Information
-
Patent Grant
-
6556174
-
Patent Number
6,556,174
-
Date Filed
Wednesday, December 5, 200122 years ago
-
Date Issued
Tuesday, April 29, 200321 years ago
-
Inventors
-
-
Examiners
- Wong; Don
- Chen; Shih-Chao
Agents
- Dryja; Michael
- Carnegie; Don J.
-
CPC
-
US Classifications
Field of Search
US
- 343 754
- 343 755
- 343 757
- 343 761
- 343 762
- 343 763
- 343 766
- 343 909
- 343 911 R
- 343 912
-
International Classifications
-
Abstract
A wave-scanning antenna is disclosed that does not require a rotary joint. The antenna produces a collimated beam that can be scanned through 360 degrees. The beam is directed perpendicular to the antenna's axis of rotation to form a disc-like surveillance volume, or at an angle above or below the perpendicular to form a cone-shaped surveillance volume. The radar's structure contains a transmitter and receiver coupled to a horn protruding through open centers of the support bearing and driven gear into the antenna housing. Energy emitted by the horn proceeds upward until deflected through an angle of 90 degrees by an angled reflector located on the axis of rotation. The energy is collected by a dielectric lens and focused into a collimated beam. Reflected energy is collected by the lens and directed by the reflector to the horn, where it is fed to a waveguide coupled to the receiver.
Description
BACKGROUND OF INVENTION
The present invention relates in general to continuous rotation scanning antennas for use in surveillance radars, and in particular to a scanning antenna configuration that does not require the use of a rotary joint.
The possibility of terrorist activity, compromise of military information, or material theft results in the need to protect various high value assets whether located in permanent or temporary sites. A desirable approach protecting such valuable assets is the establishment of a network of low power surveillance radars to provide automated perimeter security. For greatest versatility, the surveillance radars should be easily transportable and deployable in multiple emplacements in any desired positional configuration. Therefore, the surveillance radar should be small in size and have a weight low enough for single person installation.
A typical example of a multiple surveillance radar deployment is shown in FIG.
1
. An aircraft parking area
1
containing high value assets, such as aircraft
2
, is encompassed by a multiplicity of surveillance radars
3
spaced so that the detection volumes
4
provided by each radar form a continuous zone for the detection of intruders around the perimeter of the area
1
. The cost of such an installation should be affordable, and thus each surveillance radar should be designed and constructed in a manner to minimize cost while providing the required performance. The surveillance radars should provide an azimuthal scan of 360 degrees to allow for versatility of placement, and a scan rate sufficiently high that an intruder cannot traverse the radar's detection volume without being intercepted by a scan of the beam and thus detected. Operation in the millimeter wave region of the electromagnetic spectrum allows the use of a small, lightweight-scanning antenna that produces a narrow beam in azimuth for adequate resolution of target details.
The prior art employs various methods in the design of continuous rotation, 360-degree scan antenna systems, especially for microwave radars. To accomplish focusing of the transmitted beam, the antenna can employ either a parabolic reflecting element or a refracting element with a microwave feed located at the focal point of the element, a planar array made up of slotted waveguides, or equivalent electromagnetic structure, etc. One common technique for coupling the microwave signals from the antenna to the transmitter and receiver subelements is to place these subelements in the stationary portion of the radar. The transmitted and received signals are transferred to and from the antenna by a rotary joint placed upon the axis of rotation of the antenna.
Another technique is to locate much or all of the transmitter and receiver subelements with the antenna on the rotating structure, and transfer raw power and control signals from, and receiver output video to the stationary portion of the radar via slip rings coupled to the rotational axis. This technique has disadvantages of significant transmitter/receiver weight forming part of the rotating mass, a relatively uncontrolled environment for critical transmitter/receiver circuitry, and signal noise generated by the slip ring assembly.
The first described technique using a rotary joint is generally preferable. Rotary joints operating in the microwave region of the electromagnetic spectrum are widely used and provide adequate performance. However, those that operate in the millimeter wave region of the spectrum may not provide adequate performance and are prohibitively expensive for use in a low cost surveillance radar.
