Hypersonic Harmonic Exciter Reducing Drag via Acoustic Fields

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Solution Overview

Problem

Current hypersonic spacecraft travel is limited by challenges related to material selection, aircraft design, and overcoming increased friction and air resistance at speeds greater than Mach 5, where existing solutions fail to effectively manage shock waves, heating, and friction.

Innovation Solution

A hypersonic harmonic vehicle exciter system comprising a vibration inducing wave device with concentric ring bands and a harmonic sound projecting device, both cone-shaped, generating harmonic waves that converge to reduce friction and air resistance, allowing for accelerated trajectory at hypersonic speeds.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Speed

If conventional aircraft designs are used at hypersonic speeds, then structural strength must be increased to withstand heating and shock waves, but this increases weight and reduces speed efficiency

Engineering Contradiction:
Improvehypersonic speedVSAvoidaircraft weight
Core Design Contradiction:
SpeedVSWeight of moving object

Solution Approach 1:

The patent replaces conventional mechanical propulsion systems with a harmonic excitation system that uses vibration and sound waves to interact with atmospheric molecules. The vibration inducing wave device and harmonic sound projecting device create acoustic fields that propel the aircraft without traditional engines, dramatically reducing weight while achieving hypersonic speeds

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

Solution Approach 2:

The invention changes the fundamental operating parameters by using harmonic vibrations at specific frequencies to resonate with air molecules. By tuning the vibration frequency and sound wave parameters to match atmospheric conditions, the system creates efficient propulsion that reduces drag and heating effects without requiring heavy structural reinforcement

Inventive Principle:
Principle #35Parameter changes

2Speed

If aircraft speed increases to hypersonic levels, then friction and air resistance increase dramatically, but conventional methods to reduce drag increase surface area and weight

Engineering Contradiction:
Improvehypersonic speedVSAvoidfriction and air resistance
Core Design Contradiction:
SpeedVSObject-affected harmful factors

Solution Approach 1:

The patent replaces conventional aerodynamic drag reduction methods with a wave-based interaction system. The vibration inducing wave device and harmonic sound projecting device create acoustic fields that manipulate atmospheric molecules, reducing friction and air resistance through wave-matter interaction rather than traditional aerodynamic shaping

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

Solution Approach 2:

The invention uses mechanical vibration at hypersonic frequencies to interact with air molecules. The vibration inducing wave device generates harmonic oscillations that create a slipstream effect, reducing friction and drag by orchestrating molecular motion rather than fighting against it

Inventive Principle:
Principle #18Mechanical vibration

3Speed

If conventional propulsion systems are used to achieve hypersonic speeds, then engine power and fuel consumption must be increased, but this increases energy use and reduces efficiency

Engineering Contradiction:
Improvehypersonic speedVSAvoidenergy consumption
Core Design Contradiction:
SpeedVSUse of energy by moving object

Solution Approach 1:

The patent replaces conventional thermal propulsion systems with an acoustic field-based propulsion system. Instead of burning fuel to generate thrust, the vibration inducing wave device and harmonic sound projecting device use electromagnetic energy to create acoustic fields that directly interact with atmospheric molecules, dramatically reducing energy consumption

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

Solution Approach 2:

The invention uses periodic harmonic vibrations and sound waves to propel the aircraft. By applying periodic acoustic energy at resonant frequencies, the system achieves continuous thrust with minimal energy input, as the harmonic oscillations efficiently transfer energy to atmospheric molecules

Inventive Principle:
Principle #19Periodic action

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 system effectively reduces shock waves, heating, and friction, enabling hypersonic speeds by creating a slip stream, facilitating faster travel through atmospheric and other resistive media, and can be applied to various platforms, including aircraft, spacecraft, and underwater vehicles.

Implementation Method 1

the Vibration Inducing Wave Device configured to generate harmonic vibration wave patterns that converge on a convergence point forward of the Vehicle Bod/shell

Methodology Applied
Scientific EffectHarmonic vibration: Vibration

Implementation Method 2

the Hypersonic Harmonic Sound Projecting Device configured to generate a harmonic sound wave, the Hypersonic Harmonic Sound Projecting Device further configured to insert/fit therein the Vibration Inducing Wave Device

Methodology Applied
Scientific EffectSound wave: Sound

Data Source

PatentUS11220358B1Hypersonic harmonic vehicle exciter and methods of use thereof
Publication Date: 2022.01.11 WEST BRANDON
  • US11220358B1 patent drawing
  • US11220358B1 patent drawing
  • US11220358B1 patent drawing

AI summary

A hypersonic harmonic exciter system to enable hypersonic speed, including a hypersonic harmonic exciter body having a plurality angled sides forming exciter body hollow structure with an access aperture, vibration inducing wave apparatus configured to produce and project vibration harmonic waves that converge on a convergence harmonic point forward of the hypersonic harmonic exciter body, the vibration inducing wave apparatus having vibration apparatus hollow structure with a series of exterior concentrically positioned vibration inducing bands, the vibration inducing wave apparatus inserted in the exciter body hollow structure, and harmonic sound projecting apparatus configured to produce and project harmonic sound waves that converge on the convergence harmonic point forward of the hypersonic harmonic exciter body, the harmonic sound projecting apparatus having sound apparatus hollow structure with a series of exterior concentrically positioned sound emitter bands, the harmonic sound projecting apparatus inserted in the vibration apparatus hollow structure.