| 摘要 |
<p>A pylon structure (66) for mounting an engine (10) to an aircraft, characterised in that the pylon structure (66) is split into a mount beam (68) and a stub pylon (73), the mount beam (68) is a part of the engine and the stub pylon (73) is part of the aircraft. The advantage of the present invention is to facilitate easier assembly and disassembly of the engine to the aircraft.</p> |
