AU570944B2 – Method of fabricating bowl shaped antennas and micro wave antenna fabricated according to the method
– Google Patents
AU570944B2 – Method of fabricating bowl shaped antennas and micro wave antenna fabricated according to the method
– Google Patents
Method of fabricating bowl shaped antennas and micro wave antenna fabricated according to the method
Info
Publication number
AU570944B2
AU570944B2
AU24343/84A
AU2434384A
AU570944B2
AU 570944 B2
AU570944 B2
AU 570944B2
AU 24343/84 A
AU24343/84 A
AU 24343/84A
AU 2434384 A
AU2434384 A
AU 2434384A
AU 570944 B2
AU570944 B2
AU 570944B2
Authority
AU
Australia
Prior art keywords
antenna
layer
layers
enclosed
shell
Prior art date
1983-01-20
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
AU24343/84A
Other versions
AU2434384A
(en
Inventor
Stig Olof Andersson
Regis Gustafsson
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.)
Individual
Original Assignee
Individual
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.)
1983-01-20
Filing date
1984-01-18
Publication date
1988-03-31
1983-01-20
Priority claimed from SE8300281A
external-priority
patent/SE8300281D0/en
1983-01-20
Priority claimed from SE8300280A
external-priority
patent/SE8300280D0/en
1983-11-18
Priority claimed from SE8306372A
external-priority
patent/SE8306372L/en
1984-01-18
Application filed by Individual
filed
Critical
Individual
1984-08-15
Publication of AU2434384A
publication
Critical
patent/AU2434384A/en
1988-03-31
Application granted
granted
Critical
1988-03-31
Publication of AU570944B2
publication
Critical
patent/AU570944B2/en
2004-01-18
Anticipated expiration
legal-status
Critical
Status
Ceased
legal-status
Critical
Current
Links
Espacenet
Global Dossier
Discuss
Classifications
H—ELECTRICITY
H01—ELECTRIC ELEMENTS
H01Q—ANTENNAS, i.e. RADIO AERIALS
H01Q15/00—Devices for reflection, refraction, diffraction or polarisation of waves radiated from an antenna, e.g. quasi-optical devices
H01Q15/14—Reflecting surfaces; Equivalent structures
H01Q15/141—Apparatus or processes specially adapted for manufacturing reflecting surfaces
H01Q15/142—Apparatus or processes specially adapted for manufacturing reflecting surfaces using insulating material for supporting the reflecting surface
Description
e o o a and micro wave antenna fabricated according to the method.”
This invention relates to antennas of the kind including a reflecting surface collecting or focusing the radiation. Antennas of this kind are for instance radar antennas, so-called parabolic antennas for transmitting and receiv- ing for instance satellite television as well as antennas for telephone communication. Antennas of this kind have been known for several years and these antennas have been made in different ways. Up to now these antennas have had a tendency to be comparatively expensive to make or of a bad quality due to the fact that the reflecting surface must be very carefully shaped in order to allow an opti¬ mum output. Already very small deviations from the ideal surface result in essential power losses. One”fabrication method used for the fabrication of antennas of this kind is the enclosing of a metal net in a glassfiber reinforced plastic, which for instance has been shown in the US patent 2 948 896.
