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WO1996039726A1 - Systeme de reglage fin d'orientation d'antenne selon trois axes orthogonaux - Google Patents

Systeme de reglage fin d'orientation d'antenne selon trois axes orthogonaux Download PDF

Info

Publication number
WO1996039726A1
WO1996039726A1 PCT/EP1996/002200 EP9602200W WO9639726A1 WO 1996039726 A1 WO1996039726 A1 WO 1996039726A1 EP 9602200 W EP9602200 W EP 9602200W WO 9639726 A1 WO9639726 A1 WO 9639726A1
Authority
WO
WIPO (PCT)
Prior art keywords
antenna
adjustment
bracket
jaw
fine
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
PCT/EP1996/002200
Other languages
English (en)
Inventor
Cesare Bassi
Elio Deponti
Francesco Marras
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Italtel SpA
Original Assignee
Italtel SpA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Italtel SpA filed Critical Italtel SpA
Priority to AU59011/96A priority Critical patent/AU5901196A/en
Publication of WO1996039726A1 publication Critical patent/WO1996039726A1/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/12Supports; Mounting means
    • H01Q1/125Means for positioning

Definitions

  • the present invention relates to the field of support systems for antennas and specifically a system of fine antenna aiming adjustment with three orthogonal axes.
  • the aiming system which is the object of the present invention was conceived mainly for operating on integrated antenna & equipment radio systems even though it can be employed in systems with equipment in a remote location.
  • antenna aiming systems an important problem to be solved is to provide in all cases an antenna system easy to install and repair, i.e. allowing operation with the fullest ease and safety in field installation and repair.
  • Another problem is implementation of an aiming system which would facilitate as much as possible setting and adjustment operations and especially those of fine antenna aiming adjustment along three orthogonal axes to make accessible the adjustments on the antenna-support side and then the rear side of the antenna.
  • various types of antenna aiming adjustment but none capable of ensuring fine adjustment of antenna aiming along all three orthogonal axes and making accessible the adjustments on the antenna-support side and then on the rear side of the antenna.
  • the purpose of the present invention is to solve all the above mentioned problems and indicate a system of fine antenna aiming adjustment using antenna supports directable along three orthogonal axes, whose aiming is adjustable both roughly and finely by means of the appropriate use of setting and adjustment screws.
  • the various components can be directed mutually by screws which can run in slots or slits made in the components.
  • the present invention has for its subject matter a system of fine antenna aiming adjustment along three orthogonal axes, as better described in claim 1 and subsequent claims.
  • This configuration of the antenna support system allows achieving adjustment of the antenna along three orthogonal axes corresponding to elevation, azimuth and polarization by rotation of screws and/or turnbuckles arranged in positions easily reached from the rear of the antenna. Specifically, the elevation and azimuth are found in this configuration by means of side-by-side and hence easily used controls.
  • Fine adjustment of polarization finds particular advantage in those radio systems operating on crossed polarization and in particular those adopting the frequency reuse technique.
  • FIGS. 1A and 1 B show, with reference to the antenna support, a side and a top view respectively of the antenna aiming system
  • FIGS. 2A, 2B and 3 show three section planes of front views of the antenna support bracket indicated by reference number 1 on three planes perpendicular to the axes E-E of FIG. 1 B, and
  • FIGS. 4A, 4B and 4C show respectively two mutually orthogonal side views and a top view of a variant embodiment of the antenna azimuth control system.
  • the antenna 21 is rigidly set by screws 20 to a support bracket 1 which is in turn connected to an antenna supporting pole 22 of the entire system through an interface element 2 consisting of: a jaw 3 connected to the antenna supporting pole 22 by a pair of U-bolts 4 which surround the pole like a band, a round flange 8 which couples to the support bracket 1 through screws 11 which in the example described here are four in number, and in its central part two perpendicular ribs which unite on one side of the jaw 3 and on the other to the round flange 8.
  • the support bracket 1 comprises two orthogonal parts, one on which engages the antenna 21 and the other on which engages the round flange 8, with reinforcing ribs if desired between the two parts (sectioned in FIG. 1 B).
