GB2318217A - A patch aerial combined with another aerial - Google Patents
A patch aerial combined with another aerial Download PDFInfo
- Publication number
- GB2318217A GB2318217A GB9720650A GB9720650A GB2318217A GB 2318217 A GB2318217 A GB 2318217A GB 9720650 A GB9720650 A GB 9720650A GB 9720650 A GB9720650 A GB 9720650A GB 2318217 A GB2318217 A GB 2318217A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aerial
- patch
- plate
- cable
- gps
- 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.)
- Withdrawn
Links
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q21/00—Antenna arrays or systems
- H01Q21/28—Combinations of substantially independent non-interacting antenna units or systems
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/27—Adaptation for use in or on movable bodies
- H01Q1/32—Adaptation for use in or on road or rail vehicles
- H01Q1/3208—Adaptation for use in or on road or rail vehicles characterised by the application wherein the antenna is used
- H01Q1/3233—Adaptation for use in or on road or rail vehicles characterised by the application wherein the antenna is used particular used as part of a sensor or in a security system, e.g. for automotive radar, navigation systems
Landscapes
- Engineering & Computer Science (AREA)
- Computer Security & Cryptography (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Position Fixing By Use Of Radio Waves (AREA)
- Support Of Aerials (AREA)
- Details Of Aerials (AREA)
Abstract
An aerial arrangement comprises an aerial 7 with a feed cable 6 which passes through a hole 14 in the centre of a patch aerial 10. The patch aerial 10 may comprise a radiating element 11, formed by a dielectric substrate plate with a conductive layer on either side, and an amplifier located within a hosing 12. The patch aerial 10 is located within the base 1 of the aerial 7. The patch aerial 10 may be employed in a Global Positioning System (GPS) and the aerial 7 may be a monopole antenna for use in radio communications. The aerial arrangement may be mounted on the outer surface of a vehicle.
Description
1 2318217 DEVICE FOR AERIAL The invention relates to a device for an
aerial for satellite navigation.
Satellite navigation by means of the so-called GPS (Global Positioning system) is used increasingly, both for military and civil purposes. for example in vehicles and vessels.
The use of GPS presupposes a receiver with an aerial for receiving radio signals.
In connection with vehicles and vessels an externally mounted aerial is advantageous. The aerial is connected to the receiver by means of an aerial cable, typically a coaxial cable, taken through a wall or roof.
Vehicles and vessels are often already provided with aerials for communication radio, radiotelephone, broadcasting receivers and other, and it may therefore be difficult to find a suitable place for a so-called GPS aerial. Another condition is that aerial signals from 2 neighbouring aerials may to a certain extent interfere with each other.
The object of the invention is to provide a device for the simplified mounting of a GPS aerial together with 5 another aerial.
The object is reached through the features stated in the following description and subsequent claim.
Externally mounted aerials, for example aerials for communication radio, are often provided with a cone- shaped base fixed externally to a wall or a roof. The aerial element itself is electrically connected through an aerial cable, for example a coaxial cable, lead through the aerial base.
According to the invention a so-called patch aerial is used for receiving GPS signals. Such an aerial comprises a plate, an aerial plate, of synthetic material, coated with a metal on each side surface, as is known from printed circuit boards. The metal on the one side of the plate constitutes an earth plane, and the metal on the other side constitutes an aerial element.
The aerial plate is most often arranged inside a tight housing together with an amplifier which is electrically connected to the aerial plate. Further, an aerial cable is connected to the amplifier. Such GPS aerials are well known to those skilled in the art and will, therefore, not be described in further detail.
By placing such an aerial plate, for receiving GPS signals, inside the aerial base of an existing aerial, for 3 example an aerial for a communication radio, a simple and space-saving mounting of a GPS aerial is achieved.
Experiments have shown that the aerial cable to the primary aerial, i.e. the aerial mounted on the aerial base, may influence the GPS aerial inside the base. It has also turned out that this undesirable effect becomes very small if said aerial cable is first taken right through the centre of the aerial plate comprised by the GPS aerial, instead of leading the aerial cable beside and about the aerial plate. Therefore, it is a feature of the invention to lead the aerial cable through a hole at or near the centre of the aerial plate.
The invention will be described in the following by means of a non-limiting example of an embodiment, with reference to the accompanying drawings, in which Fig. 1 is a schematic side view, partly in section, of an aerial base with part of a rod aerial for a connunication radio, in which the aerial base contains an aerial plate, Fig. 2 shows, partly in section, the aerial base with the aerial plate, seen from above.
In the figure the reference numeral 1 designates an aerial base standing on a mounting plate 2 attached to a roof 3 of a vehicle not shown. Between the mounting plate 2 and the aerial base 1, and between the mounting plate 2 and the roof 3, a seal or other tightening means, which is not shown, may advantageously be provided. The aerial base 1 is secured to the mounting plate 2 by screws 4. The mounting plate 2 is preferably 4 secured to the roof 3 by screws or other securing means' not shown. In the mounting plate 2, near the centre thereof, is provided a first hole 5 for a first aerial cable 6 to a primary aerial 7 which is attached to the top of the aerial base 1 in a known manner. In the mounting plate 2 is further provided a second hole 8 for a second aerial cable 9 to a secondary aerial, in this case a GPS aerial 10 of the so-called patch type, comprising an aerial plate 11, and possibly a not shown amplifier arranged in a known manner inside an aerial housing 12. The aerial cables 6, 9 are taken through a hole 13 in the roof 3 to not shown radio equipment or GPS equipment in the vehicle.
