US 11,988,153 B2
Assembly for an aircraft gas turbine engine comprising an accessory gearbox
Florian Pierre-Yves Chaput, Moissy-Cramayel (FR); Fanélie Violaine Drevon, Moissy-Cramayel (FR); Thomas Marie Joseph De Dreuille De Longeville, Moissy-Cramayel (FR); and Quentin Pierre Henri Pigott, Moissy-Cramayel (FR)
Assigned to SAFRAN TRANSMISSION SYSTEMS, Colombes (FR)
Filed by SAFRAN TRANSMISSION SYSTEMS, Colombes (FR)
Filed on Jun. 24, 2022, as Appl. No. 17/848,966.
Claims priority of application No. 2106834 (FR), filed on Jun. 25, 2021.
Prior Publication US 2022/0412270 A1, Dec. 29, 2022
Int. Cl. F02C 7/36 (2006.01); F01D 25/24 (2006.01)
CPC F02C 7/36 (2013.01) [F01D 25/24 (2013.01); F05D 2260/4031 (2013.01)] 10 Claims
OG exemplary drawing
 
1. An assembly comprising:
a casing centered on a longitudinal axis and comprising an upstream portion, a central portion and a downstream portion arranged successively along the longitudinal axis;
an attachment system comprising a plurality of tie rods; and
an accessory gearbox arranged within a space delimited axially by the upstream portion and the downstream portion and radially by the central portion, the accessory gearbox being attached to the casing only by the attachment system, and the accessory gearbox being attached to only one of the upstream portion or the downstream portion.