B - Operations – Transporting – 64 – F
Patent
B - Operations, Transporting
64
F
B64F 5/00 (2006.01) B64C 1/14 (2006.01) B64D 43/02 (2006.01) B64D 45/00 (2006.01) G01P 5/14 (2006.01) G01P 13/02 (2006.01)
Patent
CA 2343622
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 centre (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.
Bayonne Serge
Bourgon Jean-Marc
Chauveau Bruno
Eads Airbus Sa
Goudreau Gage Dubuc
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