Structural systems with improved sidelap and buckling spans

Patent metadata

Field	Value
Publication number	US-10808403-B2
Application number	US-201916532145-A
Country	US
Kind code	B2
Filing date	Aug 5, 2019
Priority date	Mar 21, 2016
Publication date	Oct 20, 2020
Grant date	Oct 20, 2020

Abstract

The invention relates to structural panel systems which utilize different configurations to increase the flexibility of the panel systems. The increased flexibility of the panel systems may be achieved through the use of improved connection patterns and/or improved sidelap strength. The improved sidelap strength may be achieved through the use of a reinforcing member between edges of the panels or other sidelap configurations that improve the strength of the system along the sidelaps. The increased flexibility may also be achieved through the use of orienting flutes of the panels in the same direction as the supports members of the panel systems. The different aspects of the invention that improve the flexibility of the systems may be utilized alone or in combination with each other to improve the wall panel systems or roof panel systems, or combinations thereof, to improve the displacement capacity of the panel systems for in-plane shear loading.

First claim

What is claimed is:

1. A method of forming a structural panel system, comprising:
assembling a first panel and a second panel to a support structure, wherein:
the first panel comprising first flutes, opposing ends, and opposing edges comprising at least a first edge;
the second panel comprising second flutes, opposing ends, and opposing edges comprising at least a second edge;
the support structure comprises:
a first support member;
a second support member;
one or more intermediate support members, wherein the first support member, the second support member, and the one or more intermediate support members are generally parallel with each other;
a third support member; and
a fourth support member;
wherein the third support member and the fourth support member are oriented generally perpendicular to and operatively coupled to opposing ends of the first support member, the second support member, and the one or more intermediate support members; and

wherein the first flutes of the first panel and the second flutes of the second panel are oriented generally perpendicular with the first support member, the second support member, and the one or more intermediate support members and generally parallel with the third support member and the fourth support member;

assembling a sidelap formed between the first edge of the first panel and the second edge of the second panel;
assembling panel edge couplings to operatively couple the first edge of the first panel to the second edge of the second panel at the sidelap; and
assembling end support couplings to operatively couple the opposing ends of the first panel and the second panel to the first support member and the second support member; and
wherein the first panel and the second panel are void of couplings between the opposing edges and the opposing ends of the first panel and the second panel located between the first support member and the second support member, and the third support member and fourth support member where the first panel and the second panel cross at least one of the one or more intermediate support members.

2. The method of claim 1 , further comprising:
assembling edge support couplings to operatively couple the first edge of the first panel to the second edge of the second panel and to the one or more intermediate support members where the sidelap crosses at least one of the one or more intermediate support members.

3. The method of claim 1 , wherein assembling the sidelap comprises assembling a reinforcing member to the first edge of the first panel and the second edge of the second panel, wherein the reinforcing member comprises:
a first channel and a second channel;
wherein the first channel and the second channel are generally parallel to each other, and out of plane with respect to each other;
wherein when assembled the first edge of the first panel is located within the first channel, and the second edge of the second panel is located within the second channel to form the sidelap; and
wherein the panel edge couplings operatively couple the first edge of the first panel, the second edge of the second panel, and the reinforcing member together.

4. The method of claim 1 , wherein assembling the sidelap comprises forming a sidelap seam that is out-of-plane and formed from the first edge of the first panel being a male lip and the second edge of the second panel being a female lip, wherein the male lip and the female lip form the sidelap seam comprising four or more layers.

5. The method of claim 1 , wherein assembling the sidelap comprises forming a nested sidelap that is in-plane and formed from the first edge of the first panel being an in-plane edge and the second edge of the second panel being an in-plane edge, wherein the first edge and the second edge form the nested sidelap comprising three or more layers.

6. The method of claim 1 , wherein the one or more intermediate support members comprise at least three or more intermediate supports, and wherein the method further comprises:
assembling panel support couplings in a middle intermediate support of the three or more intermediate supports to reduce a buckling span of the first panel and the second panel.

7. The method of claim 1 , wherein the structural panel system comprises a ductile fluted roof panel system.

8. The method of claim 3 , wherein the reinforcing member comprises:
a first leg;
a second leg; and
a third leg;
wherein the first leg is operatively coupled to the second leg and forms the first channel; and
wherein the second leg is operatively coupled to the third leg and forms the second channel.

9. The method of claim 1 , wherein the third support member comprises a top cap and the fourth support member comprises a bottom cap for the first support member, the second support member, and the one or more intermediate support members.

10. A method of forming a structural panel system, comprising:
assembling two or more panels to a support structure, wherein:
each of the two or more panels comprise:
flutes;
opposing ends; and
opposing edges;

the support structure comprises:
a first support member;
a second support member;
one or more intermediate support members, wherein the first support member, the second support member, and the one or more intermediate support members are generally parallel with each other;
a third support member;
a fourth support member, wherein the third support member and the fourth support member are oriented generally perpendicular to and operatively coupled to opposing ends of the first support member, the second support member, and the one or more intermediate support members; and

wherein the flutes of the two or more panels are oriented generally perpendicular with the first support member, the second support member, and the one or more intermediate support members and generally parallel with the third support member and the fourth support member;

assembling a sidelap between adjacent edges of adjacent panels of the two or more panels;
assembling panel edge couplings to operatively couple the sidelap between the adjacent edges of the two or more panels; and
assembling end support couplings to operatively couple the opposing ends of the two or more panels to the first support member and the second support member; and
wherein the two or more panels are void of couplings between the opposing edges and the opposing ends of the two more panels between the first support member and the second support member, and the third support member and fourth support member where the two or more panels cross at least one of the one or more intermediate support members.

11. The method of claim 10 , further comprising:
assembling edge support couplings to operatively couple the sidelap between the adjacent panels of the two or more panels to the one or more intermediate support members where the sidelap crosses at least one of the one or more intermediate support members.

12. The method of claim 10 , wherein assembling the sidelap comprises assembling one or more reinforcing members between the adjacent edges of the adjacent panels, wherein each of the one or more reinforcing members comprise:
a first channel and a second channel;
wherein the first channel and the second channel are generally parallel to each other, and out of plane with respect to each other;
wherein when assembled in the sidelap between the adjacent edges of the adjacent panels of the two or more panels, an edge of a panel is located within the first channel, and an edge of an adjacent panel is located within the second channel; and
wherein the panel edge couplings operatively couple the edge of the panel

Assignees

• Nucor Corp

Inventors

• Bodwell Patrick Allen
• Bogh Brian Hansen
• Martin Jeffrey Reino

Classifications

• E04H9/02

  withstanding earthquake or sinking of ground (foundations E02D27/34) · CPC title

• E04H9/14

  against other dangerous influences, e.g. tornadoes, floods · CPC title

• E04D3/362

  by locking the edge of one slab or sheet within the profiled marginal portion of the adjacent slab or sheet, e.g. using separate connecting elements · CPC title

• E04C2/322 Primary

  with parallel corrugations · CPC title

• E04C2/08

  of metal, e.g. sheet metal (E04C2/26 takes precedence) · CPC title