Laminate-Faced Honeycomb Bracing for Stringed Instruments

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Solution Overview

Problem

Existing stringed instruments face challenges in achieving a balance between structural integrity and acoustic performance, particularly when using materials other than high-quality wood, as carbon fiber laminates tend to be overly damped, prone to damage, and lack the desired acoustic characteristics of wood.

Innovation Solution

A laminate-faced honeycomb or other shaped bracing structure is introduced, comprising layers of carbon fiber or fibrous laminates with a honeycomb or shaped core, providing adjustable stiffness and enhancing both structural integrity and acoustic properties by regulating vibration and resonance.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If solid carbon fiber laminates are used for soundboard bracing, then structural integrity and strength are improved, but acoustic response and tone quality deteriorate due to excessive damping and metallic sound characteristics

Engineering Contradiction:
Improvestructural integrityVSAvoidacoustic response
Core Design Contradiction:
StrengthVSReliability

Solution Approach 1:

The patent uses composite materials by combining carbon fiber laminates with foam cores to create a bracing structure that integrates the high strength of carbon fiber with the acoustic properties of foam, resolving the contradiction between structural integrity and acoustic response

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

The patent applies different material properties to different parts of the bracing structure - carbon fiber laminates provide strength in specific areas while foam cores provide acoustic response in other areas, allowing each material to optimize its local function

Inventive Principle:
Principle #3Local quality

2Strength

If carbon fiber laminates with high density are used, then structural strength is improved, but bending stiffness for a given weight deteriorates

Engineering Contradiction:
Improvestructural strengthVSAvoidbending stiffness per weight
Core Design Contradiction:
StrengthVSWeight of moving object

Solution Approach 1:

The patent uses thin carbon fiber laminate shells faced over foam cores, creating a structure that achieves high strength-to-weight ratio by placing strong material only where structurally necessary while maintaining overall lightness

Inventive Principle:
Principle #30Flexible shells and thin films

Solution Approach 2:

The composite construction of carbon fiber laminates over foam cores creates a lightweight structure with high bending stiffness, as the carbon fiber provides strength while the foam provides structural support with minimal weight

Inventive Principle:
Principle #40Composite materials

3Weight of moving object

If the face sheets of carbon laminate are made thin to reduce weight, then weight is reduced, but damage resistance to minor impacts deteriorates

Engineering Contradiction:
ImproveweightVSAvoiddamage resistance
Core Design Contradiction:
Weight of moving objectVSReliability

Solution Approach 1:

The patent uses thin carbon fiber laminate shells that are lightweight yet protected by the foam core underneath, which acts as a cushioning layer that absorbs impact energy and prevents damage to the thin face sheets

Inventive Principle:
Principle #30Flexible shells and thin films

Solution Approach 2:

The foam core is positioned between the thin carbon fiber face sheets and potential impact sources, providing beforehand cushioning that protects the delicate thin laminates from damage during minor impacts

Inventive Principle:
Principle #11Beforehand cushioning (Prior cushioning)

4Ease of manufacture

If foam or syntactic foam cores are used in bracing, then manufacturing ease and cost are improved, but acoustic response deteriorates due to excessive damping and increased weight

Engineering Contradiction:
Improvemanufacturing easeVSAvoidacoustic response
Core Design Contradiction:
Ease of manufactureVSReliability

Solution Approach 1:

The patent carefully selects and positions foam material in specific locations within the bracing structure where damping is acceptable, while leaving other areas with different acoustic requirements to resonate more freely, optimizing both manufacturing ease and acoustic response

Inventive Principle:
Principle #3Local quality

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 solution results in a uniformly strong soundboard that delivers a clean, brilliant sound while being more economical to manufacture, offering superior structural integrity and acoustic performance compared to traditional materials.

Implementation Method 1

providing adjustable stiffness and enhancing both structural integrity and acoustic properties by regulating vibration and resonance

Methodology Applied
Scientific EffectVibration: Vibration

Implementation Method 2

providing adjustable stiffness and enhancing both structural integrity and acoustic properties by regulating vibration and resonance

Methodology Applied
Scientific EffectResonance: Resonance

Implementation Method 3

comprising layers of carbon fiber or fibrous laminates with a honeycomb or shaped core, providing adjustable stiffness

Methodology Applied
Scientific EffectElasticity: Elasticity

Data Source

PatentUS20230326433A1Laminate Faced Honeycomb Bracing Structure for Stringed Instrument
Publication Date: 2023.10.12 MCP IP LLC
  • US20230326433A1 patent drawing
  • US20230326433A1 patent drawing
  • US20230326433A1 patent drawing

AI summary

A soundboard for a musical instrument is disclosed the soundboard having at least one layer of material. In some embodiments the material comprising carbon fiber, fibrous laminate material, resin or a plastic matrix and combinations thereof. At least one bracing structure is engaged to the at least one layer of material. The at least one bracing structure comprising at least one layer of honeycomb or shaped core and at least one sheet of material bonded to the honeycomb or shaped core.