US 12,258,996 B2
Probe fastening system and aircraft
Pasquale Mauro, Augsburg (DE)
Assigned to Premium Aerotec GmbH, Augsburg (DE)
Filed by Premium Aerotec GmbH, Augsburg (DE)
Filed on Oct. 6, 2023, as Appl. No. 18/377,495.
Application 18/377,495 is a division of application No. 16/207,668, filed on Dec. 3, 2018, granted, now 11,781,574, issued on Oct. 10, 2023.
Claims priority of application No. 10 2017 222 185.2 (DE), filed on Dec. 7, 2017.
Prior Publication US 2024/0044350 A1, Feb. 8, 2024
Int. Cl. F16B 5/02 (2006.01); F16B 5/00 (2006.01); B64D 43/00 (2006.01)
CPC F16B 5/025 (2013.01) [F16B 5/0088 (2013.01); B64D 43/00 (2013.01); F16B 2200/69 (2023.08); Y10T 403/1624 (2015.01)] 9 Claims
OG exemplary drawing
 
1. 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.