Information
-
Patent Grant
-
6353419
-
Patent Number
6,353,419
-
Date Filed
Thursday, March 11, 199925 years ago
-
Date Issued
Tuesday, March 5, 200223 years ago
-
Inventors
-
Original Assignees
-
Examiners
-
CPC
-
US Classifications
Field of Search
US
- 343 882
- 343 915
- 343 874
- 343 883
- 343 875
- 343 878
- 343 890
-
International Classifications
-
Abstract
A microcell having a plurality of antennas attached to an upper portion thereof is arranged to move along an interior of a guyed latticework tower. As the microcell is being raised, the antennas are in a stowed position within the confines of the tower structure. When the microcell reaches the top of the tower, the antennas are deployed by deploying mechanisms which utilize the vertical upward motion of the microcell to produce outwardly directed movement of the antennas to a deployed position. In the deployed position, the spacing between the antennas is greater than the distance between adjacent stanchions of the tower structure. The deploying motion is accomplished without additional driving motors, but is instead produced by the upward movement of the microcell driven by a winch and cable arrangement.
Description
BACKGROUND OF THE INVENTION
1. Field of the Invention
The present invention is directed to a device for deploying an antenna from a stowed position to an open deployed position. More particularly, the present invention is directed to deploying mechanisms for deploying antennas on top of a microcell which is located at the top of a tower.
2. Description of the Background Art
Standard cell site equipment is typically installed in a small block house located adjacent to a tower on which cell site antennas are mounted. The cell site radios in the block house is connected to the cell site antennas typically through hundreds of feet of coaxial cable. This arrangement produces a loss of a significant portion of the radio energy which is dissipated through the coaxial cable.
The antennas for a cell site often include a single omnidirectional whip antenna for transmitting and receiving signals, and an additional similar omnidirectional whip antenna for receiving signals. The second receive antenna is spaced some distance from the first antenna in order to provide space diversity, which ameliorates the effects of multipath fading. Multipath fading is a phenomenon in which radio signals transmitted over a large distance are received directly from the source as well as indirectly from reflected surfaces such as buildings, hills, lakes, etc. The multiple signals can combine in such a way that at certain times, the signals cancel each other, so that a highly attenuated signal is received. Spacing two receive antennas several wavelengths apart diminishes the signal fading.
SUMMARY OF THE INVENTION
The present invention is directed to a system for deploying an antenna from a stowed position to a deployed position on a tower frame having a lower section and an upper section. A carrier supporting the antenna is moveable relative to the tower frame in a direction toward the upper section, and the antenna is deployed from the stowed position to the deployed position when the carrier reaches the upper section of the tower frame.
For example, an antenna deploying mechanism moves the antennas from a stowed position within the confines of the tower structure while a microcell carrying the antennas is being raised or lowered, to a deployed position outside of the confines of the tower structure when the microcell reaches the top of the tower. The deployment can be accomplished without additional motors to move the antennas into position. Instead, the deployment mechanism can use the upward motion of the microcell provided by a winch to move the antennas from the stowed position to the deployed position. Similarly, lowering of the microcell by the winch can cause the antennas to automatically move from the deployed position to the stowed position within the confines of the tower structure.
BRIEF DESCRIPTION OF THE DRAWINGS
Other aspects and advantages of the present invention may become apparent upon reading the following detailed description and upon reference to the drawings, in which:
FIG. 1
is a perspective view showing a first embodiment of the antenna deployer of the present invention in a stowed position;
FIG. 2
is a perspective view showing the first embodiment of the antenna deployer in a deployed position;
FIG. 3
is a top schematic view of the first embodiment of the antenna deployer in a stowed position;
FIG. 4
is a top schematic view of the first embodiment of the antenna deployer in a deployed position;
FIG. 5
is a side schematic view of the first embodiment of the antenna deployer in a stowed position;
FIG. 6
is a side schematic view of the first embodiment of the antenna deployer in the deployed position;
FIG. 7
is a partial side view showing the details of the deployer socket of the first embodiment;
FIG. 8
is a partial cross-sectional view showing the details of the deployer arm of the first embodiment;
FIG. 9
is a partial cross-sectional view showing the internal components of the deployer arm of the first embodiment;
FIG. 10
is a partial cross-sectional view showing the deployer arm components of the first embodiment in a deployed position;
FIG. 11
is a perspective view showing a second embodiment of the present invention in a stowed position;
FIG. 12
is a perspective view of the second embodiment in a deployed position;
FIG. 13
is a side schematic view of the antenna deployer of the second embodiment in a stowed position;
FIG. 14
is a side schematic view of the antenna deployer of the second embodiment in a deployed position;
FIG. 15
is a perspective view showing a third embodiment of the present invention in a stowed position;
FIG. 16
is a perspective view of the third embodiment in a deployed position;
FIG. 17
is a side schematic view of the antenna deployer of the third embodiment in a stowed position;
FIG. 18
is a side schematic view of the antenna deployer of the third embodiment in a deployed position;
FIG. 19
is a perspective view of an antenna deployer according to a fourth embodiment of the present invention in a stowed position;
FIG. 20
is a perspective view of the antenna deployer of the fourth embodiment in a partially deployed position;
FIG. 21
is a perspective view of the antenna deployer of the fourth embodiment in a fully deployed position;
FIGS. 22
a
,
22
b
and
22
c
are top schematic views of the antenna deployer of the fourth embodiment showing the antenna deployer in the stowed position, the partially deployed position, and the fully deployed position, respectively, corresponding to
FIGS. 19 through 21
;
FIG. 23
is a perspective view showing a fifth embodiment of the present invention in a stowed position;
FIG. 24
is a perspective view of the fifth embodiment in a deployed position;
FIG. 25
is a side schematic view of an antenna deployer according to a sixth embodiment in a stowed position;
FIG. 26
is a side schematic view of the antenna deployer of the sixth embodiment in a deployed position;
FIG. 27
is a perspective view showing a seventh embodiment of the present invention in a stowed position;
FIG. 28
is a perspective view of the seventh embodiment in a deployed position;
FIG. 29
is a side schematic view of the antenna deployer of the seventh embodiment in a stowed position;
FIG. 30
is a side schematic view of the antenna deployer of the seventh embodiment in a deployed position; and
FIG. 31
is a perspective view of a tower showing the microcell elevating mechanism.
