Load coupling attachment systems and methods
AssigneeThe Boeing Compnay
InventorsJeffrey Weathers, Jacob Szczudlak, Jacob August Hall
Life of this patent
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AssigneeThe Boeing Compnay
InventorsJeffrey Weathers, Jacob Szczudlak, Jacob August Hall
Estimating the term…
A load-decoupling attachment system is configured to secure to a primary structure. The load-decoupling attachment system includes one or more baffle tiers. One or more beams are coupled to the one or more baffle tiers. The one or more beams include a fore end and an aft end. A fore end coupling joint is configured to secure the fore end to a first portion of the primary structure. The fore end coupling joint includes a spherical bearing that allows the fore end to rotate in relation to the first portion of the primary structure. An aft end coupling joint is configured to secure the aft end to a second portion of the primary structure. The aft end coupling joint includes a slot that allows the aft end to linearly translate in relation to the second portion of the primary structure.
A load-decoupling attachment system configured to secure to a primary structure, the load-decoupling attachment system comprising:
A load-decoupling attachment method for a primary structure, the load-decoupling attachment method comprising:
A launch vehicle comprising:
Dependencies are inferred from the claim text.