Traveling-Wave Surface Actuation for Supersonic Shock Reduction

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Solution Overview

Problem

Current approaches to manage shocks and discontinuities in supersonic fluid flows, such as those experienced by jet engines and supersonic aircraft, are inadequate as standing waves fail to effectively dampen these shocks, leading to material fatigue and reduced operational life.

Innovation Solution

Generating traveling waves along surfaces exposed to supersonic fluid flows using actuators controlled by a wave controller to alter fluid properties, either minimizing or accentuating shocks based on flow direction.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Object-affected harmful factors

If standing waves are used to dampen shocks in supersonic flow, then shock reduction is attempted, but the standing waves fail to effectively dampen shocks leading to material fatigue

Engineering Contradiction:
Improveshock intensityVSAvoidmaterial durability
Core Design Contradiction:
Object-affected harmful factorsVSReliability

Solution Approach 1:

The patent transitions from static standing waves to dynamic traveling waves that move along the surface in the direction of fluid flow. This dynamic approach allows the waves to continuously interact with incoming shocks, effectively dampening them and reducing material fatigue while maintaining shock reduction capabilities.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The traveling waves are generated through periodic actuation of the surface at frequencies matching the shock encounter frequency. This periodic action creates a rhythmic disturbance that constructively interferes with incoming shocks, enhancing the dampening effect and protecting materials from cumulative fatigue damage.

Inventive Principle:
Principle #19Periodic action

2Object-affected harmful factors

If traveling waves are generated to minimize shocks, then shock reduction is achieved, but the system complexity increases due to multiple actuators and control mechanisms

Engineering Contradiction:
Improveshock intensityVSAvoidactuator control system
Core Design Contradiction:
Object-affected harmful factorsVSDevice complexity

Solution Approach 1:

The surface is divided into multiple discrete actuator elements that can be independently controlled. Each actuator segment generates a portion of the traveling wave, and by coordinating their activation sequences, the system creates effective traveling waves without requiring a monolithic complex control mechanism.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The control system uses feedback from shock detection sensors to adjust actuator activation timing and frequency. This feedback loop allows the system to adapt to varying flow conditions and shock characteristics, optimizing shock reduction while managing control complexity through intelligent regulation.

Inventive Principle:
Principle #23Feedback

3Object-affected harmful factors

If actuators are activated at higher frequencies to match increased flow speed, then shock dampening effectiveness is maintained, but energy consumption increases

Engineering Contradiction:
Improveshock dampening effectivenessVSAvoidactuator energy consumption
Core Design Contradiction:
Object-affected harmful factorsVSUse of energy by moving object

Solution Approach 1:

The system dynamically adjusts actuator activation frequency based on measured flow velocity. When flow speed increases, the actuation frequency is increased to maintain synchronization with shock encounter frequency, preserving dampening effectiveness. When flow speed decreases, frequency is reduced to minimize energy consumption, creating an adaptive energy-efficient operation mode.

Inventive Principle:
Principle #35Parameter changes

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

The traveling waves reduce turbulence, minimize shocks, and enhance fluid flow efficiency by adjusting fluid properties, thereby improving the performance and longevity of supersonic systems.

Implementation Method 1

one or more actuators configured to selectably induce strain in the surface

Methodology Applied
Scientific EffectStrain induction: Deformation

Implementation Method 2

the one or more travelling waves interact with the supersonic fluid flow to alter one or more properties of the supersonic fluid flow

Methodology Applied
Scientific EffectWave-fluid interaction: Turbulence

Data Source

PatentUS12420915B2Systems and methods for producing traveling waves along surfaces exposed to supersonic fluid flows
Publication Date: 2025.09.23 TEXAS A&M UNIVERSITY
  • US12420915B2 patent drawing
  • US12420915B2 patent drawing
  • US12420915B2 patent drawing

AI summary

A supersonic flow system in which a supersonic flow is encountered includes a surface configured to be exposed to a supersonic fluid flow, wherein the surface includes an upstream end and a downstream end opposite the upstream end, a wave generator coupled to the surface and including one or more actuators configured to selectably induce strain in the surface, and a wave controller in signal communication with the wave generator and configured to activate the one or more actuators to induce one or more travelling waves configured to travel along the surface between the upstream end and the downstream end of the surface.