Piecewise-scheduled thrust command control for in-service thrust performance improvement of gas turbine aero-engines: A hybrid fast design approach

IF 6.1 2区 工程技术 Q2 ENERGY & FUELS Applied Thermal Engineering Pub Date : 2024-10-28 DOI:10.1016/j.applthermaleng.2024.124735
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Abstract

Gas turbine aero-engines including turbofans, as the dominant powerplant for modern civil aircraft, convert the fossil energy in the jet fuel to propulsive forces via the thermo-dynamic cycle. Unfortunately, thrust regulation capabilities of gas turbine aero-engines are inevitably affected by uncertainties in measurements and gas path degradation during the life cycle, while quantification efforts for these uncertainties by traditional random analysis methods are usually considerable. In this paper, a piecewise-scheduled thrust command controller is proposed based on the improvement of the industrial baseline controller and current measurement levels, aiming at enhancing in-service thrust performance within a tolerable computational burden for engine fleets against these uncertainties. The proposed controller is equipped with a bank of embedded thrust maps for different flight cycle segments, which is fulfilled by a hybrid fast design approach incorporating a random analysis part and an analytical design part, as a new uncertainty quantification method. An industrial baseline controller with the identified thrust mode is also designed as the comparison basis. Simulations are carried out on a validated aero-thermal turbofan engine model with publically accessible uncertainty statistics. Simulation time for constructing the embedded thrust maps of the proposed controller is decreased by 99.8% on a desktop computer, compared to Monte-Carlo approach. Meanwhile, simulation results show that the proposed controller owns a bounded and tight thrust distribution for both new and severely degraded engine fleets at the take-off state within the permitted safety margin of the engine, which mitigates the significant under-thrust consequences from the baseline controller. Hence, the uncertainty control benefits of the proposed controller and its design efficiency are guaranteed.
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用于提高燃气涡轮航空发动机在役推力性能的分片计划推力指令控制:混合快速设计方法
包括涡轮风扇在内的燃气涡轮航空发动机是现代民用飞机的主要动力装置,通过热动力循环将喷气燃料中的化石能源转化为推进力。遗憾的是,燃气涡轮航空发动机的推力调节能力不可避免地会受到测量不确定性和生命周期内气路退化的影响,而采用传统随机分析方法对这些不确定性进行量化的工作量通常相当大。本文在改进工业基线控制器和当前测量水平的基础上,提出了一种片式调度推力指令控制器,目的是在发动机机队可承受的计算负担范围内,针对这些不确定性提高在役推力性能。作为一种新的不确定性量化方法,拟议的控制器配备了用于不同飞行周期段的嵌入式推力图库,该推力图库由一种混合快速设计方法实现,其中包含随机分析部分和分析设计部分。此外,还设计了具有已确定推力模式的工业基线控制器作为比较基础。仿真是在经过验证的航空热涡扇发动机模型上进行的,该模型具有可公开访问的不确定性统计数据。与蒙特卡洛方法相比,在台式计算机上构建拟议控制器嵌入式推力图的仿真时间减少了 99.8%。同时,仿真结果表明,在发动机允许的安全裕度范围内,提议的控制器对新发动机和严重退化的发动机机队在起飞状态下都能获得有界且紧密的推力分布,从而减轻了基线控制器造成的推力不足的严重后果。因此,拟议控制器的不确定性控制优势及其设计效率得到了保证。
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来源期刊
Applied Thermal Engineering
Applied Thermal Engineering 工程技术-工程:机械
CiteScore
11.30
自引率
15.60%
发文量
1474
审稿时长
57 days
期刊介绍: Applied Thermal Engineering disseminates novel research related to the design, development and demonstration of components, devices, equipment, technologies and systems involving thermal processes for the production, storage, utilization and conservation of energy, with a focus on engineering application. The journal publishes high-quality and high-impact Original Research Articles, Review Articles, Short Communications and Letters to the Editor on cutting-edge innovations in research, and recent advances or issues of interest to the thermal engineering community.
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