Device for pressure tapping and procedure for setting it on a fuselage panel of an aircraft
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United States of America Patent
Stats
-
Sep 3, 2002
Grant Date -
Oct 18, 2001
app pub date -
Mar 20, 2001
filing date -
Apr 14, 2000
priority date (Note) -
In Force
status (Latency Note)
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Abstract
Device for pressure tapping, integrated into the fuselage of an aircraft, comprising an integrated plate (10), without discontinuity, with a pressure tapping part in the center (16). The plate (10) enters a supplementary opening (22) formed in a fuselage panel (20). The plate (10) and the panel part (20) surrounding the opening (22) are fixed on a supporting element (18) linked to the framework of the aircraft (34, 36). In the case where rivet, screw or bolt type fixations are used, they are placed at the edge of the plate (10). This arrangement facilitates assembly and improves the precision of the measurement, by suppressing any discontinuity in the measurement zone.
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