One example of prior art is the reference Waters et al., statutory invention reg. no. H966, published on Sep. 3, 1991. Waters provides a scanning antenna requiring no rotary joint for use in a shipboard environment. In the stationary portion of this design, the electromagnetic energy is collimated into a beam of significant diameter by means of a parabolic reflector. This beam is transmitted upward to a rotating assembly that by phase sensitive reflection produces two scanning, orthogonally polarized beans transmitted horizontally in opposite directions. The physical mechanism that supports the scanning assembly must provide unobstructed passage of the rather large diameter collimated beam from the stationary parabolic reflector to the rotating assembly.
In view of the above, there is a need for an improved method of transferring the millimeter wave electromagnetic energy between the rotating antenna and the transmitter and receiver subelements located in the stationary portion of the radar. Furthermore, there is a need to accomplish this without requiring the use of slip rings or a rotary joint, and by using a minimum of components in a lightweight configuration having reasonable cost. For these and other reasons, there is a need for the present invention.
SUMMARY OF INVENTION
The invention relates to a surveillance radar-scanning antenna requiring no rotary joint. The surveillance radar antenna of the invention includes a millimeter wave horn positioned on the vertical axis of rotation of the antenna and protruding through the open center of the antenna support bearing, driven gear, and a hole in the antenna housing. Divergent millimeter wave electromagnetic energy is emitted vertically by the non-rotating horn, then is deflected to the horizontal by an angled reflector before being focused by a dielectric lens into a collimated beam. The rotating antenna housing supports the angled reflector and dielectric lens. Provisions are made for vertical positioning of the dielectric lens to allow limited adjustment of the transmitted beam above or below the horizontal. Received energy reflected from distant targets is collected by the dielectric lens and directed by the angled reflector to the non-rotating horn where it is fed to a waveguide coupled to the receiver.
The present invention provides a method for the transfer of millimeter wave electromagnetic energy between a rotating antenna assembly and the transmitter and receiver subelements in the stationary structure of the radar. An advantage of the present invention is that a millimeter wave rotary joint, with its intrinsic requirement for extremely accurate tolerances and highly expensive manufacturing processes, is not required. Another advantage is that a surveillance radar incorporating the present invention does not have any moving mechanical parts in the waveguide portion of the electromagnetic energy path. Furthermore, the radar of the invention experiences no variation in energy loss due to variations in a mechanical rotary joint, and does not require the periodic replacement of an expensive rotary joint component.
In contrast to Waters, the present invention uses a support bearing and driven gear, which supports and drives the rotating antenna structure, with open inner diameters only sufficiently large to allow passage of a non-rotating millimeter wave waveguide assembly. The electromagnetic beam is emitted by a non-rotating horn and then collimated by an angled reflector and dielectric lens forming a part of the rotating portion of the antenna. Other aspects, embodiments, and advantages of the prior art will become apparent by reading the detailed description that follows, and by referring to the accompanying drawings.
BRIEF DESCRIPTION OF DRAWINGS
FIG. 1
illustrates an electronic fence made up of a multiplicity of radars to protect high value assets.
FIG. 2
is a cross-sectional view of a rotating antenna structure that does not require a rotary joint.
FIG. 3
shows a cross-sectional view of an alternate configuration of the rotating antenna structure with provisions added to allow vertical adjustment of the dielectric lens position for the purpose of aiming the transmitted beam above or below the horizontal.
FIG. 4
is a frontal view of the alternate configuration with the lens support plate in the foreground and the antenna housing in the background.
DETAILED DESCRIPTION
In the following detailed description of exemplary embodiments of the invention, reference is made to the accompanying drawings that form a part hereof, and in which is shown by way of illustration specific exemplary embodiments in which the invention may be practiced. These embodiments are described in sufficient detail to enable those skilled in the art to practice the invention. Other embodiments may be utilized, and logical, mechanical, and other changes may be made without departing from the spirit or scope of the present invention. The following detailed description is, therefore, not to be taken in a limiting sense, and the scope of the present invention is defined only by the appended claims.
The configuration of major components of a rotating antenna according to one embodiment of the invention is depicted in cross sectional view in FIG.
2
. Major components are positioned axially along two major axes
11
-
11
′ and
12
-
12
′ which are perpendicular to each other and intersect at point
13
. Stationary structure
14
contains the transmitter, receiver and signal processor subelements of the radar, and provides support for the rotating portion of the antenna.
