Variable Bleed Valve Assemblies With Acoustic Black Hole Damping
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Solution Overview
Problem
Turbine engines experience compressor instabilities and mechanical vibrations due to acoustic resonance in variable bleed valve cavities, leading to potential damage and performance issues during low-speed operations.
Innovation Solution
Incorporation of an acoustic black hole assembly within the variable bleed valve to absorb and dissipate acoustic energy, reducing resonant frequencies and vibrations in the VBV cavity.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Reliability
If the variable bleed valve cavity is closed during low-speed operations, then the valve can control bleed flow, but acoustic resonance occurs causing mechanical vibrations and potential damage
Solution Approach 1:
The patent applies the acoustic black hole principle to convert harmful acoustic resonance energy into beneficial damping effects. The ABH structure absorbs resonant acoustic waves and converts them into structural vibrations that are dissipated as heat through viscous damping in the boundary layer, thereby eliminating the harmful resonance while maintaining the valve's flow control function
Solution Approach 2:
The acoustic black hole assembly acts as an intermediary element between the acoustic field and the structural components. It mediates the interaction by absorbing acoustic energy and converting it to thermal energy through viscous dissipation, preventing the direct transmission of resonant vibrations to the compressor hardware
2Object-affected harmful factors
If the variable bleed valve cavity is open, then acoustic resonance is reduced, but bleed flow control is compromised
Solution Approach 1:
The patent segments the valve assembly into distinct functional components: the variable bleed valve door for flow control, the acoustic black hole assembly for acoustic damping, and the compressor casing for structural support. This segmentation allows the valve to operate in closed position for flow control while the ABH assembly independently manages acoustic resonance, resolving the contradiction between flow control and acoustic stability
3Object-affected harmful factors
If the acoustic black hole assembly is added to the variable bleed valve, then acoustic resonance is dampened, but device complexity increases
Solution Approach 1:
The acoustic black hole assembly is nested within the existing variable bleed valve cavity structure. The ABH structure utilizes the same spatial envelope as the valve cavity, with the porous absorber material fitted within the cavity's internal volume. This nesting approach eliminates the need for separate external damping structures, thereby limiting the increase in overall device complexity while achieving effective acoustic resonance damping
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 acoustic black hole assembly effectively dampens acoustic resonance, minimizing mechanical vibrations and preventing damage to compressor components, thereby enhancing turbine engine stability and performance.
Implementation Method 1
The ABH structure absorbs resonant acoustic waves and converts them into structural vibrations that are dissipated as heat through viscous damping in the boundary layer
Implementation Method 2
the acoustic black hole assembly effectively dampens acoustic resonance, minimizing mechanical vibrations
Data Source
AI summary
Example variable bleed valve assemblies for a gas turbine engine are disclosed herein. An example variable bleed valve assembly includes a port extending radially outward from a main flow path of the gas turbine engine, a door positioned at an exit of the port, and an acoustic black hole (ABH) assembly coupled to the door. The ABH assembly includes a body and a plurality of plates coupled to an interior surface of the body. The body defines a cavity having a depth. Each of the plurality of plates has a surface area, and the plurality of plates are arranged such that the surface areas of the plurality of plates vary along the depth in a radially outward direction of the gas turbine engine.