Yet another method of fabrication is to coat the reflecto- ry surface of the antenna with a metal, which for instance has been shown in the French patent 2 502 852, which like the device according to the US patent mentioned above is a sandwich-construction, i.e. a construction with several different layers in order to achieve a sufficient strength. These two constructions mentioned are however comparative- ly expensive to fabricate due to the great number of fab¬ rication steps as well as the amount of used parts. Nor is the desired exactness for the reflectory surface obtained. This exactness in its turn is very important in order to ensure maximum gain for the antenna. The object of the invention is therefore to define an em¬ bodiment and a method for fabrication of parabolic anten¬ nas, which is essentially simpler than known technique and at the same time, results in an improved exactness in the reflecting surface. In accordance with the invention this object is obtained
by vacuum forming the antenna or shaping this in a heated state from for instance plastic, which before the shaping can be coated with a metal layer. In this way a very exact reflecting surface for the micro wave in question is ob- tained with a comparatively cheap method. The reflector can either be made with a reflecting layer, “preferably of metal” on its front side or on the back side of a plas¬ tic layer. In case the metal layer is arranged on the outside it can not be left in this condition, but must suitably be coated or in some other way covered with a protective layer, not only to protect the metal layer, but also to prevent the parabolic antenna from functioning as a sun reflector which might burn the receiving means in the focus point. It is important that the layer in front of the reflecting surface is very thin or has a thickness related to the wave length of the radiation that is to be reflected in order to prevent power loss. In an embodiment of the invention the shaping does not only include the metal layer and a supporting plastic layer, but also a third layer, so that the metal layer is enclosed between two plastic layers, a thin one and a thicker one, in front of and behind the metal layer respectively. This shaping can take place in one common concurrent operation or in separate operations.
Several different types of material can be used for the fabrication of an antenna in accordance with the inven¬ tion. For example acrylic can be used and for instance a mixture consisting of 25 impact resistant acrylic and 75 of a not impact resistant acrylic.
In an antenna particularily adapted to northern latitudes it is possible to arrange heating of the antenna in a known manner behind the shell comprising the above mentionedlayers and to arrange a further shell behind the heating “device partly in
OMPI
order to enclose the heat and partly in order to protect the heating device. These shells enclose a closed inter¬ mediate space for the heating device, which space also serves to distribute the heated air. In one embodiment of the invention the heating layer, that can consist of re¬ sistance wires, heating cloth or the like, and the rear enclosing shell can be shaped in the same operation. Al¬ ternatively the method of foaming can be used. By appro¬ priately enclosing the heating device in this way or another which will be exemplified below it will be possi¬ ble to feed the heating device directly with a net vol¬ tage without an intermediate transformer and without safe¬ ty risks.
The shaping of the antenna preferably can be made against a positive mould, i.e. that the surface brought in contact with the mould is the front side of the antenna. In this way one also obtains the advantage that the same tool can be used independently of how many layers or how thick the antenna is to be made. In case the heating device is also enclosed in the shaping it is possible, if this consists of radial spokes holding the resistance wires, to obtain radially extending projections in the rear shell or layer, which further increases the stiffness of the antenna. Of course similar reinforcements can be obtained in other ways, for instance by the shaping of a rear shell in a separate operation, a suitable amount of space being provided for the heating device between the front and rear shell of the antenna.
It is of course also possible, in order to place a heating device between the front and rear shell, to include dist¬ ance elements of a suitable material, e.g. polyurethane. Within the scope of the invention it is of course also possible to carry out the shaping in two steps, so that the front layer or shell is first shaped according to the mould, then the rear shell or layer(s) is heated and shaped
OMPI
)
by suction or pressure over the first front shell. The invention is below to be described by way of example with reference to the drawings. Fig 1 shows a section through a part of an antenna in accordance with the in- vention while figs 2 and 3 show the suspending of the antenna.
The antenna shown in fig 1 includes a front shell, which has been given the reference numeral 1. This shell, in its turn has a rear supporting plastic layer 2, a metallic layer 3 applied on the front side of this, and about 12 urn (Micro¬ meter) thick and a Drotectinσ layer in front of the metal layer the protective layer being 130-150 μra and given the re¬ ference number 4. Instead of being built up in this way the front layer can be relatively thin, preferably 1,5 mm at the most, and coated witli metal, which on the rear side will be protected in this way in the interior of the anten¬ na. The antenna further includes a rear shell having the reference numeral 5. The front shell 1 and the rear shell 5 are then at the circumference thereof arranged close to each other and sealed with a seal 6 Cor by glueing) , that runs around the circumference of the antenna. The antenna can either be an unbroken surface or provided with a hole in the middle as is shown. The hole in the middle can be closed in the same way as at the outer edge or in the way shown with a ring 15 between the antenna shells and a rub¬ ber mold 22 gripping this distance ring 15 as well as the two antenna shells.
