Temperature-Responsive Flow Aperture for Jet Engine Thermal Control

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Solution Overview

Problem

Conventional thermal control methods in jet engines are often heavy, space-consuming, and require significant maintenance, posing challenges in aviation applications.

Innovation Solution

The implementation of a flow aperture system using a temperature-responsive material, such as high-temperature alloys or bimetallic components, that deflects to modulate fluid flow through a passageway, eliminating the need for mechanical actuators and allowing for thermally controlled flow modulation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If mechanical actuators are used for thermal control, then flow modulation capability is improved, but device weight increases

Engineering Contradiction:
Improveflow modulation capabilityVSAvoiddevice weight
Core Design Contradiction:
Ease of operationVSWeight of moving object

Solution Approach 1:

The patent replaces mechanical actuators with a thermal field-based flow modulation system. Temperature-responsive materials (such as shape memory alloys or thermally-expanding materials) directly convert thermal energy into mechanical deformation to modulate flow apertures, eliminating the need for separate mechanical actuation systems and thereby reducing device weight.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Solution Approach 2:

The patent changes the control parameter from mechanical actuation to temperature control. By varying the temperature of the temperature-responsive material, the flow aperture area is dynamically modulated. This parameter change enables flow control without mechanical moving parts, reducing overall system weight.

Inventive Principle:
Principle #35Parameter changes

2Ease of operation

If mechanical actuators are used for thermal control, then flow modulation capability is improved, but device complexity increases

Engineering Contradiction:
Improveflow modulation capabilityVSAvoiddevice complexity
Core Design Contradiction:
Ease of operationVSDevice complexity

Solution Approach 1:

The patent substitutes complex mechanical actuation mechanisms with a simpler thermal-responsive material system. The temperature-responsive material inherently provides the flow modulation function through thermal expansion or phase change, eliminating the need for motors, linkages, and control electronics associated with mechanical actuators.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Solution Approach 2:

The temperature-responsive material performs the flow modulation function autonomously in response to temperature changes, without requiring external mechanical actuation. The material self-regulates the flow aperture based on thermal input, simplifying the overall system architecture and reducing device complexity.

Inventive Principle:
Principle #25Self-service

3Ease of operation

If mechanical actuators are used for thermal control, then flow modulation capability is improved, but maintenance requirements increase

Engineering Contradiction:
Improveflow modulation capabilityVSAvoidmaintenance requirements
Core Design Contradiction:
Ease of operationVSEase of repair

Solution Approach 1:

The patent replaces mechanical actuators prone to wear and failure with solid-state temperature-responsive materials that have no moving parts. This substitution eliminates maintenance issues associated with mechanical wear, lubrication, and actuator failure, significantly reducing maintenance requirements.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Solution Approach 2:

The temperature-responsive material can be designed as a simple, replaceable component with no moving parts. If degradation occurs, the entire material element can be replaced as a single unit without complex disassembly or repair procedures, simplifying maintenance operations.

Inventive Principle:
Principle #27Cheap short-living objects (Disposable)

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

This approach enables flexible and efficient thermal control, reducing weight, space, and maintenance requirements by modulating fluid flow without mechanical actuators, thereby enhancing thermal management in jet engines.

Implementation Method 1

at least one material that deflects as a function of temperature

Methodology Applied
Scientific EffectThermal expansion: Thermal Expansion

Implementation Method 2

high-temperature alloys or bimetallic components

Methodology Applied
Scientific EffectBimetallic effect: Bi-Metallic Strip

Data Source

PatentUS11814186B2Flow aperture method and apparatus
Publication Date: 2023.11.14 GENERAL ELECTRIC CO
  • US11814186B2 patent drawing
  • US11814186B2 patent drawing
  • US11814186B2 patent drawing

AI summary

In a jet engine having a core that sources a first flow of fluid and a component (such as a fan, a pump, and/or a bleed line) that sources a second flow of fluid, and where the first flow of fluid will typically have, at least during ordinary operation, a higher temperature than the second flow of fluid, at least one flow aperture formed by a first passageway to receive at least a portion of the aforementioned second flow of fluid, wherein that first passageway is comprised of at least one material that (by design and intent) deflects as a function of temperature such that a flow of the second flow of fluid through the at least one flow aperture is thereby desirably modulated.