Patent ID: 11970278
Assignee: GENERAL ELECTRIC COMPANY
Field: Transport (Mechanical engineering)
Classification: CPC B  F  Y | IPC B  F

Claim 0:
1. A thrust mount assembly for a turbomachine, comprising:
a thrust link-lever having a first end region, a second end region, and a fulcrum region disposed between the first end region and the second end region;
a first thrust link coupled or couplable to the first end region;
a second thrust link coupled or couplable to the second end region; and
an aft engine-mount comprising a fulcrum body, the thrust link-lever coupled or couplable to the fulcrum body of the aft engine-mount at a fulcrum position of the thrust link-lever,
wherein when coupled to the turbomachine, the fulcrum position of the thrust link-lever is laterally offset and/or laterally adjustable relative to an axis of rotation of the turbomachine, and
wherein a first lever arm defined from the fulcrum position and extending towards the first thrust link differs in length from a second lever arm defined from the fulcrum position and extending towards the second thrust link.