As can be seen the shells 1 and 5 are so shaped that they define between themselves a space, in which a resistance wire 7 is placed. This is in the left part of the figure shown as secured in a holder 8 extending like spokes and provided with oblique cuts, so that the resistance wire cannot lose its grip. The parts 8 arranged like spokes are fastened to the rear antenna shell, e.g. by rivets 23 of plastic. In the right part of fig 1 the resistance
OMPI
wire 7 is placed on or in an insulating disc 9, which further improves the heating of the front side of the an¬ tenna, since the heat from the resistance wire 7 is pre¬ vented by the insulation from being led backwards. Since in the right as well as in the left embodiment an air spa¬ ce is present for air circulation behind the front shell of the antenna an even heating of the antenna front shell is ensured.
The antenna is at its outer edge elastically suspended in a circular frame. This elastic fastening is achieved by the aid of rubber elements 10, at which bolts are fastened that in turn are fastened at the antenna and the support¬ ing construction, respectively, which in fig 1 in parti¬ cular constitutes a frame 11. At the fastening point of the elastic element 10 at the antenna special washers are adapted to the circular shape of the antenna, partly to achieve a good seal and partly to allow as much freedom of movement as possible between the antenna and the sup¬ porting frame. Since several elastic fastening elements 10 are arranged around the antenna, the antenna always retains the same amount of directional stability as the supporting frame t so that in spite of the elastic arrange¬ ment of the antenna, permitting movement due to tempera¬ ture differences, the antenna always maintains its direc- tion, which is very important in order to achieve a good reception.
Fig 2 shows the supporting frame of the antenna shown in fig 1 which is shown here only schematically and given the reference numeral 12. The circular frame 11 is con- nected with further details of framework construction that is journalled in an upper journalling point 13 and can be adjusted with a screw 14 to its elevation. The journal 13, as can be seen in particular from fig 3, consists of two ears 17 and 18, a strut 16 arranged be- tween these ears and journal not shown therebetween. Since
the ears 17 and 18 are relatively far apart a good sta¬ bility is obtained even if a play should occur in the journal 13. The strut 16 is in its turn fastened to a vertical strut 19, which in turn constitutes a journal for movement in the horisontal plane in a fixed frame, that has been given the reference numeral 20 and which is intended to be fastened to a wall or mast. At one of the ears 18 is further fastened a latent strut 21 extending to a frame part 20, with which a fine adjust- ment or change of the direction of the antenna in the horizontal plane can be achieved. By mounting the strut 19 in a way known per se in parallel with the axis of the earth it is possible to use the antenna for receiving or emitting signals from several different satellites. The antenna is changed from one satellite to another only by a small change of the adjustment means 21. The adjust¬ ment means 21 can even be replaced by a device driven by an electrical motor. Finally it should be mentioned that the better precision and the improved design of the antenna in accordance with the invention results in a far stronger signal than what is the case with the known antennas , which in turn means that the antenna in accordance with the invention can be made with approximately 30 % smaller diameter than what else should have been possible.
Within the scope of the invention it is also possible to apply the reflective coating after the shaping or forming, e.g. by metal spray.
OMPI
Claims (12)
1. Method of fabricating bowl shaped antennas intended for reception or transmission of radiation with micro wave length, c h a r a c t e r i z e d .i n that the antenna is fabricated by vacuum forming or heat forming of a suit¬ able thermoplastic material to the desired shape.
2. Method according to claim 1, c h a r a c t e r i ¬ z e d i n that the material includes a supporting sheet of a thermoplastic material coated by a reflecting electrically conductive layer.
3. Method according to claim 2, c h a r a c t e r i ¬ z e d i n that the reflective layer is enclosed between two plastic layers, which are all shaped in one ope¬ ration.
