A fan assembly of a gas turbine engine, a method for fabricating a fan assembly for a gas turbine engine, and a gas turbine engine are disclosed. The fan assembly of the gas turbine engine may include a spinner section, a fan hub section aft of the spinner section, and a joint therebetween. The fan assembly may further include a support ring for internally supporting the spinner, the support ring including a first portion facing the fan hub and a second portion connected to the spinner at the joint, wherein the connection between the second portion and the joint is a bonded connection.
BONDED MOUNT RING SPINNER
2016-10-06
Patent
Electronic Resource
English
European Patent Office | 2020
|GWLB - Gottfried Wilhelm Leibniz Bibliothek | 2017