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...

Full description

Saved in:
Bibliographic Details
Main Authors CARIMALI, FELIX, LEGRAS, MICHEL J. L
Format Patent
LanguageFrench
Published 12.03.1993
Subjects
BLASTING
COMBUSTION ENGINES
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
JET-PROPULSION PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
Online AccessGet full text

Cover

More Information
Summary: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 displaceable element (7) on the upstream side. This blading (23) which is evenly distributed over the width of the said displaceable element (7) is arranged with a general orientation parallel to the geometric axis of the reverser so as to form deflecting partitions ensuring guidance to the reversed jets.
Bibliography:Application Number: CA19922077932