Coaxial Accessory Gearbox Layout for Compact Gas Turbine Packaging

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Solution Overview

Problem

As gas turbine engines become smaller, the packaging for gearboxes that transmit drive from the tower shafts to various auxiliary systems becomes a challenge due to space constraints.

Innovation Solution

A compact accessory gearbox design is implemented, where a low speed input shaft and a high speed input shaft are connected to their respective tower shafts, which are coaxial and rotate about a common axis, with an angle drive mechanism allowing the low speed and high speed tower shafts to drive accessories through bevel gears, enabling efficient transmission of power to multiple accessories while optimizing space usage.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Volume of moving object

If traditional gearbox packaging is used, then power transmission function is achieved, but space requirements increase making it unsuitable for smaller gas turbine engines

Engineering Contradiction:
Improvegearbox volumeVSAvoidpower transmission capability
Core Design Contradiction:
Volume of moving objectVSPower

Solution Approach 1:

The patent implements a nested configuration where the high-speed input shaft is positioned concentrically within the low-speed input shaft, and the high-speed tower shaft is received within the low-speed tower shaft. This nesting arrangement allows both speed inputs and tower shafts to occupy the same radial space, dramatically reducing the overall gearbox volume while maintaining full power transmission capability to multiple accessories

Inventive Principle:
Principle #7Nested doll (Nesting)

Solution Approach 2:

The patent transitions from traditional parallel shaft arrangements to a concentric/collinear arrangement where shafts are positioned along the same axis. This dimensional reorganization allows the gearbox to exploit radial space more efficiently, reducing the axial and radial footprint while preserving all power transmission paths to the accessory systems

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

2Adaptability or versatility

If separate tower shafts for low speed and high speed spools are used, then both spools can drive accessories independently, but packaging space increases

Engineering Contradiction:
Improveaccessory drive capabilityVSAvoidgearbox packaging area
Core Design Contradiction:
Adaptability or versatilityVSArea of stationary object

Solution Approach 1:

The patent merges the low-speed and high-speed tower shafts into a single collinear arrangement where both shafts rotate about a common axis. This consolidation allows both speed inputs to drive their respective accessories through shared structural elements and common mounting spaces, reducing the overall packaging area while maintaining independent accessory drive capability

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The collinear tower shaft configuration serves multiple functions simultaneously: it supports both low-speed and high-speed inputs, provides mounting points for multiple accessories, and enables angle drives to both input shafts from a single structural location. This multi-functionality reduces the number of separate components needed, thereby reducing packaging area

Inventive Principle:
Principle #6Universality (Multi-functionality)

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 design allows for efficient power transmission to multiple accessories while minimizing space requirements, enhancing the compactness and efficiency of the gearbox packaging in smaller gas turbine engines.

Implementation Method 1

each of the low speed and high speed tower shafts drive a bevel gear to in turn drive a bevel gear connected to the low speed input shaft and low speed output shaft

Methodology Applied
Scientific EffectGear: Gear

Data Source

PatentEP3696392B2Angle accessory gearbox for gas turbine engine
Publication Date: 2024.12.25 RTX CORP
  • EP3696392B2 patent drawingFigure 1
  • EP3696392B2 patent drawingFigure 2A~2C
  • EP3696392B2 patent drawingFigure 3A~4

AI summary

A gas turbine engine (20) includes a low speed input shaft (114) connected to a low speed tower shaft (97), in turn connected to a lower speed spool (30) and a high speed input shaft (110) connected to a high speed tower shaft (99), in turn connected to a higher speed spool (32). The low speed input shaft (114) is connected to drive a first plurality of accessories. The high speed input shaft (110) is connected to drive a second plurality of accessories. The high speed tower shaft (99) and the low speed tower shaft (97) are coaxial and rotate about a common axis (I). An angle drive is provided into the low speed input shaft (114) and the high speed input shaft (110), respectively.