U.S. patent number 3,795,914 [Application Number 05/290,563] was granted by the patent office on 1974-03-05 for rotating beacon antenna with polarization filter.
This patent grant is currently assigned to E-Systems, Inc.. Invention is credited to Sidney Pickles.
United States Patent |
3,795,914 |
Pickles |
March 5, 1974 |
ROTATING BEACON ANTENNA WITH POLARIZATION FILTER
Abstract
TACAN antennas emit modulated radiation from parasitic
reflecting elements associated with a central array having
radiating elements coupled to an energizing source. Signal energy
from the TACAN antenna is preferably radiated in a plane
perpendicular to the surface of the earth. Cross polarization
components of the radiated signal are absorbed by resistive wires
located in the radiation path from the central antenna array. These
resistive wires are mounted around the supporting structure of the
TACAN antenna.
Inventors: |
Pickles; Sidney (Colusa,
CA) |
Assignee: |
E-Systems, Inc. (Dallas,
TX)
|
Family
ID: |
23116573 |
Appl.
No.: |
05/290,563 |
Filed: |
September 20, 1972 |
Current U.S.
Class: |
343/756; 343/761;
343/872; 342/399; 343/774 |
Current CPC
Class: |
H01Q
15/12 (20130101); H01Q 3/14 (20130101); H01Q
17/001 (20130101) |
Current International
Class: |
H01Q
15/00 (20060101); H01Q 3/14 (20060101); H01Q
17/00 (20060101); H01Q 3/00 (20060101); H01Q
15/12 (20060101); H01q 019/00 () |
Field of
Search: |
;343/756,761,839,16R,744,872 |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
Primary Examiner: Lieberman; Eli
Attorney, Agent or Firm: Willborn; James D. Richards, Harris
& Medlock
Claims
1. An antenna emitting a rotating multilobed pattern of radiation,
comprising in combination:
a central array having radiating elements coupled to an energizing
source,
a plurality of parasitic elements disposed to revolve around said
array at a given radial distance therefrom to provide modulation of
radiation from said central array,
a first array of horizontal absorbing elements spaced about the
periphery of the revolving parasitic elements on a first diameter
to reduce complex polarization radiation from said antenna
pattern,
a second array of horizontal absorbing elements spaced one-quarter
wavelength from said first plurality on a second diameter to
further reduce complex polarization radiation, and means for
supporting said first and second array of absorbing elements on the
first and second diameters.
2. An antenna emitting a rotating multilobed pattern of radiation
as set forth in claim 1 wherein said first and second array
includes a plurality of resistive wires spaced about the periphery
of the revolving parasitic
3. An antenna emitting a rotating multilobed pattern of radiation,
comprising in combination:
a central array havin radiating elements coupled to an energizing
source,
a plurality of parasitic elements disposed to revolve around said
array at a given radial distance therefrom,
support means for positioning said plurality of parasitic elements
coupled to a drive motor and rotated thereby to cause rotation of
said parasitic elements around the central array for modulating the
electromagnetic energy radiated therefrom,
a plurality of absorbing elements attached to said support means in
proximity to said parasitic elements for reducing complex
polarization radiation from said antenna pattern,
additional support means positioned between said first support
means and said central antenna array, and
a second plurality of absorbing elements attached to said
additional support means between said first plurality of elements
and the central
4. An antenna emitting a rotating multilobed pattern of radiation
as set forth in claim 3 including a stationary radome enclosing
said support means and central array and including an additional
plurality of absorbing elements spaced from said first plurality of
elements around said
5. An antenna emitting a rotating multilobed pattern of radiation
as set forth in claim 4 wherein said first, second and third
plurality of absorbing elements are positioned horizontally to
minimize a horizontal
6. An antenna emitting a rotating multilobed pattern of radiation,
comprising in combination:
a drive motor,
a central array having radiating elements coupled to an energizing
source,
a plurality of parasitic elements disposed to revolve around said
array at a given radial distance therefrom,
support means for positioning said plurality of parasitic elements
and coupled to said drive motor and rotated thereby to cause
rotation of said parasitic elements around the central array for
modulating the electromagnetic waves radiated therefrom,
a plurality of resistive wires attached to said support means in
proximity of said parasitic elements for absorbing complex
polarization radiation from said antenna pattern,
additional suppport means positioned between said first support
means and said central array, and
a second plurality of resistive wires attached to said additional
support means between said first plurality of elements and the
central array to further absorb complex polarization radiation from
said antenna pattern.
