AU562145B2

AU562145B2 - Space frames

Info

Publication number: AU562145B2
Application number: AU32185/84A
Authority: AU
Inventors: Edwin Thomas Codd
Original assignee: Harley Systems Pty Ltd
Current assignee: Harley Systems Pty Ltd
Priority date: 1983-08-23
Filing date: 1984-08-17
Publication date: 1987-05-28
Anticipated expiration: 2004-08-17
Also published as: AU3218584A

Description

Title: "SPACE FRAMES"

BACKGROUND OF THE INVENTION (1 ) Field of the Invention

This invention relates to space frames. (2) Brief Description of the Prior Art

Space frames are extensively used in situations where shallow depth construction is required over large spans with a minimum of elastic movement under load, and a minimum number of supports. A space frame is commonly of double-layer type, with upper and lower grids of longitudinal and lateral members, or chords, the nodes, or junctions of chords, of the upper and lower grids being interconnected by oblique struts or web members. Although, in some space frame constructions, the nodes of the upper grid are aligned directly above corres ponding nodes of the lower grid, and the struts may inclu vertical struts between such nodes, more commonly the upp grid nodes are displaced both laterally and longitudinall relative to the nodes of the lower grid, so that each low grid node is equidistant from, and connected by oblique struts to, four of the nodes of the upper grid.

Other space frame constructions may include barrel vaulted and domed structures, and a dome may be of single- layer type comprising an arrangement of hexagons and penta gons, five or six chord members being co-joined at a node.

SUMMARY OF THE PRESENT INVENTION The general object of the present invention is to provide a space frame which may be of double-layer type, or of domed or other single-layer type, and which is part¬ icularly simple and economical to manufacture, assemble an erect without requiring any elaborate or costly connectors Other objects achieved in preferred embodiments of the invention are to provide such a space frame which is well suited to the economical application of weather protection and also to the application of an inner line or ceiling.

With the foregoing and other objects in view, the invention resides broadly in a space frame of the type having a multiplicity of frame members, assemblies of which have ends co-joined at nodes by connecting means, wherein, at a node, the nodal end of each of the frame members of an assembly includes two transversely stepped parts, herein called upper and lower parts; the upper par is superimposed on the lower part of the nodal end of a succeeding frame member of the assembly, and the connecti means connect together each pair of superimposed .parts.

The frame members, which may be assemblies of oblique struts as well as assemblies of chord members, are preferably tubular with their ends flattened, the flattened ends being shaped to form the transversely stepped parts and the connecting means are preferably bolts equal in number to the chord ends at the node, each passed through registering bolt holes in a pair of super- imposed parts and engaged by a nut. Other features of the invention will become apparent from the following description.

BRIEF DESCRIPTION OF THE DRAWINGS In order that the invention may be readily under- stood and carried into practical effect, parts of space frames according to the invention are shown in the accompanying drawings, wherein:-

FIG. 1 is an exploded perspective view of ends of chords and oblique struts at a lower grid node of a space frame,

FIG. 2 is a plan view of the assembled node, FIG. 3 is a view from below of the node shown in FIG. 2,

FIG. 4 is a plan view of an upper node of a space frame according to a modification of the invention, FIG. 5 is a view from below of the node shown in FIG. 4, and

FIG. 6 is an exploded perspective view of ends of chords and oblique struts at a lower grid node of a spac frame according to a further embodiment of the invention DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT Referring initially to FIGS. 1 to 3 of the drawing the chords 10 of each layer of a double-layer space fram are lengths of round-section metal tube each end of whic is flattened and also deformed to a transversely stepped formation of two substantially equal ad acent parts 11 and 12. One of these parts, when they are horizontal, i above the level of the other, the top surface of the low part 11 being substantially in the same plane as the bottom of the adjacent upper part 12, the axis of the tubular chord being in or close to this plane. The adja parts 11 and 12 are separated by a shoulder 13, and each of the stepped parts 11 and 12 is formed with a more or less central bolt hole 14. Each chord end may be flatte stepped and formed with its bolt hole in a single operat At each node of the space frame the flattened and stepped ends of the chords 10 are interfitted, the upper part 12 of each chord end overlying the lower part 11 of the next succeeding chord end. When the chord ends are interfitted, the upper faces of all upper parts 12 are substantially co-planar, the lower faces of all lower pa 11 are substantially co-planar, superimposed pair of upper and lower parts 12 and 11 are brought into registe The end edges of the stepped parts 11 and 12 of each cho 10 then, as shown in FIG. 3 abut against the shoulders 1 of the next succeeding chords, and the side edges of the stepped parts 11 and 12 of each chord bear against abut¬ ments 15, at the commencement of the flattening of the ends of the succeeding chords 10. Four bolts 16 and nuts 17 are used to interconnect rigidly the interfitted chord end parts at the node, and also to connect the ends of oblique struts or web members 18 and to secure a load distribution plate 19- Each of the struts or web members 18 is a length of round-section metal tube of lesser diameter than the chords 10, and has each end portion 20 flattened, bent t an angle to the axis of the strut, mitred so its sides are convergent at a right angle, and formed with a bolt hole 21. The bolts 16, passing through the bolt holes 21, hold the mitred side edges of succeeding struts closely adjacent, as indicated in a broken outline in FIG. 2. The load distribution plate 19 is square with four bolt holes 22 to accept the bolts 16, on which the nuts 17 are then engaged and tightened. The sides of th load distribution plate 19 then bear against abutments 2 at the commencement of the flattening of the ends of the struts 17, and the corners of the plate bear against the abutments 15 at the commencement of the flattening of the ends of the chord members 10. The four chord member 10 and the four struts 18 are thus quickly and easily connected firmly together with very great resistance to torsional stresses. As the axes of the chords of each layer of the space frame lie substantially in the one plane, and the bolts 16 will not normally extend above t level of the chords of the upper layer or below the leve of the chords of the lower level, roofing and ceiling material may be easily applied to the space frame.

