U.S. patent number 3,713,162 [Application Number 05/099,434] was granted by the patent office on 1973-01-23 for single slot cavity antenna assembly.
This patent grant is currently assigned to Ball Brothers Research Corporation. Invention is credited to Jack K. Krutsinger, Robert E. Munson.
United States Patent |
3,713,162 |
Munson , et al. |
January 23, 1973 |
SINGLE SLOT CAVITY ANTENNA ASSEMBLY
Abstract
A thin flexible wrap-around antenna assembly, particularly
suitable for use in conjunction with a propelled vehicle such as a
missile, is disclosed and generally includes a first or inner
cylindrical thin conductor that can be flush-mounted on the skin of
the propelled vehicle and a second concentrically positioned outer
cylindrical thin conductor having an axial length which is equal to
one-quarter wavelength at the anticipated operating frequency of
the antenna. The conductors are electrically connected at adjacent
transverse edges so as to define a one-quarter wavelength
open-ended coaxial cavity which is connected to a transmitter or
receiver by a combination electrical signal feed and impedance
matching assembly.
Inventors: |
Munson; Robert E. (Boulder,
CO), Krutsinger; Jack K. (Boulder, CO) |
Assignee: |
Ball Brothers Research
Corporation (Boulder, CO)
|
Family
ID: |
27184967 |
Appl.
No.: |
05/099,434 |
Filed: |
December 18, 1970 |
Current U.S.
Class: |
343/705; 343/822;
343/792 |
Current CPC
Class: |
H01Q
9/0421 (20130101); H01Q 13/18 (20130101); H01Q
1/286 (20130101) |
Current International
Class: |
H01Q
13/18 (20060101); H01Q 1/28 (20060101); H01Q
13/10 (20060101); H01Q 1/27 (20060101); H01Q
9/04 (20060101); H01q 001/28 () |
Field of
Search: |
;343/705,708,810,821,847,792,822 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Lieberman; Eli
Claims
What is claimed is:
1. A thin flexible wrap-around antenna assembly comprising: a first
thin conductor; a second thin conductor spaced from said first
conductor; conductive means connecting an edge portion of said
first conductor with an edge portion of said second conductor;
electrical signal feed means, at least a part of which is
constructed of thin ribbon-like conductive material, one portion of
which terminates connected to said first conductor and a second
portion of which terminates at a signal feed junction spaced from
said first conductor; and means for supporting said conductors and
conductive material to thereby maintain a predetermined orientation
therebetween, said means for supporting said conductors and
conductive material including nonconductive means therebetween, and
said first and second conductors, said conductive material and said
nonconductive means each comprising part of a single sheet of
dielectric material metallically cladded on opposite sides
thereof.
2. A thin flexible wrap-around antenna assembly comprising: a first
thin conductor; a second thin conductor spaced from said first
conductor; conductive means connecting a portion of said first
conductor with a portion of said second conductor; electrical
signal feed means, at least a part of which is constructed of thin
ribbon-like conductive material, one portion of which includes a
plurality of leads connected to said first conductor and spaced
apart at intervals substantially equal to one wavelength at a
predetermined operating frequency of said antenna, and a second
portion of which terminates at a signal feed junction spaced from
said first conductor; and means for supporting said conductors and
conductive material to thereby maintain a predetermined orientation
therebetween.
3. A thin flexible wrap-around antenna assembly comprising: a first
thin conductor; a second thin conductor spaced from said first
conductor; conductive means connecting a portion of said first
conductor with a portion of said second conductor; electrical
signal feed means, at least a part of which is constructed of thin
ribbon-like conductive material, one portion of which includes a
plurality of leads connected to said first conductor and suitably
dimensioned so as to transfer a plurality of substantially equal
phase and amplitude signals to said first conductor and a second
portion of which terminates at a signal feed junction spaced from
said first conductor; and means for supporting said conductors and
conductive material to thereby maintain a predetermined orientation
therebetween.
4. A thin flexible wrap-around antenna assembly comprising: a thin
conductor; electrical signal feed means, at least a part of which
is constructed of thin ribbon-like conductive material, said
electrical signal feed means including a plurality of leads one
portion of each of which terminates connected to said conductor
with said conductor connections being spaced apart at intervals
substantially equal to one wavelength at a predetermined frequency
of said antenna, and a second portion of each of which is connected
with a signal feed junction, said conductive material being
suitably dimensioned so as to provide impedance matching at the
points of connection with said conductor; and means for supporting
said conductor and conductive material to thereby maintain the
predetermined orientation therebetween.
