SEAL SUPPORT ASSEMBLY FOR A TURBINE ENGINE

Organization Name

General Electric Company

Inventor(s)

Narendra Anand Hardikar of Hamilton OH (US)

David Raju Yamarthi of Bengaluru (IN)

Rahul Anil Bidkar of Clifton Park NY (US)

Ravindra Shankar Ganiger of Bengaluru (IN)

Prateek Jalan of Bengaluru (IN)

Deepak Trivedi of Halfmoon NY (US)

SEAL SUPPORT ASSEMBLY FOR A TURBINE ENGINE - A simplified explanation of the abstract

This abstract first appeared for US patent application 18189424 titled 'SEAL SUPPORT ASSEMBLY FOR A TURBINE ENGINE

Simplified Explanation: The patent application describes a turbine engine with a seal assembly that includes a seal segment and a seal support assembly to bias the seal segment along the radial direction.

The turbine engine includes a rotor, a stator with a carrier, and a seal assembly between them.
The seal assembly consists of a seal segment with a seal face that forms a fluid bearing with the rotor.
A seal support assembly, including a prestressed spring assembly, extends from the seal segment to bias it along the radial direction.

Key Features and Innovation:

Seal assembly with a seal segment and seal support assembly.
Seal face forming a fluid bearing with the rotor.
Prestressed spring assembly biasing the seal segment.

Potential Applications: The technology can be applied in various turbine engines, including aircraft engines, power generation turbines, and industrial machinery.

Problems Solved: The technology helps improve the efficiency and performance of turbine engines by reducing leakage and enhancing sealing capabilities.

Benefits:

Enhanced sealing efficiency.
Improved turbine engine performance.
Reduced maintenance requirements.

Commercial Applications: The technology can be utilized in aerospace, power generation, and industrial sectors for improved turbine engine performance and efficiency.

Questions about Turbine Engine Seal Assembly: 1. How does the seal assembly in the turbine engine improve efficiency? 2. What are the potential applications of this technology in different industries?

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Original Abstract Submitted

A turbine engine is provided. The turbine engine defines a radial direction and includes: a rotor; a stator comprising a carrier; a seal assembly disposed between the rotor and the stator, the seal assembly comprising a first seal segment, the seal segment having a seal face configured to form a fluid bearing with the rotor; and a seal support assembly, the seal support assembly comprising a prestressed spring assembly extending from the seal segment for biasing the seal segment along the radial direction.