US3128467A - Dielectric rod radiating antenna - Google Patents

Description

April 7, 1964 n. H; LANCTOT 3,128,467

DIELECTRIC ROD RADIATING ANTENNA Filed Feb. 19, 1960 2 Sheets-Sheet 1 Fla. :1

Fia. 3 BY: Mdm?! April 7, 1964 D. H. LANcTo-r 3,128,467

DIELECTRIC ROD RADIATING ANTENNA Filed Feb. 19, 1960 2 Sheets-Sheet 2 /IVVE/V'O. DONALD H. LNCTOT ma TTIQ/Eyf United States Patent 'O 3,128,467 DIELECTRIC RGD RADIATlNG ANTENNA Donald H. Lanctot, Malibu, Calif., assigner to Don-Lan Electronics Co., Inc., a corporation of California Filed Feb. 19, 1960, Ser. No. 9,771 8 Claims. (Cl. 343-708) This invention relates generally to antennas and more particularly to an improved broad band high frequency antenna for airborne equipment.

In airborne antenna structures employed with radar equipment such as seeker, guidance, Search or fire control systems for example, a single, symmetrical direction lobe or beam characteristic is desirable. Heretofore, a directional beam has been accomplished by exponential horns, parabolic reflectors, metallic lens arrays, and the like. Such structures, while providing a directive antenna, are oftentimes relatively large and bulky, particularly for lower frequency operations. Moreover, in exposed airborne antenna systems, radomes or equivalent aerodynamic streamlining structures have been required thus further increasing bulk and Weight.

In addition to the foregoing, the use of specially designed horns, reflectors, or metallic lens type of structures for forming a desired beam, generally tends to limit the band width of the antenna to a considerable extent. This is because the directing structures are dimensioned in accordance with a contemplated wave length of operation, and large deviations from this wave length will result in similar deviations in the desired antenna pattern. Also, deviations in the wave length for these same reasons can result in serious mismatching of some of the components thus posing tuning problems.

In many installations, once a desired beam pattern is provided by any particular system, to change the beam width or lobe pattern symmetrically usually necessitates a major change in most of the directive elements of the system. Thus, there is a lack of versatility in the use of the system.

Finally, there is the ever present difculty of side lobes in the directional beam pattern. Generally, side lobes can be attenuated, canceled, or otherwise eliminated by employing more sophisticated structures, but such solutions add further to inherent bulk and cost.

From the foregoing, it will be evident that antenna design for providing desirable lobe patterns for use in missiles becomes an important and serious problem. Any additional bulk or mass in an antenna system necessarily diminishes the pay load which the missile can carry by that extent. While theoretical and even structural solutions to most of the problems encountered in providing a broad band directive antenna system can be elfected in the laboratory, as a practical matter, the resulting system is often prohibitive in size and weight for use on any high speed missile.

With all of the above in mind, it is a primary object of the present invention to provide a vastly improved general purpose broad band antenna in which extreme miniaturization is achieved thereby overcoming many of the foregoing problems encountered in airborne antennas.

More particularly, it is an object to provide a miniaturized broad band antenna for use in high speed missiles which is characterized by optimum electromagnetic radiation in a desired pattern and optimum aerodynamic streamlining to the end that radomes and other auxiliary structures are not necessary.

Another important object is to provide a broad band antenna which is simple in mechanical design and extremely rugged in construction thereby providing an ideal antenna system for use on rockets and missiles.

Another object is to provide a broad band miniature antenna having a directional beam pattern with substan- 3,128,467 Patented Apr. 7, 1964 lCC tially no side lobes and in which a given beam width may be maintained within an accuracy of i 1 Still another object is to provide an antenna in which the beam pattern may be varied by simple substitution of components in the system so that an extremely versatile antenna system results.

A particular object of the invention is to provide .a miniaturized broad band high frequency antenna capable of withstanding high temperatures of the order of 2,000" F., and high speeds of the order of Mach 6 when used on the leading edge of a control surface or nose of a supersonic missile.

Briefly, these and many other objects and advantages of this invention are attained by the use of an extremely high dielectric material as a lens for the electromagnetic energy to be radiated or received. The high dielectric constant of the material enables a considerable scaling down of all of the antenna dimensions for effecting a desired pattern because of the effective decrease in electrical Wave length of the energy in the material as compared to its wave length in air.

In a preferred embodiment, the antenna includes a hollow conducting body terminating at one end in a coaxial connector to receive input energy and at its other end in a sleeve for receiving the dielectric lens for radiating the energy. The dielectric lens itself is in the form of a solid rod having a cylindrical portion received in the sleeve and its remaining portion tapering towards a point.

