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EP2918777A1 Noise reducing vane 有权
Verfahren zur Optimierung eines SchaufelsfürRauschreduzierung

Noise reducing vane
摘要:
A gas turbine engine includes a first airflow structure (23) and a second airflow structure (36) disposed aft of the first airflow structure (29). The second airflow structure (23) includes a leading edge region (72). A thickness of the leading edge region (72) is based on a thickness of a wake (64) in the airflow produced by the first airflow structure (23) when the airflow passes between the first airflow structure (23) and the second airflow structure (36).
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