5. A thin flexible assembly adapted for use as a wrap-around
antenna, said assembly comprising: a first thin cylindrical
conductor the diameter of which is equal to a predetermined value;
a second thin cylindrical conductor the diameter of which is equal
to a value less than said predetermined value, said second
conductor being positioned concentrically within said first
conductor; conductive means connecting a portion of said first
conductor with a portion of said second conductor; electrical
signal feed means including a plurality of leads which terminate
connected to said first conductor and which are spaced apart at
intervals substantially equal to one wavelength at a predetermined
operating frequency of said antenna, said leads being constructed
of thin ribbon-like conductive material; and means for supporting
said conductors and said leads to thereby maintain the
predetermined orientation therebetween.
6. A thin flexible wrap-around antenna assembly comprising: a first
cylindrical conductor the axial length of which is substantially
equal to one-quarter wavelength at a predetermined operating
frequency of said antenna; a second cylindrical conductor
concentrically positioned within and radially spaced from said
first conductor; conductive means connecting one transverse edge of
said first conductor with an adjacent transverse edge of said
second conductor so as to form a one-quarter wavelength open-ended
coaxial cavity therebetween; electrical signal feed and impedance
matching means including a plurality of leads terminating at and to
said first conductor and circumferentially spaced apart at
intervals substantially equal to one-wavelength at said
predetermined frequency, said leads being constructed of thin
ribbon-like material integral with said first conductor and
suitably dimensioned so as to provide impedance matching at the
points of connection with said first conductor.
7. An antenna according to claim 6 wherein said electrical signal
feed means further includes a coaxial transmission line, the outer
conductive cable of which is connected to said second conductor and
the inner conductive cable of which is connected to said plurality
of leads at a predetermined point spaced from said points of
connection with said first conductor.
8. An antenna according to claim 7 wherein said leads are further
suitably dimensioned so as to transfer a plurality of substantially
equal phase and amplitude signals to said first conductor.
9. An impedance-matched antenna assembly comprising: a first
conductor; a second conductor spaced from said first conductor;
conductive means connecting a portion of said first conductor with
a portion of said second conductor; electrical signal feed means,
said feed means including a first plurality of thin ribbon-like
conductive leads which terminate connected to said first conductor
and which are suitably dimensioned so as to provide impedance
matching at the points of connection with said first conductor and
a second plurality of thin ribbon-like leads which terminate
connected to said first plurality of leads and which are suitably
dimensioned so as to provide impedance matching at the points of
connection with said first plurality of leads; and means supporting
said conductors and said first and second pluralities of leads to
thereby maintain the predetermined orientation therebetween.
10. An impedance-matched antenna assembly comprising: a first
conductor; a second conductor spaced from said first conductor;
conductive means connecting a portion of said first conductor with
a portion of said second conductor; electrical signal feed means;
said feed means including a first plurality of thin ribbon-like
conductive leads which terminate connected to said first conductor
and which are suitably dimensioned so as to provide impedance
matching at the points of connection with said first conductor, a
second plurality of thin ribbon-like conductive leads each of which
is connected to a pair of said first plurality of leads and
suitably dimensioned so as to provide impedance matching at the
points of connection with said first leads and a third plurality of
thin ribbon-like conductive leads connected to said second
plurality of leads and to a signal feed junction, said third
plurality of leads being suitably dimensioned so as to provide
impedance matching at the points of connection with said second
leads; and means supporting said conductors and said first, second
and third plurality of leads to thereby maintain the predetermined
orientation therebetween.
11. An antenna according to claim 10 wherein the distances between
said signal feed junction and the points of connection of said
first conductive leads to said first conductor are substantially
equal whereby to transfer a plurality of substantially equal phase
and amplitude signals to said first conductor.
