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EP 0 657 956 B1 |
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EUROPEAN PATENT SPECIFICATION |
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Mention of the grant of the patent: |
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20.10.1999 Bulletin 1999/42 |
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Date of filing: 19.11.1994 |
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Antenna assembly
Antennenanordnung
Agencement d'antenne
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Designated Contracting States: |
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DE ES FR GB IT |
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Priority: |
06.12.1993 AU PM277293
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Date of publication of application: |
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14.06.1995 Bulletin 1995/24 |
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Proprietor: ALCATEL |
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75008 Paris (FR) |
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Inventors: |
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- McDonald, Noel A., Dr.
Croydon,
3136 Victoria (AU)
- Harris, Mark Andrew
Wheelers Hill,
3150 Victoria (AU)
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Representative: Döring, Roger, Dipl.-Ing. et al |
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Kabelkamp 20 30179 Hannover 30179 Hannover (DE) |
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References cited: :
WO-A-93/06631 WO-A-94/27338 US-A- 4 725 845
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WO-A-93/22804 DE-A- 4 040 223
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| Note: Within nine months from the publication of the mention of the grant of the European
patent, any person may give notice to the European Patent Office of opposition to
the European patent
granted. Notice of opposition shall be filed in a written reasoned statement. It shall
not be deemed to
have been filed until the opposition fee has been paid. (Art. 99(1) European Patent
Convention).
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[0001] The invention relates to an antenna assembly for transmitting or receiving RF signals
of a given wavelength, said assembly comprising a metal feed tube member having a
feed line for connexion to an RF signal source at one end thereof, and two wire helices
of predetermined length, diameter and pitch arranged co-axially about said feed tube
in a bifilar manner, one end of each helix being coupled to the feed line.
[0002] In a communication system of the abovementioned kind, there exists a requirement
for a mast style, high gain, circularly polarised omni-directional antenna for each
mobile earth station to allow for operation at all azimuth angles. The need for high
gain requires the antennas elevation pattern to be very directional. The satellite
will appear at different angles above the horizon from mobile earth stations positioned
at different geographical locations, and therefore for maximum antenna gain at an
earth mobile station, the major radiation lobe of the station's antenna should be
adjusted to precise elevation angle vis-a-vis the satellite. Typically, the elevation
angle of a geostationary satellite for an Australian satellite communication system
presently in use is 160° E longitude and therefore the correct angle of elevation
for an associated earth station antenna for optimum gain in, for example Sydney, is
50°, whereas in Perth the correct angle of elevation of the antenna is 30°.
[0003] Antenna arrangements are known which use an array phasing method for electronically
controlling the elevation angle of the antennas radiation lobe, but this method is
complex and relatively expensive. Further, some known antenna arrangement for satellite
communication, such as a quadrifilar helical antenna have undesirable wide beam low
gain elevation lobe patterns.
[0004] The earlier, late published patent application WO 94/27338 describes a steerable
beam helix antenna for transmitting and receiving RF signals. Two wire helices are
arranged in bifilar manner within a dielectric sheet which is wound around the axis
of the antenna. The outer side of the dielectric sheet is affixed to a radome while
the inner side is affixed to a central tube. The wire helices are fed via feed lines
which are positioned within the central tube.
[0005] It is an object of the present invention to provide a simple, relatively high gain
antenna arrangement whose radiation lobe's angle of elevation can be simply adjusted.
[0006] According to the invention there is provided an antenna assembly for transmitting
or receiving RF signals of a given wavelength, in which the feed tube member has a
co-axial inner conductor as a part of the feed line, each helix being commonly coupled
with one end to the inner conductor's end and the other end of each helix being separately
fixed to a first annular-shaped suppurt member slidably encircling said feed tube
member, said assembly further including a calibrated adjustment means comprising a
tubular housing member of dielectric material that is transparent to RF energy, and
a tubular base member into which one end of said tubular housing member slidably nests,
said helices, said tubular housing member and said tubular base member having a common
axis and said tubular housing member enclosing said helices, and said first annular-shaped
support member being attached to said tubular housing member, said tubular base member
including two parallel screw channels formed in the base member's inner surface which
co-operate with two pin members extending outwardly from a portion of said tubular
housing member resting within said tubular base member such that selective partial
rotation of said tubular housing member causes a partial rotation and axial movement
of said first annular-shaped support member, whereby the pitch of said helices is
changed by a predetermined distance and the diameter of said helices is substantially
maintained, thereby changing the elevation angle of electromagnetic waves radiating
from or received by said antenna assembly at said given wavelength to a desired angle
of elevation corresponding to a selected calibration.