DETAILED DESCRIPTION
Various embodiments of the present invention will now be described in detail, with particular reference to the drawings. Throughout the drawings, like reference numerals are utilized to identify the same or similar elements.
As shown in
FIGS. 1-4
, a tower
10
includes three vertical stanchions
12
arranged at apexes of an equilateral triangle. The stanchions
12
are interconnected by a plurality of lattice members
14
which are arranged both diagonally and horizontally between adjacent stanchions
12
. The spacing between centers of the stanchions
12
is approximately 44 inches, although other sizes of towers
10
may be utilized with the present invention. One tower design that is particularly suitable for this arrangement is a guyed latticework structure, although other tower designs may be utilized. Further, a latticework style tower is considerably less expensive than a monopole of the same height.
A tower cross support
16
is located at the top of the tower
10
. The tower cross support
16
includes three equiangularly-spaced cross support members
18
which extend from the center of the triangle formed by the stanchions
12
to the apex of the triangle where the stanchions
12
are located. One of the cross support members
18
may include a pulley arrangement including a pair of pulleys
20
which are utilized with a winch
22
, discussed in more detail below, and illustrated in FIG.
31
.
A microcell
24
including cellular telephone equipment inside of a housing
26
is arranged interiorly of the tower for movement therealong. In order to reduce the loss of radio energy due to dissipation through hundreds of feet of coaxial cable, the microcell
24
is located at the top of the tower
10
with antennas
40
. In this way, only several feet of coaxial cable are needed between the antennas
40
and the microcell
24
, thereby significantly decreasing the loss of radio energy between the antennas
40
and the microcell radios. The antennas
40
are mounted to the microcell
24
, and therefore need to be raised and lowered with the microcell
24
. However, the separation distance between the antennas
40
which is required for satisfactory system performance can exceed the available space within the confines of the tower
10
.
The microcell
24
is raised and lowered by a cable
28
extending from the winch
22
, over the pulleys
20
, and which is connected to upper ends of sled-like runners
30
fixed to the microcell
24
. When maintenance is required, the microcell
24
is lowered by the winch
22
. The sled-like runners
30
assist the microcell
24
in moving up and down the tower
10
in a stable manner. The microcell
24
acts as a carrier for the components forming an antenna deployer
32
. The advantage of putting the microcell
24
within the tower
10
is that the tower structure is used to guide the microcell
24
as it is being raised and lowered. Additionally, the tower
10
provides a level of safety in the event that the microcell
24
becomes detached from the winch cable
28
.
Referring now to
FIGS. 5-10
, the antenna deployer
32
includes a deployer arm
34
including a horizontal arm member
36
and a vertical arm member
38
. An antenna
40
is attached to the distal end of the horizontal arm member
36
of the deployer arm
34
by a suitable connection, such as a threaded connection. The distal end of the horizontal arm member
36
includes a second auxiliary vertical arm member
42
which supports the lower end of the antenna
40
therein or thereon. The vertical arm members
38
,
42
and horizontal arm member
36
of the deployer arm
34
may be made of round aluminum tubing, such as 6061-T6 aluminum to support the size of antennas typically used in this application. The tubing may have has a 2½ inch diameter and a 0.065 inch wall thickness. Of course, other materials and sizes may be utilized with the present invention.
A deployer socket
44
is fixedly attached to the upper end of the microcell
24
. The deployer socket
44
receives the vertical arm member
38
of the deployer arm
34
therein. The deployer socket
44
and the vertical arm member
38
are cylindrical, tubular members coaxially aligned one within the other. The deployer socket
44
may include a plurality of gussets
46
for vertically stabilzing the deployer socket
44
with respect to the microcell
24
. The deployer socket
44
includes a vertically oriented is rectilinear guide slot
48
therein. A second identical vertically oriented rectilinear guide slot
48
is located on an opposite side of the deployer socket
44
, although the invention may be utilized with a single vertically oriented rectilinear guide slot
48
in the deployer socket
44
. The vertical arm member
38
of the deployer arm
34
includes a helical guide slot
50
therein, and contains a second helical guide slot
50
located opposite thereto, although the invention may be practiced with a single helical guide slot
50
.
