US Patent Application 18196949. SEAL ASSEMBLY FOR A TURBOMACHINE simplified abstract

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SEAL ASSEMBLY FOR A TURBOMACHINE

Organization Name

General Electric Company

Inventor(s)

Srinivasan Swaminathan of Bengaluru (IN)

Anand Madihalli Srinivasan of Bengaluru (IN)

Shalini Thimmegowda of Bengaluru (IN)

Ravindra Shankar Ganiger of Bengaluru (IN)

SEAL ASSEMBLY FOR A TURBOMACHINE - A simplified explanation of the abstract

This abstract first appeared for US patent application 18196949 titled 'SEAL ASSEMBLY FOR A TURBOMACHINE

Simplified Explanation

- The patent application is for seal assemblies used in turbomachines. - The seal assemblies consist of stationary and rotating components with at least one interface between them. - A self-lubricating lattice element made of carbon or a carbon-based material is included in the seal assembly. - The self-lubricating lattice element has a porous and compressible microstructure that can retain a liquid substance. - During engine operation, the self-lubricating lattice element can compress and expel some of the liquid substance. - This forms a layer of liquid between the rotating and stationary components of the seal assembly. - The patent application also describes self-lubricating wear sleeves for other parts of the turbomachine.


Original Abstract Submitted

This disclosure is directed to seal assemblies for a turbomachine. The seal assemblies include stationary and rotating components and at least one interface between the stationary and rotating components. The seal assembly further includes a self-lubricating lattice element made of carbon or a carbon-based material. The self-lubricating lattice element may have a porous and compressible microstructure capable of retaining a liquid substance. During engine operation, the self-lubricating lattice element can compress and expel some portion of the liquid substance to form a liquid-containing layer between the rotating and stationary components of the seal assembly. Also described herein are self-lubricating wear sleeves for use in other portions of the turbomachine.