Shock and vibration isolation for aircraft brake control valve

Details Shock and vibration isolation for aircraft brake control valve Shock and vibration isolation for aircraft brake control valve

B - Operations, Transporting

60

T

B60T 8/00 (2006.01)

Patent

CA 2758498

The shock and vibration isolation system for hard mounting of a manifold of a brake control valve includes shock and vibration isolators that can be assembled in the mounting feet of the manifold of the brake control valve. The shock and vibration isolators have a pre-selected, predetermined natural frequency operative to protect components of the brake control valve from shock and vibration. Each of the shock and vibration isolators includes a radially inner generally spool shaped rigid insert portion and a radially outer generally spool shaped vibration insulating sheath portion.

L'invention porte sur un système d'isolation contre les chocs et les vibrations pour le montage rigide d'un collecteur d'une soupape de commande de frein, lequel système comprend des isolants contre les chocs et les vibrations qui peuvent être assemblés dans les pieds de montage du collecteur de la soupape de commande de frein. Les isolants contre les chocs et les vibrations ont une fréquence naturelle prédéterminée, présélectionnée, permettant de protéger des composants de la soupape de commande de frein contre les chocs et les vibrations. Chacun des isolants contre les chocs et les vibrations comprend une partie insert rigide généralement en forme de bobine, radialement interne, et une partie gaine d'isolation contre les vibrations généralement en forme de bobine radialement externe.

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