Method for producing a closed-section portion of an aircraft provided with deformation sensors
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United States of America Patent
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Jul 26, 2016
Grant Date -
Jun 5, 2014
app pub date -
Jun 6, 2013
filing date -
Jun 11, 2012
priority date (Note) -
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status (Latency Note)
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Abstract
A method for producing a closed-section portion of an aircraft wherein a strain gauge is glued on a first face of a flat tape that, in turn, is fastened on a face of a tool comprising a rigid elongated body covered by an extensible sack. The tool supporting the tape is arranged in a cavity of an aircraft structure. A vacuum is then created to obtain the expansion of the vacuum sack and perform the pressure gluing of the tape onto a wall of said cavity. The tool is subsequently extracted from the cavity. Upon conclusion of these operations, the tape is integrally fastened onto a wall of the cavity so that any deformation applied to this wall is transmitted to said strain gauge.
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