The present invention relates to a waveguide for use in a dual polarization waveguide probe system for use with a satellite dish receiving signals broadcast by a satellite which includes two signals orthogonally polarized in the same frequency band. In particular, the invention relates to an improved waveguide for use with a low-noise block receiver into which two probes are disposed for coupling from the waveguide, desired broadcast signals to external circuitry.
In applicant's co-pending Published International Application WO92/22938, there is disclosed a dual polarization waveguide probe system in which a waveguide is incorporated into a low-noise block receiver in which two probes are located for receiving linearly polarized energy of both orthogonal senses. The probes are located in the same longitudinal plane on opposite sides of a single cylindrical bar reflector which reflects one sense of polarization and passes the orthogonal signal with minimal insertion loss and then reflects the rotated orthogonal signal. The probes are spaced λg/4 from the reflector where λg is the wavelength of the signal propagating in the waveguide. A reflection rotator is also formed at one end of the waveguide using a thin plate which is oriented at 45° to the incident linear polarization with a short circuit spaced approximately a quarter of a wavelength (λg/4) behind the leading edge of the plate. This plate splits the incident energy into two equal components in orthogonal planes, one component being reflected by the leading edge and the other component being reflected by the waveguide short circuit. The resultant 180° phase shift between the reflected components causes a 90° rotation in the plane of linear polarization upon recombination so that the waveguide output signals are located in the same longitudinal plane.
Furthermore, in applicant's co-pending International Patent Application PCT/GB96/00332, an improved dual polarization waveguide probe system was disclosed for use with a wider frequency range transmitted by new satellite systems. In this improved probe, a reflective twist plate was provided within the probe housing, the reflective twist plate having at least two signal reflecting edges so that at least two separate signal reflections are created. The multiple signal reflections enable the probe system to operate over a wider frequency range with minimal deterioration and signal output.
Although the improved version provides a better frequency response across the frequency range, it has been found that the amount of loss at the edges of the band still cause a significant performance degradation. With the increasing number of channels being used in satellite systems, it is desirable to be able to operate across the entire frequency band with substantially the same performance, to provide minimal degradation at the edges of the frequency band.
An object of the present invention is to provide an improved waveguide for use with a dual polarization probe system which obviates or mitigates the aforementioned disadvantage.
This is achieved by providing a waveguide for use with a dual polarization waveguide probe system which has a rotator which incorporates a reflecting plate in combination with a differential phase shifter in the form of a waveguide of slightly asymmetrical cross section so that orthogonal signals which travel through this portion have a different cut-off wavelength. This results in a rotator which achieves 180° of phase shift between two orthogonal components across the frequency range of signals received by the waveguide. The reflecting plate and the differential phase shifter have inverse frequency characteristics so that the combined phase shift characteristic of the rotator has a flatter frequency response across the desired frequency range.
In a preferred arrangement, the rotator consists of a single reflector plate with a single reflecting surface and the differential phase shifter has two pairs of flats cast into the waveguide bore, a first pair of flats being machined in at a first distance from the reflector plate and a second pair of flats machined nearer to the reflector plate at a second distance from the reflector plate, the second pair of flats being machined at a shallower depth than the first pair so that the flats of the second pair are nearer to the central axis of the waveguide. In an alternative arrangement, the rotator consists of a single reflector plate in an elliptical waveguide portion coupled to the cylindrical waveguide portion. The different cross-sections of the ellipse provide two different cut-off wavelengths for the orthogonal signals. The differential phase shifter may be implemented by any other suitable structure which has a slight cross-sectional asymmetry to create wavelengths with different cut-offs.
