US 12,110,803 B2
Aircraft turbine engine assembly comprising a support for equipment
Zoltan Zsiga, Moissy-Cramayel (FR); Valentin Sébastien Simon Avoyne, Moissy-Cramayel (FR); and Matthieu Bruno François Foglia, Moissy-Cramayel (FR)
Assigned to SAFRAN AIRCRAFT ENGINES, Paris (FR)
Appl. No. 18/568,168
Filed by SAFRAN AIRCRAFT ENGINES, Paris (FR)
PCT Filed May 27, 2022, PCT No. PCT/FR2022/051006
§ 371(c)(1), (2) Date Dec. 7, 2023,
PCT Pub. No. WO2022/258903, PCT Pub. Date Dec. 15, 2022.
Claims priority of application No. 2106094 (FR), filed on Jun. 9, 2021.
Prior Publication US 2024/0287917 A1, Aug. 29, 2024
Int. Cl. F01D 25/28 (2006.01); F01D 25/24 (2006.01); F02C 7/32 (2006.01)
CPC F01D 25/28 (2013.01) [F01D 25/24 (2013.01); F02C 7/32 (2013.01)] 12 Claims
OG exemplary drawing
 
1. An assembly for an aircraft turbomachine, comprising an intermediate casing hub, an equipment support having an upstream face located downstream of the intermediate casing hub, and a transfer gear box driving a power transmission shaft configured to transmit mechanical power, taken off an engine shaft of the turbomachine, to at least one upstream equipment item mounted on the upstream face of the equipment support, the upstream equipment item comprising a structural element attaching the equipment support to the intermediate casing hub.