A unique coupling means is provided within the conducting body between the connector and the base of the cylindrical section of the rod member. This 'coupling structure enables desired tuning to be achieved to provide perfect impedance matching by simply rotating the rod member itself within the sleeve through small angles.

The tapered front end portion of the rod not only provides a directing lens structure for electromagnetic energy, but also provides the desired aerodynamic streamlining necessary to minimize drag when the antenna is employed on a missile.

A better understanding of the invention will be had by referring to the accompanying drawings, in which:

FIGURE 1 is a perspective View of a preferred embodiment of the antenna of this invention;

FIGURE 2 is an enlarged view partly in cross section of the central portion of the antenna illustrated in FIG- URE l;

IFIGURE 3 is a cross section taken in the direction of the arrows 3 3 of FIGURE 2;

FIGURE 4 is a fragmentary perspective 'View partly cut-away of a modified antenna;

FIGURE 5 is a fview similar -to FIGURE 4 of still another modiiied antenna; and,

FIGURE -6 is a simple schematic diagram illustrating a beam pattern typical of Ithe antenna of this invention.

Referring rst to FIGURE 1, the antenna comprises a hollow conductingbody 10 terminating at one end in a co-axial input connector 11 and at its other end in asleeve 12. A rod member of high dielectric material includes at its rearward end acylindrical section 13 partially received within the `sleeve 12 and at its forward end atapered portion 14 andfront end portion 15. Agland nut 16 of exterior conical shape for aerodynamic streamlining is provided for securing the antenna in a desired position.

Input electromagnetic energy is fed to the antenna through the connector 11 and radiated from the dielectric rod member which serves as a lens for providing a highly eifective lobe pattern with substantitally no side lobes present.

It will be evident from t-he appearance as illustrated in FIGURE 1 that the structure is aerodynamically coni half degrees.

3 toured for minimum drag, and in actual practice, will operate under speeds as high as Mach 6 and at temperatures of 2,000 F.

The dielectric material itself may comprise, for example, sintered zirconium oxide. Alternatively, aluminum oxide or titanium `oxide may be used to provide the ydesired high dielectric constant. In some instances, the material may constitute a sintered mixture of these oxides. The resulting material is extremely strong mechanically and has a dielectric constant of from l` to 22. Thus electrical lengths within the material are reduced by a considerable factor enabling the desired miniaturization to be effected over a broad band of frequencies.

Referring to the cross-section of FIGURE 2, there is illustrated the unique coupling means in accordance with the invention for transferring electromagnetic energy from the input connector 11 to thecylindrical section 13 of the dielectric lens. As shown, the conductingbody 10 forms a con-tinuation of the outer conductor of the connector 11 and theinner conductor 17 thereof extends in co-axial alignment with thebody 10, -sleeve portion 12 and the rod member. The extreme end of theinner conductor 17 terminates in acylindrical cavity 18 telescopically receiving one end of a `co-axially disposed probe 19. By this arrangement a thermal expansion joint is provided. rThe other end of the probe 19* extends towards the base of thecylindrical 4portion 13 of the lens rod member and is curved at 20 to form a laterallybent portion 21 juxtaposed the base and connected at 22 to thebody 10. The bend itself is less than 90 degrees with respect to the longitudinal axis o-f the body and probe -so that thelateral bent portion 21 lforms an acute angle A with respect to the plane of the base of the rod member.

Thecylindrical section 13 of the rod member is provided with aconductive coating 23 surrounding only that portion of the cylindrical section within thesleeve 12. rlhis coating may be silver and as shown best in FIG- URE 3 extends `over a circumferential edge portion of the base to provide a sector shapedcoating 24. This sector shaped coating is defined by the edge of the coating on the base converging from the circumferential edge portion of the base towards the central axis of the body.

The probe itself is held in co-axial relationship and properly matched for transfer of electromagnetic energy to the laterallybent portion 21 byydielectric material 25 lling a portion of the annular space between the probe and the interior of thebody 10. As shown, thedielectric material 25 terminates in aconical surface 26 adjacent to the exit point -of the laterally bent portion `21 of the probe.