4. Method according to claim 1, c h a r a c t e r i ¬ z e d i n that the reflective layer is enclosed between two separately shaped plastic layers.
5. Method according to claim 3 or 4, c h a r a c t e r ¬ i z e d i n that the reflective layer is applied on the back of the front layer by using metal foil or flame spray techniq
6. Method according to claim 1 or 2, c h a r a c t e r i ¬ z e d i n that after the shaping of layers to a shell at the back of this electric heating means are arranged, which’ are then enclosed by a rear shell with a space therebetween so great that air circulation in the closed space can ensure an even heating.
7. Method according to any of claims 1-6, c h a r a c ¬ t e r i z e d i n that distance elements are placed be¬ tween two layers.
8. Method according to any of the preceding claims, c h a r a c t e r i z e d i n that the outer edge of the antenna is sealed after fabrication.
9. Method according to claim 8, c h a r a c t e r i z e d i n that the sealing is obtained by the aid of a rubber or plastic mould.
10. Method according to claim 1, c h a r a c t e r i ¬ z e d i n that after the fabrication of the antenna a metal layer is applied on the front side with a protec¬ tive layer applied thereon.
11. Antenna f bricated in accordance with any of the preceding claims 1-10, c h a r a c t e r i z e d i n that it includes a bowl shaped antenna element, that at its circumference is fastened in a frame by means of elastic elements preferably arranged evenly spaced over the circumference.
12. Method according to any of the claim 1-10, c h a r a c¬ t e r i z e d i n that the antenna is “given a parabolic shape.
AU24343/84A
1983-01-20
1984-01-18
Method of fabricating bowl shaped antennas and micro wave antenna fabricated according to the method
Ceased
AU570944B2
(en)
Applications Claiming Priority (6)
Application Number
Priority Date
Filing Date
Title
SE8300281
1983-01-20
SE8300281A
SE8300281D0
(en)
1983-01-20
1983-01-20
DEVICE FOR ANTENNA DEPARTMENT
SE8300280
1983-01-20
SE8300280A
SE8300280D0
(en)
1983-01-20
1983-01-20
antenna reflector
SE8306372A
SE8306372L
(en)
1983-11-18
1983-11-18
microwave antenna
SE8306372
1983-11-18
Publications (2)
Publication Number
Publication Date
AU2434384A
AU2434384A
(en)
1984-08-15
AU570944B2
true
AU570944B2
(en)
1988-03-31
Family
ID=27355283
Family Applications (1)
Application Number
Title
Priority Date
Filing Date
AU24343/84A
Ceased
AU570944B2
(en)
1983-01-20
1984-01-18
Method of fabricating bowl shaped antennas and micro wave antenna fabricated according to the method
Country Status (9)
Country
Link
EP
(1)
EP0114797A3
(en)
AU
(1)
AU570944B2
(en)
CA
(1)
CA1225510A
(en)
DK
(1)
DK431484A
(en)
ES
(1)
ES529003A0
(en)
FI
(1)
FI74839C
(en)
HU
(1)
HUT35425A
(en)
NO
(1)
NO843730L
(en)
WO
(1)
WO1984003005A1
(en)
Cited By (1)
* Cited by examiner, † Cited by third party
Publication number
Priority date
Publication date
Assignee
Title
AU590942B2
(en)
*
1986-08-04
1989-11-23
Cselt-Centro Studi E Laboratori Telecomunicazioni S.P.A.
Method of manufacturing dichroic antenna structures
Families Citing this family (3)
* Cited by examiner, † Cited by third party
Publication number
Priority date
Publication date
Assignee
Title
DE3582262D1
(en)
*
1984-01-23
1991-05-02
Showa Denko Kk
REFLECTOR FOR CIRCULAR POLARIZED WAVES.
