THRUST REVERSER AT THE DOOR OF A NACELLE OF A TURBOJET ENGINE OF AN AIRCRAFT WITH A SYSTEM FOR DIVERTING FLUIDS TO THE EXTERIOR

THRUST REVERSER AT THE DOOR OF A NACELLE OF A TURBOJET ENGINE OF AN AIRCRAFT WITH A SYSTEM FOR DIVERTING FLUIDS TO THE EXTERIOR

A thrust reverser of a nacelle of a turbojet engine of an aircraft extending about a longitudinal axis and including a fixed structure and at least one door which is rotatable between a closed position and an open position and including a downstream frame spaced axially from a downstream end edge of...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Joret, Jean-Philippe, Valleroy, Laurent Georges, Loncle, Alexis Yves-Marie, Rabineau, Jérémie
Format: Patent
Sprache:eng
Schlagworte:
BLASTING
COMBUSTION ENGINES
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
JET-PROPULSION PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
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Beschreibung
Zusammenfassung:A thrust reverser of a nacelle of a turbojet engine of an aircraft extending about a longitudinal axis and including a fixed structure and at least one door which is rotatable between a closed position and an open position and including a downstream frame spaced axially from a downstream end edge of the door by an axial clearance parallel to the longitudinal axis. The thrust reverser includes a system for diverting fluids to the exterior including at least one projection fixed onto the door or the other fixed structure and extending into the axial clearance and towards one of the fixed structure or the door, while leaving an axial gap between a free end of said projection and one of the fixed structure or the door.