18534024. A GAS TURBINE AND GENERATOR ARRANGEMENT simplified abstract (ROLLS-ROYCE plc)

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A GAS TURBINE AND GENERATOR ARRANGEMENT

Organization Name

ROLLS-ROYCE plc

Inventor(s)

Roy J. Harron of Bristol (GB)

A GAS TURBINE AND GENERATOR ARRANGEMENT - A simplified explanation of the abstract

This abstract first appeared for US patent application 18534024 titled 'A GAS TURBINE AND GENERATOR ARRANGEMENT

The abstract describes a gas turbine and generator arrangement where the gas turbine engine and the generator are spaced apart in a lateral direction, with a gearbox translating the rotation of the turbine output shaft to drive the generator.

  • Gas turbine and generator arrangement
  • Gas turbine engine and generator spaced apart horizontally or vertically
  • Gearbox translates turbine output shaft rotation to drive the generator

Potential Applications: - Power generation in various industries - Aerospace applications for aircraft propulsion systems - Marine applications for ship propulsion systems

Problems Solved: - Efficient power generation with a compact design - Improved performance and reliability of the generator system

Benefits: - Space-saving design - Enhanced power generation efficiency - Increased reliability and durability of the system

Commercial Applications: Title: Innovative Gas Turbine Generator Arrangement for Enhanced Power Generation This technology can be used in power plants, aircraft, and marine vessels for efficient power generation, leading to cost savings and improved performance in various industries.

Questions about Gas Turbine and Generator Arrangement: 1. How does the spacing between the gas turbine engine and the generator impact the overall efficiency of the system?

  The spacing allows for better heat dissipation and maintenance access, leading to improved performance and reliability.

2. What are the potential challenges in integrating the gearbox into the system for translating the turbine output shaft rotation?

  The gearbox design must be robust and efficient to ensure smooth power transmission between the turbine and the generator.


Original Abstract Submitted

A gas turbine and generator arrangement comprising a gas turbine engine () and a generator (), the gas turbine engine comprising a turbine output shaft (), characterised in that the gas turbine engine and the generator are horizontally or vertically spaced apart from each other in a lateral direction and a gearbox () translates the rotation of the turbine output shaft to drive a gearbox output shaft () which in turn drives the generator.