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Method and the device which minimize the noise which is given out when taking off and landing by the rotor aircraft

机译:使旋翼飞机起降时发出的噪音最小化的方法和装置

摘要

It includes the extra stage where this method is suitable to the rotor aircraft of type of specification, can use the rotor aircraft of standard, it is done while flying the noise sensor where consecutive measurement of sound level is arranged in the rotor aircraft of the aforementioned standard vis-a-vis the aforementioned rotor aircraft (1), making use of (C) in the said stage, and noise the operating range which is smaller than maximum A-weighted sound pressure level is decided because of the rotor aircraft of the said standard. Next, the operating range which after that accompanies the calm driving point and the wind at stage, is decided because of the rotor aircraft of specification on the basis of the operating range for the rotor aircraft of the said standard. Selective figure Figure 1
机译:它包括该方法适用于规格类型的旋翼飞机的额外阶段,可以使用标准的旋翼飞机,这是在飞行噪声传感器的同时完成的,噪声传感器在上述旋翼飞机中布置了连续的声级测量相对于前述旋翼飞机(1)的标准,在所述阶段中使用(C),并且噪声的确定范围小于最大A加权声压级,这是由于旋翼飞机的说标准。接下来,基于该标准的旋翼飞机的运行范围,根据规格的旋翼飞机,确定随后伴随着平稳的驱动点和阶段风的运行范围。<选择图>图1

著录项

  • 公开/公告号JP2007530361A

    专利类型

  • 公开/公告日2007-11-01

    原文格式PDF

  • 申请/专利权人 ユーロコプテール;

    申请/专利号JP20070505573

  • 发明设计人 メルツェ;アンリ-ジャーム;

    申请日2005-03-24

  • 分类号B64C27/04;B64C37/00;B64C27/26;

  • 国家 JP

  • 入库时间 2022-08-21 21:13:08

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