U.S. patent number 3,914,767 [Application Number 05/478,204] was granted by the patent office on 1975-10-21 for monolithic, electrically small, multi-frequency antenna.
This patent grant is currently assigned to The United States of America as represented by the Secretary of the Army. Invention is credited to Howard S. Jones, Jr..
United States Patent |
3,914,767 |
Jones, Jr. |
October 21, 1975 |
Monolithic, electrically small, multi-frequency antenna
Abstract
A projectile having a telemetry system built in which requires
an antenna ich is structurally incorporated into the nose cone of
the projectile. A dielectric material shaped to conform to the nose
cone of the projectile is adapted to be part of the projectile
exterior wall structure. A thin metallic coating is deposited on
the entire inside surface of the dielectric nose cone and the
coating is extended to cover a portion of the outside surface such
as to leave the tip of the nose cone exposed, thereby defining an
open end dielectric loaded radiator. A slot shaped aperture is
provided in the coating and is located at the base of the nose cone
so as to expose a portion of the dielectric and thereby define a
slotted dielectric loaded cavity. A plurality of metallic coated
holes are located circumferentially around the nose cone so as to
electrically separate the open ended dielectric loaded radiator
from the slotted dielectric loaded cavity. The resultant product is
a multi-frequency, monolithic conical dielectric loaded cavity
antenna.
Inventors: |
Jones, Jr.; Howard S.
(Washington, DC) |
Assignee: |
The United States of America as
represented by the Secretary of the Army (Washington,
DC)
|
Family
ID: |
23898944 |
Appl.
No.: |
05/478,204 |
Filed: |
June 11, 1974 |
Current U.S.
Class: |
343/708; 343/725;
343/769; 343/785 |
Current CPC
Class: |
H01Q
1/281 (20130101); H01Q 1/28 (20130101); H01Q
13/18 (20130101) |
Current International
Class: |
H01Q
13/18 (20060101); H01Q 1/28 (20060101); H01Q
5/00 (20060101); H01Q 13/10 (20060101); H01Q
1/27 (20060101); H01Q 001/28 () |
Field of
Search: |
;343/708,725,769,770,785 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Lieberman; Eli
Attorney, Agent or Firm: Edelberg; Nathan Gibson; Robert P.
Elbaum; Saul
Government Interests
The invention described herein may be manufactured, used and
licensed by or for the government for governmental purposes without
the payment to the inventor of any royalties thereon.
Claims
I claim as my invention:
1. In the projectile of the class wherein a signal is generated
within a projectile to be transmitted from an antenna, the
improvement comprising:
a. a dielectric material shaped to conform to the nose cone of said
projectile and adapted to be part of its exterior wall
structure;
b. a metallic coating deposited on the inside surface of said
dielectric and extending to cover a portion of the outside surface
so as to leave the tip of said nose cone exposed to define an open
end dielectric loaded radiator;
c. a slot shaped aperture in said coating located at the base of
said nose cone to expose a portion of said dielectric and thereby
define a slotted dielectric loaded cavity; and
d. a plurality of metallic coated holes in the metallic coated
portion of said nose cone circumferentially disposed to
electrically separate the open end dielectric loaded radiator from
the slotted dielectric loaded cavity.
2. The invention defined in claim 1 further comprising means for
connecting an input signal to said open end dielectric loaded
radiator, and means for connecting a separate input signal to said
slotted dielectric loaded cavity.
3. The invention defined in claim 2 further comprising a second
slot shaped aperture to define a second slotted dielectric loaded
cavity, and means for connecting an input signal thereto.
4. The invention defined in claim 3 further comprising a metallic
coated short circuit hole associated with each of said means for
connecting an input signal.
Description
BACKGROUND OF THE INVENTION
Since the advent of projectiles utilizing proximity fuzing systems,
telemetry, missile guidance, and other types of electronic
communications, a problem in the design of such systems has been to
provide an antenna which is small, compact and will not take up too
much space within the projectile. This is especially important
where the projectile has a fixed size and where space and weight
limitations are critical problems in the design of self-contained
fuzing and telemetry systems. Another problem has been to construct
antennas in small diameter bodies which can handle signals at the
lower microwave frequencies (800 to 2,500 mHz.) and which would
lend themselves to multi-elements construction. It is also
important that the electrical characteristics of these antennas
meet design specifications. This normally means that the antenna
must have certain specified radiation pattern characteristics,
impedance matching and sufficient bandwidth and gain to fulfill the
telemetry function.
Prior systems have utilized small antennas which are usually
mounted in the nose structure of the projectile. These antennas
used in prior systems normally utilized radiation elements such as
loops, stubs and ring networks that were enclosed by the dielectric
nose cone or body of the projectile. These elements have proven to
be less efficient and more difficult to design and construct, and
also far more costly to produce than is desirable for such systems.
While many of the electrical characteristics desired could have
been obtained with the use of cavity wave guide antennas, these
antennas could not be used because of their extremely large size
and heavy weight which has been inherent in the design of such
systems. It is, therefore, an object of this invention to provide a
projectile with an antenna system that uses a minimum of space
within the projectile.
It is another object of this invention to provide a small, compact
antenna system for a projectile which is efficient in its
electrical characteristics and yet is extremely lightweight.
Still another object of the invention is to provide an antenna for
a projectile which can be incorporated as part of the nose cone
structure of the projectile.
Yet another object of the invention is to provide an antenna system
for projectiles which can be easily constructed and is inexpensive
to manufacture.