The deployer socket
44
includes a pair of spaced-apart bushings
52
at upper and lower ends thereof for rotatably guiding the deployer arm
34
with respect to the deployer socket
44
. The pair of bushings
52
located between the deployer arm
34
and the deployer socket
44
may be made from a self-lubricating plastic such as celcon to provide a low-friction bearing surface. However, other types of bushings
52
may be utilized, or bearings may be utilized such as roller or ball bearings if desired.
Located interiorly of the vertical arm member
38
of the deployer arm
34
is an actuating disc
54
having a rotator pin
56
fixed thereto. With the vertical arm member
38
located within the deployer socket
44
, the rotator pin
56
is arranged to penetrate through the helical guide slot
50
of the deployer arm
34
and the rectilinear guide slot
48
of the deployer socket
44
. In this embodiment, since a pair of rectilinear guide slots
48
and a pair of helical guide slots
50
are provided, the rotator pin
56
extends through both sets of rectilinear guide slots
48
and helical guide slots
50
.
A compression spring
58
is arranged between the actuating disc
54
and the end of the vertical arm member
38
of the deployer arm
34
. The compression spring
58
is configured to bias the actuating disc
54
and rotator pin
56
to an uppermost position within the helical guide slot
50
and the rectilinear guide slot
48
. When the actuating disc
54
is in this uppermost position, the deployer arm
38
and the antenna
40
are in the stowed position.
Referring now to
FIGS. 1
,
2
,
5
and
6
, it can be seen that two of the cross support members
18
include a downwardly-depending rod
60
which serves to activate the antenna deployer
32
in this first embodiment. As the microcell
24
is raised by the winch
22
and cable
28
, a point is reached wherein the distal end of the rod
60
depending from the tower cross support member
18
engages and penetrates into the hollow interior of the vertical arm member
38
of the deployer arm
34
. As the microcell
24
is further raised, the distal end of the rod
60
engages the upper surface of the actuating disc
54
. With further upward movement of the microcell
24
, the rod
60
pushes the actuating disc
54
downwardly against the biasing force provided by the compression spring
58
. This in turn causes the rotator pin
56
to move along the helical guide slot
50
and the rectilinear guide slot
48
. Because the deployer socket
44
is fixed with respect to the microcell
24
, and thus the position of the rectilinear guide slot
48
does not change, the orientation of the rotator pin
56
with respect to the rectilinear guide slot
48
does not change. However, because the rotator pin
56
is also guided by the helical guide slot
50
, it is necessary for the deployer arm
34
, and thus the helical guide slot
50
, to rotate as the actuating disc
54
is moved downwardly. Accordingly, as the deployer arm
34
rotates, the horizontal arm member
36
of the deployer arm
34
moves from the stowed position within the confines of the triangle formed by the stanchions
12
, to the deployed position shown in
FIGS. 2 and 4
wherein the antenna
40
is spaced outwardly of the tower
10
. When two antennas
40
are in the deployed position, the spacing between the antennas
40
is approximately six feet, although other spacings may be utilized with the present invention.
When the microcell
24
is lowered, the process is reversed. The biasing force provided by the compression spring
58
forces the actuating disc
54
upwardly, thereby forcing the rotator pin
56
to move within the helical guide slot
50
to rotate the horizontal arm member
36
of the deployer arm
34
back to the stowed position. When the microcell
24
is in the filly elevated position, and the antenna
40
is in the deployed position, the microcell
24
is simply held in place by the supporting cable
28
connected to the winch
22
. Thus, it can be seen that the present invention provides a simple and efficient mechanism for deploying an antenna
40
without the use of any additional driving motors, and instead, the deployment and undeployment motions of the antenna
40
are controlled by the raising and lowering of the microcell
24
.
An antenna cable interconnecting the antenna
40
to the microcell
24
may pass through the tubing forming the horizontal arm member
36
and the vertical arm member
38
. Accordingly, a continuous passage is provided between the lower end of the vertical arm member
38
to the outer end of the horizontal arm member
36
. Further, when the deployer arm
34
is used with the auxiliary vertical arm member
42
located at the distal end of the horizontal arm member
38
, the continuous passage extends through the junction between the horizontal member
36
and both of the vertical arm members
38
,
42
so that the antenna cable may pass completely through the deployer arm
34
from one end to another. The antenna cable may exit the vertical arm member
38
through an aperture provided in a sidewall thereof at a location above where the uppermost portion of the deployer socket
44
would reach so that the deployer socket
44
would not interfere with the antenna cable. Alternatively, it is envisioned that an arrangement may be provided wherein the antenna cable passes completely through the bottom of the vertical arm member
38
, through an aperture provided centrally within the actuating disc
54
, and extends through the center of the compression spring
58
and the deployer socket
44
and into the microcell
24
.
