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发明公开
CN103032174A 用于调节至燃气涡轮的空气流的系统和方法 失效 - 权利终止

用于调节至燃气涡轮的空气流的系统和方法
摘要：
本发明涉及用于调节至燃气涡轮的空气流的系统和方法。用于调节至燃气涡轮的空气流的系统包括过滤器外壳和在过滤器外壳内的调节介质，以调节流动穿过过滤器外壳的空气的温度。调节介质的深度或密度中的至少一个横跨过滤器外壳变化。用于调节至燃气涡轮的空气流的方法包括使空气流动穿过连接于燃气涡轮的过滤器外壳和使空气横跨过滤器外壳中的调节介质流动。该方法进一步包括调节空气流以横跨过滤器外壳的尺寸减小离开过滤器外壳的空气的温差。
摘要（英）：

The invention relates to a system and a method for conditioning air flow (16) to the gas turbine. The system for conditioning air flow (16) to the gas turbine includes a filter housing (12) and a conditioning media (40) inside the filter housing (12) to adjust the temperature of the air flowing through the filter housing (12). At least one of a depth (50) or a density of the conditioning media (40) varies across the filter housing (12). The method for conditioning air flow (16) to the gas turbine includes flowing air through a filter housing (12) connected to the gas turbine and flowing the air across a conditioning media (40) in the filter housing (12). The method further includes conditioning the air flow (16) to reduce the temperature difference of the air exiting the filter housing (12) across a dimension of the filter housing (12).

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