12. A method of making an antenna for a propelled vehicle such as,
for example, a missile; said method comprising the steps of:
providing a thin flexible support sheet; providing a thin flexible
conductive layer on said support sheet; providing a thin flexible
impedance matched electrical signal feed assembly on said support
sheet; connecting said impedance matched electrical signal feed
assembly to said conductive layer at a plurality of points spaced
from one another a predetermined distance; fixing said conductive
layer and said electrical signal feed assembly to said support
sheet to thereby maintain a predetermined orientation therebetween;
and positioning said thin flexible support sheet, conductive layer
and said impedance matched electrical feed assembly
circumferentially about and to the body of said vehicle.
13. A method according to claim 12 wherein said last-mentioned step
includes the steps of wrapping said sheet about the body of said
vehicle and thereafter connecting opposite ends of said sheet
together.
14. A method according to claim 12 wherein said last-mentioned step
includes the steps of connecting opposite ends of said sheet
together and sliding the same about the body of said vehicle.
Description
BACKGROUND OF THE INVENTION
1. Field of the Invention
This invention relates generally to antennas and more particularly
to an improved single slot cavity antenna assembly.
2. Description of the Prior Art
The use of antenna assemblies for both transmission and reception
of radio signals is well known, and such antenna assemblies have
taken many diverse dimensions and/or shapes to accomplish given
objectives. Among such antennas known in the art are those useful
in conjunction with propelled vehicles including missiles and more
particularly missiles which carry instrument payloads for short
term measurement of very high altitude environmental data, which
data is transmitted from an antenna mounted on a missile to
receiving stations on the ground, which stations are often ground
tracking stations. However, monitoring has been found to be
difficult due to signal nulls encountered as the vehicles assume
different roll and aspect orientations.
Although the problem has been attacked in many ways, including the
use of refined circuitry such as automatic gain control amplifiers
which have to some effect alleviated the problem of antenna
deficiencies, there still has been a need to improve the antennas
so as to develop radiation patterns without signal lobes of varying
strength. More particularly, the antenna should be characterized by
an isotropic antenna radiation coverage, that is a pattern of
constant relative power for any orientation of the antenna. As
such, the pattern coverage is then relatively constant regardless
of the roll or aspect orientation of the rocket, thereby
facilitating data monitoring at a tracking station. The avoidance
of signal nulls as a characteristic of the antenna eliminates an
important deficiency that previously has caused temporary loss of
signal information, and in the case of an unrecovered rocket,
permanent loss thereof.
Although some previous attempts have been made to design antennas
having patterns more nearly isotropic for use in rockets carrying
environmental data sensors and associated instruments for telemetry
purposes and the like, such antennas have not completely solved the
problems in all cases due to one or more of such diverse reasons as
failing to satisfy strict aerodynamic design requirements,
exhibiting intolerable signal variations in the aspect patterns
(the signal pattern measured about the missile in a plane
containing the missile) and/or in the roll patterns (the signal
pattern measured about the missile in a plane perpendicular to the
missile axis), requiring complicated and often expensive components
due to complex design requirements, and/or requiring excessive time
and/or material in assembly so as to make antenna costs too high
for at least some intended uses. For example, the aspect and roll
radiation patterns in some antennas of recent design have been
found to fluctuate as much as 30 db from isotropic radiation, while
the required dimensions and/or costs inherent in other such
antennas have made these antennas unusable, or at least
undesirable, for many intended uses.
SUMMARY OF THE INVENTION
The present invention overcomes the aforementioned disadvantages,
as well as other disadvantages, by providing an antenna which has
an improved signal radiation pattern and which is both simple in
design and economical to make. In addition, the antenna is
particularly useful in airborne telemetry vehicles, which assume
many orientations relative to any given tracking station, since it
may be easily flush-mounted to the vehicle so as to provide a low
profile and thereby avoid any substantial increase in air drag.
As will be seen hereinafter, a preferred embodiment of the antenna
assembly according to the present invention generally comprises:
first and second spaced-apart thin conductors; conductive means
connecting a portion of the first conductor with a portion of the
second conductor; electrical signal feed means, at least a part of
which is constructed of thin ribbon-like conductive material, one
portion of which terminates connected to said first conductor and a
second portion of which terminates at a signal feed junction; and
means for supporting said conductors and conductive material to
thereby maintain the predetermined orientation therebetween.
Constructed in this manner, the antenna not only exhibits an
improved radiation pattern as will be seen hereinafter, but also is
relatively simple in design and economical to produce.
Accordingly, an object of the present invention is to provide a new
and improved antenna assembly having an improved signal radiation
pattern.
