Visible locking thrust reverser

Details Visible locking thrust reverser Visible locking thrust reverser

F - Mech Eng,Light,Heat,Weapons

02

K

F02K 1/56 (2006.01) B64D 29/06 (2006.01) F02K 1/76 (2006.01)

Patent

CA 2243057

The invention relates to thrust reversers for an aircraft turbine engine and more specifically to these thrust reversers (10) specially designed to permit visual verification that the blockers (25) are locked. This thrust reverser (10) is distinctive in that the pin (37) of the lock (36) protrudes at least partly from the wall (13, 14) radially delimiting the annular structure (12) of the thrust reverser (10) when the said pin (37) is open.

L'invention se rapporte aux inverseurs de poussée pour turbomoteurs d'aéronefs et plus particulièrement à de tels inverseurs (10) spécialement conçus pour permettre un contrôle visuel au sol du verrouillage des obturateurs (25). Un tel inverseur (10) est remarquable en ce que le pêne (37) du verrou (36) émerge au moins en partie de la paroi (13, 14) délimitant radialement la structure annulaire (12) de l'inverseur (10) lorsque ledit pêne (37) est ouvert.

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