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Publication numberUS2980215 A
Publication typeGrant
Publication dateApr 18, 1961
Filing dateNov 12, 1957
Priority dateNov 12, 1957
Publication numberUS 2980215 A, US 2980215A, US-A-2980215, US2980215 A, US2980215A
InventorsErnest Englund
Original AssigneeErnest Englund
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Tubular interlocking joint
US 2980215 A
Abstract  available in
Previous page
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Claims  available in
Description  (OCR text may contain errors)

A nl 18, 1961 Y E. ENGLUND 2,980,215

TUBULAR INTERLOCKING JOINT Filed Nov. 12, 1957 2 Sheets-Sheet 1 Z i 'EL L Q Z INVENTOR.

April 18, 1961 Filed Nov. 12. 1957 E. ENGLUND TUBULAR INTERLOCKING JOINT 2 Sheets-Sheet 2 A I mw INVENTOR.

BY 6 WWW M TUBULAR INTERLOCKING JOINT Ernest England, 118 W. Florida, Urbana, Ill.

Filed Nov. 12, 1957, Ser. No. 695,834

1 Claim. (Cl.189-34) The present invention relates to shelter structures and particularly to support members suitable for use in forming the frames of shelter structures.

In architectural engineering, a type of frame construction known generally as space-grid construction has been widely used for hemispherical dome shelters, of which the geodesic is one form, and for semi-cylindrical arch shelters resembling, in form at least, what is commonly known as the Quonset hut type of structure. Additionally, the principles of space-grid framing have been successfully used for horizontal and vertical planar wall structures, being exemplified in the latter case by what is known as curtain-wall structure.

Generally, a space-grid structural frame is made up of support members interconnected in a geometric pattern so as to form a structure of such a favorable weightto-strength ratio that it is, in fact, self supporting. To

provide shelter against the elements of nature, the spacegrid frame may carry thereon a covering skin or a lining skin, or both, of a conformable material which may be of metal, plastic, fabric and the like; or the frame may support in the spacings between the support members panels or structural units which fill the spacings and are rigidly connected to the support members for contributing to the total strength of the structure. Such a structural unit is described in the applicants copending application Serial No. 681,955, filed September 4, 1957, now abandoned. It is to improvements in support members for such frame constructions that the present invention is directed.

An object of the present invention is to provide an improved support member for frame constructions which is lightweight, simple and inexpensive to manfacture and easy to assemble.

Another object of the invention is to provide an improved support member which is easily adapted to extrusion methods of manufacture.

An additional object of the invention is an improved support member having a favorable weightto-strength ratio which is particularly well adapted for use in space-grid structures and to receive and support structural units spaced therebetween. I

A more specific object of the invention is to provide an improved support member made up of longitudinal sections that are overlapped and interlocked one with another to define a tubular cavity and which carries within the tubular cavity structure for maintaining the sections in interlock, whereby the structure is made lightweight yet rigid and strong. Inasmuch as the longitudinal sections are identical, manufacture of the support member is greatly simplified and easily accomplished by extrusion methods and permits the inclusion of projecting surfaces on which panels may be fixed and supported.

Further objects and features of the invention pertain to the particular construction and arrangement employed in attaining, the above identified objects.

The invention, both as to its structure and mode of to provide Patented Apr. 18, 1961 use, will be better understood by reference to the following specification and drawings, forming a part thereof, wherein: V

Figure 1 is a perspective view of a support member in accordance with the invention;

Figure 2 is a perspective view of an alternate embodiment of a structural member in accordance with the invention;

Figures 3A, 3B, 3C and 3D show in longitudinal crosssection a support member in accordance with the invention and filler arrangements for insertion into the cylindric cavity of the support member;

Figure 4 is an end view of an arcuate section such as used in the support member shown in Fig. 1; and

Figure Sis a top plan view of the central vertex section of a geodesic type frame structure employing support members in accordance with the invention.

