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
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.)
Filing date
Publication date
Priority claimed from SE8300280A external-priority patent/SE8300280D0/en
Priority claimed from SE8300281A external-priority patent/SE8300281D0/en
Priority claimed from SE8306372A external-priority patent/SE8306372L/en
Application filed by Individual filed Critical Individual
Publication of AU2434384A publication Critical patent/AU2434384A/en
Application granted granted Critical
Publication of AU570944B2 publication Critical patent/AU570944B2/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q15/00Devices for reflection, refraction, diffraction or polarisation of waves radiated from an antenna, e.g. quasi-optical devices
    • H01Q15/14Reflecting surfaces; Equivalent structures
    • H01Q15/141Apparatus or processes specially adapted for manufacturing reflecting surfaces
    • H01Q15/142Apparatus or processes specially adapted for manufacturing reflecting surfaces using insulating material for supporting the reflecting surface

Landscapes

  • Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Aerials With Secondary Devices (AREA)
  • Details Of Aerials (AREA)
  • Waveguide Aerials (AREA)
  • Support Of Aerials (AREA)

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
SE8300280A SE8300280D0 (en) 1983-01-20 1983-01-20 antenna reflector
SE8300281A SE8300281D0 (en) 1983-01-20 1983-01-20 DEVICE FOR ANTENNA DEPARTMENT
SE8300280 1983-07-11
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) ES8501574A1 (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
CA1232060A (en) * 1984-01-23 1988-01-26 Kenji Takemura Reflector for circular polarization antenna and process for the production thereof
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

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date 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

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
EP0114797A3 (en) 1986-05-07
EP0114797A2 (en) 1984-08-01
DK431484D0 (en) 1984-09-10
AU2434384A (en) 1984-08-15
ES529003A0 (en) 1984-11-16
WO1984003005A1 (en) 1984-08-02
ES8501574A1 (en) 1984-11-16
DK431484A (en) 1984-09-10
FI843657L (en) 1984-09-18
FI74839B (en) 1987-11-30
FI74839C (en) 1988-03-10
FI843657A0 (en) 1984-09-18
NO843730L (en) 1984-09-19
CA1225510A (en) 1987-08-18
HUT35425A (en) 1985-06-28

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