  • the flange 8 is provided with teeth 9 (better seen in FIG. 2B) which mesh with a screw 6 which can rotate in two seats 10 (of which a detail is shown in FIG. 2B) integral with the support bracket 1 around an axis having a direction orthogonal to the axis E-E (elevation axis).
  • the two seats indicated by 10' have the same function as the seats 10 but are used as an alternative if the antenna is installed in the position symmetrically opposite the antenna supporting pole 22 so that a single type of interface element 2 can be used in both cases.
  • the support bracket 1 is provided with a number of threaded holes 17 (more numberous than the screws 11) to allow setting of the interface element 2 by means of the round flange 8 and the screws 11 which are inserted in four of the threaded holes 17.
  • a number of threaded holes 17 more numberous than the screws 11 to allow setting of the interface element 2 by means of the round flange 8 and the screws 11 which are inserted in four of the threaded holes 17.
  • a turnbuckle 7 fixed on one side to the support 5, which is in turn rigidly connected to the pole by a U-bolt 14 under the jaw 3, and on the other side to the jaw 3 of the interface element 2.
  • Rough azimuth adjustment is achieved by manually rotating the support bracket 1 around the antenna supporting pole 22 after loosening the U-bolts 4 while using the support 5 to hold up the antenna system.
  • the azimuth adjustment system thus uses two components 3 and 5 which are both attached to the pole and engaged one against the other and are tightened or loosened alternately and made to run against each other.
  • the variant just described has the advantage of being usable with poles of different diameter thanks to the special pole attachment (the U-bolts).
  • rotation around the antenna polarization axis P-P is achieved by loosening the screws 20 for fixing the antenna to the support by turning the screw 16 or the screw 18, depending on the desired direction.
  • the azimuth adjustment system can be provided as shown in FIGS. 4A, 4B, 4C.
  • the jaw 3 and the U-bolts 4 of FIGS. 1 A, 1 B are replaced by a jaw 24 which is tightened on the supporting pole by means of a counter-jaw 25 and the screws 26.
  • the jaw 24 and the counter-jaw 25 have a central inner groove in ring form shown in broken lines in the FIGS..
  • the counter-jaw 25 has a central through slot 32 in whose sides are provided two ribs for support of the screws 27 and 28, which can be fitted if necessary with lock nuts.
  • the support 5 and the U-bolts 14 of the FIGS. 1A, 1B are replaced by a ring consisting of two parts 29 and 30 connected on one side by a pin 31 and on the other side, by means of appropriate side-by-side protuberances, using the screws 33.
  • the screws 27 and 28 buck on the sides of these protuberances.
  • the two parts 29 and 30 are opened to allow wrapping around the pole to which they are rigidly fastened by the screws 33. Then the jaw 24 and the counter-jaw 25 are mounted on the pole in such a manner that the ring formed by the two parts 29 and 30 remains in the central groove and the protuberances of the parts 29 and 30 emerge from the slot 32.
  • the polarization adjustment system by means of the screw 16 and 18 can be replaced by a turnbuckle of the type indicated by reference number 7 in FIG. 2A and appropriately anchored on one side of the support bracket 1 and on the other to the antenna 21 , if necessary through a reinforcing rib of the type indicated by reference number 19 in FIG. 3.
  • the round flange 8 and the support bracket 1 can be interchanged to provide the teeth 9 of the support bracket 1 and the seats 10 and 10' for the adjustment screw 6 on the round flange 8.
  • the support bracket 1 and the rear part of the antenna can be interchanged to provide the supports for the adjustment screws 16 and 18 on the rear part of the antenna, and the reinforcing rib 19 on the support bracket 1.

Landscapes

  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Support Of Aerials (AREA)

Abstract

Système de réglage fin d'orientation d'antenne au moyen de supports d'antenne pouvant être orientés selon trois axes orthogonaux et dont l'orientation peut être réglée soit de manière approximative soit de manière fine par l'utilisation appropriée de vis de mise en place et de réglage. Au moyen de mâchoires et de brides (2, 3, 5, 8) couplées de façon appropriée avec l'attache de l'antenne (1), les différents composants peuvent être orientés l'un par rapport à l'autre au moyen de vis (4, 7, 11, ... 18) pouvant se déplacer dans des fentes ou des rainures pratiquées dans les composants.
PCT/EP1996/002200 1995-06-05 1996-05-22 Systeme de reglage fin d'orientation d'antenne selon trois axes orthogonaux Ceased WO1996039726A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AU59011/96A AU5901196A (en) 1995-06-05 1996-05-22 System for fine antenna-aiming adjustment on three orthogona l axes

