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Impingement jet impingement channel system in internal cooling system

机译:内部冷却系统中的冲击射流冲击通道系统

摘要

An internal cooling system (14) having an impingement jet impingement channel system (16) for enhancing the effect of the impingement jet (18) is disclosed. The impingement jet impingement channel system (16) may have an impingement jet impingement cavity (20) offset from one or more impingement orifices (22). The plurality of impingement jet impingement channels (24) may extend radially outward from the impingement jet impingement cavity (20), forming a star pattern of impingement jet impingement channels (24), adjacent to each other. It may be formed by a plurality of ribs (26) separating the impingement jet impingement channels (24), respectively. The rib (26) forming the impingement jet impingement channel (24) may be divided into a plurality of channels (24) only once or multiple times, so that the stagnation points (28, 38, 52) The cooling capacity is increased by increasing the number. Impingement jet collision channel systems (16) include, but are not limited to, vane inserts, blade leading edge cooling systems, platforms, advanced transitions, acoustic resonators, ring segments, and the like. Etc., may be used in components.
机译:公开了一种内部冷却系统(14),其具有用于增强冲击射流(18)的效果的冲击射流冲击通道系统(16)。冲击射流冲击通道系统(16)可具有从一个或多个冲击孔(22)偏移的冲击射流冲击腔(20)。多个冲击射流冲击通道(24)可以从冲击射流冲击腔(20)径向向外延伸,从而形成彼此相邻的星状冲击射流冲击通道(24)。它可以由分别分隔冲击射流冲击通道(24)的多个肋(26)形成。形成冲击射流冲击通道(24)的肋(26)可以仅一次或多次被分成多个通道(24),从而停滞点(28、38、52)通过增加冷却能力而增加。号码。冲击射流碰撞通道系统(16)包括但不限于叶片插件,叶片前缘冷却系统,平台,高级过渡装置,声共振器,环段等。等等,可用于组件中。

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