Jet pump for a turbomachine, comprising blading for imparting rotation to active fluid

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United States of America Patent

PATENT NO 11808286
APP PUB NO 20190107125A1
SERIAL NO

16095559

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Abstract

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A jet pump for a system for supplying fluid to a turbomachine. The jet pump includes an active fluid inlet pipe including a tube delimiting the inlet pipe, and a passive fluid inlet pipe that is fluidically separated from the active fluid inlet pipe by the tube. The active fluid inlet pipe includes at least one twisted blade that is positioned within the tube and is configured to make the active fluid rotate with respect to the axis of the tube.

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Patent Owner(s)

  • SAFRAN AIRCRAFT ENGINES

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Vertenoeuil, Philippe Paris, FR 12 37

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