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Gas turbine engine with differing effective perceived noise levels at differing reference points and methods for operating gas turbine engine

机译:在不同参考点处具有不同有效感知噪声水平的燃气涡轮发动机以及用于操作燃气涡轮发动机的方法

摘要

A gas turbine engine generates noise during use, and one particularly important flight condition for noise generation is take-off. A gas turbine engine has high efficiency together with low noise, in particular from the turbine that drives the fan. The contribution of the turbine noise emanating from the rear of the engine to the Effective Perceived Noise Level (EPNL) is in the range of from 7 EPNdB and 30 EPNdB lower at a take-off lateral reference point than at an approach reference point.
机译:燃气涡轮发动机在使用过程中会产生噪音,而对于产生噪音而言,一个特别重要的飞行条件就是起飞。燃气涡轮发动机具有高效率和低噪音,特别是来自驱动风扇的涡轮机。从发动机后部发出的涡轮噪声对有效感知噪声水平(EPNL)的影响在起飞侧向参考点处比在进近参考点处低7 EPNdB到30 EPNdB。

著录项

  • 公开/公告号US10590851B1

    专利类型

  • 公开/公告日2020-03-17

    原文格式PDF

  • 申请/专利权人 ROLLS-ROYCE PLC;

    申请/专利号US201916399123

  • 发明设计人 ALASTAIR D MOORE;ROBERT J TELLING;

    申请日2019-04-30

  • 分类号G01M15/14;F02C7/24;F02C7/32;F02K3/06;

  • 国家 US

  • 入库时间 2022-08-21 11:30:41

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