Disbond Resistant Composite Stiffener Runout
AssigneeThe Boeing Company
InventorsLyle R. Deobald, Kenneth L. Brook, Timothy D. Jackson, Kenneth J. Duffie, Gregory B. Doty
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AssigneeThe Boeing Company
InventorsLyle R. Deobald, Kenneth L. Brook, Timothy D. Jackson, Kenneth J. Duffie, Gregory B. Doty
Estimating the term…
The disclosure herein provides for disbond resistant stringer runouts. Various aspects may be used independently or in combination to mitigate disbonding associated with the stiffener runout under operational loads. Aspects include a stiffener runout having rounded base flange corners. A recessed notch may be incorporated within the base flange to provide a flange termination point that is forward of the web termination point, allowing the web to terminate prior to the base flange. The web may be trimmed from a full height to a reduced height at the web termination point. The base flange may be co-bonded to the underlying composite structure via a scarf joint. Perimeter clamp radius fillers may be used to concentrate a clamping force around the perimeter of the base flange.
A method of controlling bondline separation between a composite stiffener and a composite structure, the method comprising:
A method of controlling bondline separation between a composite stiffener and a composite structure, the method comprising:
A stiffener runout, comprising:
Dependencies are inferred from the claim text.