Gas turbine stationary blade with flow guide pipe
A technology of gas turbines and draft tubes, applied in mechanical equipment, engine components, machines/engines, etc., can solve problems such as inability to arrange, achieve efficient and reasonable structural design, enhance convective cooling and impact cooling effects, and reduce casting difficulty.
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[0035] according to Figure 1-Figure 5 A gas turbine vane 2 with a draft tube is shown, including a front cavity 13, a middle cavity 14 and a rear cavity 3; the front cavity 13, the middle cavity 14 and the rear cavity 3 are arranged in sequence, and the front cavity 13, The middle cavity 14 and the rear cavity 3 are set independently of each other, and the front cavity 13, the middle cavity 14 and the rear cavity 3 respectively form air cooling passages inside the vane 2; and the rear cavity 3 is provided with an air supply cavity 5;
[0036] The vane 2 also includes a guide tube 1, the guide tube 1 is arranged inside the rear cavity 3, and an annular channel 4 is formed between the periphery of the guide tube 1 and the wall surface of the rear cavity 3, the guide tube 1 surrounds the air supply chamber 5, wherein the air supply chamber 5 and the annular channel 4 are communicated through the impact hole 6 opened on the draft tube 1; the purpose of setting the impact hole 6 i...
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