US3445854A

US3445854A - Antenna

Info

Publication number: US3445854A
Application number: US714117A
Authority: US
Inventors: John D Callaghan
Original assignee: RCA Corp
Current assignee: RCA Corp
Priority date: 1965-05-27
Filing date: 1968-03-18
Publication date: 1969-05-20
Anticipated expiration: 1986-05-20

Description

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United States Patent 3,445,854 ANTENNA John D. Callaghan, Cherry Hill, N.J., assignor to Radio Corporation of America, a corporation of Delaware Continuation of application Ser. No. 459,386, May 27, 1965. This application Mar. 18, 1968, Ser. No. 714,117 Int. Cl. H01q 15/14, 19/10 US. Cl. 343-912 Claims ABSTRACT OF THE DISCLOSURE A hollow supporting member is provided having a number of opposing holes in opposite sides thereof. Each of the holes has a collar surrounding it with the collars on at least one side of the member being located in the interior of the member, the collars being of the same material as the member and integral therewith. A rod is positioned in each pair of opposing holes so that each rod is surrounded by two of the collars, each of the two collars surrounding a rod being indented into that rod whereby the rods are firmly secured to the supporting member.

This is a continuation of my copending application Ser. No. 459,386, filed May 27, 1965, and now abandoned.

This invention relates to an improved supporting structure with a rod or rods mounted thereon.

The present art teaches the securing of a rod to a supporting structure by various means and for a variety of purposes. For example, in the fabrication of certain types of antennas, the need exists for placing antenna elements or rods perpendicular to the supporting structure or mast.

This is done by fabricating a hole in the element or rod and fabricating another hole in the mast or supporting structure. The rod can now be secured to the supporting structure or mast by conventional means, as a screw, bolt or rivet. The disadvantages of this technique are apparent. The strength of the rod is greatly impaired due to the resulting removal of material caused by the fabrication of the hole in the rod. Another disadvantage is the distortion of the rod if too much pressure is exerted by the screw, bolt or rivet. Still another disadvantage is that, if too little pressure is applied via the screw, bolt or rivet, the rod will have a tendency to rotate with respect to the supporting structure. In order to compensate for some of the above disadvantages, additional means are presently employed. Such means require additional parts, for example, various clamping arrangements, to secure the rod. While such clamping devices supply the necessary support, the additional parts, as in any manufacturing process, require fabrication and hence increase the cost of the final product. The additional parts also require additional steps thereby lengthening the manufacturing process.

An object is to provide an improved composite structure of rod supporting structure and rods constructed in accordance with said improved method.

One embodiment of the present invention entails a method of securing a rod to a supporting structure comprising the steps of forming a hole in said supporting structure so that the structural material is flared in a direction transverse to the supporting structure at the margin of the hole, inserting the rod into the hole and deforming the rod and said flared material by the application of a force transverse to said flared material and rod thereby locking the rod to the supporting structure.

The invention will be described in detail with reference to the accompanying drawing, in which:

FIG. 1 is a perspective view of a typical supporting member with holes fabricated on two parallel surfaces;

FIG. 2 is an end view of a typical supporting member "Ice showing the flared material forming a collar around the margin of the hole;

FIG. 3 is an end view of a typical supporting member showing a rod inserted through the hole, surrounded by the collar;

FIG. 4 shows a perpsective view of a typical member having a die surface;

FIG. 5 is an end view of the member having a die surface inserted in the supporting structure, with the die surface against the flared collar;

FIG. 6 is an end view of the rod firmly locked to the supporting structure;

FIG. 7 is a perspective view of a member having a die surface passing through a supporting structure containing a plurality of rods;

FIG. 8 is an end view of a supporting structure with a rod locked therein by means of indentations on outer flared collars;

FIG. 9 is an end view of a supporting structure with a rod locked therein by means of indentations on an outer flared collar and on an inner flared collar;

FIG. 10 is a perspective view of a member with a die surface passing by the top and bottom surfaces of a supporting structure;

FIG. 11 is a perspective view of a member having a fork-like structure with die surfaces;

FIG. 12 is a perspective view of a member having elongations with die surfaces; and

FIG. 13 is an end view of a rod and supporting structure inserted and held in a representative jig or fixture.

In the several figures like parts are indicated by similar reference characters.

Referring to FIGURE 1, a hollow, rectangular, elongated supporting structure 1 is shown. The structure 1 is formed with a longitudinal passage 2, with holes 3, 4 and 5 appearing on the top surface and holes 6, 7 and 8 which are in line with holes 3, 4 and 5, respectively, appearing on the bottom surface. The structure 1 may be made of metal, for example, aluminum, or a desired nonmetal material. In the specific embodiment illustrated in FIG. 1, the supporting structure 1 is about six inches long with a height and width of about inch. In other embodiments the length might be several feet, fifteen feet for example, and, assuming the support to be a hollow square, the height and width might be one foot. In general, the dimensions are such that there is restricted access to the interior of the supporting structure. In FIGURE 2 the

numerals

9 and 10 indicate collars surrounding the holes 3 and 6. The

collars

9 and 10 can be fabricated, from the supporting structure material 1, during the hole forming process; by conventional techniques, such as shaping, flaring or extruding. A method of achieving this is to use a hybrid tool configuration where the lower portion of the tool consists of a conventional drill bit and the upper portion consists of a cone-like section, such that the diameter gradually increases in a direction towards the top of the tool. With said tool, after the hole is drilled by the drill like portion; the cone-like portion of the tool is forced through the hole thereby forming a collar or flaring of the structure material. Other methods for producing the holes with collars or flaring are well known in the field and any such method is acceptable.

