blower housing (22). The space inside the rear section (20') houses a forward extension (44') of the honeycomb structure (44), or a different honeycomb structure.

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