Rotor Blade Bond Fixture With Segmented Clamps

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Solution Overview

Problem

The manufacturing and repair of rotor blades for rotary-wing aircraft face challenges in efficiently bonding sheath assemblies due to high stresses and strains from aerodynamic forces, requiring effective application of heat and pressure without damaging the blades.

Innovation Solution

A bond fixture with a heater and clamps that apply localized and constant heat and pressure, using a combination of pivotable members and a root end lift mechanism to securely hold the rotor blade, allowing for even heat distribution and pressure application through a vacuum bag.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If a bond fixture with heater and clamps is used to apply localized heat and pressure, then bonding efficiency and consistency are improved, but device complexity increases

Engineering Contradiction:
Improvebonding efficiencyVSAvoidfixture structure complexity
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The bond fixture is divided into multiple independent clamps (first clamp, second clamp, third clamp, fourth clamp) that can be positioned and adjusted separately along the rotor blade. Each clamp has its own heater and pressure application mechanism, allowing localized bonding operations at different positions without requiring a single complex centralized system.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The clamps are designed with movable and adjustable components that can be dynamically positioned along the rotor blade length. The first and second clamps can move along the upper and lower surfaces respectively, while the third and fourth clamps can position themselves on opposite sides of the blade, enabling flexible adaptation to different bonding locations and configurations.

Inventive Principle:
Principle #15Dynamics

2Manufacturing precision

If multiple clamps with pads are used to apply pressure, then bonding consistency is improved, but ease of operation deteriorates

Engineering Contradiction:
Improvebonding consistencyVSAvoidclamp operation complexity
Core Design Contradiction:
Manufacturing precisionVSEase of operation

Solution Approach 1:

The pads are designed to automatically conform to the rotor blade surface geometry through their material properties and mounting mechanisms. The first pad conforms to the upper surface while the second pad conforms to the lower surface, reducing the need for manual adjustment and positioning by operators while maintaining consistent pressure distribution across the bonding area.

Inventive Principle:
Principle #25Self-service

3Use of energy by moving object

If localized heat application is used instead of walk-in ovens, then energy efficiency is improved, but manufacturing precision requirements increase

Engineering Contradiction:
Improveenergy efficiencyVSAvoidheat distribution control
Core Design Contradiction:
Use of energy by moving objectVSManufacturing precision

Solution Approach 1:

Each clamp is equipped with its own heater that applies heat locally to the specific bonding position on the rotor blade. This localized heating approach allows precise temperature control at each bonding point independently, eliminating the need for large walk-in ovens while maintaining the thermal conditions required for consistent bonding quality.

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 enables efficient bonding of sheath assemblies to rotor blades, ensuring consistent performance and reducing the need for large walk-in ovens, while minimizing damage to the rotor blades during the bonding process.

Implementation Method 1

applying localized and constant heat and pressure to the sheath assembly laminate

Methodology Applied
Scientific EffectHeating: Heating

Implementation Method 2

applying localized and constant heat and pressure to the sheath assembly laminate through a vacuum bag

Methodology Applied
Scientific EffectVacuum: Vacuum

Data Source

PatentUS11161627B2Bond fixture for sheath assembly of rotor blade
Publication Date: 2021.11.02 SIKORSKY AIRCRAFT CORP
  • US11161627B2 patent drawing
  • US11161627B2 patent drawing
  • US11161627B2 patent drawing

AI summary

A bond fixture includes a first fixture having a heater and a plurality of clamps. Each of the plurality of clamps includes a first member and a second member rotatable between a first position and a second position. A second fixture includes a root end lift translatable vertically between a retracted position and an extended position and a root end clamp translatable along a horizontal axis. The root end clamp is configured to cooperate with the root end.