Importance

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Abstract

A latch mechanism for joining two portions of a gas turbine engine. The latch mechanism is moveable between an open and a closed position and includes a first member configured to be attachable to a first portion of a gas turbine engine and a second member pivotally attached to the first member. The first member is attached to the second member at a first position. The latch mechanism also includes a handle pivotally attached to the second member that is attached to the second member at a second position, and third member pivotally attached to the second member. The third member is attached to the second member at a third position, the third position being between the first position and the second position, and wherein the third member comprises securing means for securing the third member to a second portion of a gas turbine engine.

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First Claim