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    • 1. 发明授权
    • Low cost airfoil cooling circuit with sidewall impingement cooling chambers
    • 具有侧壁冲击冷却室的低成本翼型冷却回路
    • US06206638B1
    • 2001-03-27
    • US09249204
    • 1999-02-12
    • Christopher C. GlynnPaul S. WilsonJames A. MartusClay K. Carlson
    • Christopher C. GlynnPaul S. WilsonJames A. MartusClay K. Carlson
    • F01D518
    • F01D5/186F01D5/187F05D2230/21F05D2260/201F05D2260/202Y02T50/67Y02T50/673Y02T50/676
    • A gas turbine engine airfoil includes an airfoil outer wall having widthwise spaced apart pressure and suction sidewall sections extending chordally between leading and trailing edges of the airfoil and extending longitudinally from a base to a tip. Inside the airfoil is at least one internal cooling circuit having a plurality of longitudinally extending circuit channels between longitudinally extending internal ribs extending widthwise between the pressure and suction sidewall sections and a longitudinally extending first sidewall film cooling chamber positioned between one of the sidewall sections and a first inner wall bounding the cooling circuit. Sidewall film cooling holes extend through the pressure sidewall section from the first sidewall film cooling chamber. The internal ribs have corresponding rib angles with respect to a centerline, the first inner wall has a corresponding first wall angle with respect to the centerline, and each of the rib angles and the first wall angle are constant in a longitudinal direction from the base to the tip. In the preferred embodiment, all the inner walls are substantially parallel to each other and all the transverse ribs are substantially parallel to each other or are substantially parallel to the first and second inner walls.
    • 燃气涡轮发动机翼型件包括具有宽度方向间隔开的压力的翼型件外壁和在翼型件的前缘和后缘之间弦状延伸并且从基部纵向延伸到尖端的抽吸侧壁部分。 在翼型件内部是至少一个内部冷却回路,该内部冷却回路在纵向延伸的内部肋条之间具有多个纵向延伸的电路通道,纵向延伸的内部肋条在压力和吸入侧壁部分之间横向延伸,以及纵向延伸的第一侧壁膜冷却室,其位于一个侧壁部分和 第一内壁围绕冷却回路。 侧壁膜冷却孔从第一侧壁膜冷却室延伸穿过加压侧壁部分。 内肋相对于中心线具有对应的肋角,第一内壁相对于中心线具有相应的第一壁角,并且每个肋角和第一壁角在从基部到纵向方向上是恒定的 小费。 在优选实施例中,所有内壁基本上彼此平行,并且所有横向肋基本上彼此平行或基本上平行于第一和第二内壁。