[0007] In order that the invention may be readily carried into effect an embodiment thereof
will now be described in relation to the accompanying drawings, in which:
[0008] Figure 1 shows a bifilar helical antenna element of the antenna assembly of the present
invention.
[0009] Figure 2 shows the top section of the antenna element of Figure 1.
[0010] Figure 3 shows the bottom section of the antenna element of Figure 1.
[0011] Figure 4 shows the radome assembly within which the antenna element of Figure 1 is
enclosed.
[0012] Figure 5 shows, in cross section, details of an adjusting element of the antenna
assembly.
[0013] Figure 6 illustrates the relationship between the diameter and pitch of the antenna
element of Figure 1.
[0014] Figure 6a graphically illustrates a typical radiation pattern of the antenna element
of Figure 1.
[0015] Referring to the drawings, the antenna element comprises a copper feed tube 1 within
which is a co-axial inner conductor 2 surrounded by dielectric material 3. Feed tube
1 is fixedly attached to a base member 4 through which an RF signal is fed to the
inner conductor 2.
[0016] About feed tube 1 is formed two helices 5 and 6 of beryllium copper wire to form
a bifilar helix. One end of each helix 5, 6 is fixedly attached to an annular shaped
bottom support member 7 of dielectric material which slidably encircles feed tube
1. The other end of each helix is electrically terminated on respective contact zones
8 and 9 provided on an annular-shaped top support member 10 of dielectric material.
The top support member 10 encircles feed tube 1 and is fixedly attached thereto. The
distal end of inner conductor 2 is terminated on contact zone 9. Contact zones 8 and
9 are coupled by a cable balun 11 of a predetermined length.
[0017] The radome assembly shown in Figures 4 and 5 comprises a tubular member 12 of dielectric
material that is transparent to R.F. energy. The inside diameter of tubular member
12 is preferably equal to the diameter of the bifilar helix. Tubular member 12 nests
co-axially, in a slidable manner, within a tubular base adjustment-guide member 13.
The radome assembly further comprises a locking collar 14 which co-operates with a
screw-thread (not shown) at the end of base adjustment guide member 13.
[0018] Tubular member 12 is provided on its exterior surface with predetermined calibrations
15 for setting the required radiation lobe elevation angle. On the inner surface 16
of tubular base adjustment-guide member 13 there are provided two parallel channels
17 of a predetermined pitch for respectively co-operating with two adjustment guide
pins, one of which, 18, is shown, extending from the surface of bottom support member
7 and protruding through tubular member 12 to engage respective channels 17.
[0019] To assemble the antenna, the antenna element shown in Figure 1 is placed within the
radome assembly. Base member 4 of the antenna assembly is co-axially fixed within
the end portion of tubular base adjustment guide member 13. Adjustment guide pins
18 respectively co-operatively engage screw channels 17 so that on twisting tubular
member 12 about its axis bottom support member 7 is caused to move axially and rotate
thereby causing the pitch of the helices 5 and 6 to deform whilst maintaining the
diameter of the helices substantially constant and equal to the inner diameter of
tubular member 12 to prevent movement of the helices.
[0020] Referring to Figure 6 and 6a, the relationship between diameter and pitch of the
bifilar helical antenna element is graphically illustrated. The following formula
sets out this relationship:

Where
D = Diameter of helix in meters
P = Pitch between turns of the same helix in meters.
λ = Wavelength at radiation frequency in meters.
φ = Elevation angle in degrees.
[0021] As shown in the above formula the diameter and pitch of a given bifilar helix can
be deformed to give complete and continuous adjustment of the elevation angle φ. A
practical constraint is to maintain the diameter of the helices substantially constant
within the radome.
