EP0359504A1 - Radomes - Google Patents
Radomes Download PDFInfo
- Publication number
- EP0359504A1 EP0359504A1 EP19890309200 EP89309200A EP0359504A1 EP 0359504 A1 EP0359504 A1 EP 0359504A1 EP 19890309200 EP19890309200 EP 19890309200 EP 89309200 A EP89309200 A EP 89309200A EP 0359504 A1 EP0359504 A1 EP 0359504A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- radome
- plastics material
- layer
- reinforced plastics
- thickness
- 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- Withdrawn
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Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/42—Housings not intimately mechanically associated with radiating elements, e.g. radome
- H01Q1/422—Housings not intimately mechanically associated with radiating elements, e.g. radome comprising two or more layers of dielectric material
Definitions
- This invention relates to Radomes and production thereof.
- radomes used on flight vehicles, ie missiles and aircraft, and these vary according to the flight requirements of the vehicle.
- the three types are:
- Typical solid wall radomes are usually of the half wave-length design and vary in thickness according to the dielectric constant of the material and the wavelength of operation. Typical thicknesses would be 8mm at X-band and about 5mm at J-band with material of dielectric constant of about 4 such as can be obtained from a composite of approximately 55% glass fibre and 45% resin matrix by weight. These radomes can be made by hand lay up, autoclave moulding, filament winding and resin transfer moulding. This type of radome is usually selected where a high microwave transparency performance and structural capability are required such as in military fighter and terrain following aircraft and missile applications.
- Sandwich Radome The most common version of a Sandwich Radome is the A-sandwich consisting of a lightweight core between two skins, the core thickness being nominally a quarter of a wavelength thick for narrow-band applications but of a compromise thickness for wideband applications. Typically at X -band the core thickness will be about 8mm with skins of thickness approximately 0. 75mm and reinforcement content of around 55% glass fibre by weight as with the solid wall radome.
- the core of the sandwich is usually either a honeycomb or an expanded foam with a low dielectric constant, although there are applications which use a syntactic foam core of somewhat higher dielectric constant.
- Thin Skin Randomes are relatively unsophisticated and are basically single skins which are thin compared with the wavelength of operation. Typically, for covering an X-band radar, the skin thickness would be not greater than 1.5mm which renders them of limited application due to their poor structural capabilities.
- Rain erosion protection is normally provided by an elastomeric coating having a uniform thickness of about 0.3mm. This thickness is governed by the minimum thickness required to give protection at the same time as preserving the structural strength and/or the electrical transparency characteristics.
- Rain erosion coatings have slightly different dielectric constants to traditional laminates and, whilst their presence does not normally lead to a structural problem on solid wall radomes it can lead to a severe problem on sandwich radomes where the coating thickness of about 0.3mm has to be deducted from the outer skin thickness of about 0.75mm to maintain the electrical balance of the sandwich. This results in a significant thinning of the outer skin of the sandwich radome, weakening it structurally end encouraging failure of the skin/care bond during flight under heavy rain conditions.
- This invention is intended to provide a half wavelength radome in which sufficient fibre is placed in the axial mode to prevent buckling and in the longitudinal mode to give adequate strength in this direction thus minimising any redundant reinforcement.
- said wall comprises an outer later of elastomeric material for rain erosion protection of the radome.
- a syntactic foam mixture 1 having the same dielectric constant as the reinforcing element is applied to a base composite surface 2 to a depth which will allow it to be machined to give a total thickness which is about 0.5mm or more below that of the half wavelength design thickness.
- the remaining 0.5mm or more is built up by the application of an elastomeric rain erosion coating 3 which is then of increased thickness compared with that conventionally employed.
- the thickness of the rain erosion coating is only governed by its dielectric loss properties which will cause a marginal drop in transmission efficiency. Replacing unnecessary reinforcement and resin by syntactic foam reduces the weight to the lowest possible value consistent with structural viability with minimal change in the electrical performance.
