Stiffening of the connection between flaps in a nozzle of variable cross section
AssigneesSafran Ceramics, Safran Aircraft Engines
InventorsGilles Lepretre, Julien Tran
Life of this patent
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AssigneesSafran Ceramics, Safran Aircraft Engines
InventorsGilles Lepretre, Julien Tran
Estimating the term…
A variable section nozzle includes an ejection casing and a plurality of internal flaps arranged in a ring downstream from the ejection casing. Each internal flap is connected to the ejection casing by a movable lever pivotally mounted to the downstream end of the ejection casing. Each lever is movable between a first position in which the internal flaps are in a high position and a second position in which the internal flaps are in a folded-down position. The nozzle includes a plurality of rigid movement transmission parts distributed circumferentially around the ejection casing. Each rigid movement transmission part is connected to two adjacent levers by connecting rods, and to a control actuator. Each rigid movement transmission part can move in a direction corresponding to the axial direction of the nozzle under the action of the control actuator to move the adjacent levers between the first and second positions.
A variable section nozzle comprising:
Dependencies are inferred from the claim text.