THERMAL INSULATION ASSEMBLY

Organization Name

general electric company

Inventor(s)

Karthick Gourishankar of Bangalore (IN)

Mohandas Nayak of Bangalore (IN)

Rejin Ratnakar of Bangalore (IN)

Eric Daniel Holbrook of Vandalia OH (US)

THERMAL INSULATION ASSEMBLY - A simplified explanation of the abstract

This abstract first appeared for US patent application 20240280054 titled 'THERMAL INSULATION ASSEMBLY

Simplified Explanation: The patent application describes a thermal insulation assembly designed for high-temperature ducts in turbine engines, capable of withstanding pressures below 80 kilopascals.

The assembly includes a first foil layer facing the duct, a second foil layer spaced from the first foil layer, an insulation layer between the foils, an opacifier layer on the insulation, and a reflective layer on the opacifier.

Key Features and Innovation:

Thermal insulation assembly for high-temperature ducts in turbine engines.
Can withstand pressures below 80 kilopascals.
Includes multiple layers for effective insulation and reflection of heat.

Potential Applications: The technology can be used in various industries such as aerospace, automotive, and energy production where high-temperature ducts are present.

Problems Solved: The technology addresses the challenge of insulating high-temperature ducts in turbine engines while maintaining structural integrity under pressure.

Benefits:

Improved thermal insulation for high-temperature ducts.
Enhanced safety and efficiency in turbine engines.
Potential for energy savings due to reduced heat loss.

Commercial Applications: The thermal insulation assembly can be utilized in the aerospace industry for aircraft engines, in the automotive sector for high-performance vehicles, and in power generation for gas turbines.

Questions about Thermal Insulation Assembly: 1. How does the thermal insulation assembly improve the efficiency of turbine engines? 2. What are the key factors to consider when implementing this technology in different industrial applications?

Frequently Updated Research: Ongoing research focuses on optimizing the materials used in the thermal insulation assembly to enhance its performance and durability in high-temperature environments.

Original Abstract Submitted

a thermal insulation assembly for a duct through which high temperature fluid, greater than 500 fahrenheit, passes. the thermal insulation assembly can experience pressures less than 80 kilopascals and can be included in a turbine engine. the thermal insulation assembly includes a first foil layer confronting the duct, a second foil layer spaced from the first foil layer, an insulation layer between the first foil layer and the second foil layer, an opacifier layer provided on the insulation layer, and a reflective layer applied to the opacifier layer.