发明名称 ОБТЕКАТЕЛЬ КАМЕРЫ СГОРАНИЯ ГАЗОТУРБИННОГО ДВИГАТЕЛЯ
摘要 The shroud two circular and concentric edges on each side of openings through which supply pipes pass. A row of drillings (21) are provided on a side of the shroud, where the drillings hinders formation of a resonant cavity in the volume formed in the shroud. Locations for the drillings coincide with the separation locations to restore airflow, where the flow passes from a high pressure side towards a low pressure side.
申请公布号 RU2006103679(A) 申请公布日期 2007.08.20
申请号 RU20060103679 申请日期 2006.02.08
申请人 СНЕКМА (FR) 发明人 ДЕЗОЛЬТИ Мишель Андре Альбер (FR);КАЗАЛЕН Мишель Пьер (FR);КРЕДЕР Оливье (FR);КАЙРЕ Ален (FR)
分类号 F02C3/14 主分类号 F02C3/14
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