Another object of the present invention is to provide a new and
improved antenna assembly which is both simple in design and
economical to manufacture.
Still another object of the present invention is to provide an
antenna assembly having new and improved electrical signal feed
means connected therewith.
A further object of the present invention is to provide an antenna
of the last-mentioned type which has electrical signal feed means
connected therewith requiring only one coaxial transmission line to
be connected therewith.
Yet a further object of the present invention is to provide a new
and improved antenna assembly integrally formed with an electrical
signal feed assembly which is suitably dimensioned so as to
simultaneously provide impedance matching to said antenna.
It is another object of the present invention to provide a new and
improved thin flexible wrap-around antenna assembly which is
readily adaptable for use with a propelled vehicle such as a
missile.
Still another object of the present invention is to provide a new
and improved cylindrical omnidirectional antenna having a reduced
radiation pattern variation about the roll axis thereof.
Yet another object of the invention is to provide a new and
improved cylindrical omnidirectional antenna having a reduced
radiation pattern variation about the aspect axis thereof.
These and other objects and advantages will become apparent to
those skilled in the art from the following description of a
preferred embodiment of the present invention as illustrated in the
accompanying drawings.
BRIEF DESCRIPTION OF THE DRAWINGS
In the drawings:
FIG. 1 is an enlarged perspective view of a missile utilizing a
wrap-around antenna assembly constructed in accordance with the
present invention;
FIG. 2 is an enlarged perspective view of the antenna assembly
separated from the missile of FIG. 1;
FIG. 3 is a cross-sectional view taken generally along line 3--3 in
FIG. 2;
FIG. 4 is a partially broken-away enlarged sectional view taken
generally along line 4--4 in FIG. 3;
FIG. 5 is an enlarged flattened-out view of the antenna assembly
illustrated in FIG. 2, specifically displaying a portion of the
electrical signal feed assembly used therewith; and
FIG. 6 is a graphic representation showing an experimental antenna
gain radiation pattern utilizing the antenna of FIG. 2 mounted to
the outer surface of the missile as illustrated in FIG. 1.
DETAILED DESCRIPTION
Turning now to the drawings, wherein like components are designated
by like reference numerals throughout the various figures, a
wrap-around antenna assembly 10, constructed in accordance with the
present invention, is shown in FIG. 1 flush-mounted to a missile 12
having a metallic outer cylindrical body or skin 14 and a nose
portion 15. As will be seen hereinafter, antenna assembly 10 is
characterized by an isotropic antenna radiation coverage, that is,
an omnidirectional pattern of constant relative power for any
orientation of the antenna. As such, the pattern coverage is then
relatively constant regardless of the roll or aspect orientation of
missile 12 thereby facilitating data monitoring at a tracking
station. For purposes of description, the antenna will be
considered as a transmitting device, it being readily apparent to
those skilled in the art that the same may be used for reception
purposes also.
Turning to FIGS. 2 through 5, antenna assembly 10 is shown to
include a thin inner cylindrical conductor 18, which is preferably
constructed of copper. The conductor is adapted for flush mounting
directly to and about the skin 14 of missile 12, as illustrated in
FIG. 1, and thereby provides, in effect, a ground plane having an
axial length equal to that of the missile. Antenna 10 further
includes a second or outer cylindrical conductor 20, which is also
preferably constructed of copper, and which has an axial length
equal to or substantially equal to one-quarter wavelength at the
anticipated operating frequency of the antenna. Conductor 20 is
positioned concentrically about one end portion of conductor 18 and
is radially spaced therefrom so as to define a one-quarter
wavelength coaxial cavity 22, as illustrated best in FIG. 4.
While cavity 22 may be left void of material, for ease of
construction a dielectric layer 24, preferably
polytetrafluoroethylene (commercially available Teflon), and
particularly Teflon-fiberglass, is positioned between and supports
conductors 18 and 20. In this regard, it is to be noted that the
actual length of coaxial cavity 22 must be corrected for the
impedance producing effect of the dielectric layer. This may be
accomplished by resorting to the relationship of effective
wavelength .lambda..sub.c as a function of actual wavelength
.lambda. , which relationship is:
.lambda..sub.c = .lambda./.sqroot..epsilon..sub.R
Wherein .lambda..sub.c is the corrected wavelength in a cavity
filled with dielectric material, .lambda. is the actual wavelength
in a cavity void of material and .epsilon..sub.R is the dielectric
constant of the cavity filled material. By utilizing the above
stated equation, the length of cavity 22 easily can be corrected so
as to be "effectively" one-quarter wavelength. However, for
purposes of clarity, only the term "one-quarter wavelength cavity"
will be used hereinafter, it being understood that when the cavity
is filled with dielectric material, such as material 24, an
effective one-quarter wavelength cavity is contemplated.