The rotating portion of the antenna includes the upper portion of support bearing
15
, driven gear
16
, housing
17
and its included components, reflector support
18
, reflector
19
and lens
20
. Lens
20
is fabricated of a dielectric material having the capability of reducing the propagation velocity of millimeter wave electromagnetic energy while passing it with essentially no attenuation. The lower portion of support bearing
15
is rigidly coupled to the stationary structure
14
while its upper portion is rigidly coupled to the driven gear
16
which is in turn rigidly coupled to housing
17
. Support bearing
15
, and driven gear
16
and a hole in the lower portion of housing
17
are located coaxially along axis
11
-
11
′. This rotating assembly revolves about axis
11
-
11
′, being rotationally driven by drive gear
21
which is coupled to driven gear
16
. Drive gear
21
is coupled to a drive motor, which is not shown, by shaft
22
.
Housing
17
has the form of a cylinder, seen in cross sectional view in
FIG. 2
, with its axis being defined by axis
12
-
12
′. The cylinder is terminated at one end by lens
20
and at the other by housing end plate
23
. Included within the housing is a reflector
19
coupled to a reflector support
18
that is in turn coupled to the housing end plate
23
. Reflector
19
is supported so that its front reflecting surface coincides with the intersection of axes
11
-
11
′ and
12
-
12
′ at point
13
, and the plane of reflector
19
is tilted to form angles of substantially 45 degrees with respect to both axes
11
-
11
′ and
12
-
12
′.
Millimeter wave feed and horn structure
24
, comprising a circular waveguide coupled to a conical horn, is coaxially positioned along axis
11
-
11
′ so that it protrudes through the open inner diameters of support bearing
15
, driven gear
16
and the hole located in the bottom of housing
17
. Point
25
defines the apparent point of origin of millimeter wave electromagnetic rays emanating from the horn. Lens
20
has a finite thickness that must be considered for highly accurate determination of the paths of electromagnetic rays passing through the lens. However, for first order analysis, a point
27
can be defined which will approximate the location of an imaginary lens having equivalent focusing performance but zero thickness. The feed and horn structure
24
is positioned along axis
11
-
11
′ so that the distance along axis
11
-
11
′ from point
25
to point
13
plus the distance along axis
12
-
12
′ from point
13
to point
27
is essentially equal to the focal length of lens
20
at the frequency of operation. Millimeter wave feed and horn structure
24
is physically coupled to the stationary structure
14
and maintains a constant position as the rotating portion of the antenna rotates about axis
11
-
11
′.
The preferred embodiment of the present invention operates at a frequency of substantially 35.5 Gigahertz. Housing
17
has outer and inner dimensions of substantially 16.5 and 15.2 centimeters respectively; its overall length is defined by the appropriate spacing of lens
20
with respect to reflector
19
and a selected length of reflector support
18
to provide equal mass distribution of the housing and its coupled components fore and aft of axis
11
-
11
′. The horn portion of the horn and feed structure
24
is an axisymmetric conical structure having a cone half angle of substantially 24 degrees with respect to axis
11
-
11
′, and having a length of substantially five centimeters from apex to aperture. The horn is fed by a circular waveguide having an internal diameter optimized to the frequency of operation by the use of principles well known to those skilled in the art.
Reflector
19
is fabricated of Aluminum or similar material being highly reflective of millimeter wave energy and has reflecting surface dimensions that exceed the area impinged by the electromagnetic energy emanating from the horn. The reflector surface finish and flatness are several orders of magnitude less than the wavelength the reflected millimeter waves. Lens
20
has a piano-convex form being fabricated of a polypropylene dielectric material, and has an aperture and focal length of substantially 15.2 and 17.8 centimeters respectively. The combined distances from points
25
to
13
and from
13
to
27
are adjusted to be effectively equal to the focal length of lens
20
. The angles of reflector
19
with respect to axes
11
-
11
′ and
12
-
12
′ causes the apparent point of origin of rays emanating from the horn, point
25
, to appear to be located at point
26
on axis
12
-
12
′ when viewed from the position of lens
20
. Adjusting the vertical position of horn and feed structure
24
can be accomplished to optimize the focus of the beam emanating from lens
20
. After adjustment, its position is fixed with respect to the stationary structure
14
.