An antenna deployer
70
according to a second embodiment of the present invention will now be described, with particular reference to
FIGS. 11-14
. In the second embodiment, the cross support members
18
of the tower do not have a rod
60
extending downwardly therefrom. Instead, the cross support members
18
include a knob or protrusion
72
on a lower side thereof although alternatively the lower side may simply be flat. However, the protrusion
72
on the cross support member
18
tends to locate the antenna deployer
70
into position prior to rotating into the deployed position. In the second embodiment, the deployer socket
74
does not include the rectilinear guide slot
48
as in the first embodiment. Instead, a pin
76
is fixed in position to the deployer socket
74
. A vertical arm member
78
of the deployer arm
80
includes a helical guide slot
82
which receives the pin
76
therein.
A compression spring
84
is located within the deployer socket
74
and is compressed between the end of the vertical arm member
78
of the deployer arm
80
and the base of the deployer socket
74
. As the microcell
24
is raised, a point is reached where the upper end of the vertical arm member
78
engages the protrusion
72
on the cross support member
18
. Further raising of the microcell
24
having the deployer socket
74
fixed thereto causes the pin
76
to move along the helical guide slot
82
in the vertical arm member
78
of the deployer arm
80
.
Because the position of the deployer socket
74
is fixed, and the position of the pin
76
is fixed, the vertical arm member
78
must rotate as the deployer socket
74
is raised because of the engagement of the pin
76
within the helical guide slot
82
. Therefore, the raising of the microcell
24
causes the deployer arm
80
to rotate from the stowed position shown in
FIG. 11
to the deployed position shown in FIG.
12
.
When the microcell
24
is lowered, the compression spring
84
forces the vertical arm member
78
of the deployer arm
80
upwardly in a direction away from the microcell
24
, causing the deployer arm
80
to move the antenna
40
into the stowed position because of the interaction of the helical guide slot
94
following the constraint provided by the pin
76
. In this embodiment, a pair of spaced-apart pins
76
, or one double-ended pin
76
, extending into both sides of the deployer socket
74
, is utilized and which follows a pair of opposed helical slots
82
. However, it should be understood that a single pin
76
and a single helical guide slot
82
may be utilized to produce the rotational movement of the deployer arm
80
from the linear movement of the microcell
24
and deployer socket
74
.
An antenna deployer
90
according to a third embodiment of the present invention will now be explained, with particular reference to
FIGS. 15 through 18
. In the embodiment shown in
FIG. 15
, the cross support members
18
include a downwardly-depending rod
92
. The distal end of the downwardly-depending rod
92
includes a helical slot
94
provided in a sidewall thereof. A deployer socket
96
is fixed to the upper end of the microcell
24
, and a vertical arm member
98
of a deployer arm
100
is located fully within the deployer socket
96
. In this third embodiment, a spring is not required between the lower end of the vertical arm member
98
of the deployer arm
100
and the base of the deployer socket
96
. A pin
102
is fixedly attached and extends across the hollow portion of the vertical arm member
98
.
As the microcell
24
is raised, and consequently the antenna deployer
90
is raised, a point is reached wherein the downwardly-depending rod
92
enters into the hollow portion of the vertical arm member
98
. Upon further raising of the microcell
24
, the helical slot
94
in the downwardly-depending rod
92
engages the pin
102
extending across the hollow portion of the vertical arm member
98
. Continued raising of the microcell
24
and the antenna deployer
90
causes the vertical arm member
98
to rotate by the action of the pin
102
sliding along the helical slot
94
in the downwardly-depending rod
92
. This is because the orientation of the helical slot
94
in the downwardly-depending rod
92
is fixed with respect to the tower
10
and to the microcell
24
. Thus, it is necessary for the vertical arm member
98
to rotate as the microcell
24
is further raised. This causes the horizontal arm member
36
to swing outwardly and move the antenna
40
from the stowed position shown in
FIG. 15
to the deployed position shown in FIG.
16
. When the microcell
24
is lowered, a reverse process occurs wherein the weight of the antenna
40
and deployer arm
100
causes them to remain within the deployer socket
96
and to rotate with respect to the downwardly-depending rod
92
by the interaction of the pin
102
following the helical slot
94
in the downwardly-depending rod
92
.
An antenna deployer
110
accordingly to a fourth embodiment of the present invention will now be described, with particular reference to
FIGS. 19 through 22
. In the fourth embodiment, the tower cross support
16
includes a single downwardly-depending rod
112
located at the center of the tower cross support
16
, which is centrally located within the triangular area formed by the three stanchions
12
. The distal end of the downwardly-depending rod
112
includes a helical slot
114
as in the third embodiment.
The antenna deployer
110
of the fourth embodiment includes a central horizontal arm
116
rotatably mounted to the top of the microcell
24
and centrally thereof Each end of the central horizontal arm
116
includes a horizontal arm member
118
pivotally connected thereto. A distal end of each of the horizontal arm members
118
includes an antenna
40
extending upwardly therefrom. Located at the center of the central horizontal arm
116
is a socket
120
having a pin
122
extending across a hollow interior portion thereof.
