A gas turbine engine according to an example of the present disclosure includes a mount arrangement including a gas turbine engine, an adapter ring extending circumferentially around the gas turbine engine and mounted to both the gas turbine engine and to an aircraft beneath the gas turbine engine, and at least one thrust link including a first end mounted to the gas turbine engine fore of the adapter ring, and an opposite second end mounted to the adapter ring above the gas turbine engine.
ADAPTER RING FOR ABOVE-WING MOUNTING OF BELOW-WING ENGINE
2019-01-31
Patent
Electronic Resource
English
ADAPTER RING FOR ABOVE-WING MOUNTING OF BELOW-WING ENGINE
European Patent Office | 2021
|