Invention Grant
- Patent Title: Wind tunnel balance and system with wing model and wind tunnel balance
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Application No.: US14326885Application Date: 2014-07-09
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Publication No.: US09606019B2Publication Date: 2017-03-28
- Inventor: Michael Kordt
- Applicant: Airbus Operations (GmbH
- Applicant Address: DE Hamburg
- Assignee: Airbus Operations GmbH
- Current Assignee: Airbus Operations GmbH
- Current Assignee Address: DE Hamburg
- Agency: Greer, Burns & Crain Ltd.
- Priority: DE102013213675 20130712
- Main IPC: G01M9/00
- IPC: G01M9/00 ; G01M9/04 ; G01M9/06 ; G01L5/16

Abstract:
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.
Public/Granted literature
- US20150013445A1 WIND TUNNEL BALANCE AND SYSTEM WITH WING MODEL AND WIND TUNNEL BALANCE Public/Granted day:2015-01-15
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