Apparatus for monitoring an aircraft flap and application of a dynamometric rod
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United States of America Patent
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Nov 27, 2007
Grant Date -
Jun 1, 2006
app pub date -
Jul 15, 2003
filing date -
Jul 16, 2002
priority date (Note) -
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status (Latency Note)
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Abstract
A dynamometric rod intended to form a pivot for fixing an aircraft wing flap, includes a cylindrical body (10) with a hexagonal head (12) and a threaded end-piece (14). The dimensions and other characteristics of the body (10), head (12) and end-piece (14) correspond to those of pivots normally used for fixing wing flaps. The aforementioned body (10) is provided with a groove (16) which can be provided with a small depth of several tenths of a millimetre and which forms a simple gap which prevents contact between a branch of a clamp or an arm of the flap and the rod at the groove (16). In addition, a sensitive element (18) is positioned at the groove and is very tightly sealed closed. The invention is suitable for aircraft flaps.
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