With the foregoing Idescribed coupling arrangement, a variable inductive coupling is effected between the sector shapedcoating 24 and laterallybent portion 21. Tuning of this coupling Ifor maximum power transfer from the probe -to the rod member can be effected by slight rotations yof the rod member within thesleeve 12 as indicated by thearrow 27 in FIGURE l or 27 in FIGURE 3. For example, small rotations through angles less than the angle of convergence of the sector shaped coating will provide a iine tuning for transfer of energy for a given mode of excitation in the rod member. `On the other hand, a rotation of thedielectric rod member 13 through ninety degrees to reposition the sector shapedcoating 24 to the position illustrated at 24 in dotted lines in FIGURE 3, for example, will alter the mode of excitation to provide circular polarization.

It has been found that by employing a coupling means as described, a near perfect impedance match from the input connector to the radiating medium can be achieved over a very broad frequency range. In this respect, the acute angle A formed by the laterally .bent portion 21 with respect to the sector shaped coating is important and in a preferred embodiment is approximately two and one Thus, the capacitance between different portions of the laterally bent part of the probe and the sector shaped conductive coating fvaries along the length of the laterally bent portion;` not only as a consequence of the variable spacing because of the angle A but also because of the convergence of the sector shaped coating itself. The equivalent tuned circuit provided by the coupling struct-ure is thus very broad to enable broad band operation with excellent power transfer throughout the band range.

Generally the type of pattern or lobe can be controlled by the diameter of the dielectric rod member or lens. This in turn is determined by the frequency mode of the energy in the lens. For example, the rod may function as a circular wave guide supporting the TE-ll mode. With this type of operation, the beam width of the lobe can be controlled by varying the length of the dielectric member. IBecause of the telmcoped connection of thesection 13 in thesleeve 12, it is a simple matter to remove -the rod member itself and insert another rod member of different length in accordance with a desired beam width.

In instances requiring an extremely narrow beam width such Ias in iilre control or tracking operations, modifications other than :a 4change in length of the antenna lens structure may be effected.

Referring to FIGURE 4, for example, there is shown a modified ,antenna structure comprising :a conducting body `having a sleeve 2S for receiving acylindrical portion 29 of a dielectric rod. This cylindrical portion is partially coa-ted with a highly conductive `material as indicated at C10 and is coupled to a laterallybent probe portion 31 all as described in detail in connection with FIG- URES l, 2, and 3.

In FIGURE 4, the remaining portion of the dielectric rod member extend-ing trom thesleeve 28 is provided with a plurality ofconductive bands 32, 33, 34,4and 35. These bands are of progressively decreasing axial spacing, as indica-ted by the successive dimensions d1, d2, d3 and d4, and of progressively decreasing wid-th, as indicated by S1, S2, S3, 4and S4 in ia direction away from the sleeve towards the extreme end of the rod member. Essentially, these conductive bands serve as directors i-n a manner analogous to the directors employed in a Yagi array.

An even narrower beam width may be -achieved in yet another manner as illustrated in FIGURE 5. In this modification, there is sho-wn a body member having asleeve portion 36 receiving `a cylindrical section A37 of a rod member provided with aconductive coating 38 for coupling to the lateralbent portion 39 of a probe all as described heretofore in connection with FIGURES 1, 2, and 3. The remaining portion of thedielectric rod member 37 however terminates in a frontcylindrical cavity 40 provided with a metallic coating or lining 41. This cavity is Iarranged to receive a cylindrical section of anadditional rod memiber 42 of decreased diameter. Similarly, therod member 42 is provided with a frontcylindrical cavity 43 andconductive lining 44 for receiving the cylindrical section or rear portion of anotherdielectric rod 45 of further reduced diameter. Therod 45 in turn may be provided with a frontcylindrical cavity 46 andliner 47 for receiving an end rod 4S terminating in a front point.

There is thus provided a plurality of additional rod members of progressively decreasing diameter telescoped in end to end relationship. The operation is analogous to a plurality of optical lens axially aligned and dimensioned to provide :a pencil like beam of light. By this method, the resulting electromagnetic beam width can be reduced to substantially four degrees.

FIGURE 6 illustrates by way tof example, anantenna 49 in which the principal lobe pattern Si) is outlined schematically. The beam width :angle is indicated by the letter B. As shown, anyside lobes 51 are virtually eliminated. Further, for the TE-ll mode, the E and H held patterns ,are substantially identical.

From the foregoing description, it will be evident that the present invent-ion has provided a greatly improved broad band antenna. The features of streamlining and miniaturization renders the antenna extremely useful for missile applications wherein weight and space are at a premium. Not only is tuning extremely simplified by the simple expedient of rotating the `dielectric lens or rod member within the cylindrical sleeve, but this construction also enables substitution of dilerent lenses to be elected in a simple manner thereby providing greater versatility. Moreover, the feeding is linear throughout thereby again iacilitating aerodynamic design .and minimizing overall dimensions.