- the fibre can be laid up on a male mould 4 in a unidirectional manner to avoid any crimping which occurs when using woven material. It can be laid up as a unidirectional weave or it can be filament wound, the latter being less desirable as it leads to a high glass content which, whilst otherwise acceptable, raises difficulties in providing syntactic foam of suitably high matching dielectric constant. Furthermore, the use of filament winding for application of the fibre has to be followed by machining away excess fibre laid in the longitudinal direction whereas, using the other techniques and this invention, machining the glass/resin composite can be avoided altogether.
- the basic fibre-resin laminate could be laid up in a female mould 5 and the syntactic foam mixture 1 applied to the inside of the component followed again by machining to a size to allow for the application of the rain erosion coating to the outside.
Abstract
A radome of which the wall comprises a single strength-providing layer made of reinforced plastics material and a syntactic foam layer having a dielectric constant substantially matching that of the reinforced plastics material layer, the thickness of said wall being substantially equal to one half the wavelength of the radiation which is to pass through the radome.
Description
- This invention relates to Radomes and production thereof.
- There are currently three types of radomes used on flight vehicles, ie missiles and aircraft, and these vary according to the flight requirements of the vehicle. The three types are:
- 1. solid wall radomes
- 2. sandwich radomes which can be designed using a number of cores and skins
- 3. thin skin radomes
- Typical solid wall radomes are usually of the half wave-length design and vary in thickness according to the dielectric constant of the material and the wavelength of operation. Typical thicknesses would be 8mm at X-band and about 5mm at J-band with material of dielectric constant of about 4 such as can be obtained from a composite of approximately 55% glass fibre and 45% resin matrix by weight. These radomes can be made by hand lay up, autoclave moulding, filament winding and resin transfer moulding. This type of radome is usually selected where a high microwave transparency performance and structural capability are required such as in military fighter and terrain following aircraft and missile applications.
- The most common version of a Sandwich Radome is the A-sandwich consisting of a lightweight core between two skins, the core thickness being nominally a quarter of a wavelength thick for narrow-band applications but of a compromise thickness for wideband applications. Typically at X -band the core thickness will be about 8mm with skins of thickness approximately 0. 75mm and reinforcement content of around 55% glass fibre by weight as with the solid wall radome. The core of the sandwich is usually either a honeycomb or an expanded foam with a low dielectric constant, although there are applications which use a syntactic foam core of somewhat higher dielectric constant.
- Thin Skin Randomes are relatively unsophisticated and are basically single skins which are thin compared with the wavelength of operation. Typically, for covering an X-band radar, the skin thickness would be not greater than 1.5mm which renders them of limited application due to their poor structural capabilities.
- Whilst some radomes on missiles need to be protected against rain erosion damage, this is not usually the case and a requirement for protection arises mainly in aircraft nose and wing leading edge applications. Rain erosion protection is normally provided by an elastomeric coating having a uniform thickness of about 0.3mm. This thickness is governed by the minimum thickness required to give protection at the same time as preserving the structural strength and/or the electrical transparency characteristics. Rain erosion coatings have slightly different dielectric constants to traditional laminates and, whilst their presence does not normally lead to a structural problem on solid wall radomes it can lead to a severe problem on sandwich radomes where the coating thickness of about 0.3mm has to be deducted from the outer skin thickness of about 0.75mm to maintain the electrical balance of the sandwich. This results in a significant thinning of the outer skin of the sandwich radome, weakening it structurally end encouraging failure of the skin/care bond during flight under heavy rain conditions.
- By and large, and certainly up to X-band, solid wall half wavelength radomes are structurally over-strong and, as a result, are unnecessarily heavy, a penalty which has to be accepted to achieve satisfactory microwave performance. Radomes tend to fail structurally by buckling.
- This invention is intended to provide a half wavelength radome in which sufficient fibre is placed in the axial mode to prevent buckling and in the longitudinal mode to give adequate strength in this direction thus minimising any redundant reinforcement.
