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公开(公告)号：US09080770B2
公开(公告)日：2015-07-14
申请号：US13154208
申请日：2011-06-06
CPC分类号： F23R3/06 , F23R3/54 , F23R2900/03041 , Y02T50/675
摘要： A combustor for a gas turbine engine is provided. The combustor includes an inner liner; an outer liner circumscribing the inner liner; and a combustor dome having a first edge coupled to the inner liner and a second edge coupled to the outer liner. The combustor dome forms a combustion chamber with the inner liner and the outer liner. The combustion chamber receives air flow through the inner and outer liners, and the combustor dome is configured to bifurcate the air flow at the combustor dome into a first stream directed to the inner liner and a second stream directed to the outer liner.
摘要翻译： 提供了一种用于燃气涡轮发动机的燃烧器。 燃烧器包括内衬; 限定内衬的外衬套; 以及燃烧器穹顶，其具有联接到内衬套的第一边缘和联接到外衬套的第二边缘。 燃烧室顶部形成具有内衬和外衬的燃烧室。 燃烧室接收通过内衬和外衬层的空气流，并且燃烧器圆顶被构造成将燃烧室顶部处的空气流分叉为指向内衬的第一流和指向外衬套的第二流。
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公开(公告)号：US20120304647A1
公开(公告)日：2012-12-06
申请号：US13154208
申请日：2011-06-06
CPC分类号： F23R3/06 , F23R3/54 , F23R2900/03041 , Y02T50/675
摘要： A combustor for a gas turbine engine is provided. The combustor includes an inner liner; an outer liner circumscribing the inner liner; and a combustor dome having a first edge coupled to the inner liner and a second edge coupled to the outer liner. The combustor dome forms a combustion chamber with the inner liner and the outer liner. The combustion chamber receives air flow through the inner and outer liners, and the combustor dome is configured to bifurcate the air flow at the combustor dome into a first stream directed to the inner liner and a second stream directed to the outer liner.
摘要翻译： 提供了一种用于燃气涡轮发动机的燃烧器。 燃烧器包括内衬; 限定内衬的外衬套; 以及燃烧器穹顶，其具有联接到内衬套的第一边缘和联接到外衬套的第二边缘。 燃烧室顶部形成具有内衬和外衬的燃烧室。 燃烧室接收通过内衬和外衬层的空气流，并且燃烧器圆顶被构造成将燃烧室顶部处的空气流分叉为指向内衬管的第一流和指向外衬套的第二流。
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