[0022] In use, the user of a mobile earth station equipped with an antenna arrangement of
the present invention would adjust the elevation angle of the radiated lobe when necessary
by twisting tubular member 12 to align a predetermined calibration 15. The calibrations
may be geographical labels such as a city name. After the antenna's radiation lobe
elevation angle is adjusted, tubular member 12 is locked by tightening locking caller
14.
1. An antenna assembly for transmitting or receiving RF signals of a given wavelength,
said assembly comprising a metal feed tube member (1) having a feed line for connexion
to an RF signal source at one end thereof, and two wire helices (5,6) of predetermined
length, diameter and pitch arranged co-axially about said feed tube in a bifilar manner,
one end of each helix (5,6) being coupled to the the feed line, characterized in that the feed tube member (1) has a co-axial inner conductor (2) as a part of
the feed line, each helix (5,6) being commonly coupled with one end to the inner conductor's
(2) end and the other end of each helix (5,6) being separately fixed to a first annular-shaped
support member (7) slidably encircling said feed tube member (1), said antenna assembly
further includes a calibrated adjustment means comprising a tubular housing member
(12) of dielectric material that is transparent to RF energy, and a tubular base member
(13) into which one end of said tubular housing member (12) slidably nests, said helices
(5,6), said tubular housing member (12) and said tubular base member (13) having a
common axis and said tubular housing member (12) enclosing said helices (5,6), and
said first annular-shaped support member (7) being attached to said tubular housing
member (12), said tubular base member (13) including two parallel screw channels (17)
formed in the base member's (13) inner surface which co-operate with two pin members
(18) extending outwardly from a portion of said tubular housing member (12) resting
within said tubular base member (13) such that selective partial rotation of said
tubular housing member (12) causes a partial rotation and axial movement of said first
annular-shaped support member (7), whereby the pitch of said helices (5,6) is changed
by a predetermined distance and the diameter of said helices (5,6) is substantially
maintained, thereby changing the elevation angle of electromagnetic waves radiating
from or received by said antenna assembly at said given wavelength to a desired angle
of elevation corresponding to a selected calibration.
2. An antenna assembly as claimed in claim 1, characterized in that a second annular-shaped support member (10) fixed to an end section of said
metal feed tube (1) is included, said second annular-shaped support member (10) including
contact means for coupling said one end of each helix (5,6) to said the inner conductor's
(2) said other end.
3. An antenna assembly as claimed in claim 2, characterized in that said contact means comprises two contact zones (8,9) each of which is respectively
connected to a said one end of a helix, one of said contact zones (9) being further
connected to the inner conductor's (2) said other end, said contact zones (8,9) being
coupled by a balun cable means (11) of a predetermined length.
4. An antenna assembly as claimed in any one of claims 1 to 3, characterized in that said tubular housing member (12) includes calibration means (15) thereon.
5. An antenna assembly as claimed in claim 4, characterized in that said calibration means (15) comprise markings indicating geographic locations.
6. An antenna assembly as claimed in any one of claims 1 to 5, charaterized in that locking means (14) for releasably locking said tubular housing member (12)
to said tubular base member (13) are included.
7. An antenna assembly as claimed in any one of the preceding claims, characterized in that said wire helices (5,6) are formed from beryllium copper wire.