Modications that fall clearly within the scope and spirit of :this invention will occur to those skilled in the art. The broad band antenna is therefore not to be thought of las limited solely to the particular embodiments set forth merely for illustrative purposes.

What is claimed is:

1. A broad ibiand high frequency antenna comprising, in combination: 4a hollow conducting body terminaing at one end i-n a co-axial connector and :at i-ts other end in a sleeve -in co-axial valignment with said connector; Ia rod member of high dielectric material having a cylindrical section received within said sleeve and rotatable therein, the remaining portion of said rod extending from` the end of said sleeve in .axial alignment therewith; a probe co-:axially disposed within said body having one end connected to the inner conductor of said connector and its other end terminating in a laterally bent portion in juxtaposed relationship to the base of said cylindrical section, said laterally `bent portion being bent less than 90 degrees with respect to the taxis of said body to form an acute angle with the plane of said base, the extreme end of said bent portion being connected to said body; and a conductive coating surrounding the exterior cylindrical surf-ace of that portion 'of said cylindrical section `of said rod within said sleeve, said coating extending over a circumferential edge portion `yci" said base at the end of said cylindrical section to provide la sector shaped coating on said base, said sector shaped coating lbein-g defined by converging edges of said coating extending from said circumferential edge portion towards the central axis of said rod, said laterally bent portion and said sector shaped coating constituting ya coupling ffor transferring electromagnetic energy passed into said connector to said rod member, said trod member serving as la directive lens for said electromagnetic energy, rotation of said rod member through small angles less than the angle of convergence of said sector shaped coating servi-ng to vary the position of said sector shaped coating with respect to said laterally bent portion of said probe to tune said coupling for maximum power transfer, tand rotation of said rod member over ninety degrees serving to alter the mode of excitation of said electromagnetic energy in said rod member transferred from said connector to said rod memlber.

2. The subject matter of claim 1, in which the inner conductor of said connector terminates in a front cavity telescopically recieving said one end of said probe to provide a thermal expansion joint; and dielectric material lling at least a portion of the annular space between said probe and the interior walls of said body, said dielectric material supporting said probe in co-axial relationship in said body and terminating in a conical surface at said laterally bent portion to provide an impedance match between said connector and said laterally bent portion.

3. The subject matter of claim 2, in which the remaining portion of said rod member tapers towards a point in a direction away from said sleeve and includes a plurality of conducting bands of decreasing axial spacing and decreasing width in said direction to provide director elements for said electromagnetic energy.

4. The subject matter of claim 2, in which the remaining portion of said rod member terminates in a plurality of additional rod members having cylindrical sections of successively decreased diameter respectively, the foreward ends of said additional rod members having cylindrical cavities for receiving the cylindrical sections of the next successive rod members respectively to hold said rods in partially telescoped, co-axial, end to end relationship, the last of said additional rods terminating at its free end in a point; and conductive linings in said cavities respectively surrounding those portions of said cylindrical sections received therein.

5. A broad band high frequency antenna comprising, in combination:

a hollow conducting body terminating at one end in a co-axial connector and at its other end in a sleeve;

a rod member having a cylindrical section Within said sleeve, the remaining portion of said rod extending from the end of said sleeve, said connector, sleeve, and rod member all being co-axially aligned;

coupling means within said body between said connector and cylindrical section of said rod member for transferring electromagnetic energy passed into said connector to said rod member, said rod member functioning as a wave guide for radiating said electromagnetic energy, said coupling means including a probe telescopically coupled at one end to the inner conductor of said co-axial connector to provide a thermal expansion joint and terminating at its other end in a laterally bent portion in juxtaposed relationship to the base of said cylindrical section of said rod member and connected at its end to said sleeve; and

a conductive coating over a portion of said base in spaced relationship to said laterally bent portion, whereby the degree of coupling of electromagnetic energy from said laterally bent portion to said conductive coating can be varied by rotating said cylindrical section about its longitudinal axis Within said sleeve.

6. The subject matter of claim 5, in which said conductive coating is sector shaped With the edges of said sector converging from a circumferential edge portion of said base towards the longitudinal axis of said cylindrical section, said laterally bent portion of said probe forming an acute angle with the plane of said base.

7. The subject matter of claim 5, in which the remaining portion of said rod member tapers towards a point in a direction away from said sleeve and includes a plurality of conducting bands of decreasing axial spacing and decreasing width in said direction to provide director elements for said electromagnetic energy.