Similarly to the actuation of the antenna deployer
90
of the third embodiment, in the fourth embodiment, as the microcell
24
is raised, the pin
122
in the socket
120
of the central horizontal am
116
becomes engaged in the helical slot
114
in the downwardly-depending rod
112
attached to the tower cross support
16
. Further upward movement of the microcell
24
and the antenna deployer
110
causes the pin
122
to slide along the helical slot
114
in the downwardly-depending rod
112
, thus causing the central horizontal arm
116
of the antenna deployer
110
to rotate as the pin
122
follows the helical slot
114
. As the central horizontal arm
116
of the antenna deployer
110
rotates, the horizontal arm members
118
rotate therewith to a point where the horizontal arm members
118
engage deflector blocks
124
attached to the tower
10
. The deflector blocks
124
cause the horizontal arm members
118
to move away from the central horizontal arm
116
through a position shown in
FIG. 20
, to the deployed position shown in FIG.
21
. The length of the central horizontal arm
116
is sized so that it does not contact the deflector blocks
124
, while the length of the horizontal arm members
118
are sized so that, upon rotation of the central horizontal arm
116
, the horizontal arm members
118
engage the deflector blocks
124
to deflect the horizontal arm members
118
into the deployed position upon further rotation of the central horizontal arm
116
.
To return the antenna
40
to the stowed position, the microcell
24
is lowered, causing the central horizontal arm
116
to rotate as the pin
122
in the socket
120
follows the helical slot
114
of the fixed downwardly-depending rod
112
. Additional deflector blocks
124
are utilized to assist movement of the horizontal arm members
118
to the stowed position beside the central horizontal arm
116
. In
FIGS. 19 through 21
, the tower cross support
16
has been removed from the figures for clarity.
An antenna deployer
130
according to a fifth embodiment and an antenna is deployer
132
according to a sixth embodiment of the present invention will now be described with respect to
FIGS. 23 through 26
. As shown in
FIGS. 23 and 24
, a tower cross support
134
located across the tower
10
is not formed as a planar unit, but is instead formed by three cross support members
136
extending upwardly and inwardly from the top end of each of the stanchions
12
. A ring
138
having an aperture
140
therein is located at the junction of the upper ends of each of the cross support members
136
. toward the upper guide
146
. During this movement, the antenna support members
148
are pushed outwardly until a point is reached where the lower guide
144
abuts the upper guide
146
and cannot move upwardly any further, and the antennas
40
are in the fully deployed position as shown in FIG.
26
.
The antenna deployer
130
of the fifth embodiment shown in
FIGS. 23 and 24
is configured slightly different from the antenna deployer
132
of the sixth embodiment shown in
FIGS. 25 and 26
, but operation is similar. In the antenna deployer
130
of the fifth embodiment shown in
FIGS. 23 and 24
, mid-portions of the linkage members
150
on each side of the support pole
142
are pivotally connected to form a pantograph mechanism. Additionally, the antenna support members
148
comprise a fixed portion
160
and a slidable collar portion
162
. A spring (not shown in
FIGS. 23 and 24
) may be used to assist the movement of the antenna support members
148
to the stowed position upon lowering of the microcell
24
. However, due to the geometry of the antenna deployer
130
, the movement to the stowed position occurs due to gravity. Also, as shown in
FIGS. 23-26
, an additional antenna
40
or a lightning rod may be located at the top of the support pole
142
which may pass freely through the fixed ring
138
on the tower cross support
134
.
An antenna deployer
170
according to a seventh embodiment of the present invention will now be described, with particular reference to
FIGS. 27 through 30
. In the seventh embodiment, three antennas
40
are affixed to the microcell
24
. Accordingly, three antenna deployers
170
are utilized for moving the antennas
40
from the stowed position shown in
FIG. 27
to the deployed position shown in
The antenna deployer
132
according to the sixth embodiment shown in
FIG. 25
includes a support pole
142
fixed to the upper portion of the microcell
24
. A lower guide
144
is fixedly attached to the support pole
142
, and an upper guide
146
is located above the lower guide
144
and which is slidable along the support pole
142
. A pair of antenna support members
148
are located on opposite sides of the support pole
142
. Linkage members
150
are located between the upper guide
146
and each of the antenna support members
148
, and linkage members
150
are also located between the lower guide
144
and each of the antenna support members
148
. The connection points between the linkage members
150
and tie upper guide
146
, lower guide
144
, and antenna support members
148
are freely pivotable. A tension spring
152
is arranged between the antenna support members
148
which tends to bias the antenna support members
148
toward one another so that the antennas
40
will tend to assume a stowed position. Alternatively, a compression spring may be arranged between the upper guide
146
and the lower guide
144
to bias he upper guide
146
and the lower guide
144
apart, whereby the antennas
40
will be biased toward one another to the stowed position.
To deploy the antennas
40
, the microcell
24
is raised until a point is reached where the upper guide
146
contacts the ring
138
of the tower cross support
134
, and further upward movement of the upper guide
146
is prohibited. However, the upper end of the support pole
142
may pass through the aperture
140
in the ring
138
and may be further elevated above the tower cross support
134
. As the support pole
142
continues to move upwardly, the lower guide
144
also continues to move upwardly FIG.
28
. Each antenna deployer
170
includes a horizontal arm member
172
. The horizontal arm member
172
assumes a horizontal orientation only in the deployed position. However, the horizontal arm member
172
assumes approximately a 45° angle with respect to horizontal in the antenna stowed position, as shown in FIG.
