发明名称 IMPROVED GROUP OF HOLES OF COMBUSTION CHAMBER LININGS OF GAS TURBINE ENGINE WITH LOW DYNAMIC OF COMBUSTION AND EMISSIONS
摘要 FIELD: machine building.SUBSTANCE: internal casing contains the internal wall element that contains a group of the first holes and a group of the second holes. The internal wall element encloses the combustion volume of the combustion chamber. The group of the first holes contains the first holes, through which fluid flows, and that are located in the first surface density. The group of the second holes contains the second holes, through which the fluid flows, and that are located in the second surface density. The first surface density differs from the second surface density. The external casing contains the external wall element that contains a group of additional first holes and a group of additional second holes. The external wall element of the external casing at least partially encloses the internal wall element of the internal casing such, that between the internal wall element and external wall element a clearance is ensured. The group of the additional first holes contains the additional first holes, through which the fluid flows, and that are located in the additional first surface density. The group of the additional second holes contains the additional second holes, through which fluid flows, and that are located in the additional second surface density. The additional first surface density differs from the additional second surface density.EFFECT: creation of the combustion chamber with the reduced instability of burning and lesser emissions.12 cl, 6 dwg
申请公布号 RU2582378(C1) 申请公布日期 2016.04.27
申请号 RU20140142880 申请日期 2012.12.05
申请人 SIMENS AKTSIENGEZELLSHAFT 发明人 DZHAJATUNGA CHARITKH
分类号 F23R3/06 主分类号 F23R3/06
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