1. Antennenbaugruppe zum Senden und Empfangen von HF-Signalen mit einer gegebenen Wellenlänge,
wobei die Baugruppe ein Metallzuleitungsröhren-Element (1) mit einer Zuleitung zur
Verbindung mit einer HF-Signalquelle an einem Ende davon und zwei Drahtspiralen (5,
6) mit vorher festgelegter Länge, Durchmesser und Steigung umfasst, die auf bifilare
Weise koaxial um die Zuleitungsröhre angeordnet sind, wobei ein Ende jeder Spirale
(5, 6) mit der Zuleitung verbunden ist, dadurch gekennzeichnet, dass das Zuleitungsröhrenelement (1) einen koaxialen inneren Leiter (2) als Teil
der Zuleitung aufweist, wobei ein Ende jeder Spirale (5,6) mit dem Ende des inneren
Leiters (2) und das andere Ende jeder Spirale (5, 6) gesondert an einem ersten ringförmigen
Halteelement (7) befestigt ist, das das Zuleitungsröhrenelement (1) verschiebbar umgibt,
wobei die Antennenbaugruppe außerdem ein kalibriertes Einstellmittel enthält, das
ein röhrenförmiges Gehäuseelement (12) aus elektrisch isolierendem Material, das durchlässig
für HF-Energie ist, und ein röhrenförmiges Basiselement (13) umfasst, in das ein Ende
des röhrenförmigen Gehäuseelementes (12) verschiebbar hineingeschoben ist, wobei die
Spiralen (5, 6), das röhrenförmige Gehäuseelement (12) und das röhrenförmige Basiselement
(13) eine gemeinsame Achse aufweisen und das röhrenförmige Gehäuseelement (12) die
Spiralen (5, 6) umschließt und das erste ringförmige Halteelement (7) an dem röhrenförmigen
Gehäuseelement (12) befestigt ist, wobei das röhrenförmige Basiselement (13) zwei
in der Innenfläche des Basiselementes (13) geformte parallele schraubenförmige Kanäle
(17) enthält, die mit zwei Stiftelementen (18) im Wirkeingriff sind, die sich von
einem Teil des röhrenförmigen Gehäuseelementes (12) nach außen erstrecken, das sich
im röhrenförmigen Basiselement (13) befindet, so dass eine selektive Teilrotation
des röhrenförmigen Gehäuseelementes (12) eine Teilrotation und eine axiale Bewegung
des ersten ringförmigen Halteelementes (7) bewirkt, wobei die Steigung der Spiralen
(5, 6) um einen festgelegten Betrag geändert und der Durchmesser der Spiralen (5,
6) im wesentlichen beibehalten wird, wodurch der Erhebungswinkel von elektromagnetischen
Wellen, die bei der gegebenen Wellenlänge von der Antennenbaugruppe abgestrahlt werden
oder von ihr empfangen werden, zu einem gewünschten Erhebungswinkel geändert werden,
der einer ausgewählten Kalibrierung entspricht.
2. Antennenbaugruppe nach Anspruch 1, dadurch gekennzeichnet, dass ein zweites ringförmiges Halteelement (10) enthalten ist, das an einem Endabschnitt
der Metallzuleitungsröhre (1) befestigt ist, wobei das zweite ringförmige Halteelement
(10) Kontaktmittel zum Verbinden des einen Endes jeder Spirale (5, 6) mit dem anderen
Ende des inneren Leiters (2) enthält.
3. Antennenbaugruppe nach Anspruch 2, dadurch gekennzeichnet, dass das Kontaktmittel zwei Kontaktbereiche (8, 9) umfasst, wobei jeder mit dem einen
Ende einer Spirale verbunden ist, wobei einer der Kontaktbereiche ausserdem mit dem
anderen Ende des inneren Leiters (2) verbunden ist, wobei die Kontaktbereiche (8,
9) durch ein Kabelsymmetrieglied (11) mit einer festgelegten Länge verbunden sind.
4. Antennenbaugruppe nach irgendeinem der Ansprüche 1 bis 3, dadurch gekennzeichnet, dass das röhrenförmige Gehäuseelement (12) darauf Kalibriermittel (15) enthält.
5. Antennenbaugruppe nach Anspruch 4, dadurch gekennzeichnet, dass das Kalibriermittel (15) Markierungen enthält, die geografische Standorte anzeigen.
6. Antennenbaugruppe nach irgendeinem der Ansprüche 1 bis 5, dadurch gekennzeichnet, dass ein Blockiermittel (14) zum lösbaren Verriegeln des röhrenförmigen Gehäuseelementes
(12) auf dem röhrenförmigen Basiselement (13) enthalten ist.
7. Antennenbaugruppe nach irgendeinem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass die Drahtspiralen (5, 6) aus Beryllium-Kupfer-Draht gebildet werden.
