Propfan turbine engine

Power plants – Reaction motor – Interrelated reaction motors

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Details

244 53B, F02K 302, B64B 124

Patent

active

051779579

ABSTRACT:
A propfan turbine engine for an aircraft has a shroud and on the leading edge of the shroud, has one or several, preferably two, separate sector-like annular profile parts which via actuating devices can be moved from the shroud such that slots can be formed between the profile parts and the shroud. This arrangement prevents dangerous air-flow separations on the outside of the upper shroud region and on the inside of the lower shroud region at large angles of attack of the aircraft engine for both high and low power operation.

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patent: 4620679 (1986-11-01), Karanian
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patent: 5014933 (1991-05-01), Harm et al.

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