Turbine Blade Rack Control via Radial Sliding Guides

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Solution Overview

Problem

Existing control systems for pivotally-mounted blades in turbine engines face challenges in efficiently controlling all blades due to space constraints and high operational temperatures and speeds, particularly when using bevel gears inside a polygonal ring, which limits their effectiveness.

Innovation Solution

An actuator ring with racks that mesh with the blades' teeth, allowing for precise angular positioning, where the racks are mounted on the ring with guides that enable sliding movements to maintain accurate meshing and resist centrifugal and thermal expansions, ensuring reliable operation across a wide range of temperatures and speeds.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Volume of moving object

If bevel gears are arranged inside the polygonal ring to control blade angular positions, then the control mechanism is compact, but it becomes difficult or impossible to control all blades due to space constraints

Engineering Contradiction:
Improvecontrol device volumeVSAvoidblade control completeness
Core Design Contradiction:
Volume of moving objectVSReliability

Solution Approach 1:

The patent moves the control mechanism from the interior of the polygonal ring to its exterior periphery. Racks are mounted on the outer circumference of the ring, allowing each rack to engage with corresponding teeth on each blade independently. This dimensional relocation resolves the space constraint problem by utilizing the available peripheral space around the ring rather than the confined interior volume.

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

2Device complexity

If racks are rigidly fixed to the ring, then the structure is simple, but thermal expansion and centrifugal forces at high speeds cause deformation and loss of accurate meshing

Engineering Contradiction:
Improverack mounting structureVSAvoidtooth meshing accuracy
Core Design Contradiction:
Device complexityVSManufacturing precision

Solution Approach 1:

The patent transitions from a rigid fixed connection to a dynamic adjustable connection. Each rack is mounted on the ring via mounting means that allow relative movement in the radial direction. This dynamic mounting enables the racks to self-adjust their positions radially in response to thermal expansion and centrifugal forces, maintaining accurate tooth meshing despite environmental changes and high-speed operation.

Inventive Principle:
Principle #15Dynamics

3Area of stationary object

If the control device is located downstream from the blade support ring, then it has more space, but it occupies a larger volume and is less efficient

Engineering Contradiction:
Improveavailable spaceVSAvoidcontrol efficiency
Core Design Contradiction:
Area of stationary objectVSProductivity

Solution Approach 1:

The patent utilizes the peripheral dimension of the ring structure rather than moving downstream. By mounting racks on the outer circumference of the ring, the design achieves both compact positioning (maintaining control efficiency) and adequate space (utilizing peripheral area). This eliminates the need to relocate downstream while still providing sufficient mounting space for all racks.

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

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

The solution allows for reliable and efficient control of blade angular positions with minimal volume occupation, maintaining accurate tooth pitch and resisting deformation, thus ensuring durable operation under high-speed and high-temperature conditions.

Implementation Method 1

resisting centrifugal and thermal expansions

Methodology Applied
Scientific EffectThermal expansion: Thermal Expansion

Implementation Method 2

resisting centrifugal and thermal expansions

Methodology Applied
Scientific EffectCentrifugal force: Centrifugal Force

Implementation Method 3

suitable for sliding firstly relative to the ring along the radial direction specific to each guide, and secondly relative to the rack along a movement direction that is substantially radial and specific to the rack

Methodology Applied
Scientific EffectFriction: Friction

Data Source

PatentUS9068574B2Assembly having a control device with racks for controlling the angular position of pivotally-mounted blades in a turbine engine
Publication Date: 2015.06.30 SAFRAN AIRCRAFT ENGINES SAS
  • US9068574B2 patent drawing
  • US9068574B2 patent drawing
  • US9068574B2 patent drawing

AI summary

An assembly in a turbine engine for controlling plural toothed pivotally-mounted blades arranged in azimuth around the axis of the turbine engine and including an actuator ring controlling a position of the blades. Racks mounted on the ring present corresponding sets of teeth meshing with the set of teeth of a respective one of the blades to place it in a selected angular position, and they are held in the radial direction by radial positioning mechanism fastened to the blade. Each rack is mounted on the ring by plural guides spaced apart circumferentially around the ring, that connect together movements of the rack and of the ring in the circumferential direction, and that are configured to slide relative to the ring, for each guide in its own radial direction, and relative to the rack in a direction of movement that is substantially radial and specific to the rack.