The present invention generally relates to a flexible terminal point for lattice work constructions, and more particularly to such constructions subjected to dynamic forces.

Dynamic forces are usual when considering lattice work constructions of many different kinds, for example with buildings and parts of buildings such as floors and roofs, and so on which are subjected to varying forces, with pillars, towers, masts, bridges and all kind of other constructions which can be subjected to gravitational loads or side loads as a result of strong winds and so on. A special field where large dynamic forces arise are lattice work constructions which wholy or partially are in water and are there subjected to varying loads and high dynamic stresses resulting from wind and waves. Examples of such constructions are bridge foundations, wave brakers, habour piers docks or work platforms e.g. oil derricks.

The elements of a lattice work construction which are brought to a single terminal point, always attempt to change the relative angles between the elements as the construction is subjected to normal loading. Unusual forces ^* directly applied upon at the cross bars of the lattice work construction increases the need for flexibility of the terminal points. Conventionally, the design of lattice work terminal points are such that relative changes in the angles between the elements is restricted, creating concentrations of stress in an area where the material's fatigue strength is already reduced as a result of directional changes of the forces applied. The danger of fatigue failure is exaggerated further in cases where the inflicted loads change direction and cause stresses with changing sign in the terminal point's fittings.

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To eliminate the named problems it has been suggested that the terminal points fitting should be made flexible, so that the lattice work element is allowed in some degree to be movable, reducing the risk for fatigue failure. Such flexibility of termal points fittings is known through for example, the German Patent 1 459 963 and 2 421 758. These terminal points fittings are formed as ball joints, where the ball and socket are fastened in lattice work element and terminal plate or such like of the lattice work. These known types of joints are intended as simple methods of assembly and also allow for a certain movement between the different parts. These constructions are however, mainly suitable for lighter lattice work dimensions, and have the disadvantage that terminal point fittings can be subjected to both tension and compression stresses. Tension forces can cause the edges of the socket which partly encloses the ball, to be drawn out, giving rise to play even to the extent that the ball * can be pulled out of the socket. To make it possible for a de-mountable ball joint, or of the ball from its socket, the known constructions are made up of a large number of parts, -of which many must be adjusted or tightened on assembly.

This invention endeavours to solve the problem of a simple and effective terminal point fitting, which allows a certain flexibility beween the elements of the lattice work, which is simple to assemble and adjust, and which is well suited for large and heavy lattice work constructions.

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A special aspect of this invention concerns the el mination of problems caused by dynamic forces of changing direction in terminal points fittings. Pre-tensioning of the terminal point causes the directional changes of dynamic loads to result in stresses of varying magnitude only, and the stress variations are reduced considerably in the pre-tensioned terminal point means by the transference of forces to the compressed parts of trie . fitting. This construction achieves much improved properties of strength in comparison with constructions which allow directional changes of stresses from tension to compression.

A development of the invention ^" is that the terminal point

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fitting is formed with three different but co-acting elements, which are arranged to bring about the named pre-tension, and where the one.el.ement is subjected to compression forces only and the other element to tension forces only. By this arrangement the possibility arises to design the tensioned parts of the means considering tensile stress properties only, and the compressed parts which are not so sensitive for varying loads can be made of simpler material and design.

Futher characteristics of the invention will be evident from the following detailed specification in which reference will be made to the accompanying drawings.

In the drawings figure 1 digrammatically shows a part of a lattice work construction of simple type. Figure 2 shows on a larger scale a part of a lattice work construction in figure 1. Figure 3 shows a section through line III-III in figure 2. Fi¬ gures 4, 5, 6 and 7 show four different alternative versions of the flexible terminal point according to the invention. Figure 8 diagramatically pretensionings advantageous effect upon the stress curve of the terminal means while under dynamic forces.

As in figure 1 shown example of a lattice work construction, comprises two struts or bars 1, 2 with several zig-zag cross bars 3 beween them, of which only one is drawn. The cross bars 3 are attached to the struts by terminal point fittings, which are showns diagrammatically in figures 2 and 3. The cross bars 3 are at each end attached by a terminal means 5 comprising a terminal tube 6 with an outer end 7 and an inner end 8. To secure the terminal means 5, the strut or bar 1 is provided with a diametrial junction-plate 9, which is welded to the inside of the strut or bar, and which has a center hole 10, the purpose of which will be described below. Terminal means 5 runs at an angle through the side of and into the strut or bar 1, and inserted into the junction plate 9 so that the inner end 8 lies flash with the periphery of hole 10 while the outer end 7 is positioned outside the strut or bar.