7. An antenna emitting a rotating multilobed pattern of radiation
as set forth in claim 6 including a stationary radome enclosing
said support means and central array and including an additional
plurality of resistive wires spaced from said first plurality of
elements around said stationary
8. An antenna emitting a rotating multilobed pattern of radiation
as set forth in claim 7 wherein said first, second and third
resistive wires are positioned horizontally to minimize a
horizontal polarization component from the radiation pattern of
said antenna.
Description
This invention relates to a system and device for eliminating or
minimizing complex polarization radiation from an antenna
structure, and more particularly to a system and device for
absorbing radiation from a central array prior to reflection from
oblique metal surfaces.
Beacon antennas producing a rotating multilobe pattern have been
employed to radiate signals to distance measuring and radio
navigation receiving equipment, these signals are modulated by
rotation of parasitic elements around a central antenna array. One
such antenna, commonly known as a TACAN antenna, is described in U.
S. Pat. No. 2,803,821, issued to Sidney Pickles et al. Such an
antenna employs a vertically disposed radiating element as a
central array with one vertical parasitic element a given distance
from the central array and additional parasitic elements equally
spaced about the central radiating element, all at a second
distance from the central array. As the parasitic elements are
rotated about the central array, a rotating multilobe pattern of
radiation is produced. Receiving equipment responsive to the
radiation from the antenna detects a fundamental modulation of the
beacon signal due to the rotation of the one parasitic element and
a harmonic modulation due to rotation of the other parasitic
elements.
As far as transmitting antennas are concerned, it is known that one
part of the power delivered by a feed line, cable, wave guide or
similar device to the antenna is radiated, another part is
dissipated and another part is returned toward the central array by
way of reflection. Various means have been devised in the past to
eliminate, or at least to reduce, radiation reflection that
produces a cross polarization radiation from the antenna. Known
techniques include radiation absorbing devices that are mounted
adjacent to the antenna to absorb radiation in a chosen
direction.
Where such reflection radiation is allowed to be transmitted, a
complex polarization pattern is transmitted to the receiving
equipment of the air navigation system. Such complex polarization
radiation contains navigational errors.
In an air navigation system, a receiver responds to modulations
produced by the parasitic elements rotating about a central antenna
array to obtain azimuth information at any point about the
radiating station. The phase of the modulation at the receiving
point with respect to an omnidirectionally radiated reference
signal determines the obserber's azimuth. If the transmitting
antenna produces radiation polarized in a plane other than the
preferred vertical orientation, the modulation phase of the
radiation polarized other than the desired direction may well be
different from the correct modulation signal. Where a receiver
knows of the cross polarization radiation, some corrective action
may be taken. However, a receiver at a considerable distance from
the transmitter antenna oriented so as to respond to the undesired
signal, may indicate an azimuth different from the true azimuth
from the direct radiated signal and not be aware of the error. This
problem becomes particularly significant when the receiving
equipment is airborne, and wherein the aircraft maneuvers into
turns or banks which gives azimuth indications from time to time
that differ substantially, producing uncertainty in the data
presented.
A feature of the present invention is to obviate the above
disadvantages by absorbing the reflected energy to minimize or
eliminate a cross polarization component from a radiated pattern.
In the case of an antenna consisting of a central array and
parasitic elements, this result is achieved by displacing from the
central array, in the region of parasitic elements, an absorber so
that radiation is absorbed without reflection to structural
surfaces that provide the cross polarization radiation.
In accordance with one embodiment of the invention, an antenna
emitting a rotating multilobe pattern of radiation includes a
central array having radiating elements coupled to an energizing
source. A plurality of parasitic elements are disposed to revolve
around the central array at a given radial distance therefrom to
provide modulation of the radiation from the central array.
Surrounding at least a portion of the parasitic elements is a
radiation absorber for reducing complex polarization radiation from
the antenna pattern.
A more complete understanding of the invention and its advantages
will be apparent from the specification and claims and from the
accompanying drawings illustrative of the invention.
