GAS TURBINE ENGINE COMBUSTION CHAMBER WITH DEFLECTORS MADE OF COMPOSITE WITH CERAMIC MATRIX Russian patent published in 2014 - IPC F23R3/28 

Abstract RU 2507452 C2

FIELD: engines and pumps.

SUBSTANCE: gas turbine engine combustion chamber incorporates deflector secured at combustion chamber bottom wall. It has opening to fit fuel-air mix feeder in place. Said deflector has opening mating that on combustion chamber bottom wall and having circular cylindrical section of fastening to said wall. Said cylindrical part has transverse groove interacting with metal case crosswise teeth engaged with said wall and centering bowl. One of bowl ends is secured at said housing. Said centering bowl includes cylindrical part arranged with clearance inside deflector cylindrical section even at cold combustion chamber. Said clearance can be decreased and even eliminated at the chamber operating chambers.

EFFECT: longer life.

7 cl, 7 dwg

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RU 2 507 452 C2

Authors

Djuval' Sil'Vehn

Ehrnandez Did'E Ippolit

Ljunel' Romehn Nikolja

Dates

2014-02-20Published

2009-06-10Filed