Turbomachine Gearbox Efficiency Rating for Oil Flow Sizing

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Geared turbofan engines face increased complexity due to the inclusion of a gearbox, making engine development and manufacturing more difficult, necessitating improved methods for efficiency and precision.

Innovation Solution

The introduction of a gearbox efficiency rating (GER) formula, Q(D1.56T)1.53, which aids in the development and simplification of geared turbofan engines by quantifying gearbox efficiency based on oil flow rate, fan diameter, and net thrust, allowing for optimized gearbox configuration and oil flow estimation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If a gearbox is included in a turbofan engine to allow different rotational speeds for power turbine and bypass fan, then operational efficiency and power production are improved, but device complexity increases making development and manufacturing more difficult

Engineering Contradiction:
Improvepower productionVSAvoidengine complexity
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The patent introduces a gearbox efficiency rating parameter that quantifies the relationship between gearbox oil flow rate, fan diameter, and net thrust. This parameter enables systematic optimization of gearbox configurations by changing key operational parameters (oil flow rate Q, fan diameter D, net thrust T) to achieve desired efficiency levels while managing complexity through standardized rating criteria.

Inventive Principle:
Principle #35Parameter changes

2Productivity

If a gearbox is included in a turbofan engine to allow different rotational speeds for power turbine and bypass fan, then operational efficiency is improved, but manufacturing difficulty increases

Engineering Contradiction:
Improveoperational efficiencyVSAvoidmanufacturing difficulty
Core Design Contradiction:
ProductivityVSEase of manufacture

Solution Approach 1:

The patent establishes manufacturing guidance based on the gearbox efficiency rating parameter, which correlates oil flow rate, fan diameter, and net thrust to predicted efficiency levels. This enables manufacturers to select from standardized gearbox configurations that meet target efficiency criteria, simplifying the manufacturing decision-making process while maintaining operational efficiency.

Inventive Principle:
Principle #35Parameter changes

3Productivity

If gearbox oil flow rate is increased to improve gearbox efficiency, then operational efficiency is improved, but engine complexity and oil system requirements increase

Engineering Contradiction:
Improvegearbox efficiencyVSAvoidoil system complexity
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The patent uses the gearbox efficiency rating parameter to systematically determine appropriate oil flow rate values based on fan diameter and net thrust requirements. Rather than arbitrarily increasing oil flow rate, the method calculates the specific flow rate needed to achieve target efficiency levels, optimizing the balance between gearbox efficiency and oil system complexity.

Inventive Principle:
Principle #35Parameter changes

Data Source

PatentUS11486312B2Gearbox efficiency rating for turbomachine engines
Publication Date: 2022.11.01 GE AVIO SRL
  • US11486312B2 patent drawing
  • US11486312B2 patent drawing
  • US11486312B2 patent drawing

AI summary

A turbomachine engine can include an unducted fan assembly, an unducted vane assembly, a core engine, a gearbox, and a gearbox efficiency rating. The unducted fan assembly can include a plurality of fan blades. The unducted vane assembly can include a plurality of vanes, and the vanes can, in some instances, be disposed aft of the fan blades. The core engine can include one or more compressor sections and one or more turbine sections. The gearbox includes an input and an output. The input is coupled to the one or more turbine sections of the core engine and comprises a first rotational speed, the output is coupled to the unducted fan assembly and has a second rotational speed, and a gear ratio of the first rotational speed to the second rotational speed is within a range of 4.1-14.0. The gearbox efficiency rating is 0.10-1.8.