Grommet assembly for composite panels
AssigneeTridair Industries
InventorRoy Warkentin
Life of this patent
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Abstract
An assembly for installing and using a grommet in a panel of composite material for attachment to a substructure, having interposed therebetween a layer of a compressible gasket material, includes a flared grommet with a spacer disposed between the flare and the panel to protect the panel corners in the grommet flaring operation, to distribute the concentrated load imposed on the panel when the grommet end is flared, and to shim the flared end against the substructure to eliminate the imposition of an unsupported load on the panel as a fastener connecting the grommet and substructure is drawn up to secure the panel and substructure together.
Claims4
An assembly for attaching a panel of relatively brittle composite material to a substructure, separated therefrom with a layer of gasket material compressible to a maximum limit, comprising:
- (1) aligned circular holes in the panel and the substructure;
- (2) the gasket material defining a space radially around the holes and axially between the panel and the substructure;
- (3) a structural grommet disposed in the panel hole and having a radially flared end extending into the space for securing the grommet in the panel;
- (4) fastening means disposed in the grommet and the hole in the substructure for drawing the panel and substructure together and compressing the gasket material;
- (5) spacer means interposed between the panel inner face and the flared grommet end;
- and,
- (6) the spacer means and grommet end having a combined thickness in the axial direction of the space between the panel and substructure greater than the thickness of the gasket material at its limit of maximum compressibility.
Dependencies are inferred from the claim text.