Readily changeable isolator and method of assembly therefor

F - Mech Eng,Light,Heat,Weapons – 16 – F

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F16F 1/38 (2006.01) F16F 1/393 (2006.01)

Patent

CA 2309979

An isolator (26) and assembly method therefor. The isolator (26) is particularly useful for aircraft thrust reverser doors, and the like, and includes an outer member (28), and an isolator component (29). The outer member (28) has a central axis (A-A), a generally non-planar inner peripheral surface (32), and first and second axially extending slotted entryways (48, 48'). The isolator component (29) preferably includes a component axis (B-B), an inner member (30) having an external radial peripheral surface (33), and an elastomer or metal mesh member (40) surrounding said external radial peripheral surface (33). The isolator component (29) is assembled and retained within said outer member (28) by insertion endwise through said first and second slotted entryways (48, 48'), and rotating 90~ such that the component axis (B-B) is substantially aligned with the central axis (A-A).

Cette invention concerne un isolateur (26) et une méthode de montage s'y rapportant. Cet isolateur (26) convient particulièrement pour les coquilles d'inverseur de poussée des aéronefs et autres dispositifs analogues; il comprend un élément extérieur (28) et un organe d'isolation (29). L'élément extérieur (28) présente un axe central (A-A), un surface périphérique interne (32) généralement non plane ainsi qu'une première et une seconde gorge (48, 48') longitudinales disposées axialement. L'organe d'isolation (29) présente de préférence un axe (B-B), un élément interne (33) avec une surface (33) périphérique radiale externe et un élément grillagé (40) en élastomère ou en métal entourant cette surface périphérique (33). L'organe d'isolation (29) est emboîté dans l'élément extérieur (28) par l'intermédiaire des gorges (48, 48'), puis tourné sur 90· de telle sorte que l'axe (B-B) et l'axe central (A-A). soient pour ainsi dire alignés l'un sur l'autre.

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