Space frame connector

• US 8,739,492 B2
• Filed: 07/09/2009
• Issued: 06/03/2014
• Est. Priority Date: 07/09/2008
• Status: Active Grant

• Current Assignee: Skyfuel Incorporated
• Original Assignee: Skyfuel Incorporated
• Inventors: Hawkins, Robert, Farr, Adrian L., Gee, Randall C.
• Primary Examiner(s): Triggs, Andrew J
• Application Number:
  US12/500,467
• Publication Number:
  US 20100005752A1
• Time in Patent Office: 1,790 Days
• Field of Search: 526/531, 526/532, 526/551, 403/169, 403/170, 403/171, 403/176
• US Class Current: 52/653.1
• CPC Class Codes: E04B 1/1903 Connecting nodes specially adapted therefor
• CPC Class Codes: E04B 1/1909 with central cylindrical connecting element
• CPC Class Codes: E04B 2001/1918 with connecting nodes having flat radial connecting surfaces
• CPC Class Codes: E04B 2001/193 with flattened connecting parts, e.g. ends
• CPC Class Codes: E04B 2001/1963 Screw connections with axis at an angle, e.g. perpendicular, to the main axis of the strut
• CPC Class Codes: Y02B 10/20 Solar thermal
• CPC Class Codes: Y10T 403/34 Branched

Abstract

A space frame connector is provided for attaching an oblique strut tube to an axial chord of a space frame. The space frame connector includes a collar adapted to fit over an axial chord. The collar is equipped with one or more attachment flanges. The space frame connector also includes a strut tube having an extrusion flange formed in at least one of its ends. The extrusion flange is made up of two parallel leaves that define a slot between them. The slot is sized and shaped to fit over an attachment flange on the collar that is positioned over the axial chord. The extrusion flange can be formed using simple press and punch tools. Space frames used to support solar energy collector arrays can be assembled in the field, including formation of the extrusion flanges on the oblique strut tubes, or multiple strut tubes can be attached to axial chords and compactly packed and transported to the field for use in constructing space frames, for example for supporting large parabolic trough solar collectors.

Claims

1. A method of constructing a three-dimensional space frame comprising:

providing one or more axial chords;

equipping each of said axial chords with a collar adapted to fit entirely around said axial chord, said collar comprising one or more attachment flanges having a width;

providing one or more oblique strut tubes each having a first end and a second end;

equipping one of said ends of said oblique strut tubes with one or more extrusion flanges; and

attaching said oblique strut tubes to said axial chords by attaching said extrusion flanges to said attachment flanges, said extrusion flanges comprising first and second parallel leaves defining a slot therebetween, said slot having a width substantially equal to said width of said attachment flanges;

wherein said first and second parallel leaves are provided in first and second planes positioned parallel to each other;

wherein said attachment flange and said extrusion flange comprise attachment holes sized and positioned such that said attachment holes can be aligned during use to receive an expandable structural fastener that passes through the aligned holes;

wherein both of said first and second parallel leaves are in contact with said attachment flange; and

wherein said expandable structural fastener expands to contact said first and second parallel leaves and said attachment flange; and

attaching a solar reflector to said three-dimensional space frame.

2. The method of claim 1 further comprising attaching multiple oblique strut tubes to said axial chords to form a node.

3. The method of claim 1 further comprising attaching multiple oblique strut tubes to multiple axial chords to form multiple nodes.

4. The method of claim 3 further comprising equipping the oblique strut tubes that have been equipped with an extrusion flange with an additional extrusion flange at the other end.

5. The method of claim 4 further comprising attaching said multiple oblique strut tubes to multiple collars on said axial chords;

and rotating said oblique strut tubes such that unattached ends are in position to be attached to another axial chord.

6. The method of claim 5 further comprising attaching an extrusion flange at the unattached end of each oblique strut tube to another axial chord.

7. A solar energy concentration system comprising:

a three-dimensional space frame comprising;

one or more axial chords; and

one or more space frame connectors for attaching an oblique strut tube to said axial chord of said space frame, said space frame connectors comprising;

a collar adapted to fit entirely around said axial chord, said collar comprising one or more attachment flanges having a width; and

said oblique strut tube comprising an extrusion flange at an end thereof;

said extrusion flange comprising first and second parallel leaves defining a slot therebetween, said slot having a width substantially equal to said width of said attachment flange;

wherein said first and second parallel leaves are provided in first and second planes positioned parallel to each other;

wherein said attachment flange and said extrusion flange comprise attachment holes sized and positioned such that said attachment holes are aligned during use to receive an expandable structural fastener that passes through the aligned attachment holes;

wherein both of said first and second parallel leaves are in contact with said attachment flange;

wherein said expandable structural fastener expands to contact said first and second parallel leaves and said attachment flange; and

a parabolic solar collector supported by the three-dimensional space frame.

8. The system of claim 7, wherein two or more of said oblique strut tubes are attached to said axial chords.

9. The space frame connector of claim 7, wherein said first and second parallel leaves each have a thickness selected from a range of 0.065 to 0.125 inches.

10. The space frame connector of claim 7, wherein a thickness of said first or second parallel leave and a thickness of said attachment flange have a ratio selected from a range of 1:

1.5 to 1;

8.

11. The space frame connector of claim 7, wherein a thickness of said first or second parallel leave is less than a thickness of said attachment flange.

12. The space frame connector of claim 7 wherein said extrusion flange is integrally formed from the end of said oblique strut tube.

13. The space frame connector of claim 7 wherein said extrusion flange is a component of an end connector attached to the end of said oblique strut tube.

14. The space frame connector of claim 7 wherein said oblique strut tube comprises an extrusion flange at each end thereof.