According to a first aspect of the present invention, there is provided a waveguide for use with a dual polarization waveguide probe system for receiving at least two signals which are orthogonally polarized, the waveguide comprising a waveguide tube into which at least two orthogonally polarized signals are received for transmission therealong, the waveguide having:
Preferably, the rotator plate has a single reflecting edge portion across the width of the waveguide. Conveniently, the differential phase shifter is provided by an asymmetric structure in the form of flats cast into the interior of the waveguide structure. Preferably, two flats are provided on each side, the flats being parallel with and extending along the waveguide from the reflector plate. Alternatively, the slightly asymmetric portion is provided by an elliptical waveguide. Advantageously, the upstream flats are machined a greater distance into the waveguide surface than the downstream flats with the first (downstream) flats forming an impedance matching structure.
Conveniently, the waveguide differential phase shifter is provided by at least two pairs of stepped flats. Alternatively, the asymmetric portion may be provided by a smooth transition along the waveguide without a clear step instead of the flats. The smooth transition will be cast into the side of the waveguide parallel to the reflecting edge portion.
According to a second aspect of the present invention, there is provided a method of receiving at least first and second orthogonally polarized signals in a frequency range in a single waveguide and providing at least two outputs in a common longitudinal plane for providing a flatter characteristic across the frequency range, the method comprising the steps of,
The signal reflector and rotator is formed by the combination of a differential phase shifter and a reflector plate. The differential phase shifter is orientated at 45° to the incident signal such that a phase shift is introduced between the first and second component of the orthogonal (horizontal) signal. A further phase shift is introduced by the reflecting plate downstream. The combination of these gives 180° phase shift between the two components on recombination, providing a resultant signal in the plane of said second probe.
According to another aspect of the present invention there is provided a dual polarization waveguide probe structure, said structure having a waveguide, first and second probes disposed in the waveguide separated by a first reflector, the first and second probes and the reflector being disposed in the same plane, a second probe signal provider for providing a polarized component to the second probe, the second probe provider comprising a signal reflector and rotator for reflecting and rotating a polarized component for reception by the second probe, the reflector and rotator comprising a reflected edge portion for reflecting a first component of the polarized signal, and a differential phase shifter provided by a slightly asymmetrical waveguide portion and a waveguide short circuit for providing a reflected second component with a different cut-off wavelength from the first component, the first and second components having inverse frequency characteristics which when recombined provide a flatter frequency characteristic across the frequency range.
These and other aspect of the invention will become apparent from the following description when taken in combination with the accompanying drawings, wherein like reference numerals refer to like and corresponding parts of the various drawings, in which:
a, 6b, 6c and 6d are graphs comparing the responses of the dual polarization waveguide probe system with the waveguide according to the embodiments shown in FIGS. 1 to 4, wherein
a and 7b show rotators with alternative arrangements of flats in the waveguide wall.
a and 8b show cross-sectional views through alternative slightly different differential phase shifters of the waveguide.
a,
10
b are side and longitudinal cross-sectional views through a waveguide with no reflector or twist plate and a differential phase shifter of flats only;
a and 13b show longitudinal sections of waveguides, similar to
Reference is first made to FIGS. 1 to 4 of the drawings in which a low-noise block receiver, generally indicated by reference numeral 10, is adapted to be mounted to a satellite receiving dish in a way which is well known in the art. As is also known, the low-noise block receiver 10 is arranged to receive high frequency radiation signals from the satellite dish and to process these signals to provide an output which is fed to a cable 12 which is, in turn, connected to a satellite receiver decoder unit (not shown in the interests of clarity). The block receiver 10 includes a waveguide 14 which is shown partly broken away in the interests of clarity to depict the interior components. The waveguide is cylindrical and is metal. The waveguide has front aperture 16 for facing a satellite dish for receiving electromagnetic radiation from a feed horn 18, shown in broken outline, which is mounted on the front of the waveguide. The waveguide and feed horn 18 are substantially the same as that disclosed in applicant's co-pending International Application PCT/GB96/00332 and WO 92/22938. Accordingly, disposed in the waveguide in the same longitudinal plane is a first probe 20, a reflective post 22 and a second probe 24 as shown in
It will be seen that the reflector plate is thin and has a single leading edge 34 which is orthogonal to the waveguide axis. Edge 34 is a fixed distance from the short circuit 32. With this arrangement, as best seen in
Referring now to FIGS. 1 to 4, in the interior of the waveguide two sets of flats, 36, 38, are cast in the side of the waveguide. In the embodiment shown, the two sets of flats 36, 38, which are disposed parallel to the reflector plate 30 as best seen in
In operation, signals from a satellite dish enter the waveguide 14 via the horn 18 and aperture 16 and, in accordance with known principles, are transmitted along the waveguide 14. The signals which are broadcast by the satellite include two sets of signals which are orthogonally polarized in the same frequency band and these are represented by vectors V1 and V2 (best seen in
Since V2P and V2O have different guide wavelengths, there will be a resultant phase shift between them per unit length of waveguide. This phase shift is a function of frequency, more phase shift being obtained at lower frequency. This can be seen by the graph shown in
As the signals travel along the waveguide the vertically polarized signal V1 is received by the first probe 20 which, as it is spaced by λ/4 from the reflecting post 22, ensures the maximum field at the probe and hence optimum coupling to the probe. The probe 20 has no effect on the horizontally polarized signal V2 which continues to pass along the waveguide.