FR2616102A3
(en)
*
1987-06-05
1988-12-09
Duplessy Henry
Method of manufacturing a parabolic antenna and antenna obtained by this method
GB2308012B
(en)
1995-12-05
1999-11-17
Northern Telecom Ltd
A radiation shielding device
Citations (3)
* Cited by examiner, † Cited by third party
Publication number
Priority date
Publication date
Assignee
Title
US2742387A
(en)
*
1953-09-28
1956-04-17
Lavoie Lab Inc
Reflector for electromagnetic radiations and method of making same
US3574258A
(en)
*
1969-01-15
1971-04-13
Us Navy
Method of making a transreflector for an antenna
US4188358A
(en)
*
1976-03-29
1980-02-12
U.S. Philips Corporation
Method of manufacturing a metallized plastic reflector
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Assignee
Title
US2679003A
(en)
*
1950-05-27
1954-05-18
Motorola Inc
Heater system for microwave antennas
FR2117807B1
(en)
*
1970-12-11
1973-12-28
Girondon Michel
DE2227563A1
(en)
*
1972-06-07
1974-01-10
Krupp Gmbh
PARABOLIC MIRROR
FR2426343A1
(en)
*
1978-05-16
1979-12-14
Bony Gilbert
Plastics sandwich telecommunication parabolic reflector – has integral deicing heating element laid on honeycomb structure
FR2502852B1
(en)
*
1981-03-26
1985-06-14
Sadones Henri
REFLECTOR IN PARTICULAR FOR LARGE SATELLITE TELECOMMUNICATIONS RECEIVING ANTENNAS
JPS58170103A
(en)
*
1982-03-30
1983-10-06
Matsushita Electric Ind Co Ltd
Production of parabola antenna
1984
1984-01-16
CA
CA000445329A
patent/CA1225510A/en
not_active
Expired
1984-01-18
AU
AU24343/84A
patent/AU570944B2/en
not_active
Ceased
1984-01-18
HU
HU84672A
patent/HUT35425A/en
unknown
1984-01-18
EP
EP84850019A
patent/EP0114797A3/en
not_active
Withdrawn
1984-01-18
WO
PCT/SE1984/000013
patent/WO1984003005A1/en
active
IP Right Grant
1984-01-19
ES
ES529003A
patent/ES529003A0/en
active
Granted
1984-09-10
DK
DK431484A
patent/DK431484A/en
not_active
Application Discontinuation
1984-09-18
FI
FI843657A
patent/FI74839C/en
not_active
IP Right Cessation
1984-09-19
NO
NO843730A
patent/NO843730L/en
unknown
Patent Citations (3)
* Cited by examiner, † Cited by third party
Publication number
Priority date
Publication date
Assignee
Title
US2742387A
(en)
*
1953-09-28
1956-04-17
Lavoie Lab Inc
Reflector for electromagnetic radiations and method of making same
US3574258A
(en)
*
1969-01-15
1971-04-13
Us Navy
Method of making a transreflector for an antenna
US4188358A
(en)
*
1976-03-29
1980-02-12
U.S. Philips Corporation
Method of manufacturing a metallized plastic reflector
Cited By (1)
* Cited by examiner, † Cited by third party
Publication number
Priority date
Publication date
Assignee
Title
AU590942B2
(en)
*
1986-08-04
1989-11-23
Cselt-Centro Studi E Laboratori Telecomunicazioni S.P.A.
Method of manufacturing dichroic antenna structures
Also Published As
Publication number
Publication date
ES8501574A1
(en)
1984-11-16
HUT35425A
(en)
1985-06-28
DK431484D0
(en)
1984-09-10
EP0114797A3
(en)
1986-05-07
FI843657L
(en)
1984-09-18
FI74839B
(en)
1987-11-30
EP0114797A2
(en)
1984-08-01
ES529003A0
(en)
1984-11-16
WO1984003005A1
(en)
1984-08-02
NO843730L
(en)
1984-09-19
FI74839C
(en)
1988-03-10
CA1225510A
(en)
1987-08-18
DK431484A
(en)
1984-09-10
AU2434384A
(en)
1984-08-15
FI843657A0
(en)
1984-09-18
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