The aerial cable 6 to the primary aerial 7 is taken through a hole 14 in the aerial plate 11 near the centre thereof, and also through the aerial housing 12, which encloses the aerial plate 11. It is possible, of course, for the aerial plate 11 to be mounted directly, without being enclosed in an aerial housing 12.
The aerial cables 6 and 9 are shown directly connected to the primary aerial 7 and the GPS aerial 11 respec tively. Especially for the primary aerial 7 it will be of advantage if a separable contact is arranged on the aerial cable, either on the upper side of the housing 12 or in a recess 15 in the mounting plate 2, prefera bly in the side of the mounting plate 2 facing the roof 3. It is considered to be well known to a person skilled in the art to fit necessary contacts on aerial cables, and such contacts are, therefore, not shown.
Claims (1)
- CLAIM1. Device for aerial for satellite navigation, in which is used, for the reception of position signals, an aerial (10) of a type comprising an aerial plate (11), which is provided on each side with a conductive coating, which is connected, possibly by way of an amplifier, to an aerial cable (9) connecting the aerial (11) to equipment for receiving position signals, c h a r a c t e r i z e d i n that the aerial (11) is arranged inside an aerial base (1) which holds a primary aerial for another purpose such as radio communication, and in which an aerial cable (6) to a primary aerial (7) is taken through the aerial (11) near the centre of the aerial plate (11).
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
NO964202A NO304809B1 (en) | 1996-10-04 | 1996-10-04 | Device by antenna |
Publications (2)
Publication Number | Publication Date |
---|---|
GB9720650D0 GB9720650D0 (en) | 1997-11-26 |
GB2318217A true GB2318217A (en) | 1998-04-15 |
Family
ID=19899908
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB9720650A Withdrawn GB2318217A (en) | 1996-10-04 | 1997-09-29 | A patch aerial combined with another aerial |
Country Status (4)
Country | Link |
---|---|
DE (1) | DE19742084A1 (en) |
FR (1) | FR2754396B1 (en) |
GB (1) | GB2318217A (en) |
NO (1) | NO304809B1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6271797B2 (en) | 1999-06-18 | 2001-08-07 | R. A. Miller Industries, Inc. | Combination antenna mount |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE20221959U1 (en) | 2002-05-16 | 2009-11-19 | Kathrein-Werke Kg | antenna array |
DE202012011334U1 (en) * | 2012-11-27 | 2013-12-16 | Thales Deutschland Gmbh | Adapter for arranging at least one antenna on a motor vehicle |
US10150432B2 (en) * | 2017-03-20 | 2018-12-11 | Ford Global Technologies, Llc | Autonomous vehicle conversion |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0590955A2 (en) * | 1992-09-30 | 1994-04-06 | Loral Aerospace Corporation | Multiple band antenna |
GB2272575A (en) * | 1992-11-02 | 1994-05-18 | Gec Ferranti Defence Syst | Dual band antenna |
EP0747993A2 (en) * | 1995-06-06 | 1996-12-11 | Harada Industry Co., Ltd. | Three-wave receiving antenna apparatus |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5099249A (en) * | 1987-10-13 | 1992-03-24 | Seavey Engineering Associates, Inc. | Microstrip antenna for vehicular satellite communications |
US5523761A (en) * | 1993-01-12 | 1996-06-04 | Trimble Navigation Limited | Differential GPS smart antenna device |
DE29500961U1 (en) * | 1995-01-13 | 1995-06-14 | Richard Hirschmann GmbH & Co., 72654 Neckartenzlingen | Antenna arrangement |
-
1996
- 1996-10-04 NO NO964202A patent/NO304809B1/en not_active IP Right Cessation
-
1997
- 1997-09-24 DE DE1997142084 patent/DE19742084A1/en not_active Ceased
- 1997-09-26 FR FR9712000A patent/FR2754396B1/en not_active Expired - Lifetime
- 1997-09-29 GB GB9720650A patent/GB2318217A/en not_active Withdrawn
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0590955A2 (en) * | 1992-09-30 | 1994-04-06 | Loral Aerospace Corporation | Multiple band antenna |
GB2272575A (en) * | 1992-11-02 | 1994-05-18 | Gec Ferranti Defence Syst | Dual band antenna |
EP0747993A2 (en) * | 1995-06-06 | 1996-12-11 | Harada Industry Co., Ltd. | Three-wave receiving antenna apparatus |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6271797B2 (en) | 1999-06-18 | 2001-08-07 | R. A. Miller Industries, Inc. | Combination antenna mount |
Also Published As
Publication number | Publication date |
---|---|
NO304809B1 (en) | 1999-02-15 |
DE19742084A1 (en) | 1998-04-16 |
GB9720650D0 (en) | 1997-11-26 |
NO964202D0 (en) | 1996-10-04 |
FR2754396A1 (en) | 1998-04-10 |
NO964202L (en) | 1998-04-06 |
FR2754396B1 (en) | 1999-08-20 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |