Probe fastening system and aircraft
AssigneePremium Aerotec GmbH
InventorPasquale Mauro
Life of this patent
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Abstract
A probe fastening system has a plate having at least one coupling-on recess and having at least one alignment element, which is arranged in the outer region of the plate, a backplate which has a fastening device for the fastening of a static probe and at least one recess which corresponds with the alignment element, at least one peelable shim which corresponds with the alignment element and which is arranged between the plate and the backplate, at least one alignment device which corresponds with the alignment element, and a coupling-on element which defines a cavity and which is designed for isobarically coupling the static probe onto the coupling-on recess.
Claims9
A probe fastening system, comprising:
- a plate having at least one coupling-on recess and having a plurality of alignment elements arranged in an outer region of the plate, wherein the plurality of alignment elements comprises a plurality of protrusions integrally formed with the plate;
- a backplate having a fastening device for the fastening of a static probe and a plurality of recesses corresponding with the plurality of alignment elements;
- a plurality of peelable shims corresponding with the plurality of alignment elements and arranged between the plate and the backplate;
- a plurality of alignment devices corresponding with the plurality of alignment elements;
- and
- a coupling-on element defining a cavity and configured for isobarically coupling the static probe onto the coupling-on recess;
- wherein each of the plurality of alignment elements comprises an external thread;
- and each of the plurality of alignment devices comprises a nut with an internal thread adapted to the external thread of a respective one of the plurality of alignment elements.
Dependencies are inferred from the claim text.