29
. One end of the horizontal arm member
172
includes a vertical arm member
174
fixedly attached thereto at a right-angle. A pivot
176
is located at the junction between the horizontal arm member
172
and the vertical arm member
174
for pivotally connecting the antenna deployer
170
to a vertical support member
178
extending upwardly from the upper surface of the microcell
24
. The distal end of the vertical arm member
174
of the antenna deployer
170
is attached to one end of a tension spring
180
. The other end of the tension spring
180
is fixed to the microcell
24
. The opposite end of the horizontal arm member
172
includes an antenna support member
182
to which the antenna
40
is fixed.
As the microcell
24
is raised along the tower
10
, the horizontal arm members
172
and the antennas
40
are oriented at approximately a 45° angle with respect to horizontal. As the microcell
24
is raised, the antennas pass above the cross support members
18
of the tower cross support
16
, until a point is reached where the horizontal arm members
172
engage portions of the cross support members
18
. Further upward movement of the microcell causes the horizontal arm members
172
to move downwardly against the abutting forces provided by the cross support members
18
. As the horizontal arm members
172
move downwardly toward the horizontal position shown in
FIG. 28
, the tension springs
180
are stretched to increase the forces provided by the springs
180
, until a point is reached where the microcell
24
is in an uppermost position and the antennas
40
are in the fully deployed position shown in
FIGS. 28 and 30
.
When it becomes necessary to lower the microcell
24
, for example for maintenance or the like, the lowering of the microcell
24
allows the horizontal arm members
172
to move angularly upwardly, pivoting about the pivot
176
with the force being provided by the tension springs
180
. Once the antennas
40
are in the stowed position, the microcell
24
can be filly lowered to the ground.
In each of the above embodiments, actuation of the antenna from the stowed position to the deployed position is accomplished by the interaction of the antenna deployer with a fixed member at the upper end of the tower. The antennas are automatically moved from the stowed position to the deployed position, and from the deployed position to the stowed position, without necessitating the use of additional motors for driving the antenna deployers. The deploying motion and collapsing motion is accomplished by the upward movement of the microcel
24
, which upward movement is provided by a winch
22
and an associated cable
28
.
Although the present invention has been described with a microcell
24
moving within the confines of the tower frame, it should be understood that the present invention may also be utilized with the antenna deployer and/or microcell
24
moving on the outside of the tower frame. Also, although the present invention has been described as utilizing deployers which utilize the upward movement of the microcell
24
to provide the actuation of the deployers to move the antennas
40
from the stowed position to the deployed position, it should be understood that other deploying mechanisms may be utilized which do not use the upward movement of the microcell to cause actuation. For example, a deploying mechanism may be utilized with the present invention whereby, once the antennas
40
have been raised to the desired position, a mechanism is actuated to deploy the antennas
40
. The actuating mechanism may comprise an electrical switch, motor, solenoid, or spring-catch which may be activated by remotely pressing a button pulling a string, or otherwise signaling the actuating mechanism to deploy the antennas
40
.
What has been described is merely illustrative of the application of the principles of the present invention. Those skilled in the art will recognize that these and various other modifications, arrangements and methods can be made to the present invention without strictly following the explanatory applications illustrated and described herein and without departing from the spirit and scope of the present invention.
Claims
- 1. An apparatus for deploying an antenna from a stowed position to a deployed position on a tower frame having a lower section and an upper section, said apparatus comprising:a carrier supporting said antenna, said carrier being movable relative to said tower frame within an interior space of said tower frame in a direction toward said upper section; and an antenna deployer for deploying said antenna from said stowed position to said deployed position when said carrier reaches said upper section of said tower frame.
- 2. The apparatus according to claim 1, said antenna deployer comprising a pair of spaced-apart deploying devices for deploying a pair of antennas to deployed positions such that said antennas are spaced apart by a distance greater than a longest interior width dimension of said tower frame.
- 3. The apparatus according to claim 1, said antenna deployer converting longitudinal movement of said carrier into lateral deploying movement of said antenna.
- 4. The apparatus according to claim 1, further comprising an elevating device for moving said carrier from said lower section to said upper section.
- 5. The apparatus according to claim 4, said elevating device comprising a winch and cable mechanism.
- 6. The apparatus according to claim 1, said antenna deployer comprising:a socket fixed to said carrier; a first arm member partially received within said socket; and a second arm having one end fixed to said first am, and another end supporting said antenna.
- 7. The apparatus according to claim 1, said antenna deployer comprising:a first arm rotatably secured to said carrier; and a second arm having one end pivotally attached to said first arm, and another end supporting said antenna.
- 8. The apparatus according to claim 7, further comprising a third arm having one end pivotally attached to said first arm, and another end supporting a second antenna.
- 9. The apparatus according to claim 1, said antenna deployer comprising:a support pole attached to said carrier, said support pole including a lower guide member fixed thereto, and an upper guide member slidable therealong; a first arm having a first end pivotally ached to said upper guide member; a second arm having a first end pivotally attached to said lower guide member; an antenna support member attached to one of said first arm and said second arm; and a connector pivotally interconnecting said first arm to said second arm.