In transmit operation, millimeter wave electromagnetic energy proceeds up the circular waveguide portion of the horn and feed structure
24
to point
25
and then is dispersed into a conical volume by the horn. Each elemental segment of this energy forms a ray that proceeds from the horn appearing to have come from point
25
, until it impinges upon reflector
19
to be reflected in accordance with well known laws of reflection from a flat reflective surface. Upon leaving the surface of reflector
19
, the solid cone of electromagnetic rays proceeds to the rear surface of lens
20
. While passing through the dielectric lens the rays are focused into a substantially collimated beam having an initial diameter essentially equal to the aperture of lens
20
, or 15.2 centimeters. A central ray
28
proceeds from point
25
along axis
11
-
11
′ until reaching reflector
19
at point
13
, next proceeds to point
27
located in lens
20
, and then passes through the center of the lens undeviated continuing along a path that is an extension of axis
12
-
12
′. The path of this central ray
28
defines the direction of propagation of the beam formed by the antenna.
Ray
29
and ray
30
are peripheral rays defined by the maximum aperture limit of lens
20
. After being reflected by reflector
19
, these rays appear to have originated at point
26
and proceed to the lower and upper regions of lens
20
. They are then diffracted by their angles of incidence with respect to the first surface and the curvature of the lens at the points of ray exit in accordance with the dielectric constant of the lens and the well-known Snell's law. The paths of rays
29
and
30
proceeding from the lens are substantially parallel to that of the central ray
28
. Although
FIG. 2
is a two-dimensional depiction of that vertical plane which contains both axes
11
-
11
′ and
12
-
12
′, those skilled in the art will recognize that reflecting surface
19
is a two-dimensional surface, lens
20
has a circular aperture, and that rays emanating from point
25
will, after reflection from reflecting surface
19
, substantially fill the planer aperture of lens
20
. The electromagnetic energy exiting lens
20
has the form of a collimated beam, with diameter essentially the same as the aperture of the lens. Factors such as spherical aberration and manufacturing tolerances of low cost dielectric lenses result in some spreading of the emitted beam. One example of the preferred embodiment provided a transmitted beam width of some 3.6 degrees.
During receive operation, a portion of the transmitted beam is reflected from the target back to the antenna where the received energy impinging upon the lens
20
follows essentially a reverse path through the antenna until it arrives at point
25
and proceeds down the circular waveguide to the receiving subsystem within the stationary structure
14
. The described configuration produces a linearly polarized beam with the polarization rotating as the antenna structure sweeps through a 360-degree search pattern. Both analysis and experiment have shown that the area illuminated on targets of interest by the radar beam typically has a surface roughness significantly exceeding a half wavelength of the operational frequency, which is some 4.2 millimeters. Therefore, the rotating polarized beam has no effect on overall radar performance.
When deploying a multiplicity of radars incorporating the present invention in configurations similar to that shown in
FIG. 1
, it may be found that the terrain is not flat and thus it may be necessary to place a radar in a depression or at the top of a knoll with the requirement that the radar maintain surveillance of the area surrounding its position. The antenna configuration shown in
FIG. 2
produces a beam pattern having the form of a horizontal disc with the radar rotating antenna at its center. If deployed at the bottom of a depression, the search range would be limited due to the radar beam impinging upon the sides of the depression a short distance away from the radar. If placed on a knoll, the disc-like beam pattern would be located progressively further above the surface as the distance from the radar increased, possibly allowing an intruder to crawl under the beam. Such situations make it highly desirable to adjust the antenna so that the path of the beam will be either above or below the plane formed by the rotation of axis
12
-
12
′ about axis
11
-
11
′.
FIG. 3
presents an alternate configuration for housing
17
and the coupling of the lens
20
thereto. A portion of the cylindrical housing nearest the lens is replaced with a conical section
40
that is coupled to a mounting plate
41
.
