Gas turbine combustor, particularly for an aircraf

专利名称：Gas turbine combustor, particularly for an

aircraft engine

发明人：Coutandin, Daniele申请号：EP02007907.5申请日：20020409公开号：EP1249663A2公开日：20021016

专利附图：

摘要：A gas turbine combustor (5), in particular for an aircraft engine (1), has at leastone chamber (14), through which combustion gas flows in use, and which is defined by alateral wall (15) with channeling (60) for feeding cooling air into the chamber (14) and

cooling the lateral wall (15); part of the channeling (60) is defined by at least one doublewall (31, 32, 36) for guiding a relative stream (F1, F2) of cooling air into the chamber (14) ina tangential direction with respect to the lateral wall (15).

申请人：FIATAVIO S.p.A.

地址：Via Nizza 312 10127 Torino IT

国籍：IT

代理机构：Cerbaro, Elena, Dr.

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