- According to one aspect of the present invention, there is provided a radome of which the wall comprises a single strength-providing layer made of reinforced plastics material and a syntactic foam layer having a dielectric constant substantially matching that of the reinforced plastics material layer, the thicknes of said wall being substantially equal to one half the wavelength of the radiation which is to pass through the radome.
- According to another aspect of the present invention there is provided equipment for transmitting and/or receiving electromagnetic radiation and a radome through which said radiation passes and of which the wall comprises a single strength-providing layer made of reinforced plastics material and a syntactic foam layer having a dielectric constant substantially matching that of the reinforced plastics material layer, the thickness of said wall being substantially equal to one half the wavelength of the radiation which is to pass through the radome.
- Preferably said wall comprises an outer later of elastomeric material for rain erosion protection of the radome.
- Reference will now be made by way of example to the accompanying drawing in which:-
- Figure 1 is cross-sectional diagram of a male mould for use in the invention, and
- Figure 2 is a cross-sectional diagram of a female mould for use in the invention.
- Referring to the figures following impregnation and cure, a syntactic foam mixture 1 having the same dielectric constant as the reinforcing element is applied to a
base composite surface 2 to a depth which will allow it to be machined to give a total thickness which is about 0.5mm or more below that of the half wavelength design thickness. The remaining 0.5mm or more is built up by the application of an elastomericrain erosion coating 3 which is then of increased thickness compared with that conventionally employed. The thickness of the rain erosion coating is only governed by its dielectric loss properties which will cause a marginal drop in transmission efficiency. Replacing unnecessary reinforcement and resin by syntactic foam reduces the weight to the lowest possible value consistent with structural viability with minimal change in the electrical performance. - As shown in figure 1, which is given by way of example only, the fibre can be laid up on a male mould 4 in a unidirectional manner to avoid any crimping which occurs when using woven material. It can be laid up as a unidirectional weave or it can be filament wound, the latter being less desirable as it leads to a high glass content which, whilst otherwise acceptable, raises difficulties in providing syntactic foam of suitably high matching dielectric constant. Furthermore, the use of filament winding for application of the fibre has to be followed by machining away excess fibre laid in the longitudinal direction whereas, using the other techniques and this invention, machining the glass/resin composite can be avoided altogether.
- Alternatively, as shown in figure 2, the basic fibre-resin laminate could be laid up in a
female mould 5 and the syntactic foam mixture 1 applied to the inside of the component followed again by machining to a size to allow for the application of the rain erosion coating to the outside. - Using the techniques described above, it may be possible to achieve:-
- 1. A method of making radomes where the fibres are placed to maximum effect and no machining of the structural element is required.
- 2. A radome which has the adequate strength and an electrical performance similar to that of a solid half wavelength radome but which is lighter.
- 3. A method whereby fine tuning of the radome wall can be achieved without interfering with the resin/glass composite, thus preserving the integrity of the structural element.
Claims (6)
1. A radome of which the wall comprises a single strength-providing layer made of reinforced plastics material and a syntactic foam layer having a dielectric constant substantially matching that of the reinforced plastics material layer, the thickness of said wall being substantially equal to one half the wavelength of the radiation which is to pass through the radome.
2. A radome according to claim 1, wherein said wall comprises an outer layer of elastomeric material for rain erosion protection of the radome.
