Within previous EU projects, possible modifications to the engine components have been investigated, that would allow for an optimised aerodynamic or acoustic design of the EGV （exit guide vanes） of the TEC （turbin...Within previous EU projects, possible modifications to the engine components have been investigated, that would allow for an optimised aerodynamic or acoustic design of the EGV （exit guide vanes） of the TEC （turbine exit casing）. However, the engine weight should not be increased and the aerodynamic performance must be at least the same. This paper compares the sound power level of a state-of-the-art TEC （reference TEC） with typical EGVs with an aerodynamically optimised TEC configuration for the engine operating point approach. It is shown that a significant weight reduction （only bladings considered） and reduction in engine length can be achieved but the sound power level for the fundamental tone （lst blade passing frequency） for this acoustically important operating point is increased. It is also shown that the losses of the aerodynamical optimised EGVs are higher for this off design point but significantly lower at the aero design point. Measurements were conducted in the STTF （subsonic test turbine facility） at the Institute for Thermal Turbo machinery and Machine Dynamics, Graz University of Technology. The inlet guide vanes, the LPT （low pressure turbine） stage, and the EGVs have been designed by MTU Aero Engines.展开更多
以双层隔振系统为研究对象,建立双层隔振系统的三维有限元模型。在给定的刚度范围内,单独改变设备隔振器刚度值或者底座隔振器刚度值时发现,任意一层隔振器刚度的变化对各级隔振均产生一定的影响。从底座隔振器与设备隔振器刚度比的角...以双层隔振系统为研究对象,建立双层隔振系统的三维有限元模型。在给定的刚度范围内,单独改变设备隔振器刚度值或者底座隔振器刚度值时发现,任意一层隔振器刚度的变化对各级隔振均产生一定的影响。从底座隔振器与设备隔振器刚度比的角度出发,对两层隔振器的刚度进行适配,研究结果表明:在刚度适配时,可能出现振动传递过程中振动放大的情况;当刚度比相同时,在刚度值较小的工况下传递到底座上的振动加速度级比刚度值较大的工况小,同时其整体隔振效果也更好;在所计算的工况中,最优刚度适配工况下的整体隔振效果比最差刚度适配工况提高9.8 dB,传递到底座的振动加速度级降低12.3 d B,辐射声功率级总值降低12.8 dB。展开更多
文摘Within previous EU projects, possible modifications to the engine components have been investigated, that would allow for an optimised aerodynamic or acoustic design of the EGV （exit guide vanes） of the TEC （turbine exit casing）. However, the engine weight should not be increased and the aerodynamic performance must be at least the same. This paper compares the sound power level of a state-of-the-art TEC （reference TEC） with typical EGVs with an aerodynamically optimised TEC configuration for the engine operating point approach. It is shown that a significant weight reduction （only bladings considered） and reduction in engine length can be achieved but the sound power level for the fundamental tone （lst blade passing frequency） for this acoustically important operating point is increased. It is also shown that the losses of the aerodynamical optimised EGVs are higher for this off design point but significantly lower at the aero design point. Measurements were conducted in the STTF （subsonic test turbine facility） at the Institute for Thermal Turbo machinery and Machine Dynamics, Graz University of Technology. The inlet guide vanes, the LPT （low pressure turbine） stage, and the EGVs have been designed by MTU Aero Engines.
文摘以双层隔振系统为研究对象,建立双层隔振系统的三维有限元模型。在给定的刚度范围内,单独改变设备隔振器刚度值或者底座隔振器刚度值时发现,任意一层隔振器刚度的变化对各级隔振均产生一定的影响。从底座隔振器与设备隔振器刚度比的角度出发,对两层隔振器的刚度进行适配,研究结果表明:在刚度适配时,可能出现振动传递过程中振动放大的情况;当刚度比相同时,在刚度值较小的工况下传递到底座上的振动加速度级比刚度值较大的工况小,同时其整体隔振效果也更好;在所计算的工况中,最优刚度适配工况下的整体隔振效果比最差刚度适配工况提高9.8 dB,传递到底座的振动加速度级降低12.3 d B,辐射声功率级总值降低12.8 dB。