FIG. 4
shows a front view of the alternate configuration with the mounting plate
41
in the background and a lens support plate
42
in the foreground. Lens
20
is coupled to the lens support plate
42
that is held in position against the mounting plate
41
by four fasteners
43
. Four slots
44
located in the mounting plate
41
and four holes for the fasteners similarly located in the lens support plate
42
allow fasteners
43
to be used to couple the lens support plate to the mounting plate in a range of vertical positions with respect to the cylindrical axis of the housing
17
. A vertical axis
45
-
45
′ passes through the center of the lens
20
and is parallel to the axis
11
-
11
′, about which the antenna rotates. A horizontal axis
46
-
46
′ is coincident with and orthogonal to the axis
12
-
12
′ and defines the vertical center of the housing
17
. A horizontal axis
47
-
47
′passes through the center of the lens
20
and can occupy any of a number of positions above, on, or below the axis
46
-
46
′, with its limits defined by the extent of the positions of the fasteners
43
in the slots
44
. The lens
20
is positioned above the axis
46
-
46
′ in both
FIGS. 3 and 4
. An axis
48
-
48
′, seen in
FIG. 3
, is orthogonal to both axes
45
-
45
′ and
47
-
47
′, and is parallel to the axis
12
-
12
′.
In
FIG. 3
, the position of the lens
20
has been raised with respect to that which it occupied in FIG.
2
. No changes have been made in the positions of the feed and horn structure
24
or reflector
19
; therefore, the apparent point of origin of rays emanating from the horn, point
25
, continues to appear to be located at point
26
on axis
12
-
12
′ when viewed from the position of the lens
20
. A ray
50
can be traced from point
25
to point
49
on the reflector
19
where its path is reflected toward point
27
at the center of the lens
20
in accordance with the laws of reflection well known to those skilled in the art. A ray
50
passes through the center of the lens
20
undeviated and proceeds from the lens making a small positive angle with respect to the axis
48
. Note that the ray
50
can be considered to have come from point
26
, proceeding in a straight line through points
49
and
27
toward distant targets.
Peripheral rays
51
and
52
are defined by the maximum aperture of the lens
20
. After being reflected by the reflector
19
, these rays appear to have originated at point
26
and proceed to the lower and upper regions of the lens
20
where they are diffracted by the dielectric constant of the lens and the ray angles of incidence with respect to the first surface and the curvature of the lens at the points of ray exit. The paths of rays
51
and
52
proceeding from the lens are substantially parallel to that of the central ray
50
. Although
FIG. 2
is a two-dimensional depiction of that vertical plane which contains the axes
11
-
11
′,
12
-
12
′, and
48
-
48
′, those skilled in the art will recognize that the reflecting surface
19
is a two-dimensional surface, the lens
20
has a circular aperture, and that rays emanating from point
25
will, after reflection from the reflecting surface
19
substantially fill the planer aperture of the lens
20
. The electromagnetic energy exiting the lens
20
has the form a collimated beam, with diameter essentially the same as the aperture of the lens.
The axis
48
-
48
′ is parallel to the axis
12
-
12
′ with the separation between them being defined by a distance
53
. When the distance
53
is not zero, the angle that the radar beam makes with respect to a horizontal plane is approximately given by Beam angle=arctan (distance
53
/lens
20
focal length). In the preferred embodiment of the present invention, slots
44
have a length sufficient to provide an adjustment range of the distance
53
of plus and minus 1.5 centimeters that allows elevating or depressing the beam angle by a maximum of approximately five degrees.
It is noted that, although specific embodiments have been illustrated and described herein, it will be appreciated by those of ordinary skill in the art that any arrangement is calculated to achieve the same purpose may be substituted for the specific embodiments shown. For instance, the values presented above in conjunction with
FIGS. 2
,
3
, and
4
describe one embodiment of the present invention. Those skilled in the art will recognize that equivalent performance will be provided by operation at other wavelengths, and in particular at some 76 Gigahertz, and with other dimensions for the various components. A rectangular waveguide and horn structure can also be used in lieu of the circular structures. This application is intended to cover any adaptations or variations of the present invention. Therefore, it is manifestly intended that this invention be limited only by the claims and equivalents thereof.
