Open-channel stiffener

Patent metadata

Field	Value
Publication number	US-10220935-B2
Application number	US-201615264324-A
Country	US
Kind code	B2
Filing date	Sep 13, 2016
Priority date	Sep 13, 2016
Publication date	Mar 5, 2019
Grant date	Mar 5, 2019

Abstract

An open-channel stiffener for stiffening a panel has a bonding flange for bonding the stiffener to the panel through a bondline formed between the bonding flange and the panel to form a stiffened panel. The open-channel stiffener has a cross-sectional shape that aligns, or substantially aligns, a shear center of the stiffener with a centroid of the stiffener and aligns the shear center proximate an edge of the bondline, and removes the need for a radius filler noodle. A plurality of perforations may be formed through the bonding flange to permit an adhesive to wick into the perforations and create a mechanical interlock between the bonding flange and the panel.

First claim

The invention claimed is:

1. An open-channel stiffener for stiffening a panel, the open-channel stiffener comprising a bonding flange having a width defined by two longitudinal edges for bonding the stiffener to the panel through a bondline formed between the bonding flange and the panel, the stiffener having a cross-sectional shape comprising a curved connector portion extending from one of the longitudinal edges and a web extending from the curved connector portion, the web positioned over the bondline and the curved connector portion positioned to extend beyond an edge of the bondline, and the cross-sectional shape is configured to substantially align a shear center of the stiffener with a centroid of the stiffener and to align the shear center proximate the edge of the bondline.

2. The stiffener of claim 1 , further comprising a plurality of perforations through the bonding flange that permit an adhesive to wick into the perforations to create a mechanical interlock between the bonding flange and the panel.

3. The stiffener of claim 2 , further comprising a plurality of raised areas that create a texture on a bonding surface of the bonding flange to provide a flow path for an adhesive between the bonding flange and the panel.

4. The stiffener of claim 2 , wherein the plurality of perforations have a larger diameter opening on a top surface of the bonding flange and a smaller diameter opening on a bonding surface of the bonding flange.

5. The stiffener of claim 1 , wherein the cross-sectional shape of the stiffener further comprises a cap positioned generally parallel to the bonding flange and over the bondline, the web positioned between and generally perpendicular to the cap and the bonding flange, and a second curved connector portion extending between the cap and the web.

6. The stiffener of claim 5 , wherein the second curved connector portion is positioned to extend beyond the edge of the bondline.

7. The stiffener of claim 1 , wherein the stiffener is comprised of a thermoplastic or thermoset material.

8. The stiffener of claim 1 , wherein the cross-sectional shape of the stiffener further comprises a cap positioned generally parallel to the bonding flange and over the bondline, the web positioned between and at an acute angle relative to the bonding flange and the cap, and a second curved connector portion extending between the cap and the web.

9. The stiffener of claim 1 , wherein the web comprises a curved web and the curved connector portion having a radius smaller than a radius of the curved web.

10. A stiffened panel comprising an open-channel stiffener bonded to a panel, the open-channel stiffener comprising a bonding flange having a width defined by two longitudinal edges for bonding the stiffener to the panel through a bondline formed between the bonding flange and the panel, the stiffener having a cross-sectional shape comprising a curved connector portion extending from one of the longitudinal edges and a web extending from the curved connector portion, the web positioned over the bondline and the curved connector portion positioned to extend beyond an edge of the bondline, and the cross-sectional shape is configured to substantially align a shear center of the stiffener with a centroid of the stiffener and to align the shear center proximate the edge of the bondline.

11. The stiffened panel of claim 10 , wherein the bonding flange has a plurality of perforations that permit an adhesive to wick into the perforations to create a mechanical interlock between the bonding flange and the panel.

12. The stiffened panel of claim 10 , wherein the cross-sectional shape of the stiffener further comprises a cap positioned generally parallel to the bonding flange, the web positioned between and generally perpendicular to the cap and the bonding flange, and a second curved connector portion extending between the cap and the web.

13. The stiffened panel of claim 12 , wherein the second curved connector portion is positioned to extend beyond the edge of the bondline.

14. A method of stiffening a panel, comprising the steps of:
forming an open-channel stiffener comprising a bonding flange having a width defined by two longitudinal edges for bonding the stiffener to the panel through a bondline formed between the bonding flange and the panel, the stiffener having a cross-sectional shape comprising a curved connector portion extending from one of the longitudinal edges and a web extending from the curved connector portion, the web positioned over the bondline and the curved connector portion positioned to extend beyond an edge of the bondline, and configuring the cross-sectional shape to substantially align a shear center of the stiffener with a centroid of the stiffener and to align the shear center proximate the edge of the bondline; and
bonding the bonding flange of the stiffener to the panel.

15. The method of claim 14 , further comprising the step of forming a plurality of perforations through the bonding flange; and wherein the bonding step comprises applying adhesive on a top surface of the bonding flange such that the adhesive flows through the perforations and into the bondline to create a mechanical interlock between the bonding flange and the panel.

16. The method of claim 14 , further comprising the step of forming a plurality of raised areas that create a texture on a bonding surface of the bonding flange or the panel to provide a flow path for an adhesive between the bonding flange and the panel.

17. The method of claim 14 , wherein the step of forming the stiffener further comprises positioning a cap generally parallel to the bonding flange, positioning the web between and generally perpendicular to the cap and the bonding flange, and a second curved connector portions extending between the cap and the web.

18. The method of claim 17 , further comprising positioning the second curved connector portion to extend beyond the edge of the bondline.

19. The method of claim 14 , further comprising preparing a bonding surface of the bonding flange prior to bonding the bonding flange to the panel with one or more surface treatments selected from the group consisting of grit blasting, sanding, plasma etching, laser ablation and peel ply.

Assignees

• Boeing Co

Inventors

• Deobald Lyle R
• Dilligan Matthew A
• Rinn Aaron N
• Ramnath Madhavadas

Classifications

• B29L2031/3076

  Aircrafts (blades, propellers B29L2031/08) · CPC title

• B29C66/0224

  with removal of material · CPC title

• B64C3/185

  Spars · CPC title

• B29C66/474

  said single elements being substantially non-flat · CPC title

• B64C3/26 Primary

  Construction, shape, or attachment of separate skins, e.g. panels · CPC title