United Technologies Corporation

Raytheon Technologies Corporation

Rtx Corporation

Eric Weston Awtry

Kevin Kassel

Lauren Dohse

An assembly for use with a gas turbine engine includes a block housing, a main bell crank, a bell crank, and a sync rod. The main bell crank extends between a main bell crank first end and a main bell crank second end that is connected to an actuator. The bell crank extends between a bell crank first end and a bell crank second end that is pivotally supported by the block housing. The sync rod is connected the main bell crank first end and the bell crank first end. The sync rod defines a first tab disposed proximate a first side and extends beyond a face of the sync rod.

Bell crank and bar assembly

A variable vane assembly according to an example of the present disclosure includes an actuator. A connection linkage is pivotable by the actuator. A component receives direct input from the connection linkage providing a cam surface. A driving linkage is interfaced with the cam surface. A variable vane is coupled to the driving linkage. The pivoting of the component and cam surface causes the driving linkage to pivot the vane.

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Hartford, CT, United States of America

Eric Weston Awtry