Thus, for operation at a carrier frequency of, for example, 2.2 GHz
and utilizing a dielectric such as polymerized tetrafluoroethylene,
.lambda. is approximately equal to 5.4 inches and .epsilon..sub.R
is approximately 2.5. Solving the aforestated equation yields a
.lambda..sub.c of approximately 3.4 inches. Therefore, the
effective one-quarter wavelength cavity of this example is slightly
less than 1 inch in length.
Returning to FIG. 2, it can be seen that the entire left-hand
transverse edge of inner conductor 18 is electrically shorted to
the entire adjacent transverse edge of outer conductor 20. This can
be accomplished in any suitable manner such as, for example, by the
utilization of soldering material 26. In this way, the one-quarter
wavelength coaxial cavity may be defined as a continuous open-ended
cavity electrically shorted at one end, that is, at the soldering
end 26, and having an open circuit defining a circumferential slot
28 a distance one-quarter wavelength therefrom.
Cavity 22 may be excited by signal energy produced at a source 30,
as seen in FIG. 3, which may be located within missile 12 and which
may be of conventional type such as, for example, a unit having an
appropriate power source and radio frequency oscillator modulated
in accordance with data signals from external environmental sensor
devices. In this regard, an electrical signal feed assembly 32,
operating in the TEM mode, is provided for coupling source 30 to
inner and outer conductors 18 and 20.
Feed assembly 32 includes a coaxial transmission line 34 having
outer and inner conductive cables 36 and 38 extending from within
source 30 where they are connected to the appropriate components.
The otherwise free end of outer conductive cable 36 is electrically
connected to inner conductor 18 while the otherwise free end of
inner conductive cable 38 is connected to the input of a
combination multiple feed and impedance-matching network or
assembly 40, which is a feature of the present invention and part
of assembly 32 and which is to be described hereinafter.
The connections of the outer and inner conductive cables of
transmission line 34 with conductor 18 and assembly 40,
respectively, may be accomplished in any suitable manner, so long
as the inner conductive cable is appropriately insulated from inner
conductor 18. In this regard, a jack assembly, illustrated in FIG.
3, is provided and generally comprises an externally threaded
female connector 42 having an integral shoulder 44 suitably mounted
to the inner surface of conductor 18 and an internal insulating
sleeve 46, the opening of which is axially aligned with an aperture
48 provided radially through antenna 10. Female connector 42 is
adapted to receive a cooperating internally threaded male connector
50 mounted to the otherwise free end of conductive cable 36, as
illustrated in FIG. 3. In this manner, the last-mentioned
conductive cable is electrically connected to inner conductor 18.
The inner conductive cable 38 of coaxial transmission line 34 is
positioned through insulating sleeve 46 and aligned aperture 48 for
connection to combination multiple feed and impedance-matching
network 40.
Turning to FIG. 5, attention is directed to the combination
multiple feed and impedance-matching network 40 which is supported
on the exposed side of dielectric layer 24 and which comprises a
plurality of thin ribbon-like leads constructed preferably of and
displaying the same thinness as outer cylindrical conductor 20. In
this regard, it has been found that the most favorable radiation
patterns emanating from slot 28 of cavity 22 are developed when the
cavity is excited in the TEM mode with a plurality of signals of
uniform phase and amplitude provided at feed points generally
designated by the reference numeral 53. These feed points are
separated about the periphery of the slot 28 (on outer conductor
20) at intervals equal to or substantially equal to one wavelength
(as corrected for the dielectric material 24 in cavity 22) at the
aforestated anticipated operating frequency. Accordingly, assembly
40 includes a first plurality of leads 52, common ends of which are
preferably integrally formed with, but in any case terminated at
feed points 53.