An additional object of the invention is to provide a new and
unique antenna design having low input impedance and good
bandwidth.
A further object of this invention is to provide an antenna design
having multi-frequency design capabilities with good electrical
isolation.
Yet another object of this invention is to provide an antenna
design which reduces rf leakage to the other electronic components
within the nose cone.
These and other objects and advantages of the invention will become
more apparent with reference to the following specification,
drawings and appended claims.
SUMMARY OF THE INVENTION
Briefly, in accordance with this invention, a projectile is
provided having a telemetry system which is built entirely into the
nose cone structure. A dielectric material shaped to conform to the
nose cone of the projectile is adapted to be part of the exterior
wall of the projectile. The dielectrical material is provided with
a metallic coating deposited so as to cover the entire inside
surface of the nose cone and to extend so as to cover a portion of
an outside surface. The tip of the dielectric nose cone structure
remains exposed so as to define an open end dielectric loaded
radiator. A slot shaped aperture is provided at the base of the
nose cone in the form of an exposed portion of the dielectric
material and this defines a slotted dielectric loaded cavity. A
plurality of metallic coated holes located in the metallic coated
portion of the nose cone and circumferentially disposed around the
nose cone provide an electrical separation between the open end
dielectric loaded radiator and the slotted dielectric loaded
cavity.
BRIEF DESCRIPTION OF THE DRAWINGS
The specific nature of the invention, as well as other objects,
aspects, uses and advantages thereof, will clearly appear from the
following description and from the accompanying drawings in
which:
FIG. 1 is a perspective view of the nose cone of a projectile in
accordance with this invention;
FIG. 2 illustrates an inside view of the nose cone of FIG. 1.
FIG. 3 illustrates the radiation patterns of the open ended cavity
section of the antenna in accordance with the present invention;
and
FIG. 4 illustrates the radiation patterns of a single cavity in
accordance with the invention.
DESCRIPTION OF THE PREFERRED EMBODIMENT
Referring now to FIG. 1, nose cone 10 consists of a dielectric
material such as epoxy fiberglas 12. The dielectric material is
provided with a metallic coating 13 which covers the entire inside
of the nose cone and extends over the edge 14 and onto the exterior
surface 11 of the nose cone. This coating is typically in the form
of a copper plated surface which is coated on the dielectric
material by means of a conventional electroless plating
technique.
The base portion of nose cone 10 is provided with two radiating
slots 15 and 16 which constitute a dual dielectric loaded cavity
witih circumferential radiating slots. These slots simply
constitute etched or exposed portions of the dielectric material
12. Each section of the dual cavity has its maximum radiating field
normal to the axis of the cone and is fed from a coaxially input
connector 21 and 22. If desired, both cavities can be fed from a
common source and phased in such a manner as to get maximum
radiation off the side or along the axis of the cone. Associated
with each coaxially input feed is a shorting post 18 and 19. This
shorting post extends through the dielectric material and connects
the outer conductive coating 11 with the inner conductive coating
13. The two shorting posts thereby distinguish and define the two
separate slotted dielectric loaded cavities.
At the forward end or apex of nose cone 10 is the open ended
dielectric cavity which radiates surface waves through the exposed
dielectric 12 into free space. This portion of the antenna has its
maximum radiation normal to the axis of the nose cone, with nodes
along the axis. Again a coaxially input feed 26 (see FIG. 2) is
provided in the upper half of the nose cone and associated
therewith a shorting post 20 is located diametrically opposed
thereto.
A plurality of closely spaced copper plated holes 17 are disposed
circumferentially in the plated portion of the nose cone. These
closely spaced holes form a conducting barrier which electrically
separates the open end dielectric loaded radiator located at the
tip of the nose cone from the dual slotted dielectric loaded cavity
located at the base of the nose cone. Of course, it is possible to
replace the plurality of closely spaced holes with a single exposed
ring or slot of dielectric material.
The typical nose cone size of the present invention is 3 inches
high with a 2 inch base diameter. The dielectric materials from
which the nose cone is made have a wall thickness of approximately
three-sixteenths inch and a dielectric constant of about 4. The
antenna has a low input impedance, about a 5 percent bandwidth
where the VSWR is 2.0, and operates in the low S-band region. The
radiation pattern of this portion of the antenna is shown in FIG.
3. The radiation pattern of one section of the dual cavity antenna,
located at the base of the cone, is illustrated in FIG. 4. These
radiation patterns and measurements were taken with the antenna
assembly mounted on a cyclindrical body structure. It is, of
course, possible to have other designs of this multi-frequency
antenna. For example, the dual cavity could be a single cavity,
designed to operate at a much lower frquency. Also, ther are many
choices of dielectric materials which can be used that would change
the operating frequency and vary the performance. Other designs
utilizing a ridge incorporated in the cavity will change the
frequency and bandwidth as desired. The conductive coating can be
made out of copper, gold, silver, steel or platinum. The dielectric
materials can typically be made out of epoxy fiberglass, teflon,
plastic or ceramic.
It will be appreciated that the antenna described herein eliminates
many of the problems and difficulties that plagued prior art
systems. A multi-frequency operating antenna system has been
designed which is of a one piece integrated construction, is
rigidly small and is provided with good electrical isolation.
Because the dielectric material is fully plated on the inside, rf
leakage to other circuits and components is materially reduced. The
system requires no additional space and permits the inside of the
nose cone to be utilized for other purposes.
It should be understood that the invention is not limited to the
exact details of construction shown and described herein, for
obvious modifications will occur to persons skilled in the art.
* * * * *