CA2077932
A jet engine thrust reverser comprises displaceable elements (7) integrated in the closed position within the outer wall of the jet engine duct and capable, in the open position, of deflecting the flow passing through the said duct. Elements, in the form of blading (23), are arranged inside each dis...
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Main Authors | , |
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Format | Patent |
Language | French |
Published |
12.03.1993
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Subjects | |
Online Access | Get full text |
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