公开(公告)号：US4695247A

公开(公告)日：1987-09-22

申请号：US833268

申请日：1986-02-26

申请人： Yoshiki Enzaki ,  Kazuki Kitahara ,  Satoru Terasaka ,  Kenji Mori ,  Takeshi Kimura

发明人： Yoshiki Enzaki ,  Kazuki Kitahara ,  Satoru Terasaka ,  Kenji Mori ,  Takeshi Kimura

IPC分类号： F23R3/06 ,  F23R3/00 ,  F23D14/02

CPC分类号： F23R3/002 ,  F05B2260/201 ,  F05B2260/202 ,  F05B2260/2241

摘要： A combustor of a gas turbine having a double wall construction in one part of the combustor, wherein an outer plate is formed with a multiplicity of cooling air inlet apertures and an inner plate is formed with a multiplicity of cooling air outlet apertures. The inner and outer plates are connected together by a multiplicity of connectors formed of heat conductive material and define therebetween a space. The cooling air inlet apertures are greater in diameter but smaller in total area than the cooling air outlet apertures which are inclined at an angle of 30 degrees. Cooling air introduced into the space through the cooling air inlet apertures impinge on the inner surface of the inner plate and performs impinge cooling while the connectors perform pin fin cooling. The cooling air also performs film cooling as it flows along the outer surface of the inner plate after cooling the walls of the cooling air outlet apertures while being released.

摘要翻译： 一种燃气轮机的燃烧器，其具有在燃烧器的一部分中的双壁结构，其中外板形成有多个冷却空气入口孔，并且内板形成有多个冷却空气出口孔。 内板和外板通过由导热材料形成的多个连接件连接在一起，并在其间限定空间。 冷却空气入口孔的直径更大，总面积小于以30度倾斜的冷却空气出口孔。 通过冷却空气入口孔引入空间的冷却空气撞击内板的内表面，并且在连接器执行销散热冷却时进行冲击冷却。 当冷却空气在释放时冷却冷却空气出口孔的壁之后，冷却空气也会沿着内板的外表面流动。