Segmented link members eliminate preload requirements by absorbing assembly tolerances while maintaining structural redundancy.
Engine attachment uses a single end fitting with a stop ring to secure the mounting pin.
Positioning hydrogen fuel pipes inside structural tubes minimizes pylon cross sections and improves aerodynamic performance.
Radial centering features on bushings align the through-axle to prevent damage during installation of turbine engine suspension systems.
Continuous warp yarns form arcuate portions in multilayer woven composites, distributing mechanical forces to enhance strength without adding weight.
Intermediary wearing parts absorb contact forces between connecting rods and yoke walls to control tilting and prevent structural wear.
Distributed bolt row reduces secondary moments and bulk, enabling closer pylon positioning to wing box.
An integrated afterbody mount case with radial spokes connects the nacelle to the pylon.
A pivotable shackle assembly with linked components adjusts geometry to maintain equal load distribution across engine case lugs.