Claims
- 1. An apparatus for use in directing a collimated electromagnetic beam to any heading within a disc-shaped volume, the disc-shaped volume formed by scanning of the collimated electromagnetic beam through 360 degrees about a center of the disc-shaped volume, comprising:a stationary structure; a housing coupled to the stationary structure such that the housing is rotatable about a rotational axis, the rotational axis being fixed perpendicular to a surface of the stationary structure, the housing having a longitudinal axis intersecting the rotational axis and extending perpendicular to the rotational axis, a continuous void axially centered on the rotational axis and extending from within the stationary structure to within the housing; an emitter and receiver coupled to the stationary structure, located on the rotational axis, and protruding through the continuous void, the emitter capable of emitting electromagnetic energy and the receiver responsive to the electromagnetic energy; a reflecting surface located within the housing at the intersection of the rotational axis and the longitudinal axis and rigidly coupled to the housing, the reflecting surface positioned at an angle of substantially 45 degrees with respect to the rotational axis and capable of deflecting the emitted electromagnetic energy through a directional change of substantially 90 degrees; and, a focusing mechanism coupled to the housing and axially centered on the longitudinal axis, the focusing mechanism capable of collecting the emitted electromagnetic energy and focusing the emitted electromagnetic energy into a beam axially centered about an extension of the longitudinal axis.
- 2. The apparatus of claim 1, wherein the electromagnetic energy emitted by the emitter is in a cone-shaped volume within the housing and axially centered on the rotational axis.
- 3. The apparatus of claim 2, wherein the electromagnetic energy after reflection is axially centered about the longitudinal axis.
- 4. The apparatus of claim 1, wherein the focusing mechanism is capable of bi-directional processing of the electromagnetic energy.
- 5. The apparatus of claim 1, wherein the housing is coupled to the stationary structure by a coupling mechanism.
- 6. The apparatus of claim 5, wherein the coupling mechanism comprises:a support bearing coupled to the stationary structure and axially positioned about the rotational axis, the support bearing having a circular void through its center, the circular void being axially centered on the rotational axis; and, a driven gear coupled to the support bearing and to the housing, the driven gear being axially positioned about the rotational axis and having a circular void through its center, the circular void being axially centered on the rotational axis.
- 7. The apparatus of claim 1, wherein the continuous void comprises:a void in the surface of the stationary structure being aligned with the void in the support bearing; and, a void in the surface of the housing being aligned with the void in the driven gear, where the voids in the surface of the stationary structure, the support bearing, the driven gear and the housing are of similar diameter and axially centered about the rotational axis.
- 8. The apparatus of claim 1, wherein the emitter and receiver comprise:a millimeter waveguide coupled to a source of millimeter wave electromagnetic energy and to a receiver capable of extracting target information from received millimeter wave signals; and, a millimeter wave horn coupled to the millimeter waveguide and being capable of emitting and collecting millimeter wave electromagnetic energy, and transferring the energy from and to the millimeter waveguide.
- 9. The apparatus of claim 1, wherein the focusing mechanism comprises a lens having a positive focal length and being fabricated of a dielectric material having the capability of reducing the propagation velocity of millimeter wave electromagnetic energy while passing it with essentially no attenuation.
- 10. The apparatus of claim 9, wherein the lens is fabricated of a polypropylene dielectric material.
- 11. An apparatus for use in directing a collimated electromagnetic beam to any heading within a volume formed between two adjacent conical surfaces, the two adjacent conical surfaces being defined by upper and lower extent of the collimated electromagnetic beam as the beam is scanned through 360 degrees about a rotational axis, comprising:a stationary structure; a housing coupled to the stationary structure by a coupling means allowing the housing to rotate about the rotational axis, the rotational axis being fixed perpendicular to a surface of the stationary structure, the housing having a longitudinal axis intersecting the rotational axis and extending perpendicular to the rotational axis; a continuous void axially centered on the rotational axis, the continuous void extending from within the stationary structure through the coupling means to within the housing; an emitting and receiving means coupled to the stationary structure, located on the rotational axis, and protruding through the continuous void, the emitting and receiving means capable of emitting electromagnetic energy into a cone shaped volume within the housing with the cone shaped volume being axially centered on the rotational axis, and the emitting and receiving means responsive to electromagnetic energy within the cone shaped volume that is propagating toward the emitting and receiving means; a reflecting surface located within the housing at the intersection of the rotational axis and the longitudinal axis being rigidly coupled to the housing, the reflecting surface positioned at an angle of substantially 45 degrees with respect to the rotational axis and capable of deflecting the emitted electromagnetic energy through a directional change of substantially 90 degrees, after reflection the cone shaped volume of emitted electromagnetic energy being axially centered about the longitudinal axis; a focusing means being axially centered on a focusing means axis and capable of collecting the emitted electromagnetic energy in the cone shaped volume and focusing the emitted electromagnetic energy into a collimated beam, the focusing means capable of bi-directional processing of electromagnetic energy; and, an adjustable coupling means for coupling the focusing means to the housing and capable of fixing the position of the focusing means axis parallel to the longitudinal axis and at any of multiple positions further away or closer to the surface of the stationary structure than the position of the longitudinal axis.