- 10. The apparatus according to claim 9, said support pole including an antenna attached thereto.
- 11. The apparatus according to claim 9, said support pole including a lightning rod attached thereto.
- 12. The apparatus according to claim 9, said connector pivotally interconnecting a mid-portion of said first arm to a mid-portion of said second arm.
- 13. The apparatus according to claim 9, wherein said connector is fixed to said antenna support member.
- 14. The apparatus according to claim 9, wherein a second end of said first arm and a second end of said second arm are pivotally attached to said connector.
- 15. The apparatus according to claim 1, said antenna being located within an interior space of said tower frame when in said stowed position, and said antenna being opened laterally outside of said interior space when in said deployed position.
- 16. The apparatus according to claim 1, wherein said carrier includes said antenna deployer.
- 17. An apparatus for deploying an antenna from a stowed position to a deployed position on a tower frame having a lower section and an upper section, said apparatus comprising:a carrier supporting said antenna, said carrier being movable relative to said tower frame in a direction toward said upper section; and an antenna deployer for deploying said antenna from said stowed position to said deployed position when said carrier reaches said upper section of said tower frame, said upper section of said tower frame including an actuating member for contacting a portion of said antenna deployer when said carrier reaches said upper section of said tower frame.
- 18. The apparatus according to claim 17, said actuating member comprising an abutment which prevents further upward movement of said portion of the antenna deployer.
- 19. An apparatus for deploying an antenna from a stowed position to a deployed position on a tower frame having a lower section and an upper section, said apparatus comprising:a carrier supporting said antenna, said carrier being movable relative to said tower frame in a direction toward said upper section; and an antenna deployer for deploying said antenna from said stowed position to said deployed position when said carrier reaches said upper section of said tower frame, said antenna deployer comprising a spring for biasing said antenna toward said stowed position.
- 20. An apparatus for deploying an antenna from a stowed position to a deployed position on a tower frame having a lower section and an upper section, said apparatus comprising:a carrier supporting said antenna, said carrier being movable relative to said tower frame in a direction toward said upper section; and an antenna deployer for deploying said antenna from said stowed position to said deployed position when said carrier reaches said upper section of said tower frame, said antenna deployer comprising: a socket fixed to said carrier; a first arm member partially received within said socket; a second arm having one end fixed to said first arm, and another end supporting said antenna; at least one rectilinear slot located in a sidewall of said socket; at least one helical slot located in a sidewall of said first arm; and an actuating disk located within said first arm, said actuating disk having at least one pin extending therefrom and located within an intersecting portion of said rectilinear slot and said helical slot.
- 21. The apparatus according to claim 20, said antenna deployer further comprising a spring located between said actuating disk and a bottom end of said first arm.
- 22. The apparatus according to claim 20, said upper section of said tower frame including an actuating member for contacting a portion of said antenna deployer when said carrier reaches said upper section of said tower frame, said actuating member comprising a rod extending from a cross support member of said tower frame, one end of said rod being receivable within said first arm for contacting and moving said actuating disk along said first arm, thereby causing said first arm to rotate as said helical slot follows said pin in said rectilinear slot.
- 23. An apparatus for deploying an antenna from a stowed position to a deployed position on a tower frame having a lower section and an upper section, said apparatus comprising:a carrier supporting said antenna, said carrier being movable relative to said tower frame in a direction toward said upper section; and an antenna deployer for deploying said antenna from said stowed position to said deployed position when said carrier reaches said upper section of said tower frame, said antenna deployer comprising: a socket fixed to said carrier; a first arm member partially received within said socket; a second arm having one end fixed to said first arm, and another end supporting said antenna; at least one helical slot located in a sidewall of said first arm; and at least one pin extending inwardly from a sidewall of said socket, said pin being located within said helical slot.
- 24. The apparatus according to claim 23, said antenna deployer further comprising a spring located between a bottom end of said socket and a bottom end of said first arm.
- 25. The apparatus according to claim 23, said upper section of said tower frame including an actuate member for contacting a portion of said antenna deployer when said carrier reaches said upper section of said tower frame, said actuating member comprising a knob extending from a cross support member of said tower frame, said knob contacting and moving said first arm along said socket, thereby causing said first arm to rotate as said helical slot follows said pin in said socket.
- 26. An apparatus for deploying an antenna from a stowed position to a deployed position on a tower frame having a lower section and an upper section, said apparatus comprising:a carrier supporting said antenna, said carrier being movable relative to said tower frame in a direction toward said upper section; and an antenna deployer for deploying said antenna from said stowed position to said deployed position when said carrier reaches said upper section of said tower frame, said antenna deployer comprising: a socket fixed to said carrier; a first arm member partially received within said socket; a second arm having one end fixed to said first arm, and another end supporting said antenna; at least one pin extending inwardly from an interior of said first arm; and an actuating member located at said upper section of said tower frame for contacting a portion of said antenna deployer when said carrier reaches said upper section of said tower frame, said actuating member comprising a rod extending from a cross support member of said tower frame, one end of said rod including at least one helical slot in a sidewall thereof, said one end of said rod being receivable within said first arm and movable therealong with said pin being located in said helical slot, thereby causing said first arm to rotate as said pin follows said helical slot.
