Non-Axisymmetric Brush Seal Assembly for Flutter and Leakage
Find Innovative SolutionsGenerate Solutions
Solution Overview
Problem
Brush seals in gas turbine engines face issues with air flow leakage and self-feeding vibrations due to the axisymmetric bristle tip projection surface, leading to structural integrity problems and potential failure of the rear seal runner.
Innovation Solution
A non-axisymmetric bristle tip projection surface is designed by varying the position and width of the gap between the bristle tips and the seal land, using annular bristle packs with different thicknesses and configurations to reduce flutter and enhance sealing effectiveness.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Ease of manufacture
If an axisymmetric bristle tip projection surface is used, then the brush seal assembly is easier to manufacture, but air flow leakage and self-feeding vibrations increase
Solution Approach 1:
The patent applies asymmetry by designing a non-axisymmetric bristle tip projection surface where the bristle tips are positioned at different radial distances from the central axis. Specifically, the bristle pack includes bristles at a first radial distance and other bristles at a second radial distance that is different from the first radial distance. This asymmetric configuration disrupts the symmetric flow patterns that cause self-feeding vibrations and air leakage, thereby improving reliability while maintaining manufacturing feasibility through straightforward bristle arrangement methods.
2Reliability
If a non-axisymmetric bristle tip projection surface is used, then sealing effectiveness and structural integrity are improved, but device complexity increases
Solution Approach 1:
The patent applies local quality by creating zones with different bristle characteristics within the same bristle pack. Specifically, certain bristles are positioned at a first radial distance with specific properties while other bristles are positioned at a second radial distance with different properties. This allows localized optimization of sealing performance in different circumferential zones, improving overall reliability without requiring complete redesign of the entire seal assembly, thus limiting the increase in device complexity.
3Object-affected harmful factors
If the gap position and width are varied along the circumference, then flutter magnitude is reduced, but manufacturing precision requirements increase
Solution Approach 1:
The patent applies asymmetry to the gap configuration by positioning the gap between the bristle tips and the seal land such that the gap position and width vary circumferentially. Specifically, the gap is positioned at different locations and with different widths at different circumferential positions, creating an asymmetric flow path that disrupts flutter-inducing vibrations. This approach reduces harmful flutter magnitudes while the manufacturing precision requirements are managed through the modular bristle pack design that allows for controlled variation in gap dimensions.
Data Source
AI summary
There is disclosed a brush seal assembly including at least one annular bristle pack. The at least one annular bristle pack extends circumferentially around a central axis of the brush seal assembly. The at least one annular bristle pack has bristles extending along longitudinal axes from roots to free tips. The bristles extend toward a cylindrical plane of a the seal land. Projections of the free tips on the cylindrical plane define a bristle tip projection surface being non-axisymmetric. A method of operating a brush seal assembly is also disclosed.


