Acoustic Panel Securement for Turbine Engine Noise Reduction
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Solution Overview
Problem
Existing acoustic panels in turbomachines face challenges in securement to the fan casing, particularly in metallic and composite engines, requiring improved securement mechanisms for noise reduction while simplifying installation and repair processes.
Innovation Solution
The implementation of a securement mechanism comprising a plurality of acoustic panel members with forward and aft rails, secured by releasable fastening assemblies and threaded fasteners, allowing for circumferential and axial fixation relative to the fan casing, with optional securement rings for composite casings, facilitating easy removal and replacement of panel members.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Reliability
If acoustic panels are secured to the fan casing using traditional fastening methods, then noise mitigation is achieved, but installation and repair complexity increases
Solution Approach 1:
The acoustic panel is divided into multiple modular segments that can be independently installed and removed. Each segment contains acoustic material between forward and aft rails, allowing partial replacement without removing the entire panel assembly, thus simplifying maintenance while maintaining noise mitigation effectiveness.
Solution Approach 2:
A securement ring is introduced as an intermediary component between the acoustic panel and the fan casing. The securement ring simplifies the fastening process by providing a standardized interface with multiple apertures for fasteners, reducing installation complexity while ensuring reliable noise mitigation through stable panel positioning.
2Reliability
If acoustic panels are firmly secured to prevent movement, then noise mitigation effectiveness is maintained, but fretting damage increases
Solution Approach 1:
Padding elements are positioned between the acoustic panel and the securement ring to prevent direct metal-to-metal contact. This cushioning layer absorbs vibrations and prevents fretting damage while maintaining the panel's fixed position for effective noise mitigation.
Solution Approach 2:
The securement ring acts as an intermediary that distributes fastening forces across multiple attachment points, reducing stress concentration and preventing direct contact between the acoustic panel and the fan casing, thereby minimizing fretting damage while maintaining noise control.
3Stability of the object's composition
If multiple fasteners are used to secure acoustic panel members, then circumferential and axial stability is achieved, but manufacturing and maintenance complexity increases
Solution Approach 1:
The securement ring serves multiple functions: it provides circumferential support, axial positioning, and standardized fastening interfaces. By consolidating these functions into a single component with multiple apertures, the design achieves stability while reducing the number of separate fastening operations required.
Solution Approach 2:
The acoustic panel is segmented into modular members that can be independently secured using standardized fasteners through the securement ring. This segmentation allows for simplified manufacturing of individual components and easier maintenance through selective replacement, reducing overall complexity despite using multiple fasteners.
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 solution enhances securement, reduces manufacturing and maintenance complexities, and maintains effective noise mitigation by ensuring radial, circumferential, and axial stability of the acoustic panels, thereby reducing fretting damage and simplifying the installation and repair processes.
Implementation Method 1
acoustic material disposed therebetween
Data Source
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AI summary
An aircraft engine includes a rotating structure (28) and a casing (52a) circumferentially surrounding the rotating structure (28). The aircraft engine further includes an acoustic panel (56a) for noise reduction circumferentially surrounding the rotating structure (28). The acoustic panel (56a) is disposed proximal the casing (52a). Furthermore, the acoustic panel (56a) includes a plurality of acoustic panel members (60a). In addition, the acoustic panel (56a) is secured to the casing (52a) by at least one securement mechanism (128) such that the acoustic panel (56a) is substantially circumferentially fixed relative to the casing (52a).