Foldable Hanger for Gas Turbine Cooling Liner

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Solution Overview

Problem

Current gas turbine engine exhaust ducts require a significant amount of cooling air, leading to performance penalties, and the use of multiple individual cooling liner segments results in weight, manufacturing, and sealing inefficiencies due to redundant parts and non-desirable joints, especially in swivelable exhaust ducts with complex configurations.

Innovation Solution

A foldable attachment hanger system is used to attach a cooling liner to the exhaust duct case, allowing for reduced joints and improved sealing efficiency, weight reduction, and simplified assembly by enabling axial growth and minimizing the number of joints between cooling liner segments, which are designed to rotate through bearing systems.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If multiple individual cooling liner segments are assembled within the duct, then the cooling liner can be installed in swivelable exhaust ducts with complex configurations, but the number of joints increases leading to weight penalty, manufacturing complexity, and sealing inefficiency

Engineering Contradiction:
Improveadaptability to swivelable exhaust duct configurationsVSAvoidnumber of joints between cooling liner segments
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The exhaust duct is divided into multiple swivelable segments connected by bearing joints, allowing the duct to articulate between cruise and hover configurations. The cooling liner is correspondingly segmented to fit within each duct section, with the foldable hanger system enabling each segment to be independently installed and positioned.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The foldable attachment hanger system transitions from a folded configuration during assembly (to pass through bearing joints) to an unfolded configuration during operation (to provide structural support). This dynamic transformation reduces the number of permanent joints needed while maintaining adaptability to the swivelable duct structure.

Inventive Principle:
Principle #15Dynamics

2Adaptability or versatility

If multiple individual cooling liner segments are assembled within the duct, then the cooling liner can accommodate bearing systems, but weight and manufacturing penalty increase due to redundant parts

Engineering Contradiction:
Improveability to pass through bearing jointsVSAvoidweight of cooling liner segments and fastening hardware
Core Design Contradiction:
Adaptability or versatilityVSWeight of moving object

Solution Approach 1:

Multiple cooling liner segments are merged into a single continuous structure where possible, eliminating redundant joints and associated hardware. The foldable hanger system serves multiple functions: it provides structural support, enables thermal expansion, and facilitates assembly, replacing what would otherwise require multiple separate fastening mechanisms.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The foldable attachment hanger system performs multiple functions simultaneously: it structurally supports the cooling liner, accommodates thermal expansion, and enables the liner to pass through bearing joints during assembly. This multi-functionality eliminates the need for separate components for each function, reducing overall weight.

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

3Adaptability or versatility

If multiple individual cooling liner segments are assembled within the duct, then the cooling liner can be installed in articulated ducts, but sealing efficiency decreases due to numerous joints

Engineering Contradiction:
Improvecompatibility with articulated duct structureVSAvoidsealing efficiency between cooling liner segments
Core Design Contradiction:
Adaptability or versatilityVSReliability

Solution Approach 1:

The foldable hanger system is deployed dynamically during assembly to provide support, then folded back to create a smoother, more continuous surface. This reduces the number of permanent discontinuities in the cooling liner structure, improving sealing efficiency while maintaining compatibility with the articulated duct.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The cooling liner segments are designed with flexible sealing surfaces that can accommodate minor misalignments between segments. The foldable hanger system provides support while allowing the liner material to conform and seal effectively across joint regions, maintaining sealing integrity despite the articulated duct structure.

Inventive Principle:
Principle #30Flexible shells and thin films

4Strength

If a rigid attachment system is used to fasten cooling liner segments to the duct case, then structural support is provided, but thermal growth is constrained and assembly access is limited

Engineering Contradiction:
Improvestructural support of cooling linerVSAvoidaccess for installation and maintenance
Core Design Contradiction:
StrengthVSEase of operation

Solution Approach 1:

The attachment hanger system transitions from a folded state during assembly (providing access through bearing joints) to an unfolded state during operation (providing structural support). This dynamic configuration allows the system to satisfy both requirements at different stages without compromise.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The hanger system changes its geometric parameters (folded vs. unfolded configuration) to adapt to different operational requirements. During assembly, the folded configuration provides access; during operation, the unfolded configuration provides the necessary structural support while allowing thermal expansion.

Inventive Principle:
Principle #35Parameter changes

5Reliability

If cooling air flow is increased to maintain positive pressure in the cooling liner, then cooling effectiveness improves, but engine performance penalty increases

Engineering Contradiction:
Improvecooling liner pressure maintenanceVSAvoidengine performance penalty from extracted cooling air
Core Design Contradiction:
ReliabilityVSLoss of energy

Solution Approach 1:

The cooling liner is segmented to fit within the swivelable duct sections, allowing cooling air to be contained more effectively within the liner structure. This segmentation, combined with the foldable hanger support system, improves pressure maintenance efficiency, reducing the total cooling air flow required to maintain positive pressure.

Inventive Principle:
Principle #1Segmentation

Data Source

PatentUS7975488B2Low profile attachment hanger system for a cooling liner within a gas turbine engine swivel exhaust duct
Publication Date: 2011.07.12 RTX CORP
  • US7975488B2 patent drawing
  • US7975488B2 patent drawing
  • US7975488B2 patent drawing

AI summary

An exhaust duct assembly includes a cooling liner spaced apart from an exhaust duct case that articulate for use in a short take off vertical landing (STOVL) type of aircraft. The cooling liner assembly is attached to the exhaust duct case through a foldable attachment hanger system. The foldable attachment hanger system provides a low profile (foldable up/down) for a limited access installation envelope typical of a three bearing swivel duct (3BSD) which rotates about three bearing planes to permit transition between a cruise configuration and a hover configuration. In this way, each cooling liner segment may be formed as a complete cylindrical member requiring joints only between the swivelable duct sections.