Referring now to the drawings, there is shown in Figure 1 a support member 10 in accordance with the invention made up of interlocked arcuate sections 11 and 12 and a cylindric sleeve 13 split'longitudinally into two sections 13a and 13b. The arcuate sections 11 and 12 are identical and as best shown from the cross-sectional view of Figure 4 the arcuate section 11 is made up of an inner surface 15 and an outer surface 16. The inner surface 15 is a concave cavity extending from a blunted end 17 to a sharpened end 18 and is defined by a semi-cylindric surface 14 extending from the blunted end 17 and terminated at a diametrically opposed surface 19, a slot 20 of which the surface 19 forms one side and a curved surface 21 extending between the slot 20 and the pointed end 18. The center of curvature of the curved surface 21 is concentric with that of the semi-cylindric surface 14 and the radius of curvature is slightly larger than that of the semi-cylindric.

The outer surface 16 of section 11 is shaped to conform generally to that of the inner surface 15 and includes a projection or key 22 at the blunt surface 17 joined to a curved surface 23 having the same length, the same center of curvature and the same radius of curvature as the curved surface 21, and which continues into a curved surface 24 of gradually diminishing curvature which is terminated in a fiat surface 25. Another curved surface 26 taking a shape inverse to that of the surface 24 extends from the pointed end 18 of the section 11 to the flat surface 25. At the fiat surface 25 a deep slot 27 is formed which extends inwardly towards the center of curvature of the surfaces 14, 21 and 23. The key 22 conforms to the shape of the slot 20 so that when the section 11 is mated with a correspondingly identical section, such as section 12 indicated by the dotted lines in Figure 4, the sections interlock at the slot 20 and at the key 22 to define a symmetrical support member having a cylindric cavity 27.

It is to be understood that the shape of the outer surface 16 is not critical to the practice of the invention, the configuration shown in Fig. 4 being selected as one that provides a structure of thickness resistive to flexing forces and accommodates apertures or slots, such as the slot 27, into which structural units or panels can be mounted. Accordingly, the outer surface 16 can be formed in accordance with the usage to which thesupport member is to be put and can be made up of flat or rounded surfaces, and include apertures and projections of either a continuous or an intermittent nature. As pointed out, the structure of Figures 1 and 4 has been selected as being particularly well adapted for use in carrying the structural units of the above-mentioned copending application.

Illustrative of the variations that may be introduced into the outer surface 16 of an arcuate section is the showing in Figure 2 wherein there is shown a support member 3t) made up of arcuate sections 31 and 32 and a cylindric sleeve 33 split longitudinally into two sections 33A and 333. The arcuate section 31 is identical to the arcuate section 32 and the inner surface 35 thereof is identical to the inner surface 15 shown in Figure 4. The outer surface 35 is more of a box shape including a pair of spaced apart slotted flanges 37 and 38. The outer surface configuration shown in this instance is designed to accommodate and carry a pair of spaced apart panels so as to provide a double wall structure with a dead air space insulating cavity.

The cylindric sleeves 13 and 33 employed, respectively, in support members it) and 30 are inserted into the cylindric cavity defined by the arcuate sections of the support members for maintaining the sections in interlock. Though the cylindric sleeves are shown to be longitudinally split into two segments, they could be unitary. The split cylindric is illustrated because it is believed by use of such an arrangement the tighter fit can be achieved within the cylindric cavity. in actual practice the split need not be longitudinal with the axis of the sleeve but it could be helical, wedge shaped or of any other convenient configuration.

Alternative structures for maintaining the arcuate sections interlocked are shown in Figures 3A, 3B, 3C and 3D. Figure 3A shows a longitudinal cross-sectional view of the support member and a short cylindrical stub 41 which is closed at its end 42, open at its end 43 and includes therein at least one partial longitudinal slot 44. At its end 43 the cylindric stub is preferably slightly larger than the cylindric cavity of the support member 10 so that when placed within the cylindric cavity the s ub flexes at the slot t4 and fits snugly to the cavity. Figure 3B shows in longitudinal cross-section the support member 10 carrying therein a slotted cylindric sleeve 45-. The cylindric sleeve 45 is preferably of a greater diameter than the diameter of the cylindric cavity and is longitudina'lly slotted either parallel to the axis thereof or in a helical pattern and is fitted snugly within the cavity. Figure 3C shows in longitudinal cross-section a support member it carrying therein spheres 541 such as tennis balls, ping pong balls, and the like, and of a diameter to fit snugly within the cylindric cavity of the support member. Figure 3B shows in cross-sectional view the support member 10 carrying therein a helical spring 55 which is made of resilient material and preferably of a diameter slightly larger than the diameter of the cylindric cavity.

