Double Helical Gearbox Layout for Turbine Vibration Reduction

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Solution Overview

Problem

Vibrations in the gearbox of a gas turbine engine due to variations in torque transfer caused by geometry and manufacturing tolerances affect the durability and life of both the gearbox and associated turbine engine components.

Innovation Solution

The use of double helical gears with specific helix angles and circumferential offsets in the gearbox to reduce transmission errors and vibrations, achieved by offsetting gear teeth on the star gear to control harmonic levels and improve torque transfer efficiency.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of manufacture

If conventional single helical gears are used in the gearbox, then the structure is simple and easy to manufacture, but transmission errors and vibrations increase due to geometry and manufacturing tolerances

Engineering Contradiction:
Improvegear manufacturing simplicityVSAvoidtorque transfer stability
Core Design Contradiction:
Ease of manufactureVSReliability

Solution Approach 1:

The gear teeth are segmented into two distinct helical sets (first and second plurality of gear teeth) with different helix angles, allowing each set to compensate for different types of manufacturing tolerances and geometric variations, thereby reducing overall transmission errors while maintaining manufacturability

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The invention changes the helix angle parameter between the two sets of gear teeth, with the first plurality having a first helix angle and the second plurality having a second helix angle different from the first. This parameter variation allows the gear set to accommodate manufacturing tolerances and reduce transmission errors across different operating conditions

Inventive Principle:
Principle #35Parameter changes

2Reliability

If precision manufacturing is applied to reduce transmission errors, then torque transfer stability improves, but manufacturing complexity and cost increase

Engineering Contradiction:
Improvetorque transfer stabilityVSAvoidgear structure complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

Rather than requiring extreme manufacturing precision, the invention changes the operational parameters by using two sets of gear teeth with different helix angles. This allows the system to achieve stable torque transfer through parameter diversity rather than precision manufacturing, reducing both manufacturing complexity and device complexity

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The gear incorporates a composite structure with two different helical tooth sets, analogous to composite materials, where each tooth set serves a complementary function in handling different aspects of torque transfer and error compensation, achieving high reliability without excessive manufacturing precision

Inventive Principle:
Principle #40Composite materials

3Reliability

If double helical gears with different helix angles are used, then transmission errors and vibrations are reduced, but manufacturing complexity increases

Engineering Contradiction:
Improvevibration reductionVSAvoidgear manufacturing complexity
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The gear is segmented into two distinct helical tooth systems that can be manufactured and assembled as separate components or integrated in a modular fashion, reducing the overall manufacturing complexity compared to a monolithic double helical gear design while maintaining vibration reduction benefits

Inventive Principle:
Principle #1Segmentation

Data Source

PatentEP3828441B1Turbine engine gearbox
Publication Date: 2025.10.22 RTX CORP
  • EP3828441B1 patent drawingFigure 1
  • EP3828441B1 patent drawingFigure 2
  • EP3828441B1 patent drawingFigure 3~4

AI summary

An example method of controlling performance of gearbox of a gas turbine engine includes establishing a gear characteristic of a plurality of double helical gears each disposed about a respective axis in a gearbox. Performance of the plurality of double helical gears is controlled by selecting a circumferential offset distance between a first plurality of gear teeth spaced apart from a second plurality of gear teeth on each of the plurality of double helical gears in response to the established gear characteristic.