- 专利标题: Wind tunnel balance and system with wing model and wind tunnel balance
-
申请号: US14326885申请日: 2014-07-09
-
公开(公告)号: US09606019B2公开(公告)日: 2017-03-28
- 发明人: Michael Kordt
- 申请人: Airbus Operations (GmbH
- 申请人地址: DE Hamburg
- 专利权人: Airbus Operations GmbH
- 当前专利权人: Airbus Operations GmbH
- 当前专利权人地址: DE Hamburg
- 代理机构: Greer, Burns & Crain Ltd.
- 优先权: DE102013213675 20130712
- 主分类号: G01M9/00
- IPC分类号: G01M9/00 ; G01M9/04 ; G01M9/06 ; G01L5/16
摘要:
A wind tunnel balance, with a tunnel wall adaptor configured to fasten the wind tunnel balance to a wall of a wind tunnel, an actuator housing connected to the tunnel wall adaptor, a plurality of force sensors arranged between the actuator housing and the tunnel wall adaptor and which are configured to detect forces acting on the actuator housing, a pivot coupling, by means of which an airfoil model of an aircraft can be pivotably coupled to the actuator housing, and a plurality of piezoelectric actuators arranged in the actuator housing and which are configured to controllably deflect an airfoil model mounted on the pivot coupling in three spatial directions.
公开/授权文献
信息查询