It is understood that the cylindric sleeves and structures shown in Figures 3A to 3D are inserted into the cylindric cavity defined by the support member in order to force the arcuate sections thereof into interlocking relationship at the surfaces of overlap. The support member so presented is then unitary, light and strong and may be employed in a geodesic type of structure such as is illustrated in part in Fig. 5. Therein the support members 10 are arranged in a frame structure Si by means of fastening devices 51 of any suitable form such, for example, as those described in the R. B. Fuller Patent No. 2,682,235, issued June 29, 1954. As previously noted, the support members 16 are adapted to support within the open spaces appropriate construction units or panels such as described in the applicants copending application.

Though the invention has been described in terms of support member made up of arcuate sections, it is understood that the support member may take any cross-sectional configuration, and that the sections thereof may be angular as well as arcuate. The sections which go to make up the support member, are believed to be particularly well adapted to an extrusion method of manufacture. They may be made of metal, aluminum having been found to be an easily extrudable material, or plastic with or without reinforcing fibers and laminates. The advantage of this type of manufacture is that obviously the lengths of the arcuate sections are indeterminate and the shapes which may be given to the outer surfaces is completely flexible being determined entirely by the dies used with the extrusion machinery. Molding or centrifugal casting operations are considerably more expensive and provide members of limited lengths. Additionally, considerable advantage can be achieved from having a support member made up of longitudinal sections in that movement and positioning of the members is greatly simplified by the reduced weight of the fractional parts that go to make up this structural member. Sections of considerable length, for example, 20 feet, can be easily moved by two men and raised into construction position, the sections being joined in the construction position and the internal expansion member being inserted thereafter. This provides a structure that is not only inexpensive and easy to manufacture, but is of considerable advantage in use.

In view of the foregoing disclosure, it is obvious that there hm beenpresented herein an improved support member that is light of weight yet rigid and strong, convenient and easy to handle, and easily adapted to extrusion methods of manufacture. While the arrangement described and presented herein is at present considered to be preferred, it is understood that variations and modification may be made therein and it is intended to cover in the appended claim all such variations and modifications as fall within the true spirit and scope of the invention.

What is claimed is:

A frame member comprising a plurality of longitudinally extending, laterally curved sections arranged in radial overlap to define in composite a cavity, each of said sections overlapping and underlapping respectively adjacent sections and being longitudinally slotted on the surface of overlap and being longitudinally keyed on the surface of overlap for interlocking said section with adjacent sections, and means conformable to the dimension of said tubular cavity including a sectioned column coextensive with the length of said frame member for maintaining said sections in interlock.

References tilted in the file of this patent UNITED STATES PATENTS 1,596,360 Krey Aug. 17, 192 6 FOREIGN PATENTS 951,882 France Apr. 25, 1949 275,333 Switzerland Aug. 1, 1951 145,433 Australia Feb. 27, 1952

Patent Citations
Cited PatentFiling datePublication dateApplicantTitle
US1596360 *Apr 13, 1926Aug 17, 1926Joseph Krey HermanStructural unit
AU145433B * Title not available
CH275333A * Title not available
FR951882A * Title not available
Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US3125196 *Feb 2, 1960Mar 17, 1964 Screen
US4106423 *Oct 28, 1976Aug 15, 1978General Dynamics CorporationWeather covers for tankers
US7874762Sep 17, 2009Jan 25, 2011Shaw & Sons, Inc.Dowel device with closed end speed cover
US8007199Dec 16, 2010Aug 30, 2011Shaw & Sons, Inc.Dowel device with closed end speed cover
U.S. Classification138/157, D25/122, 52/81.2, 52/664, 52/282.1, D25/13
International ClassificationF16B3/00, E04B7/10, E04C3/04
Cooperative ClassificationE04B7/105, E04C2003/0417, E04C2003/0413, E04C3/04, F16B3/00, E04C2003/0452, E04C2003/043, E04C2003/0439
European ClassificationE04C3/04, E04B7/10C, F16B3/00