Joints for composite laminated panels and beams
AssigneeB/E Aerospace, Inc.
InventorMark R. Gurvich
Life of this patent
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Abstract
A joint for use with a composite laminated component is disclosed herein. The joint includes a component including a partial U-shaped trapezoidal cavity and a triangular component. The partial trapezoidal component includes a base extending in a first direction, a first side extending away from the base at a first angle from the first direction, a second side extending away from the base at a second angle from the first direction and toward the first side, and an opening defined by the first side and the second side. The triangular component is coupled to the base and extending orthogonally away from the base in a second direction and toward the opening.
Claims8
A system of interlocked components, comprising:
- a composite component including a first portion, a second portion, and a finite-length edge split between the first portion and the second portion;
- and
- a joint including:
- a component including a partial U-shaped trapezoidal cavity, including:
- a base extending in a first direction;
- a first side extending away from the base at a first angle from the first direction;
- a second side extending away from the base at a second angle from the first direction and toward the first side;
- and
- an opening defined by the first side and the second side and configured to receive the composite component;
- and
- a triangular component integral with the base and extending orthogonally away from the base in a second direction toward the opening, the triangular component configured to insert into the split.
Dependencies are inferred from the claim text.