Cast Compressor Case Cooling Cavity for Faster Tip Clearance Response

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Existing compressor cases for gas turbine engines face challenges in blade tip clearance control, requiring complex and costly manufacturing processes, and limited options for modifying the exterior to manage system response effectively due to the need to mount engine accessories.

Innovation Solution

A compressor case design featuring a cooling cavity with a vane stage and trunnion bearing, where the cavity walls are cast and welded to form a U-shaped end channel, allowing for airflow to control temperature and optimize tip clearance, while maintaining minimal interference with external components for accessory mounting.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Manufacturing precision

If the wall thickness of the compressor case is increased to control blade tip clearance, then the system response is slowed down, but blade tip clearance control is improved

Engineering Contradiction:
Improveblade tip clearance controlVSAvoidsystem response speed
Core Design Contradiction:
Manufacturing precisionVSSpeed

Solution Approach 1:

The patent applies local quality by creating a cooling cavity with selective wall thickness distribution. The cavity walls are thinner in specific regions to enable faster thermal response for blade tip clearance control, while other parts of the compressor case maintain sufficient thickness for structural integrity. This localized variation in wall thickness allows differential thermal response where needed without compromising overall case strength.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The patent implements dynamics by enabling active thermal management through the cooling cavity. Temperature control systems can dynamically adjust the thermal state of the case by controlling cooling airflow through the cavity, allowing the system to respond actively and rapidly to blade tip clearance requirements rather than relying solely on static wall thickness.

Inventive Principle:
Principle #15Dynamics

2Speed

If the wall thickness of the compressor case is decreased to speed up system response, then blade tip clearance control is worsened, but system response is improved

Engineering Contradiction:
Improvesystem response speedVSAvoidblade tip clearance control
Core Design Contradiction:
SpeedVSManufacturing precision

Solution Approach 1:

The cooling cavity enables local quality optimization by concentrating thermal control capabilities in specific regions where blade tip clearance management is critical. The cavity walls are strategically positioned and sized to provide enhanced thermal response locally without requiring the entire case to be thin-walled, thus maintaining overall structural integrity while achieving fast response where needed.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The patent employs pneumatic principles by using controlled airflow through the cooling cavity to manage thermal conditions. Cooling air is directed through the cavity to actively control case temperature and thermal expansion, enabling rapid system response to blade tip clearance requirements through fluid-based thermal management rather than relying solely on conductive heat transfer through thick walls.

Inventive Principle:
Principle #29Pneumatics and hydraulics

3Manufacturing precision

If complex manufacturing processes are used to modify the exterior of the cases for tip clearance control, then tip clearance control is improved, but manufacturing complexity and cost increase

Engineering Contradiction:
Improvetip clearance controlVSAvoidmanufacturing process complexity
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

The patent merges the cooling cavity formation into the primary case manufacturing process. The cooling cavity is integrated into the case structure and can be formed during the original casting or machining operations, eliminating the need for separate complex modification processes. This integration achieves precise tip clearance control capability while avoiding additional manufacturing steps and associated costs.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The cooling cavity serves multiple functions: it provides thermal management for blade tip clearance control, acts as a structural element within the case, and can accommodate instrumentation or other components. This multi-functionality reduces the need for separate dedicated systems and simplifies the overall manufacturing approach compared to adding specialized external modifications.

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

4Manufacturing precision

If the exterior of the cases is modified to provide tip clearance control, then tip clearance control is improved, but options are limited due to accessory mounting requirements

Engineering Contradiction:
Improvetip clearance controlVSAvoidexterior modification options
Core Design Contradiction:
Manufacturing precisionVSAdaptability or versatility

Solution Approach 1:

The cooling cavity is nested within the existing case structure, utilizing the internal volume of the case rather than modifying the exterior surface. This nested configuration provides tip clearance control functionality while preserving the external geometry required for accessory mounting. The cavity is positioned and sized to fit within the case walls without protruding or interfering with external component attachment points.

Inventive Principle:
Principle #7Nested doll (Nesting)

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 enables active cooling or heating of the compressor case, improving blade tip clearance control and system stability, and allows for thinner cavity walls that are more responsive to system dynamics, enhancing engine performance.

Implementation Method 1

a port, formed in the cavity outer wall, for directing an airflow into the cooling cavity

Methodology Applied
Scientific EffectConvection: Convection

Implementation Method 2

improving blade tip clearance control and system stability

Methodology Applied
Scientific EffectThermal expansion: Thermal Expansion

Data Source

PatentEP4431706A1Cast compressor case with a cooling cavity
Publication Date: 2024.09.18 RTX CORP
  • EP4431706A1 patent drawingFigure 1
  • EP4431706A1 patent drawingFigure 2
  • EP4431706A1 patent drawingFigure 3

AI summary

A compressor having: a case (110) with a forward annular portion (120) and an aft annular portion (140), spaced apart from each other and cast as a unitary member; a cavity forward wall (160) extending from the forward annular portion (120) to a first inner end (170); a cavity aft wall (180) extending from the aft annular portion (140) to a second inner end (190); a cavity outer wall (200) extending between the forward and aft annular portions (120, 140); a cavity inner wall (220) extending between the cavity forward and aft walls (160, 180), at or near the first and second inner ends (170, 190), a cooling cavity defined between the cavity forward, aft outer and inner walls. The compressor also has a vane stage (260) that includes a vane (270) extending from a tip (280) to a root (290), and a trunnion bearing (300) extending radially from the root (290) to a trunnion bearing outer end (310), through the inner cavity inner wall (220) and the cavity outer wall (200).