OMNIDIRECTIONAL ANTENNA ASSEMBLY

Abstract: An omnidirectional antenna assembly for use with a satellite and others includes a turnstile antenna, a first (44) and a second (46) reflector which are positioned to face each other, and a third reflector (48) connecting the first and second reflectors to each other. The third reflector is provided with a frustoconical configuration and made of good conductor, whereby the range of antenna gain is broadenen.

Description: The present invention relates to an omnidirectional antenna assembly having a wide range of antenna gain and applicable to a satellite and others. More particularly, the present invention is concerned with an omnidirectional antenna assembly whose gain range is broadened by combining a reflector of a turnstile antenna and another reflector, e. g., a reflector constituting part of a satellite body or a reflector of a biconical antenna or like antenna which serves as a second antenna in relation to the turnstile antenna. A turnstile antenna is an omnidirectional antenna which is extensively used with a satellite and others. The turnstile antenna has a reflector which is spaced from and electrically connected to another reflector by a feeder cable. A problem with such an antenna is that the primary radiation from one of the reflectors and the secondary reflection (reflected wave) from the other reflector interfere with each other, resulting that at angles ϑ of radiation pattern adjacent ±90° great ripples are developed and the level is sharply lowered to reduce range of gain available. A biconical antenna, the combination of a turnstile antenna and a biconical antenna, and the like are also known in the art as omnidirectional antennas, but they have the same problem as the turnstile antenna. All embodiment of the invention to be described aims to provide an omnidirectional antenna assembly which is free from the interference of the primary and secondary radiations as caused by the independent reflectors and, therefore, attains a wider range of antenna gain. Previously made proposals known to the applicants will be described below, together with embodiments of the invention which are given by way of examples, with references to the accompanying drawings in which:- Fig. 1: is a perspective view of a prior art turnstile antenna with a reflector; Fig. 2: is an external view of a prior art antenna assembly made up of a turnstile antenna and a biconical antenna; Fig. 3: shows a chart representative of a radiation pattern particular to any of the antennas of Figs. 1 and 2; Fig. 4: is a perspective view showing an omnidirectional antenna in accordance with the present invention; Fig. 5: is a chart representative of a radiation pattern particular to the antenna of Fig. 4; Fig. 6: is a perspective view showing another embodiment of the present invention; Fig. 7: is a sectional side elevation of the antenna assembly of Fig. 6; and Fig. 8: is a chart representative of a gain pattern particular to the antenna assembly of Fig. 6 and 7. To better understand the present invention, a brief reference will be made to prior art antenna assemblies. Referring to Fig. 1, a prior art turnstile antenna is shown and generally designated by the reference numeral 10. As shown, the turnstile antenna 10 includes a reflector 12 on which turnstile elements, or whip elements, 14 are mounted. Another reflector 16 which constitutes part of a satellite body is provided in such a manner as to face the reflector 12 while being spaced from the latter. The reflectors 12 and 16 are electrically connected to each other by a feeder cable 18. On the other hand, Fig. 2 shows an antenna which is implemented with the combination of the turnstile antenna 10 of Fig. 1 and a biconical antenna 20 which is also known in the art. In the arrangement of Fig. 2, the reflector 16 of the biconical antenna 20 serves as a second antenna. Fig. 3 shows a radiation pattern particular to any of the prior art antennas as shown in Figs. 1 and 2. As shown in Fig. 3, at angles ϑ adjacent ±90° and onward, great ripples and sharp falls of the level occur due to the inteference of the primary reflection from the reflector 12 and the secondary reflection (reflected wave) from the reflector 16, critically limiting the range of practical use. Referring to Fig. 4, an omnidirectional antenna assembly embodying the present invention is shown. This antenna assembly, generally 40, is made up of four whip elements, or turnstile elements 42, a first reflector 44, and a second reflector 46 which is mounted on a satellite body, not shown. The first and second reflectors 44 and 46 are connected to each other by a frustoconical reflector 48. In this configuration, the reflectors 44 and 46 and the frustoconical reflector 48 apparently constitute a single solid reflecting body. It will be seen from the radiation pattern of Fig. 5 that such a reflecting body allows waves to be propagated even to the back of the reflectors due to radio frequency (FR) current, which flows through the frustoconical section. Specifically, the radiation pattern of Fig. 5 shows that a gain lower than peak gain by 5 dBi is maintained over the angle ϑ of approximately ±140°, i.e., radiation occurs over a far broader angular range than in the prior art antennas. Referring to Fig. Figs. 6 and 7, another embodiment of the present invention is shown. An omnidirectional antenna assembly 60 of this particular embodiment is constituted by the combination of a turnstile antenna 62 for telecommand/ranging reception and another type of antenna, e.g., a biconical antenna 64 for telemetry/ranging transmission, so that among various applications the application to a satellite may be facilitated. In a prior art combination of a turnstile antenna and a biconical antenna, e.g., the combination type antenna 22 of Fig. 2, the reflection pattern of the turnstile antenna is prevented from reaching the back of the reflector due to the influence of the reflector 16, as shown in Fig. 3. In contrast, in the antenna assembly 60 in which the reflectors 44 and 72 are connected to each other by the frustoconical reflector 48, the reflection pattern covers even the back, as shown in Fig. 8. In detail, as shown in Figs. 6 and 7, the turnstile antenna 62 is mounted on the top of the biconical antenna 64 and provided with the four whip elements 42, reflector 44, and frustoconical reflector 48. The whip elements 42 are connected to a hybrid type combiner 66 which is accommodated in a space that is defined by the frustoconical reflector 48. When the turnstile antenna 62 receives circularly polarized waves, induced signals on each elements 42 of the antenna 62 are equal in amplitude, but different in quarter phase between nearby elements 42. These four induced signals are combined by the hybrid combiner 66 to become one signal and fed to a transponder, not shown. The antenna radiation pattern is axially symmetrical cardioid from +Z axis which is the center axis of the assembly 60, as shown in Fig. 6. The biconical antenna 64 comprises a number of inclined slots 66 (slant angle of approximately 45°) equally spaced about the circumference of an outer conductor 70 of coaxial line, and two circular plate reflectors 72 and 74. A double coaxial line 76 is disposed in a central part of the antenna 64 for inputting and outputting RF signals. The antenna 64 radiates left-hand circular polarized (LHCP) wave in the perpendicular plane to the Z axis. It has the peak gain on the direction perpendicular to the Z axis and generates an axially symmetrical troidal RF pattern. The antenna gain pattern shown in Fig. 8 was produced under the conditions of a frequency of 6. 17 GHz, a receive (Rx) polarization of RHCP (right-hand circular polarized) wave, and a measured plane of  = 0°. In Fig. 6, assume a coordinates system of the antenna assembly 60. Then, the plane of  = 0° is the X-Z plane. In summary, it will be seen that the present invention provides an omnidirectional antenna assembly in which two reflectors are interconnected by a frustoconical reflector to allow a reflection pattern to reach even the back of the reflectors, broadening the range of antenna gain. Various modifications will become possible for those skilled in the art after receiving the teachings of the present disclosure without departing from the scope of the invention as defined in the appended claims.

