M3SQRD wrote I work on spacecraft composite structures for a living. So far I’ve only been able to find velocity stack and CF-to-aluminum ring (secures the velocity stack to the ITB) bonded joint failures on the Eventuri CF plenum design. It’s not surprising that the Eventuri velocity stacks have separated from the plenum due to its poorly designed bonded joint that’s subjected to primary adhesive peel loading (weakest load path for an adhesively bonded joint). Using a large blob of adhesive to create a generous radius adds zero peel strength. The metallic ring that secures to the ITB is a single lap shear joint with practically zero bond area. The CF plenum is subjected to structure-borne random vibration from the engine rpm, thermally-induced loads due to CTE mismatch as well as secondary inertial and acoustic loadings. I doubt they performed any type of dynamic analysis to predict loads and then used the predicted loads in structural analyses to show their design can withstand its structural loading environments.
Share sentiments, that with 'similar' knowledge and experience with multiple composite types and processes for both commercial and military applications [flights controls, jet engine power plant systems & more].
To produce 'relatively' complex geometries, with compound curvatures along with tight tolerancing reliably and consistently, this typically requires significant capital investment, development, and testing...meaning time & money.
[material system, process selection, inspection, prototype testing].
My take from years of development experience there's likely fundamental root causes and factors aside from material system selection...
Build Processes:
- Hand or manual lay-up - Extremely operator dependent
- Bonding - Autoclave, Resin Pressure Molding and others [compatible with/material selections]
- Nondestructive Inspection (NDI) - Proper methods, equipment, use to identify defects like cracks, voids, or material variations.
Based pics observations alone, raises questions regarding production units long-term robustness for intended operating environment, build consistency, along with likely 'workarounds' [i.e. 'random/excess' internal epoxy applications].
Certainly not bashing, since when one decides to purchase/install aftermarket components that experience dynamic loads/forces WE knowingly accept more risks than OE. These issues are by no means unique to Eventuri or similar suppliers.
And so it goes with aftermarket ==> Forces in tension...
> Speed to market
> Cost
> Quality
> 'Trade-offs'
...thoughts, comments?