Compressor air drawing off system

Details Compressor air drawing off system Compressor air drawing off system

B - Operations, Transporting

64

D

B64D 33/00 (2006.01) B64D 13/00 (2006.01) B64D 15/02 (2006.01) F02C 6/08 (2006.01)

Patent

CA 2398422

A flow of compressed air originating from a compressor stream (3) is drawn off through first orifices (13) towards ducts (5, 6) leading outside the casing, creating a flow division through adjacent cavities (11, 12) in the casing (1). These arrangements make it possible to carry a large air flow even if the cavity cross sections (11, 12) are small.

Un courant d'air comprimé provenant d'un flux de compresseur (3) est soutiré par les premiers orifices (13) à travers les conduites (5, 6) menant à l'extérieur du tubage, créant une division du courant par les cavités adjacentes (11, 12) du tubage (1). Ces dispositions permettent de transporter un grand courant d'air, même si les sections transversales de la cavité (11, 12) sont petites.

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