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Identify the actual hinge, stop contact and connected load path.

Hinged Carbon Fiber Panels: Keep the Opening Stop Load in the Assembly Review

A hinged panel’s opening stop determines where movement is arrested. Show how that stop force passes through the hardware and supporting structure. A carbon fiber skin should not be assumed to carry an unspecified stop load simply because it closes the opening.

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Attached mass locations belong in an assembly centre-of-gravity review.

Carbon Fiber Tube Assemblies: Total Mass Does Not Locate the Centre of Gravity

A tube assembly’s total mass does not identify where that mass acts. Fittings and attached equipment can move the centre of gravity even when the bare tube stays unchanged. Include the complete installed configuration when balance or support reactions matter to the application.

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Conceptual CT acquisition geometry only; no equipment capability or settings are specified.

X-Ray CT of Composite Parts: Define the Inspection Objective and Limits

X-ray computed tomography can reconstruct three-dimensional information from radiographic data, but the usable inspection result depends on the component and setup. Specify the inspection objective, assessed region and reporting basis. A detailed-looking volume image is not automatic proof that every defect or dimension has been resolved.

X-Ray CT of Composite Parts: Define the Inspection Objective and Limits Читать далее "