- 27. An apparatus for deploying an antenna from a stowed position to a deployed position on a tower frame having a lower section and an upper section, said apparatus comprising:a carrier supporting said antenna, said carrier being movable relative to said tower frame in a direction toward said upper section; and an antenna deployer for deploying said antenna from said stowed position to said deployed position when said carrier reaches said upper section of said tower frame, said antenna deployer comprising: a first arm rotatably secured to said carrier; a second arm having one end pivotally attached to said first arm, and another end supporting said antenna; a socket fixed to said first arm; and at least one pin extending inwardly from an interior of said socket.
- 28. The apparatus according to claim 27, said upper section of said tower frame including an actuating member for contacting a portion of said antenna deployer when said carrier reaches said upper section of said tower frame, said actuating member comprising a rod extending from a cross support member of said tower frame, one end of said rod including at least one helical slot in a sidewall thereof, said one end of said rod being receivable within said socket and moveable therealong with said pin being located in said helical slot, thereby causing said first arm to rotate as said pin follows said helical slot.
- 29. The apparatus according to claim 28, further comprising at least one guide member attached to said tower frame for guiding said second arm into said deployed position as said first arm is rotated.
- 30. An apparatus for deploying an antenna from a stowed position to a deployed position on a tower frame having a lower section and an upper section, said apparatus comprising:a carrier supporting said antenna, said carrier being movable relative to said tower frame in a direction toward said upper section; and an antenna deployer for deploying said antenna from said stowed position to said deployed position when said carrier reaches said upper section of said tower frame, said antenna deployer comprising: a support pole attached to said carrier, said support pole including a lower guide member fixed thereto, and an upper guide member slidable therealong; a first arm having a first end pivotally attached to said upper guide member; a second arm having a first end pivotally attached to said lower guide member; an antenna support member attached to one of said first arm and said second arm; a connector pivotally interconnecting said first arm to said second arm; and a spring for biasing said antenna support member toward said support pole.
- 31. An apparatus for deploying an antenna from a stowed position to a deployed position on a tower frame having a lower section and an upper section, said apparatus comprising:a carrier supporting said antenna, said carrier being movable relative to said tower frame in a direction toward said upper section; and an antenna deployer for deploying said antenna from said stowed position to said deployed position when said carrier reaches said upper section of said tower frame, said antenna deployer comprising: a support pole attached to said carrier, said support pole including a lower guide member fixed thereto, and an upper guide member slidable therealong; a first arm having a first end pivotally attached to said upper guide member; a second arm having a first end pivotally attached to said lower guide member; an antenna support member attached to one of said first arm and said second arm; and a connector pivotally interconnecting said first arm to said second arm, said upper section of said tower frame including an actuating member for contacting a portion of said antenna deployer when said carrier reaches said upper section of said tower frame, said actuating member comprising a ring having an aperture therein through which said support pole may slidably pass, said upper guide member abutting said ring, thereby preventing further upward movement of said upper guide member.
- 32. An apparatus for deploying an antenna from a stowed position to a deployed position on a tower frame having a lower section and an upper section, said apparatus comprising:a carrier supporting said antenna, said carrier being movable relative to said tower frame in a direction toward said upper section; and an antenna deployer for deploying said antenna from said stowed position to said deployed position when said carrier reaches said upper section of said tower frame, said antenna deployer comprising: a support member attached to said carrier; a deployer arm having a first end portion pivotally attached to said support member and a second end portion supporting said antenna; and a spring connected between said deployer arm and said carrier for biasing said antenna toward said stowed position.
- 33. The apparatus according to claim 32, said deployer arm comprising a first arm and a second arm, said first arm supporting said antenna, said second arm having said spring connected thereto, wherein said first arm assumes approximately a 45° angle with respect to horizontal when said antenna is in said stowed position.
- 34. The apparatus according to claim 33, wherein said first arm is approximately horizontal when said antenna is in said deployed position.
- 35. The apparatus according to claim 33, said upper section of said tower frame including an actuating member for contacting a portion of said first arm when said carrier reaches said upper section of said tower frame to prevent further upward movement of said portion of said first arm.
- 36. A method of deploying an antenna from a stowed position to a deployed position on a tower frame, the antenna being supported by a carrier, said method comprising the following steps:raising said carrier relative to said tower frame within an interior space of said tower frame with said antenna in said stowed position; and then deploying said antenna from said stowed position to said deployed position.
- 37. A method of deploying an antenna from a stowed position within an interior space of a tower frame to a deployed position where the antenna is opened laterally outside of the interior space, the antenna being mounted to a deploying mechanism supported by a carrier, said method comprising the following steps:raising said carrier along said tower frame and within said interior space with said antenna in said stowed position; contacting said deploying mechanism with a member located at an upper section of said tower frame; and deploying said antenna to said deployed position by further raising said carrier.
US Referenced Citations (3)
Number |
Name |
Date |
Kind |
3952984 |
Dimitry |
Apr 1976 |
A |
3959795 |
Foster |
May 1976 |
A |
5537125 |
Harrell, Jr. et al. |
Jul 1996 |
A |