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Wind tunnel sting, wind tunnel sting damper, and method therefor

机译:风隧道刺,风隧道刺痛,以及其中的方法

摘要

A wind tunnel sting comprising a support member and a wind tunnel sting damper. The support member having a first support-member end configured for coupling with a wind tunnel, and a second support-member end configured for coupling with a balance. The wind tunnel sting damper having a reactive member, and a viscoelastic member disposed between the reactive member and the support member wherein, the reactive member is sized relative to the support member so as to radially compress the viscoelastic member against the support member.
机译:一种风洞钉,包括支撑构件和风洞刺痛。 具有第一支撑构件端端的支撑构件构成用于与风隧道连接,以及配置用于与平衡耦合的第二支撑构件端。 具有反应构件的风隧道测力器,以及设置在反应构件和支撑构件之间的粘弹性构件,其中,反应构件相对于支撑构件尺寸,以径向压缩粘弹性构件抵靠支撑构件。

著录项

  • 公开/公告号US11169048B2

    专利类型

  • 公开/公告日2021-11-09

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号US201916571418

  • 发明设计人 BRYAN D. MCGRANAHAN;MATHEW L. RUEGER;

    申请日2019-09-16

  • 分类号G01M9;G01M9/06;G01M9/04;G01M9/08;F16F7/10;

  • 国家 US

  • 入库时间 2022-08-24 22:08:52

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