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DESIGN AND ANALYSIS OF A NEW ACCESSORY GEARBOX HOUSING FOR A GAS TURBINE ENGINE

机译:新型燃气轮机附件箱的设计与分析

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Accessory Gearbox (AGB) Housing is one of the most critical components of a gas turbine engine that lies between the core engine & the aircraft. The function of the AGB Housing is to provide support for the gear drive assembly that transfers power from the engine to the engine accessories and to the power takeoff drive for the aircraft accessories. The housing also functions as an oil tight container and passageway for lubrication. In addition, the AGB housing provides mount points to attach engine/aircraft support accessories, including the engine mount points to the aircraft. The complexity in predicting AGB housing behavior under the gear loading, engine loading and engine induced vibration is one of the main challenges of designing a new gearbox with minimum weight. To address these issues, the current paper presents for the first time the design-analysis of a new lightweight AGB housing for a turboshaft engine, based on the following three major requirements: i) gear bearing pads strength & stiffness capability, ii) AGB mount pads (for accessories and for engine) load carrying capability, and, iii) vibratory response (mainly high cycle fatigue (HCF) response) of the AGB housing. A 3-D Finite Element Analysis (FEA) model of the AGB housing was developed using the proposed initial design. Various design modifications, involving several interrelated, iterative steps, were then carried out by adjusting and modifying the housing wall thickness, placement & sizes of internal ribs and external gussets, including additional geometric modifications to satisfy the design objectives. The result is a robust, lightweight AGB housing design, eliminating the need for some of the required testing for the qualification of the new gearbox, indicating a significant cost savings. This paper also discusses in detail the methodology for the gear bearing pad strength/stiffness calculation, the FEA modeling techniques for the application of mount loads and gear bearing loads under operating & flight maneuver conditions, and, a methodology for addressing a combined HCF & LCF (Low Cycle Fatigue) response of the housing.
机译:附件变速箱(AGB)外壳是位于核心发动机和飞机之间的燃气涡轮发动机的最关键组件之一。 AGB机壳的功能是为齿轮传动组件提供支撑,该组件将动力从发动机传递到发动机附件以及飞机附件的动力输出驱动器。外壳还用作油密容器和润滑通道。此外,AGB机壳提供了安装点,可将发动机/飞机支撑配件(包括发动机安装点)安装到飞机上。在齿轮载荷,发动机载荷和发动机引起的振动下预测AGB壳体性能的复杂性是设计重量最小的新型变速箱的主要挑战之一。为了解决这些问题,本论文首次提出了基于以下三个主要要求的用于涡轮轴发动机的新型轻质AGB壳体的设计分析:i)齿轮垫的强度和刚度能力; ii)AGB安装垫(用于附件和发动机)的承载能力,以及iii)AGB外壳的振动响应(主要是高周疲劳(HCF)响应)。使用建议的初始设计开发了AGB外壳的3-D有限元分析(FEA)模型。然后,通过调整和修改外壳的壁厚,内部肋骨和外部角撑板的位置和尺寸,进行涉及多个相互关联的迭代步骤的各种设计修改,包括满足设计目标的其他几何修改。结果是坚固,轻巧的AGB外壳设计,消除了对新变速箱鉴定进行某些必要测试的需要,从而显着节省了成本。本文还详细讨论了齿轮轴承瓦块强度/刚度计算的方法,在操作和飞行操纵条件下施加安装载荷和齿轮轴承载荷的FEA建模技术以及解决HCF和LCF组合问题的方法(低周疲劳)外壳的响应。

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