| 摘要 |
<p>A core engine 9 for a gas turbine engine 10 is provided. The core engine 9 has a rotational axis 11, a casing 8, and further comprises a gearbox assembly 25, a radial drive arrangement 64, pipes and connections 32 and a connection structure 7. The radial drive arrangement 64 drivingly connects the core engine 9 to the gear box assembly 25, the pipes and connections 32 extend from the gearbox 25 to the core engine 9 and the gearbox 25 is radially spaced from the casing 8 by the connection structure 7. A method of assembling the gas turbine engine 10 comprises the steps of axially translating the core engine 9 and the fan casing 22 so that the gearbox 25 is adjacent the fan casing 22 and attaching the gearbox assembly 25 to the fan casing 22.</p> |
