H2020Individual fellowship2021–2023

BRAVO · Establishing Blend Repair limit of blisks –from A perspective of Vibration amplificatiOn

Horizon 2020 — Marie Skłodowska-Curie Actions

Duration
2021-03-15 → 2023-04-30
EU contribution
€183,473
Participants
1
Scheme
MSCA-IF

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Results in brief

Establishing Blend Repair limit of blisks –from A perspective of Vibration amplificatiOn

Blisks are extensively used in the fan/compressor sections of advanced aeroengines, due to their reduced-weight and increased-performance benefits. However, they also suffer from notorious disadvantages of technical difficulty and high cost arising from the repair process if inevitable blade damages in service occur, e.g., foreign object damages and wear, etc. Efficient sustainment of the extremely expensive blisks requires that damaged blades can be cost-effectively repaired by blending operations with high reliability. Structural dynamics evaluations for the repaired blisks are of significant importance to ensure continued safe operation with minimal risk of failure. However, currently limited understanding of blending effects on the structural dynamics of blisks challenges the rational determination of blend limits, i.e., the maximum allowable blend size, location and number in a damaged blisk. One of the principal reasons is that blisks are susceptible to high-level blade vibration due to inevitable blade mistuning. Blade mistuning arises primarily from the scatters of blade geometry profiles due to manufacturing tolerance. Moreover, blend repairs of the blades during maintenance can also induce relatively large geometry variances. The underlying fundamental issue is whether or not the blends will exacerbate the intrinsic geometric mistuning such that the blisk is subject to excessive vibration level and fails from high cycle fatigue. In fact, the accurate modelling and dynamic analysis of geometrically mistuned blisks has been a long-standing issue in both the academic and industrial communities. In pursuit of an improved blade geometric mistuning evaluation capability, the BRAVO project focuses on development of the high-fidelity dynamic modeling, analysis and experimental verification techniques specifically for blisks with both intrinsic small geometry mistuning and blend repairs, based on the state-of-the-art 3D optical geometry scanning technology. The BRAVO project aims to develop a comprehensive vibration evaluation tool for industrial designers to predict the risks and benefits of possible blend repairs within damaged blisks. A parallel goal of the MSCA Individual Fellowship is to enhance the fellow’s professional maturity and scientific independence as a research group leader.

Data: CORDIS, © European Union

Project objective

Efficient sustainment of the extremely expensive blisks in advanced aeroengines requires that damaged blades can be cost-effectively repaired by blending operations with high reliability. However, limited understanding of blending effects on the forced response of blisks challenges the rational determination of blend limits, i.e., the maximum allowable blend size, location and number in a damaged blisk. The underlying fundamental issue is whether or not the blends will exacerbate the intrinsic geometric mistuning such that the blisk is subject to excessive vibration level and fails from high cycle fatigue.The project BRAVO aims to develop a comprehensive vibration evaluation tool for blended blisks and establish the repair philosophy on blend limits. By employing the state-of-the-art 3D optical geometry scanning technology, geometry variances due to both blends and intrinsic blade geometric deviations can be effectively accounted for. Major scientific advances include:Novel deterministic methodologies of forced response analysis for blended blisks relying on the optically based as-measured model.Holistic vibration evaluation of blended blisks by comparing the as-measured-model-based simulations, modal tests, bench test under traveling wave excitation and spinning rig tests.Innovative probabilistic assessment for predictive evaluation of a population of possible blends and further determination of a tailored blend limit for a damaged blisk.A highly interdisciplinary collaboration will benefit both the ER with extensive experience in bladed disk dynamics, and the supervisor possessing top-level research capability in blade vibration testing. With deepened competence in both technical and transferable skills, the ER will reach a high level of professional maturity and scientific independence as a group leader. Results will potentially exert a strong industrial impact for repair contractors, contributing to the competitiveness of European aviation industry.

Original text from CORDIS.

Participants

  • POLITECNICO DI TORINO · TorinoCoordinatorItaly

Links

Data: CORDIS, © European Union