Referring to the drawings:
FIG. 1 is a pictorial view of a biconical horn TACAN antenna
employing radiation absorbing wires surrounding outer parasitic
elements;
FIG. 2 is a pictorial representation of an oblique metal surface
receiving incident radiation polarized in one direction and
reflecting radiation polarized in a second direction;
FIG. 3 is a half-section of a biconical horn TACAN antenna
employing multiple layers of radiation absorbing elements;
FIG. 4 is a cross-section of an antenna system having a rotating
drum supporting parasitic elements for both 15 and 135 Hz
modulation revolving about a central antenna array enclosed within
a radome supporting radiation absorbing elements; and
FIG. 5 is a pictorial view of a shipboard mounted radio navigation
antenna structure including radiation absorbing elements positioned
on a protective radome.
Referring to FIG. 1, there is shown a biconical horn TACAN beacon
antenna including a central antenna array 10 supplied energy
through a coaxial type transmission line 12 supplying RF energy to
the antenna. Typically, the transmission line may comprise an outer
conductor and an inner conductor wherein said outer conductor
provides a rigid support member as well as a conductor. Energy from
the main transmission line 12 is fed to the central antenna array
that includes choke joints 14 and 16 located at the apex of conical
members 18 and 20, respectively. The central antenna array 10 may
be a multi-element array consisting of two half wavelength dipoles
stacked on top of one another. A pulsed radio frequency is fed to
the antenna through the main RF feed transmission line 12. A more
complete description of such a central antenna array may be found
in the copending application of Sidney Pickles et al, Ser. No.
224,783, filed Feb. 9, 1972 entitled RADIO FREQUENCY ANTENNA
SYSTEM, as assigned to the assignee of the present invention.
The lower conical member 20 is supported on a cylinder 22 of a
dielectric material. This cylinder 22 is rotated by a drive motor
24 through a gear drive 26. The cylinder 22 (not shown in its
entirety for purposes of clarifying the drawing) extends between
the conical member 20 and the conical member 18 to provide a rigid
structure between the two members 18 and 20. This cylinder between
the members 18 and 20 has a length equivalent to one-quarter
wavelength of the frequency energizing the antenna and transfers
the rotating motion of the conical member 20 to the conical member
18. Thus, both the members 18 and 20 are rotated about the central
antenna array 10 in accordance with standard TACAN antenna
operation as described in the patent to Sidney Pickles referred to
earlier or the previously identified application.
Radio frequency energy emitting from the central antenna array 10
has no directivity in the horizontal plane. To convey bearing
information to a receiver, pulses from the central array are
amplitude modulated. Such modulation is provided by two vertical
parasitic elements 28 mounted to the rotating cylinder 22 between
the members 18 and 20 and thus rotate about the central antenna
array 10. Only one of the two parasitic elements is illustrated in
FIG. 1. The distance between the central antenna array 10 and the
parasitic elements 28 along with the speed of rotation of the drum
22 establishes the modulation frequency applied to the pulses from
the central antenna array.
To improve the accuracy of bearing information transmitted from the
central antenna array 10, a group of nine parasitic elements 30 are
mounted to rotate with the parasitic elements 28 about the central
antenna array. These nine parasitic elements 30 rotate around the
central antenna array with the parasitic elements 28 and modify the
cardioid radiation pattern from the antenna. As illustrated in FIG.
1, each of the nine parasitic elements 30 comprises three separate
sections mounted to a supporting strand 32 extending between the
conical members 18 and 20. It will be noted that depending on the
radiation pattern required from the antenna system, the parasitic
elements 30 could be a single element instead of the three section
elements shown.
In addition to providing a rigid support for the parasitic elements
30, the conical members 18 and 20 also improve the gain and
bandwidth of the antenna. However, the oblique metal surfaces
provide an undesirable means of shifting the plane of polarization
of signals radiated omnidirectionally from the parasitic elements
28 and 30.
Referring to FIG. 2, the shifting of polarization is illustrated
with an incident wave 34, as radiated from the parasitic elements
of the antenna of FIG. 1, striking an oblique metal surface 36,
such as either of the conical members 18 or 20, and this energy is
reflected as a wave 38. The signal in one plane of polarization as
given by the wave 34 impinges on the metal surface 36 making an
oblique angle with the plane of polarization of the incident wave.
The plane of polarization of the reflected signal is shifted from
the plane of the impinging signal. The reflected wave 38 may have a
plane of polarization shifted by as much as 90.degree. from the
incident wave polarization; the degree of shift is an unknown
making it difficult to provide a corrective adjustment.
