US 12,337,979 B2
Engine pylon for fastening an aircraft engine
Michael Berjot, Toulouse (FR); Pierre-Antoine Combes, Toulouse (FR); Marc De Nicola, Toulouse (FR); and Jean-Baptiste Vignes, Toulouse (FR)
Assigned to Airbus Operations SAS, Toulouse (FR)
Filed by Airbus Operations SAS, Toulouse (FR)
Filed on Apr. 4, 2024, as Appl. No. 18/626,575.
Claims priority of application No. 2303417 (FR), filed on Apr. 6, 2023.
Prior Publication US 2024/0336365 A1, Oct. 10, 2024
Int. Cl. B64D 27/40 (2024.01)
CPC B64D 27/402 (2024.01) 6 Claims
OG exemplary drawing
 
1. An engine pylon for fastening an engine of an aircraft, the engine pylon having:
a structure configured to be fastened beneath a wing of the aircraft and having two lateral faces, wherein the structure has a tunnel with two ends passing therethrough, wherein each of the two ends of the tunnel emerges at one of the two lateral faces,
a spreader housed in the tunnel and fastened in an articulated manner to each lateral face by a first connection point, wherein a first end of the spreader has a first bore, and wherein a second end of the spreader has two second bores each configured to form a second connection point with the engine, and
a rod fastened in an articulated manner to said first bore and having two third bores each configured to form a third connection point with the engine.