Assembly 40 further includes a plurality of T-shaped leads 54, two
of which are shown in FIG. 5, a third plurality of leads 56 and an
input lead 58, all of which combine to connect the first plurality
of leads 52 to the inner conductive cable 38 of coaxial
transmission line 34 at a signal feed junction designated by the
reference numeral 59. As illustrated in FIG. 5, the head of each
T-shaped lead connects a pair of adjacent leads 52 while the leads
56 substantially form a partial band around dielectric layer 24
connecting the base of each T-shaped lead to input lead 58. In this
regard, it is to be noted that dielectrical layer 24 maintains the
predetermined orientation between the aforestated leads as well as
the inner and outer conductor.
Leads 52, 54, 56, and 58 are suitably dimensioned (length, width
and thickness) so as to provide continuous impedance-matching
between coaxial transmission line 34 and open-ended cavity 22. With
the impedance of coaxial transmission line 34 being appropriately
chosen so as to match the impedance of source 30, it is readily
apparent that there is substantially a perfect impedance match
between the source and antenna 10 which, of course, provides for a
more efficient antenna. In addition, the distance between input 58
or signal feed junction 59 and each feed point 53 is equal. In this
manner, combination multiple feed and impedance-matching assembly
40 separates the input signal from coaxial transmission line 34
into a plurality of equal phase and amplitude signals and transfers
the same to feed points 53 for exciting cavity 22 in the most
favorable manner possible.
While assembly 40 is formed in the manner illustrated in FIG. 5 and
includes four paths to conductor 20, it is to be understood that
the invention, as contemplated, is not limited thereto. For
example, there may be any number of feed points and paths depending
upon the circumference of conductor 20. Accordingly, the paths
between input 58 and feed points 53 may take on various dimensions
and designs so long as the aforedescribed impedance matching and
input signal separation functions are preserved. In this regard,
the latter function is assured if the paths are of equal
distances.
With antenna device 10 constructed in the aforedescribed manner,
attention is now directed to a preferred method of making the same.
As stated above, inner and outer cylindrical conductors 18 and 20
are preferably constructed of copper. More specifically, these
conductors are preferably parts of a sheet of microstrip, that is,
copper-clad layers supported by and on opposite sides of a sheet of
dielectric material such as polytetrafluoro ethylene (commercially
available Teflon), the dielectric sheet being dielectric material
24 illustrated in FIG. 2.
The method of making antenna 10 utilizing the aforedescribed sheet
of microstrip includes the step of removing various portions of one
of the copper-cladded layers from the intermediate dielectric
insulating sheet so as to provide an integral configuration
including outer conductor 20 and combination multiple feed and
impedance matching network 40. This may be accomplished in any
suitable manner, but is most preferably accomplished by resorting
to conventional printed circuitboard techniques, that is, by
photo-etching processes. Thereafter, adjacent transverse edges of
the copper-cladded layers are electrically connected together such
as, for example, by the utilization of solder 26 illustrated in
FIG. 2, and aperture 48 is provided through the laminated material
at the input or signal feed junction of network 40. A suitable jack
assembly of the type described above, is then soldered or otherwise
suitably mounted over the aperture and to the non-etched conductive
layer in the manner illustrated in FIG. 3.
If the antenna assembly is to be used in the manner shown in FIG.
1, that is, as a wrap-around or cylindrical flush-mounted antenna,
the longitudinal edges of the microstrip or laminated material are
suitably connected together by any suitable means such as apertures
61 provided through opposite ends of the material as illustrated in
FIG. 5. In this regard, construction of antenna device 10 is
facilitated by connecting only the lengthwise edges of the
intermediate dielectric layer 24 as illustrated by gaps 60 and 62
representing the unconnected lengthwise edges of inner and outer
conductors 18 and 20, respectively. So long as these gaps are small
relative to the operating wavelength of the antenna, they may be
neglected as having no substantial effect on either the antenna
impedance or radiation pattern. In this regard, the longitudinal
edges of the laminated material may be connected together after the
antenna assembly is wrapped around the body of the propelled
vehicle or they may be initially connected together whereupon the
assembly is then slid over and about the vehicle's body.
