IP Library › Granted Patent US 12,571,325
Granted Patent B2
US 12,571,325 · App. 18/148,530 · Granted Mar 10, 2026

Thermoelectric generator for a turbine engine

Inventors: Vishnu Das K (Bengaluru, IN); Vinaykumar Shrimantrao Patil (Bengaluru, IN); Manish Singhal (Bengaluru, IN); Ravindra Shankar Ganiger (Bengaluru, IN)
Assignee: General Electric Company
F01D15/10F01D11/24H10N10/01H10N10/17B33Y10/00B33Y80/00F05D2220/76
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Quick Facts
Patent No.
US 12,571,325
App. No.
18/148,530
Granted
Mar 10, 2026
Kind
B2
Abstract

A thermoelectric generator for a turbine engine is provided. The turbine engine can include a core having a casing surrounded by an engine cowl. The thermoelectric generator is attached to or formed integrally with the casing. The thermoelectric generator includes a power generation module formed by a plurality of thermocouples that utilize a temperature differential between a hot side and a cold side of the casing to generate electrical power. In one aspect, an electrically insulative layer is positioned between the casing and the power generation module. In another aspect, the thermoelectric generator includes a phase change material pack that includes an inner layer and an outer layer, the power generation module being positioned between the inner layer and the outer layer. In other aspects, the thermoelectric generator can be additively manufactured on the casing or another structural component of the turbine engine.

Claims (20)

1 . A thermoelectric generator for a turbine engine, comprising:

a casing including an outer surface and an inner surface, the inner surface facing a core air flowpath of the turbine engine and the outer surface facing an under cowl cavity;

a power generation module formed of a plurality of thermocouples arranged on the outer surface of the casing in a serpentine configuration, the power generation module being directly exposed within the under cowl cavity; and

an electrically insulative layer or a first layer of a phase change material, the electrically insulative layer or the first layer of the phase change material being positioned between the outer surface of the casing and the power generation module.

2 . The thermoelectric generator for a turbine engine of claim 1 , wherein the thermoelectric generator extends annularly around the metallic structural component or is one of a plurality of thermoelectric generators electrically coupled with one another.

3 . The thermoelectric generator for a turbine engine of claim 1 , wherein the power generation module and the electrically insulative layer are formed integrally with the casing.

4 . The thermoelectric generator for a turbine engine of claim 1 , wherein each one of the plurality of thermocouples includes a hot side plate formed of an electrically conducting material, a cold side plate formed of electrically conducting material, and a semiconductor array positioned between the hot side plate and the cold side plate.

5 . The thermoelectric generator for a turbine engine of claim 4 , wherein the casing is formed of a metallic material, and further comprising an electrically insulative layer positioned between the casing and the cold side plate.

6 . The thermoelectric generator for a turbine engine of claim 5 , wherein the electrically insulative layer is a thin film ceramic coating.

7 . The thermoelectric generator for a turbine engine of claim 4 , further comprising a phase change material pack that includes an inner layer and an outer layer.

8 . The thermoelectric generator for a turbine engine of claim 7 , wherein the hot side plate, the semiconductor array, and the cold side plate are positioned between the inner layer and the outer layer of the phase change material pack.

9 . The thermoelectric generator for a turbine engine of claim 8 , and wherein the inner layer is received within a recess of the casing.

10 . The thermoelectric generator for a turbine engine of claim 1 , wherein an engine cowl defines an under cowl cavity and the power generation module and the electrically insulative layer are disposed within the under cowl cavity.

11 . The thermoelectric generator for a turbine engine of claim 1 , further comprising:

an active clearance control system that directs a cooling fluid onto a cold side of the thermoelectric generator.

12 . The thermoelectric generator for a turbine engine of claim 1 , wherein the casing separates a relatively cool cavity from a relatively hot cavity, and wherein the casing is positioned such that a hot side of the thermoelectric generator is directly exposed to the relatively hot cavity and a cold side of the thermoelectric generator is directly exposed to the relatively cool cavity.

13 . The thermoelectric generator for a turbine engine of claim 1 , wherein the casing is one of a compressor casing, a combustor casing, or a turbine casing.

14 . The thermoelectric generator for a turbine engine of claim 1 , wherein the serpentine configuration comprises a first portion extending along the axial direction, and a second portion connected with the first portion and extending along the circumferential direction.

15 . The thermoelectric generator for a turbine engine of claim 1 , wherein the casing separates a relatively cool cavity from a relatively hot cavity, and wherein the casing defines a port in which the thermoelectric generator is received, the thermoelectric generator being positioned such that at least a part of the thermoelectric generator is positioned within the relatively hot cavity, the thermoelectric generator has an electric insulative layer and a power generation module, the electric insulative layer defines one or more perforations that enable relatively hot fluid from the relatively hot cavity to directly contact the power generation module.

16 . The thermoelectric generator for a turbine engine of claim 1 , wherein the casing is a bleed duct casing.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 30, 2022
From: K, VISHNU DAS; PATIL, VINAYKUMAR SHRIMANTRAO; SINGHAL, MANISH; GANIGER, RAVINDRA SHANKAR
To: GENERAL ELECTRIC COMPANY
Reel/Frame 062243/0416 →
Priority Claims (1)
IN 202211062291 · Nov 1, 2022 · national
Continuity (1)
Related Publication 20240141800A1 · May 2, 2024
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