Patent ID: 9278764
Filing Date: 2016-03-08
CPC Classification: B23P,B64F,B65D,F16D,Y10T

Claim Text:
1. An aircraft brake assembly container, comprising: a first container portion of an at least three container portions having an at least one channel therein and releasably securing an at least one cradle member therein with an at least one portion extending from the at least one cradle member to engage and move within said at least one channel and having an at least one void section; a second container portion having an at least one channel therein and releasably securing an at least one cradle member therein with an at least one portion extending from the at least one cradle member to engage and move within said at least one channel and with an at least one void section such that said second container portion is identical to said first container portion, said first and second container portions of an at least three container portions fittingly engaging with a third container portion of an at least three container portions, said third container portion of an at least three container portions coupling to each of the first and second container portions and filling the void section in each portion with a corresponding tab portion extending from both a top and a bottom of the third container portion into the identical first and second container portions and said second of an at least three container portions is stacked atop said third container portion which is stacked atop said first of the at least three container portions to form said aircraft brake assembly container; an at least one securement device for securing said first portion and second portion to said third portion, wherein the at least one cradle member in each of the first and second of the at least three container portions is moved along the respective at least one channel in the respective container portion such that an aircraft brake assembly is cradled thereon wherein the aircraft brake assembly is supported when in the container in a horizontal orientation relative to the container, and wherein the at least one void portion provided on said first or second of the at least three container portions allows an aircraft undercarriage or brake axle to penetrate the container and couple to the aircraft brake assembly when the third of the at least three container portions is removed.