Nova Patents
EP1510757A3

Gas turbine combustor

Abstract

A gas turbine combustor includes a combustion liner in which a combustion region is formed; and a housing provided for a wall of the combustion liner in a predetermined circumferential region of the combustion liner to form a resonance space between the combustion liner and the housing. The combustion region and the resonance space are connected by a plurality of combustion liner through-holes, and a circumferential length of the housing is longer than a diameter of the combustion liner.

EP1510757A3, drawing sheet 1
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Term

Term ended

Projected expiry passed 27 August 2024, 2.1 years ago.

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