A navigation aid receiver responding to energy from the antenna of
FIG. 1 may be oriented such that the desired signal is rejected and
the undesired signal processed giving wrong modulation phase and
erroneous azimuth orientation direction.
To preclude radiation in any but the desired polarization plane,
absorbing wires 40 are supported on the supporting strands 32
around the mouth of the biconical horn in a plane or planes at
right angles to the normal plane of electric stress of the antenna.
These wires 40 act as absorbers for unwanted polarization energy
and minimize reflections from the parasitic elements 30 back to the
oblique surfaces of the conical members 18 and 20.
Referring to FIG. 3, there is shown a half section of a biconical
horn TACAN antenna modified from the antenna of FIG. 1. The TACAN
antenna of FIG. 3 is enclosed within a stationary radome 42 of a
fiberglass or other dielectric material. Within the radome 42, the
antenna includes a rotating drum 44, also of a dielectric material,
and conical members 46-49. Not shown in FIG. 3 is the central
antenna array in accordance with standard TACAN antenna design.
Mounted within the mouth formed by the conical members 46 and 47 is
a styrofoam support 50 having a cylindrical configuration and
supporting on the inner wall thereof two absorbing wires 52 and 53.
Similarly, mounted at the mouth formed by the conical members 48
and 49 is a styrofoam support 54 supporting on an inner wall
absorbing wires 56 and 57.
Between the outer surface of the styrofoam supports 50 and 54 and
the inner surface of the rotating drum 44 are 135 Hz parasitic
elements 58. Additional parasitic elements 58 are spaced at
40.degree. intervals around the interior surface of the rotating
drum 44.
Mounted to the outer wall of the rotating drum 44 are absorbing
wires 60-67. By properly spacing the absorbing wires 52-57 from the
absorbing wires 60-67, improved absorption of reflected energy is
provided. To provide maximum reflected energy absorption between
the absorbing wires 52-57 and the absorbing wires 60-67, the
styrofoam supports 50 and 54 have a cross sectional thickness of
approximately one-quarter wavelength of the radiated energy.
Providing a quarter wavelength thickness to the styrofoam supports
50 and 54 displaces the energy passing the elements 52-57 by
180.degree. from the energy reflected by the absorbing wires
60-67.
To further improve the minimizing of reflected radiation from the
conical members 46-49, absorbing wires 68-83 are supported on the
outer wall of the stationary radome 42. Again, the spacing between
the absorbing wires 60-67 and the absorbing wires 68-83 is such so
as to provide 180.degree. out-of-phase reflections between these
two sets. To provide such a 180.degree. out-of-phase displacement,
the spacing between the outer wall of the rotating drum 44 and the
outer wall of the stationary radome 42 is approximately one-quarter
wavelength at the radiated energy.
In operation of the antenna of FIG. 3, incident energy from the
central antenna array as reflected from the omnidirectional
elements 58 strikes the absorbing wires 52-57. Here some of the
energy is dissipated, some is reflected back in the direction of
the source, and some proceeds on toward the next set of absorbing
wires 60-67. At this point, energy from the first set of absorbing
wires experiences further dissipation, reflection and transmission
to the absorbing wires 68-83. It will be noted, that for each of
the wires 52-57 there are two wires supported on the outer wall of
the rotating drum 44. With this arrangement, the magnitude of
reflection from the wires 60-67 may be a little larger than
reflections from the wires 52-57 so that a wave of lesser size when
either reflection is turned toward the central array.
Energy transmitted from the wires 60-67 strikes the wires 68-83
where it experiences additional dissipation, reflection, and
transmission. Note again, that for each of the wires in the set
supported by the rotating drum 44 there are two wires supported on
the stationary radome 42. The reflection at the wires 68-83 is
adjusted so as to reduce the size of the second reflection again by
phase opposition. This reduced resultant then mates with the first
reflection, as described, but on more equal terms resulting in a
minimizing of reflection back to the energy source. After absorbing
energy in the wires 52-57, 60-67 and 68-83, any remaining signal
passing beyond the confines of the absorbing system is appreciably
reduced from the original of the unwanted polarization. It should
be noted, that energy at right angles to the plane of the absorbing
wires in each of the various sets passes through the absorber
system and induces no current therein. Hence, a wave polarized at
right angles to the plane of the wires passes through the absorber
system without attenuation.