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
ITMI95A001167 1995-06-05
ITMI951167A IT1275306B (it) 1995-06-05 1995-06-05 Sistema di regolazione fine del puntamento d'antenna secondo tre assi ortogonali

Publications (1)

Publication Number Publication Date
WO1996039726A1 true WO1996039726A1 (fr) 1996-12-12

Family

ID=11371743

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP1996/002200 Ceased WO1996039726A1 (fr) 1995-06-05 1996-05-22 Systeme de reglage fin d'orientation d'antenne selon trois axes orthogonaux

Country Status (4)

Country Link
AU (1) AU5901196A (fr)
IT (1) IT1275306B (fr)
WO (1) WO1996039726A1 (fr)
ZA (1) ZA964541B (fr)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2310542B (en) * 1996-02-26 2000-10-11 Fujitsu Ltd Mounting for antenna unit
FR2802582A1 (fr) * 1999-12-21 2001-06-22 Sagem Dispositif de fixation d'un equipement sur un mat
EP1227544A3 (fr) * 2001-01-30 2005-01-19 Andrew AG Antenne de type réflecteur parabolique avec un dipositif de fixation d'ajustage et un procédé de ajuster une telle antenne
EP2309588A1 (fr) 2009-09-29 2011-04-13 Andrew LLC Procédé et appareil pour l'ajustement d'antenne de réflecteur à polarisation fine
US8866695B2 (en) 2012-02-23 2014-10-21 Andrew Llc Alignment stable adjustable antenna mount
US9065172B2 (en) 2013-05-23 2015-06-23 Commscope Technologies Llc Mounting hub for antenna

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2120856A (en) * 1982-05-11 1983-12-07 Thorn Emi Ferguson Antenna assembly
EP0304656A1 (fr) * 1987-08-12 1989-03-01 Siemens Aktiengesellschaft Antenne directionnelle pour systèmes relais
GB2231484A (en) * 1989-03-15 1990-11-21 Cambridge Computer Bracket assembly for a dish antenna
US5440319A (en) * 1993-10-01 1995-08-08 California Amplifier Integrated microwave antenna/downconverter
US5508712A (en) * 1994-03-28 1996-04-16 P-Com, Inc. Self-aligning wave guide interface

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2120856A (en) * 1982-05-11 1983-12-07 Thorn Emi Ferguson Antenna assembly
EP0304656A1 (fr) * 1987-08-12 1989-03-01 Siemens Aktiengesellschaft Antenne directionnelle pour systèmes relais
GB2231484A (en) * 1989-03-15 1990-11-21 Cambridge Computer Bracket assembly for a dish antenna
US5440319A (en) * 1993-10-01 1995-08-08 California Amplifier Integrated microwave antenna/downconverter
US5508712A (en) * 1994-03-28 1996-04-16 P-Com, Inc. Self-aligning wave guide interface

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2310542B (en) * 1996-02-26 2000-10-11 Fujitsu Ltd Mounting for antenna unit
FR2802582A1 (fr) * 1999-12-21 2001-06-22 Sagem Dispositif de fixation d'un equipement sur un mat
EP1111290A1 (fr) * 1999-12-21 2001-06-27 Sagem Sa Dispositif de fixation d'un équipement sur un mât
EP1227544A3 (fr) * 2001-01-30 2005-01-19 Andrew AG Antenne de type réflecteur parabolique avec un dipositif de fixation d'ajustage et un procédé de ajuster une telle antenne
EP2309588A1 (fr) 2009-09-29 2011-04-13 Andrew LLC Procédé et appareil pour l'ajustement d'antenne de réflecteur à polarisation fine
US8760361B2 (en) 2009-09-29 2014-06-24 Andrew Llc Method and apparatus for fine polarization reflector antenna adjustment
US8866695B2 (en) 2012-02-23 2014-10-21 Andrew Llc Alignment stable adjustable antenna mount
US9065172B2 (en) 2013-05-23 2015-06-23 Commscope Technologies Llc Mounting hub for antenna

Also Published As

Publication number Publication date
AU5901196A (en) 1996-12-24
ZA964541B (en) 1996-12-12
ITMI951167A1 (it) 1996-12-05
ITMI951167A0 (it) 1995-06-05
IT1275306B (it) 1997-08-05

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