Bleed-off device in a bypass turbojet

Details Bleed-off device in a bypass turbojet Bleed-off device in a bypass turbojet

2005-09-06

2005-09-06

Tyler, Cheryl (Department: 3746)

Power plants

Reaction motor

Interrelated reaction motors

C060S262000, C060S785000

Reexamination Certificate

active

06938407

ABSTRACT:
This object is achieved by the bleed-off means comprising means for tapping air from the primary duct which are arranged upstream of the intermediate casing and means for evacuating the air tapped into the secondary duct downstream of the support arms, these means comprising conduits arranged around the intermediate casing under the platforms.

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