- 12. The apparatus of claim 11, wherein the coupling means for coupling the stationary structure to the housing comprises:a support bearing coupled to the stationary structure and axially positioned about the rotational axis, the support bearing having a circular void through its center, the circular void being axially centered on the rotational axis; and, a driven gear coupled to the support bearing and to the housing, the driven gear being axially positioned about the rotational axis and having a circular void through its center, the circular void being axially centered on the rotational axis.
- 13. The apparatus of claim 11, wherein the continuous void comprises:a void in the surface of the stationary structure being aligned with the void in the support bearing; a void in the surface of the housing being aligned with the void in the driven gear; and the voids in the surface of the stationary structure, the support bearing, the driven gear and the housing being of similar diameter and axially centered about the rotational axis.
- 14. The apparatus of claim 11, wherein the emitting and receiving means comprises:a millimeter waveguide coupled to a source of millimeter wave electromagnetic energy and to a receiver capable of extracting target information from received signals; and a millimeter wave horn coupled to the millimeter waveguide and being capable of emitting and collecting millimeter wave electromagnetic energy, and transferring the energy from and to the millimeter waveguide.
- 15. The apparatus of claim 11, wherein the focusing means comprises a lens having a positive focal length and being fabricated of a dielectric material having the capability of reducing the propagation velocity of millimeter wave electromagnetic energy while passing it with essentially no attenuation.
- 16. The apparatus of claim 15, wherein the lens is fabricated of a polypropylene dielectric material.
- 17. The apparatus of claim 11, wherein the adjustable coupling means comprises:a flange coupled to the housing having an opening axially centered about the longitudinal axis, the opening larger than the aperture of the focusing means, the flange having a flat outer surface normal to the longitudinal axis and having a multiplicity of slots through the flange symmetrically positioned at locations on the outer surface, the slots running parallel to the plane formed by the rotational axis and the longitudinal axis; a support plate coupled to the outer diameter of the focusing means having a mating surface compatible with the flat outer surface of the flange, and having circular holes positioned to match the locations of the slots and to cause the focusing means axis to be coincident with the longitudinal axis when the circular holes align with the center of the slots; and adjustable fasteners compatible with and passing through the holes and the slots to fix the relative position of the support plate with respect to the flange, thus allowing selection of any position for the focusing means within the limits of the slots.
- 18. An apparatus for use in directing a collimated electromagnetic beam to a heading within a disc-shaped volume formed by scanning of the collimated electromagnetic beam about a center of the disc-shaped volume, comprising:a stationary structure;a housing coupled to the stationary structure such that the housing is rotatable about a rotational axis;an emitter and receiver coupled to the stationary structure on the rotational axis, the emitter capable of emitting electromagnetic energy and the receive responsive to the electromagnetic energy; a reflecting surface on the housing on the rotational axis and capable of deflecting the electromagnetic energy emitted through a directional change; and, a focusing mechanism coupled to the housing and capable of collecting and focusing the electromagnetic energy emitted into a beam.
- 19. The apparatus of claim 18, wherein the housing further has a longitudinal axis intersecting the rotational axis and extending perpendicular to the rotational axis.
- 20. The apparatus of claim 19, wherein the reflecting surface is on the housing at an intersection of the rotational axis and the longitudinal axis, and the beam is axially centered about the longitudinal axis.
US Referenced Citations (8)
Number |
Name |
Date |
Kind |
3848255 |
Migdal |
Nov 1974 |
A |
4312002 |
Stewart |
Jan 1982 |
A |
4504835 |
Howard et al. |
Mar 1985 |
A |
4670754 |
Zacchio |
Jun 1987 |
A |
H966 |
Waters et al. |
Sep 1991 |
H |
6075492 |
Schmidt et al. |
Jun 2000 |
A |
6307522 |
Alexanian |
Oct 2001 |
B1 |
6396448 |
Zimmerman et al. |
May 2002 |
B1 |