Aircraft engine annular shroud comprising an opening for the insertion of blades

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United States of America Patent

PATENT NO 9879549
SERIAL NO

14112071

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Abstract

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An aircraft engine annular shroud includes, on its internal surface, a peripheral annular groove able to accept a plurality of blade roots; an insertion opening for inserting the blade roots into the annular groove; and a closure device for closing off the insertion opening.

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Patent Owner(s)

Patent OwnerAddress
SAFRAN AIRCRAFT ENGINES75015 PARIS

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Dezouche, Laurent Gilles Le Coudray Montceau, FR 10 76

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