Referring to FIG. 4, there is shown an antenna structure having
high frequency and low frequency parasitic elements revolving about
a stationary central antenna array. In this embodiment of the
invention, the biconical members are not incorporated into the
antenna structure; however, other oblique metal surfaces within the
system will produce an unwanted cross polarization component
without the absorbing wires as described.
Attached to the rotating shaft of a spin motor (not shown), such as
described in the copending application of Sidney Pickles et al,
Ser. No. 224,783, is a flange 84 that supports a rotating drum 86.
As mentioned previously, preferably the rotating drum is of a thin
dielectric material and is a spiral wound support for nine split
sets of high frequency parasitic elements 88 (only one set shown).
The nine sets of parasitic elements 88 are spaced around the drum
86 at 40.degree. intervals, and, in the embodiment shown, are
adhered to the outside surface with an adhesive.
Also rotating with the drum 86 is a support tube 90 by means of a
collar 92. The support tube 90 supports the split low frequency
parasitic elements 94 (only one set shown) on spaced filaments 96
extending between collars 98. Enclosing the entire assembly of the
support tube 90 and the parasitic elements 94 is a guard 100 of a
thin dielectric material. To maintain a spaced relationship between
the drum 86 and the tube 90, the upper end of the tube is fitted
with a positioning ring 102 fastened to the upper wall of the drum
86. Secured to this positioning ring are selectable balance weights
104 that are chosen to provide an equal weight balance to the
structure.
The central antenna array 10 as shown in FIG. 1 connects to a
coaxial cable through a connector in a conventional manner. The
central antenna array 10 is stationary mounted with respect to a
support plate 106.
Encircling the support tube 90 on the outer wall thereof are
absorbing wires 108-118 adhered to the surface of the tube by an
adhesive. Substantially polarization pure radiation is emitted from
the central antenna array 10 and reflected from the parasitic
elements 94; however, due to the inherent characteristics of the
antenna array 10 and the elements 94, a small cross polarization
component strikes the absorbing wires 108-118 wherein some of this
unwanted component of energy is dissipated, some is reflected back
in the direction of the source, and some proceeds outward from the
antenna structure. After absorbing energy in the wires 108-118, any
remaining cross polarization component of the signal passing beyond
the confines of the absorbing system is appreciably reduced from
the original of the unwanted polarization. The absorbing wires
108-118 also have an effect to minimize cross polarization
resulting from radiation reflected from the omnidirectional
elements 88 mounted to the drum 86.
Referring to FIG. 5, there is shown a radio navigation antenna as
used with Distance Azimuth Measuring Equipment (DAME) systems.
Typically, such antenna structures are used with a radio navigation
systems for shipboard installations and are motion stabilized along
an axis coinciding with the keel of the ship by means of supporting
structure including an adaptor 120 conventionally attached atop the
ship's mast. The adaptor 120 supports at its upper end a mounting
yoke 122 including a mounting plate 124. Attached to the under side
of the mounting plate 124 is a motor assembly 126 including a spin
motor as described in the copending application of Sidney Pickles
et al, Ser. No. 224,783.
Attached to the mounting plate 124 is a flange 128 that has bolted
thereto a radome 130 enclosing a central antenna array and
parasitic element assembly as shown and described in the
application of Sidney Pickles et al, Ser. No. 224,783, except with
conical shaped emitting elements instead of the cylindrical shape
as illustrated. Mounted to the outer surface of the radome 130 are
absorbing wires 132-144. These may be adhered to the radome 130 by
means of an adhesive.
As radiated energy leaves the central array it illuminates the
parasitic elements to provide amplitude modulation to the radiated
energy. Some of the energy emitted by the central array from the
oblique metal surfaces thereof is radiated in a direction to
produce a cross polarization component. This energy strikes the
absorbing wires 132-144 where the energy is attenuated such that
any remaining cross polarization signal passing beyond the confines
of the system is appreciably reduced from the original of the
unwanted polarization.
While several embodiments of the invention, together with
modifications thereof, have been described in detail herein and
shown in the accompanying drawings, it will be evident that various
further modifications are possible without departing from the scope
of the invention.
* * * * *