Claims: An omnidirectional four-element whip antenna assembly (60) including a first disk shaped reflector (44) having an outer perimeter, four whip elements (42) mounted on a first side of the first reflector (44) on which the whip elements (42) receive electromagnetic waves reflected by the first reflector (44), a second reflector (46) and means (18) electrically connecting the first and second reflectors (44) (46), characterised in that the electrical connecting means (18) includes a frustoconical shaped reflector (48) which, at one end, is located on and connected to a second side of the first reflector (44), the frustoconical reflector being flared away from the outer perimeter of the first reflector (44) and the other end of the frustoconical reflector (48) being connected to the second reflector (46). An omnidirectional antenna assembly as claimed in claim 1, wherein the second reflector (46) is made of a material which is electrically conductive. An omnidirectional antenna assembly as claimed in claim 1, wherein the second reflector (46) constitutes a part of a body of an apparatus on which the antenna assembly (60) is supported. An omnidirectional antenna assembly as claimed in claim 1, wherein the second reflector (46) forms part of a further antenna (64). An omnidirectional antenna assembly as claimed in claim 4, wherein the further antenna (64) is a biconical antenna. An omnidirectional antenna assembly as claimed in claim 1, wherein the said reflector (46) is disk shaped.

Inventors: MOCHIZUKI, AKIO C/O NEC CORPORATION
Applicants: NEC CORPORATION
Application year: 1987
Main classification: H01Q21
IPC codes: H01Q21, H01Q19, H01Q1