Controlled bypass inlet duct

Power plants – Combustion products used as motive fluid – With safety device

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Details

55306, F02C 7052

Patent

active

049726722

ABSTRACT:
A separating inlet duct (14) is provided with a reduced arm, bypass throat section (46) to restrict the bypass flow (18b) during periods of high speed aircraft flight. An ejector (34) ensures a minimum bypass flow (18b) during hover or low speed flight. An icing resistance baffle (40) having a rounded leading edge (42) defines the sized throat section (46).

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