8. The subject matter of claim 5, in which the remaining portion of said rod terminates in a plurality of additional rod members having cylindrical sections of successively decreased diameter respectively, the forward ends of said additional rod members having cylindrical cavities for receiving the cylindrical sections of the next successive rod members respectively to hold said rods in partially telescoped, co-axial, end to end relationship, the last of said additional rods terminating at its free end in a point; and conductive linings in said cavities respectively surrounding those portions of said cylindrical sections received therein.

References Cited in the 'le of this patent UNITED STATES PATENTS 2,407,690 Southworth Sept. 17, 1946 2,761,137 Van Atta Aug. 28, 1956 2,761,139 Dillon Aug. 28, 1956 2,823,381 Martin Feb. 11, 1958 2,880,399 Murphy Mar. 31, 1959 2,921,277 Goubau Jan. l2, 1960 2,973,491 Maciszewski Feb. 28, 1961 2,977,593 Kienow Mar. 28, 1961 FOREIGN PATENTS 1,086,790 France May 4, 1955

Claims (1)

1. A BROAD BAND HIGH FREQUENCY ANTENNA COMPRISING, IN COMBINATION: A HOLLOW CONDUCTING BODY TERMINATING AT ONE END IN A CO-AXIAL CONNECTOR AND AT ITS OTHER END IN A SLEEVE IN CO-AXIAL ALIGNMENT WITH SAID CONNECTOR; A ROD MEMBER OF HIGH DIELECTRIC MATERIAL HAVING A CYLINDRICAL SECTION RECEIVED WITHIN SAID SLEEVE AND ROTATABLE THEREIN, THE REMAINING PORTION OF SAID ROD EXTENDING FROM THE END OF SAID SLEEVE IN AXIAL ALIGNMENT THEREWITH; A PROBE CO-AXIALLY DISPOSED WITHIN SAID BODY HAVING ONE END CONNECTED TO THE INNER CONDUCTOR OF SAID CONNECTOR AND ITS OTHER END TERMINATING IN A LATERALLY BENT PORTION IN JUXTAPOSED RELATIONSHIP TO THE BASE OF SAID CYLINDRICAL SECTION, SAID LATERALLY BENT PORTION BEING BENT LESS THAN 90 DEGREES WITH RESPECT TO THE AXIS OF SAID BODY TO FORM AN ACUTE ANGLE WITH THE PLANE OF SAID BASE, THE EXTREME END OF SAID BENT PORTION BEING CONNECTED TO SAID BODY; AND A CONDUCTIVE COATING SURROUNDING THE EXTERIOR CYLINDRICAL SURFACE OF THAT PORTION OF SAID CYLINDRICAL SECTION OF SAID ROD WITHIN SAID SLEEVE, SAID COATING EXTENDING OVER A CIRCUMFERENTIAL EDGE PORTION OF SAID BASE AT THE END OF SAID CYLINDRICAL SECTION TO PROVIDE A SECTOR SHAPED COATING ON SAID BASE, SAID SECTOR SHAPED COATING BEING DEFINED BY CONVERGING EDGES OF SAID COATING EXTENDING FROM SAID CIRCUMFERENTIAL EDGE PORTION TOWARDS THE CENTRAL AXIS OF SAID ROD, SAID LATERALLY BENT PORTION AND SAID SECTOR SHAPED COATING CONSTITUTING A COUPLING FOR TRANSFERRING ELECTROMAGNETIC ENERGY PASSED INTO SAID CONNECTOR TO SAID ROD MEMBER, SAID ROD MEMBER SERVING AS A DIRECTIVE LENS FOR SAID ELECTROMAGNETIC ENERGY, ROTATION OF SAID ROD MEMBER THROUGH SMALL ANGLES LESS THAN THE ANGLE OF CONVERGENCE OF SAID SECTOR SHAPED COATING SERVING TO VARY THE POSITION OF SAID SECTOR SHAPED COATING WITH RESPECT TO SAID LATERALLY BENT PORTION OF SAID PROBE TO TUNE SAID COUPLING FOR MAXIMUM POWER TRANSFER, AND ROTATION OF SAID ROD MEMBER OVER NINETY DEGREES SERVING TO ALTER THE MODE OF EXCITATION OF SAID ELECTROMAGNETIC ENERGY IN SAID ROD MEMBER TRANSFERRED FROM SAID CONNECTOR TO SAID ROD MEMBER.

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