首页> 外国专利> DEVICE CONTAINING A REACTION REVERSOR AND THE DRIVE SYSTEM OF THE SPECIFIED REACTION REVERSOR

DEVICE CONTAINING A REACTION REVERSOR AND THE DRIVE SYSTEM OF THE SPECIFIED REACTION REVERSOR

机译:包含反作用器的装置和特定反作用器的驱动系统

摘要

1. A device comprising a thrust reverser (20) and a drive system of said thrust reverser (20), wherein said thrust reverser (20) includes at least one hood (30) linearly moving in a direction substantially parallel to the longitudinal axis nacelles alternately between the closed position in which it provides aerodynamic continuity of the nacelle and the open position in which it opens a passage for the deflected flow in the nacelle, said hood (30) being extended by at least one section of the adjustable nozzle (40), neighing at least one panel (41), mounted to rotate at least one position at which the nozzle cross-section changes, while this system contains drive means (60) that provide linear and rotary movement of these hoods (30), respectively and a panel (41) of the nozzle (40), wherein the device is characterized by the presence of downstream fixation means (80) of the nozzle (40) and hood (30), and the downstream fixation means (80) have at least two reversible states, one of which is pre represents a closed state in which the downstream fixation means (80) can fix the nozzle panel (41) (40) with the hood (30) in the position of changing the nozzle exit section. 2. The device according to claim 1, characterized in that in the forward thrust mode and at the stages of changing the nozzle section (40), the downstream fixation means (80) are in the open state, while in the reverse thrust mode, the downstream means (80) are in the closed state, allowing the nozzle (40) to move together with the hood (30) relative to the nacelle in the downward direction along �
机译:1.一种包括反推力器(20)和所述反推力器(20)的驱动系统的装置,其中,所述反推力器(20)包括至少一个罩(30),所述罩在基本上平行于纵向轴线机舱的方向上线性地移动。在其提供机舱的空气动力学连续性的关闭位置和其为机舱中的偏转流打开通道的打开位置之间交替进行,所述罩(30)由可调喷嘴(40)的至少一个部分延伸。 ),至少与一个面板(41)相邻,该面板安装成旋转喷嘴横截面变化的至少一个位置,而该系统包含驱动装置(60),该驱动装置分别提供这些罩(30)的线性和旋转运动。喷嘴(40)的面板(41),其中该装置的特征在于喷嘴(40)和罩(30)的下游固定装置(80)的存在,并且下游固定装置(80)具有至少两个可逆状态,其中之一ch为闭合状态,下游固定装置(80)可利用罩(30)将喷嘴板(41)(40)固定在改变喷嘴出口部的位置。 2.根据权利要求1所述的装置,其特征在于,在正向推力模式中和在改变喷嘴部分(40)的阶段,下游固定装置(80)处于打开状态,而在反向推力模式中,下游装置(80)处于关闭状态,使喷嘴(40)与发动机罩(30)一起相对于机舱沿向下方向移动。

著录项

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号