In FIGURE 3 there is shown a rod 11 inserted into the holes 3 and 6, the flared or extruded material forming the

collars

9 and 10 surrounding the rod 11. The rod 11 can be formed of rolled metal formed into a tube-like configuration or can be made of any other suitable material. A U-shaped elongated member 12 is shown in FIGURE 4. Near the end of the member 12, a bead or die surface 13 is provided at the two ends of the U. The dimension represented by reference 14 designates the dimension from the outer most point on the die surface 13 to the back wall of the member 12. This dimension 14 is made somewhat longer than the distance between the collar 9 (and the collar Within the support structure 1 and the adjacent wall of said support structure. The die surface 13 of the U-shaped member 12 is made of a material harder than that of the support structure 1 to prevent excessive wear during the herein described method.

A form of the method will be described in connection with FIGURE 7. An additional rod is shown inserted through the holes 4 and 7 on the structure; and a further rod 16 is shown inserted through the holes 5 and 8 on the structure 1. The member 12 of FIGURE 4 is inserted in the longitudinal cavity 2 of the support structure 1. As the member 12 is forced through the cavity 2 in the direction indicated by the arrow the progress of the member 12 is hampered first by the engaging of the collars or flaring surrounding the

rods

15 and 16 with the beads or die surfaces 13 of the U-shaped member 12 and then by the engaging of the beads 13 with the

collars

9 and 10 which surround rod 11. By forcing the U-shaped member 12 through the cavity 2 by suitable means, not shown, the die surfaces 13 are made to exert a force transverse to the collars. Hydraulic, air or other force exerting means can be employed. Referring to

collars

9 and 10, for example, the bead or die surfaces 13 force the engaged area of the

collars

9 and 10 inwardly, creating a similar indentation upon the rod 11. By this means the rod 11 is locked in its position with the supporting structure 1. This step in the operation is shown in FIGURE 5.

From this it can be easily visualized that the member 12 in conjunction with its die surfaces 13 performs the same operation upon each

rod

15, 16 and associaated collars as it does on rod 11 and

collars

9 and 10 as the member 12 is forced. through the longitudinal cavity 2 of the support member 1. When the U-shaped member 12 is forced past all the collars and rods, each rod will be locked in its position within the support structure 1. The member 12 can be easily pulled out from either end as the indentation formed will allow clearance of the bead or die surface. It is also clear that the same U-shaped member 12 inverted, or another suitable member will perform the identical operation upon the opposite side of the collar by moving the member through the longitudinal cavity 2 with its outer wall against the opposite Wall of the supporting structure 1.

FIG. 11 illustrates a fork-like member 17 that will cause both sides of the collars around the respective holes 3 through 8 to be indented into the rods as the member 17 is forced past such collars and rods via the longitudinal cavity 2. This member 17 can then be removed from the supporting structure 1, in a direction opposite to the direction in which the force was exerted.

An end view of the final composite structure is shown in FIGURE 6. Reference 18 indicates the typical indentations necessary to secure the rod in the supporting structure.

FIGURES 8 and 9 show configurations that will lock the rod in the supporting structure by slightly different variations of the same method. If reference is made to FIG. 10 there is shown a perspective view of a plurality of rods in a supporting structure 1 where the

collars

9 and 10 are formed by a similar process, as herein before described, but on the outside of the parallel surfaces of the supporting structure 1. The support structure 1 may be solid or hollow for this operation. Here the U-shaped member 12 having die surfaces 13 passes over the support structure and in doing so exerts a force upon each collar and rod, thereby indenting such combination exactly as in the former case, causing said rods to be locked in said supporting structure. The final composite structure produced by this variation in method is shown in FIGURE 8. The indentations referenced as 18 firmly lock the rod in the support structure.

It should be noted that the previously described operations require a suitable jig or fixture to keep the assembly, consisting of the support structure and rods, secure and properly oriented during the application of force by the member having a die-shaped surface. FIGURE 13 shows a supporting structure 1 and rod 11 secured in position within a representative fixture or jig 19. The fixture 19 can be firmly secured to a table or other body, not shown. The supporting structure 1 is held in position by the two clamp-like structures designated as 21. These in turn can be positioned by means of the adjustable bolt arrangements 22. The assembly consisting of

elements

21 and 22 and the side wall of the fixture constitutes a vise-like configuration.