Because the reflecting post 22 is vertically oriented, the signal V2 is not reflected by the post and continues to pass along the waveguide and also passes the second probe 24 for the same reason. As the horizontally polarized signal V2 hits the front edge of the signal reflector and rotator (the start of the flats), the signal is split into V2P and V2O as seen in
Reference is now made to
In this regard, reference is made to
c is a graph of signal return loss (dB. versus frequency) which shows that there is less signal loss across the entire frequency range compared to the existing stepped twist plate and that there is a broader band of frequency for minimal return loss which shows a general improvement across the frequency band.
Referring to
In some cases, an insertion loss may occur over a relatively narrow bandwidth of a few MHz. This is believed to be due to manufacturing tolerances which result in a slight asymmetry of the twist plate/reflector plate. One solution to this problem has been to place small semi-cylindrical protuberances 40, 42 on the reflector plate 30 as shown in
Reference is also made to
For example,
Various modifications may be made to the rotator structure for use with the waveguide as hereinbefore described without departing from the scope of the invention. For example, a single parallel flat may also be used or two or more pairs of flats may be machined into the side of the waveguide as shown in
It will be appreciated that the principal advantage of the present invention is that the reflecting and rotating arrangement allows the LNB to be used across the existing satellite bandwidth but which provides a much better frequency characteristic at the upper and lower frequency limits. This allows an increased number of channels to be used across the entire frequency band with substantially the same performance, that is providing minimal degradation at the edges of the frequency band. A further advantage of this arrangement is that it can be used with existing manufacturing techniques and does not require any special fabrication. It will also be understood that this particular apparatus and methodology may be applied to providing bandwidth improvements at frequency ranges outside the aforementioned Astra frequency range.
Number | Date | Country | Kind |
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9618744.8 | Sep 1996 | GB | national |
The present application is a continuation of application Ser. No. 11/061,561, filed on Feb. 18, 2005, now abandoned, which is a continuation of application Ser. No. 10/684,173, filed on Oct. 10, 2003, now abandoned, which is a continuation of application Ser. No. 10/094,187, filed on Mar. 8, 2002, now abandoned, which is a continuation of application Ser. No. 09/254,771, filed on Jul. 12, 1999, now abandoned, which is a continuation of Application Serial No. PCT/GB97/02428, filed on Sep. 9, 1997.
Number | Date | Country | |
---|---|---|---|
Parent | 11061561 | Feb 2005 | US |
Child | 11592795 | Nov 2006 | US |
Parent | 10684173 | Oct 2003 | US |
Child | 11061561 | Feb 2005 | US |
Parent | 10094187 | Mar 2002 | US |
Child | 10684173 | Oct 2003 | US |
Parent | 09254771 | Jul 1999 | US |
Child | 10094187 | Mar 2002 | US |
Parent | PCT/GB97/02428 | Sep 1997 | US |
Child | 09254771 | Jul 1999 | US |