In the modification shown in FIGS. 4 and 5, a spac frame mode is the junction of five chords 24 and five struts 25 secured, together with a load distribution pla 26, by five bolts 27 and nuts 28. The chords 24 are sim to the chords 10 before described with reference to FIGS 1 , 2 and 3 except in that the flattened and stepped end portions of the chords 25 are mitred at their extremitie to an angle of 144 so that the angled outer end edges

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The struts 25 again are similar to the struts 18 of FIGS. 1, 2 and 3 except in that their flattened end 32, as indicated in broken outline in FIG. 5, are mitred to an angle of 72° for close abutment when the parts at the node are held by the five bolts 27. The sides of the pentagon-shaped load distribution plate 2 bear against abutments 33 at the commencement of the flattening and bending of the ends 32^' of the struts 25 It will be readily apparent that the invention is applicable to a space frame in which six chords and si struts are secured together by six bolts, the flattene and stepped chord ends, and the flattened strut ends, being appropriately mitred for maximum resistance to torsional stress.

It should be understood, too, that in the constru ion of a domed space frame, in which five chord members are co-joined in some of the nodes, and six chords are co-joined in others, the struts will be omitted if the structure is to be of single-layer type; and the axis o each chord, instead of being parallel to the planes of the stepped end parts, will be at a small angle to them depending upon the curvature of the overall domed structure.

The parts shown in FIG. 6 are for interconnection as a node of a space frame in which corresponding chord 34 of upper and lower grids have their axes in the same vertical plane, and the axes of the struts 35 also lie in the vertical planes through the axes of the chords. The chords 34, in this case, are similar to the chords 10 described with reference to FIGS. 1, 2 and 3, each with its ends flattened and transversely stepped to for adjacent parts 36 and 37 at different levels, separated by a shoulder 38, and with a bolt hole 39 through each. Each of the struts 35, which is of about the same diameter as the chords 34, has its end flattened, bent to an angle to the axis of the strut, and transversely stepped to form two adjacent parts 40 and 41 with a bol hole 42 through each. The chord ends are interfitted a before described, and the strut ends are interfitted similarly and superimposed on the assembly of interfitt chord ends. In this example, two similar square load distribution plates 43 are provided, each with four bol holes 44, and one is located above, the other below, th assembly the parts of which are secured rigidly togethe by four bolts and nuts (not shown).

Space frames according to the invention will be found to be very effective in achieving the objects for which they have been devised. Instead of elaborate con ectors being required, the nodal connections are effect simply and economically by bolts equal in number to the chords to be co-joined, each engaged by a nut. In most cases all chord members will be identical, and all obli struts or web members will also be identical, the ends the chord and strut members being simply and easily sha for interconnection. At a side of a space frame grid where, for example, three instead of four chords are connected at a node, or at a corner of the structure where two chords only are connected, simple stepped and apertured filler pieces (not shown) are used for incorp ation in the node assembly in place of the stepped chor ends which are interfitted in the other nodes of the sp frame. The nodes and/or the struts may of course be other than round-section tubes; for example angle members or channels with ends appropriately shaped may be used.

The foregoing and many other modifications of construct al detail and design, which will be readily apparent to persons skilled in the art, are considered to lie withi the scope of the invention hereinafter claimed.

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Claims

CLAIMS:

1. A space frame comprising a multiplicity of frame members, assemblies of which have ends co-joined at nodes by connecting means, wherein, at a node: the nodal end of each of the frame members of a assembly includes transversely stepped upper and lower parts, the upper part is superimposed on the lower part of the nodal end of a succeeding frame member of the assembly, and the connecting means connect together each pair superimposed parts.

2. A space frame according to Claim 1 wherein: the frame members are tubular, each with its nod end flattened and shaped to form to the said transversely stepped parts, the upper face of the lower part being sub¬ stantially in the same plane as the lower face of the uppe part.

3- A space frame according to Claim 2 wherein: the axis of the frame member is substantially in or parallel to, the said plane.

4. A space frame according to either of Claims 2 or 3 wherein: each tubular frame member has abutments at the commencement of the flattened end thereof, and the sides of the said stepped parts bear against the said abutments of succeeding frame members.

5. A space frame according to any one of the precedin claims wherein: a shoulder extends between the transversely step upper and lower parts, and the extremities of the said stepped parts of eac frame member bear against the said shoulders of the succee ing frame members.

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6. A space frame according to any one of the preceding claims wherein: the said frame members consist of chords of the space frame, and an assembly of oblique strut members converge to the node have ends secured thereto by the said connecting means.

7. A space frame according to Claim 6 wherein: the nodal ends of the strut members are flattened, mitred and secured by the connecting means in adjacent abuting arrangement.

8. A space frame according to Claim 7 wherein: each strut member is tubular with an abutment at the commencement of its flattened end, and the connecting means secure on the nodal ends of the strut members a load distribution plate having sides bearing on the abutments of the strut members.

9. A space frame according to Claim 6 wherein: the nodal end of each of the strut members includes transversely stepped upper and lower parts, the upper part of each being superimposed on the lower part of the succeeding strut member.

10. A space frame according to any one of the preceding claims wherein: the connecting means consist of bolts each passing through registering bolt holes in parts superimposed at the node.

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