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Home › Turbine engine including an improved means for adjusting the flow rate of a cooling air flow sampled at the output of a high-pressure compressor using an annular air injection channel

Turbine engine including an improved means for adjusting the flow rate of a cooling air flow sampled at the output of a high-pressure compressor using an annular air injection channel

US Patent 8402770 · Granted Mar 26, 2013

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