G - Physics – 01 – F
Patent
G - Physics
01
F
G01F 23/296 (2006.01) B60K 15/06 (2006.01) B64C 3/34 (2006.01) B64D 37/02 (2006.01) H02G 3/22 (2006.01)
Patent
CA 2736578
An aircraft panel which is a wall of a fluid tank when in use, the panel comprising a skin layer with an outer surface which is an aerodynamic surface of an aircraft when in use; a hole in the skin layer; an ultrasonic gauge which is mounted to an inner surface of the skin layer adjacent to the hole in the skin layer; and an access panel which covers the hole and can be removed to gain access to the gauge.
L'invention concerne un panneau d'aéronef qui constitue une paroi de réservoir de fluide lors de l'utilisation, le panneau comprenant une couche de revêtement comportant une surface externe qui constitue une surface aérodynamique d'un aéronef lors de l'utilisation; un orifice ménagé dans la couche de revêtement; une jauge à ultrasons qui est montée sur une surface interne de la couche de revêtement adjacente à l'orifice ménagé dans la couche de revêtement; et un panneau d'accès qui recouvre l'orifice et peut être retiré afin d'accéder au dispositif de mesure.
Beale James
Pettitt Bryn
Airbus Operations Limited
Battison Williams Dupuis
LandOfFree
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