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公开(公告)号：EP1363075B1
公开(公告)日：2011-05-04
申请号：EP03253083.4
申请日：2003-05-16
CPC分类号： F23R3/002 , F23R3/06 , F23R3/60 , F23R2900/03041 , F23R2900/03042
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2.发明公开Heat shield panels for use in a combustor for a gas turbine engine 有权Hitzeschildplattenfüreine Gasturbinenbrennkammer
公开(公告)号：EP1363075A2
公开(公告)日：2003-11-19
申请号：EP03253083.4
申请日：2003-05-16
CPC分类号： F23R3/002 , F23R3/06 , F23R3/60 , F23R2900/03041 , F23R2900/03042
摘要： The present invention relates to heat shield panels 18, 22 or liners to be used in combustors for gas turbine engines. The heat shield panels 18, 22 each comprise a hot side 33 and a cold side 31 and at least one isolated cooling chamber 56 on the cold side 31. Each cooling chamber has a plurality of cooling film holes 32 for allowing a coolant, such as air, to flow from the cold side 31 to the hot side 33. A combustor having an arrangement of heat shield panels or liners is also described.
摘要翻译： 本发明涉及用于燃气涡轮发动机的燃烧器中的隔热板18,22或衬垫。 隔热板18,22各自包括热侧33和冷侧31以及冷侧31上的至少一个隔离冷却室56.每个冷却室具有多个冷却膜孔32，用于允许诸如 空气，从冷侧31流到热侧33.还描述了具有隔热板或衬垫布置的燃烧器。
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公开(公告)号：EP1363075A3
公开(公告)日：2005-07-13
申请号：EP03253083.4
申请日：2003-05-16
CPC分类号： F23R3/002 , F23R3/06 , F23R3/60 , F23R2900/03041 , F23R2900/03042
摘要： The present invention relates to heat shield panels 18, 22 or liners to be used in combustors for gas turbine engines. The heat shield panels 18, 22 each comprise a hot side 33 and a cold side 31 and at least one isolated cooling chamber 56 on the cold side 31. Each cooling chamber has a plurality of cooling film holes 32 for allowing a coolant, such as air, to flow from the cold side 31 to the hot side 33. A combustor having an arrangement of heat shield panels or liners is also described.
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