It can be seen that the jig or fixture 19, although only a typical representation, can accommodate a member having die surfaces, such as the member shown in FIG. 4, 7, 10, 11 or 12, and consequently may act upon the

collars

9 and 10 whether they are as shown in FIGS. 9 and 13 or are as shown in FIGS. 2 and 8.

While the diagrams show rectangular supporting structures it is clear that the support structure may take any other desired shape, such as square, hexagonal, oval, round or even irregular as required. The member having a die-shaped surface will preferably be given a corresponding shape as to enable it to exert the required force. It is also clear that a member could be so devised as to perform an operation resulting in a composite structure as represented in FIG. 9. This can be done with a member having characteristics of both the member shown in FIG. 7 and the member shown in FIG. 10. If reference is made to FIG. 12, the member 25 shown will perform the operation resulting in the composite structure shown in FIG. 9. It is also clear that the holes fabricated in the support structure can take on any irregular shape corresponding to any type of rod to be inserted in such holes.

A feature of applicants invention is that no parts other than the rod and support structure itself are required to firmly lock the rod on the support structure. No rivets, clamps, or other means are needed. The invention is particularly useful in applications where a large number of rods are to be supported. In the past, each rod had to be secured in turn so that each rod required a separate, individual operation involving a number of different steps. By the present invention, a plurality of rods can be substantially simultaneously locked to a support structure by a single action, namely, the movement of the die member. Further, since it is not necessary to drill holes in the rods or otherwise remove surface portions of the rods, the rods are not structually weakened.

What is claimed is:

1. Apparatus comprising a hollow supporting member that is long as compared with its transverse dimensions so that it is of pipe-like configuration, said member being of such size and relative dimensions that there is restricted access to the interior of said member, said member having holes in one side thereof which are spaced along the length of said member and also having holes in the opposite side of said member which are directly opposite the holes in said one side whereby there are pairs of opposing holes, each of said holes in said one side having a collar surrounding it with said collars located in the interior of said member, a rod positioned in each pair of opposing holes whereby each rod is surrounded by and is in contact with one of said collars, each of said collars being indented into each of said rods whereby said rods are firmly secured to said supporting member.

2. The combination as claimed in claim 1 wherein said collars are of the same material as said member and are integral therewith.

3. Apparatus comprising a hollow supporting member that is long as compared with its transverse dimensions so that it is of pipe-like configuration, said member being of such size and relative dimensions that there is restricted access to the interior of said member, said member having holes in one side thereof which are spaced along the length of said member and also having holes in the 0pposite side of said member which are directly opposite the holes in said one side whereby there are pairs of opposing holes, each of said holes having a collar surrounding it, at least the collars on one side of said member being located in the interior of said member, said collars being of the same material as said member and being integral therewith, a rod positioned in each pair of opposing holes so that each rod is surrounded by two of said collars, each of said two collars surrounding a rod being indented into that rod whereby said rods are firmly secured to said supporting member.

4. Apparatus comprising a hollow supporting member that is long as compared with its transverse dimensions so that it is of pipe-like configuration, said member being of such size and relative dimensions that there is restricted access to the interior of said member, said member having holes in one side thereof which are spaced along the length of said member and also having holes in the opposite side of said member which are directly opposite the holes in said one side whereby there are pairs of opposing holes, each of said holes having a collar surrounding it and located in the interior of said member, said collars being of the same material as said member and being integral therewith, a rod positioned in each pair of opposing holes so that each rod is surrounded by and is in contact with two of said collars, each of said two collars in contact with a rod being indented into that rod whereby said rods are firmly secured to said supporting member.

5. An antenna comprising a hollow mast that is long compared with its transverse dimensions so that it consists of a pipe-like configuration, said mast being of such size and relative dimensions that there is restricted access to the interior of said mast, said mast having holes in one side thereof which are spaced along the length of said mast and also having holes in the opposite side thereof which are directly opposite the holes in said one side whereby there are pairs of opposing holes, each of said holes having a collar surrounding it and located in the interior of said mast, said collars being of the same material as said mast and being integral therewith, a refiector rod-like member positioned in each pair of opposing holes so that each member is surrounded by and is in contact with two of said collars, each of said two collars in contact with a member being indented into that member whereby said members are firmly secured to said mast.

References Cited UNITED STATES PATENTS 472,893 4/ 1892 Little. 1,093,914 4/1914 Close. 1,288,706 12/ 1918 Shanahan et a1. 1,519,166 12/ 1924 Rauch. 2,744,674 5/ 1956 Smith.

3,074,149 1/1963 Rademaker et a1. 29--520 X 3,325,879 6/1967 Morkoski 29--432.2 X

FOREIGN PATENTS 759,550 10/1956 Great Britain.

875,367 8/ 1961 Great Britain.

893,410 4/ 1962 Great Britain. 1,151,838 2/1958 France.

1,335,923 7/ 1963 France. 1,335,924 7/1963 France.

CHARLIE T. MOON, Primary Examiner.

US. Cl. X.R. 343818