Having described the manner in which antenna assembly 10 is
constructed, attention is now directed to the manner in which it
operates in combination with missile 12, that is, with the inner
cylindrical conductor 18 being flush mounted to and about missile
skin 14 as illustrated in FIG. 1. As stated above, open-ended
coaxial cavity 22 is excited in the TEM mode by a plurality of
equal phase and amplitude signals (preferably radio frequency
signals) originating from a source, such as source 30, mounted
within the missile. Cavity 22, which is defined by one-quarter
wavelength outer conductor 20 and inner conductor 18, has an
impedance characteristic of effectively a one-quarter wavelength
coaxial transmission line which is short-circuited at the end
opposite feed points 53 by solder connection 26, the impedance
characteristic being matched to that of source 30 by network
40.
In the case where the operating wavelength of antenna device 10 is
much less than the circumference of missile 12, the cylindrical
conductor 20 and the missile skin 14 (along with flush-mounted
inner conductor 18) form a "fat" asymmetric dipole. Specifically,
it has been found that the antenna of the present invention
operates better as frequency increases and operates particularly
well at frequencies within the VHF, UHF and microwave bands
generally, and at the aforestated frequency of 2.2 GHz. In this
regard, reference is made to a pending application of Robert E.
Munson, Ser. No. 787,912, filed Dec. 30, 1968, which discloses a
cavity antenna similar in operation to the present invention, but
which structurally is entirely different. It should be apparent
that the short circuit 26 at the forward end of cavity 22, as
illustrated in FIG. 2, presents a negligible impedance which
effectively transforms back as an open circuit at feed points 53
circumscribing antenna slot 28 or one-quarter wavelength from the
short circuited end. The apparent open circuit is effectively in
parallel with the radiation impedance of the "fat" asymmetrical
dipole. Since the antenna 10 has a large diameter in terms of
wavelength, the impedance across the asymmetrical dipole is real
and divides between the feed points.
As stated above, FIG. 3 represents a broken-away sectional view of
antenna assembly 10 illustrated in FIG. 2. Assuming the antenna is
mounted to missile 12 in the manner shown in FIG. 1, dashed lines
64 illustrate the signal energy emanating from slot 28 and more
particularly the approximate instantaneous direction of the
electric field existing between conductor 20 and missile skin 14
making up the asymmetrical dipole. The direction of the field is
reversed (not shown) at every half-wavelength from the rearward end
of the cavity 22 in both the fore and aft directions of the missile
since the polarity of cylindrical conductor 20 relative to the aft
portion of skin 14 is constantly changing in accordance with the
frequency of the oscillatory feed signal.
Referring to FIG. 6, an aspect radiation pattern developed by
antenna assembly 10 utilized in the manner illustrated in FIG. 1 is
shown wherein the axis of the missile was positioned substantially
within the plane containing the pattern and wherein the assembly
was operated at a frequency of 2.2 GHz. It is to be understood that
this particular frequency is provided for illustrative purposes
only and is not intended to limit the invention, the assembly
operating equally well at other desired frequencies.
The pattern, representing the antenna gain relative to linear
isotropic radiation, is substantially representative within one db
of the infinite number of aspect radiation patterns which may be
utilized to define a figure of revolution about the missile axis.
More particularly, the radiation pattern of FIG. 6 is substantially
representative of the pattern contained in any plane defining a
cross-section through the figure of revolution produced by all
aspect patterns containing the axis of the missile.
It readily may be appreciated that deep nulls exist only directly
forwardly (0.degree.) and rearwardly (180.degree.) of the missile,
that is, at the tip and tail thereof. As is well known, tip and
tail pattern nulls in a telemetry missile are usually of little
concern. As can also be seen from FIG. 6, the remainder of the
signal pattern displays an average strength variation between
signal peaks and nulls in the aspect plane of less that 5 db. Thus,
the improved antenna device is highly favorable for receipt or
transmission of electromagnetic signal energy to or from the
missile without any appreciable loss in signal due to the vehicle
orientation.
It is to be understood that while antenna assembly 10 has been
described both operationally and in construction as a cylindrical
flush mountable type antenna displaying an omnidirectional
radiation pattern, the invention is not limited thereto.
Specifically, antenna device 10 may be substantially flat or only
partially curved so as to provide a more directional radiation
pattern while retaining the various advantagous features recited
above. In addition, although only one embodiment of the invention
has been shown and described, various modifications as may appear
to those skilled in the art are intended to be within the
contemplation of the invention as defined in the scope of the
claims.
* * * * *