1. Un mécanisme d'antenne destiné à la transmission et à la réception d'ondes radio d'une
longueur d'onde déterminée, ce mécanisme comprend un tube métallique d'antenne (1)
comportant une ligne d'alimentation permettant de le raccorder à une source de signal
d'ondes radio à une extrémité, il comprend également deux fils en hélices (5,6) possédant
une longueur, un diamètre et un pas d'hélice prédéterminés disposés suivant le même
axe autour de ce tube d'antenne de façon bifilaire, un extrémité des hélices (5,6)
est reliée à la ligne d'alimentation, l'invention est caractérisée par le fait que le tube d'antenne (1) possède un conducteur interne coaxial (2) appartenant
à la ligne d'alimentation, une extrémité des deux hélices étant reliée en commun à
une des extrémités du conducteur interne (2), et les autres extrémités des deux hélices
(5,6) étant reliées séparément à une pièce support annulaire primaire (7) qui peut
coulisser sur l'élément tubulaire (1), ce mécanisme d'antenne comprend aussi un dispositif
d'ajustement étalonné composé d'un boîtier tubulaire (12) en matériau diélectrique
transparent au rayonnement des ondes radio, et une embase tubulaire (13) dans laquelle
une des extrémités du boîtier tubulaire (12) est guidée en translation, ces hélices
(5,6), ce boîtier tubulaire (12) et cette embase tubulaire (13) possèdent un axe commun,
le boîtier tubulaire (12) enferme les hélices (5,6), la pièce support annulaire primaire
(7) est fixée sur le boîtier tubulaire (12), l'embase tubulaire (13) comporte deux
rainures de guidage (17) usinées dans sa face interne et destinées au guidage de deux
pions de guidage (18) montés sur le diamètre externe du boîtier tubulaire (12) qui
lui-même est maintenu dans l'embase tubulaire (13) qui autorise une rotation axiale
partielle limitée du boîtier tubulaire (12) qui provoque un mouvement de rotation
et de translation partiel de la pièce support annulaire primaire (7), lors de ce déplacement
le pas des hélices (5,6) est modifié d'une longueur déterminée et le diamètre des
hélices (5,6) est maintenu de façon substantielle, cette opération permettant de modifier,
l'angle d'élévation du rayonnement d'ondes électromagnétiques reçu ou transmis par
le mécanisme d'antenne suivant une longueur d'onde prédéterminée, sur une valeur d'angle
d'élévation correspondante à la calibration sélectionnée.
2. Un mécanisme d'antenne suivant la revendication d'invention 1 et caractérisé par la présence d'un support annulaire secondaire (10) fixé sur une section d'extrémité
du tube d'antenne (1), ce support annulaire secondaire (10) comporte un dispositif
de contact servant à relier une des extrémités de chaque hélice (5,6) à l'autre extrémité
du conducteur interne (2).
3. Un mécanisme d'antenne suivant la revendication d'invention 2 et caractérisé par le fait que ce dispositif de contact comprend deux zones de contact (8,9) dont chacune
d'entre elles est reliée respectivement à l'extrémité d'une des hélices, une des zones
de contact (9) étant reliée également à l'autre extrémité du conducteur interne (2),
ces zones de contact (8,9) sont reliées par un câble (Balun) transformateur d'entrée
(11) pour une longueur d'onde prédéterminée.
4. Un mécanisme d'antenne suivant une des revendications d'invention 1 à 3 et caractérisé par le fait que le boîtier tubulaire (12) comprend un dispositif de calibration étalonné
(15).
5. Un mécanisme d'antenne suivant la revendication d'invention 4 et caractérisé par le fait que ce dispositif de calibration étalonné (15) comporte l'indication de lieux
géographiques.
6. Un mécanisme d'antenne suivant une des revendications d'invention 1 à 5 et caractérisé par la présence d'un dispositif de verrouillage commutable (14) du boîtier tubulaire
(12) sur l'embase tubulaire (13).
7. Un mécanisme d'antenne suivant une des revendications d'invention précédentes et caractérisé par le fait que les brins d'hélices (5,6) sont fabriqués en fil de cuivre au béryllium.