In the shown example terminal means 5 is circular, but can also be square, rectangular or any other shape. In a similar

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manner, terminal means 5 is secured in a single junction plate, but as can be seen by the dotted lines in figure 3, the construction can- be arranged to have two junction plates 9' between which the terminal means is secured. In cases where the terminal means is formed by square or rectangular sections, the two junction plates 9' can be utilized as two of the sides of the terminal means.

To achieve a terminal which is flexible in all directions, the outer end 7 of the terminal means is formed as a bearing socket 11, which flexibly receives the outer end 12 of the cross bar 3. Figure 4 shows that.the flexibility of the joint is effected by a rubber pad or other elastic meaterial inserted in . the bearing socket 11, and by forming the outer end of the cross bar to a flat or rounded end-piece 14, which lies against the elastic pad 13 and through which runs a tie-rod, threaded in both ends, with nuts 16, 17 to enable securing of the cross-bar 3 to- the terminal means 5.

A terminal means is normally subjected to varying loads of different kinds, of which the most unfavourable can cause changing tension and compression stresses. A load curve of such unfavourable loading is shown by curve 17 of figure 8. If however the terminal means is pre-tensioned, the curve 17 will be elevated as shown in the diagram, and if pre-tensioning is sufficient the curve will lie completely ove the zero axis, whereby the terminal means is subjected to stresses of only one * sign. This is shown by curve 18. By diverting forces into a separate compression element and a separate tension element, the compression element 5 can be arranged to have a larger area and thereby a lower stress concentration and can therefore be manufactured from conventional low grade material. The tension element can on the other hand be made from high grade cold drawn material, where the area can be kept small and the stress factor high. If this terminal is pre-tensioned and is then subjected to changing pull and push forces from the cross-bar 3 and conveyed to junction plate 9, the said forces are separated and the push forces are conveyed through the compression element 5 with the

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larger area, and pull foces are taken up _# by the tension element 15, which due to pre-tension retains a virtually constant strain, and the forces remain in proportion to the areas of the elements. In figure 8 the curve 19 illustrates the important reduction of stress varitations achieved by pre-tensioning. For dynamically loaded constructions, the magnitude of strain and number of variations of strain are crucial for their life spun. Thus the terminal point is designed as a terminal means 5, which takes upp all compression forces, and another means 15 which takes up tension forces. At the same time the cross bar 3 is allowed to swing freely in all directions relative to the terminal means 5 by the action of the elastic pad 13.

Figure 4 showns that the tie-rod 15 is a stiff rod. When the cross-bar 3 is subjected to large swinging movements in relation to the terminal means 5, the cross bar end piece 14 tends to lift the nut 16 by forcing against the edge of the nut, this effect . can be eliminated by making the tie-rod 15 bendable for example by using a flexible wire or steel cable with many elements.

The means can even be formed as shown in figure 5, where the cross bar 3 and end piece 14 is shaped having a convex surface 19 away from the means 5, and beween the convex surface 19 and nut 16 a concave shaped socket 20 is positioned. Suitably, the axial hole through the end-piece 14 is to some extend larger than the tie-rod 15, and the ^' cross bar with the end-piece 14 can move in any direction, whereby the end-piece 14 slides under the matching surface of the socket 20 and the tie-road 15 maintains its position and tension.

Figure 6 shows an alteraπtive design of the invention where the terminal means 5 outer end 7 is formed as part of a concave socket 11' and the cross-bars and -piece 14' is matchingly convex and can slide in the socket 11'. Even in this case the nut 16, as a result of a substantial swing of the cross-bar, can be partly lifted from the end-piece 14' and to eliminate this disadvantage, the means can be designed as in figure 7 where the end-piece 14' is formed on its inside to a concave socket matching the bearing ball 21 which remains stationary in relation to the terminal

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means 5 as the end piece 14" can rotate. It is shown in the figure ^' that in this case two tie-rods 15, 15* has been used, which run through the socket IT, the end-p-iece 14" and the bearing ball 21, it is obvious that one tie-rod can be used, or three or more.

It is obvious that the terminal means shown in the drawings as a plain construction can also, according to the invetion, be used in three dimensional constructions and that the terminal means can also be used in situations other than lattice work constructions, where a securing method for tubes or bars is required and which can withstand strong fluctuating forces.

It is also obvious for the expert that the drawing show embodiments of the invention as illuminating examples only. And that all kinds of modifications may be presented in the scope of the following patent claims. For example, pretensioning of the terminal can be made of any other means than the shown threaded- tie-rods or that the terminal means can be secured by other means than the shown junction plate. However, the junction plate provides a strong securing method relative to the strut's or bar's thin material. When securing with a junction plate, advantage can be gained by cenralizing the load lines from several cross bars to one point in the strut or the bar, which optimizes an advantageous loading situation.