Patent ID: 11867074
Assignee: ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
Field: Engines, pumps, turbines (Mechanical engineering)
Classification: CPC F | IPC F

Claim 0:
1. A gas turbine engine, comprising: having
a casing part radially delimiting a bypass channel,
an accessory gearbox arranged outside of the bypass channel,
wherein the accessory gearbox is connected to the casing part, in an adjacent connection region near the casing part and in a remote connection region remote from the casing part,
a connecting element connecting between the casing part and the remote connection region of the accessory gearbox,
wherein a longitudinal axis of the connecting element includes an angle in a range of 75° to 115° with a vertical axis of the accessory gearbox, and
the connecting element being configured to vary a distance between the remote connection region of the accessory gearbox and an attachment point of the connecting element to the casing part such that a deformation of the casing part and a resulting position change of the attachment point cause a deflection of the accessory gearbox which is less than a deflection of the accessory gearbox when there is an unchanged length of the connecting element.