Connector assembly for gas turbine engines
AssigneeGeneral Electric Company
InventorJan Christopher Schilling
Life of this patent
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AssigneeGeneral Electric Company
InventorJan Christopher Schilling
Estimating the term…
A connector assembly for mounting turbomachinery including a link connector to be coupled to a clevis. The clevis includes a pair of arms and an opening that extends therethrough. The link connector includes a first end that includes an elastomer portion that defines an opening. The connector assembly further includes a support washer having an opening extending therethrough adjacent the link connector elastomer portion, and a fastener inserted through the clevis opening, the support washer opening, and the link connector elastomer opening to couple the link connector and the support washer to the clevis such that the link connector is coupled between the clevis arms by the fastener, and such that the support washer thermally insulates at least a portion of the link connector elastomer portion. At least a portion of the connector assembly being configured to shear when subjected to a predetermined load such that loading induced to the connector assembly is transmitted through the link connector elastomer portion.
A connector assembly, said connector assembly comprising:
A connector assembly for a gas turbine engine, said connector assembly comprising:
Dependencies are inferred from the claim text.