3. A radome according to claim 1 or 2, wherein the foam layer is outside the reinforced plastics material layer.
4. A radome according to claim 1 or 2, wherein the foam layer is inside the plastics material layer.
5. A radome substantially as hereinbefore described with reference to the accompanying drawings.
6. Equipment for transmitting and/or receiving electromagnetic radiation and a radome through which said radiation passes and of which the wall comprises a single strength-providing layer made of reinforced plastics material and a syntactic foam layer having a dielectric constant substantially matching that of the reinforced plastics material layer, the thickness of said wall being substantially equal to one half the wavelength of the radiation which is to pass through the radome.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8821741 | 1988-09-14 | ||
GB888821741A GB8821741D0 (en) | 1988-09-14 | 1988-09-14 | Radomes |
Publications (1)
Publication Number | Publication Date |
---|---|
EP0359504A1 true EP0359504A1 (en) | 1990-03-21 |
Family
ID=10643695
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP19890309200 Withdrawn EP0359504A1 (en) | 1988-09-14 | 1989-09-11 | Radomes |
Country Status (2)
Country | Link |
---|---|
EP (1) | EP0359504A1 (en) |
GB (1) | GB8821741D0 (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5184141A (en) * | 1990-04-05 | 1993-02-02 | Vought Aircraft Company | Structurally-embedded electronics assembly |
US20120075161A1 (en) * | 2010-05-17 | 2012-03-29 | Robert Elwell | Radome |
WO2013037811A1 (en) | 2011-09-12 | 2013-03-21 | Dsm Ip Assets B.V. | Composite radome wall |
WO2014057051A1 (en) | 2012-10-12 | 2014-04-17 | Dsm Ip Assets B.V. | Composite antiballistic radome walls and methods of making the same |
WO2015000926A1 (en) | 2013-07-02 | 2015-01-08 | Dsm Ip Assets B.V. | Composite antiballistic radome walls and methods of making the same |
US9985347B2 (en) | 2013-10-30 | 2018-05-29 | Commscope Technologies Llc | Broad band radome for microwave antenna |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3780374A (en) * | 1971-03-11 | 1973-12-18 | Sumitomo Electric Industries | Radome with matching layers |
GB1357003A (en) * | 1971-02-04 | 1974-06-19 | British Aircraft Corp Ltd | Production of foamed synthetic resin materials |
WO1981000993A1 (en) * | 1979-10-03 | 1981-04-16 | Goodrich Co B F | Composite leading edge for aircraft |
EP0155599A2 (en) * | 1984-03-22 | 1985-09-25 | Dornier Gmbh | Radome material |
US4615933A (en) * | 1984-04-06 | 1986-10-07 | Rogers Corporation | Radome structure and method of manufacture thereof |
-
1988
- 1988-09-14 GB GB888821741A patent/GB8821741D0/en active Pending
-
1989
- 1989-09-11 EP EP19890309200 patent/EP0359504A1/en not_active Withdrawn
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1357003A (en) * | 1971-02-04 | 1974-06-19 | British Aircraft Corp Ltd | Production of foamed synthetic resin materials |
US3780374A (en) * | 1971-03-11 | 1973-12-18 | Sumitomo Electric Industries | Radome with matching layers |
WO1981000993A1 (en) * | 1979-10-03 | 1981-04-16 | Goodrich Co B F | Composite leading edge for aircraft |
EP0155599A2 (en) * | 1984-03-22 | 1985-09-25 | Dornier Gmbh | Radome material |
US4615933A (en) * | 1984-04-06 | 1986-10-07 | Rogers Corporation | Radome structure and method of manufacture thereof |
Non-Patent Citations (1)
Title |
---|
IEE PROCEEDINGS-F, vol. 128, no. 7, December 1981, pages 451-464, Old Woking, Surrey, GB; G.A.E. CRONE et al.: "Design and performance of airborne radomes: a review" * |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5184141A (en) * | 1990-04-05 | 1993-02-02 | Vought Aircraft Company | Structurally-embedded electronics assembly |
US20120075161A1 (en) * | 2010-05-17 | 2012-03-29 | Robert Elwell | Radome |
CN103221304A (en) * | 2010-05-17 | 2013-07-24 | 码科泰克公司 | Radome |
US9115967B2 (en) * | 2010-05-17 | 2015-08-25 | Mactek Corporation | Radome |
CN106972253A (en) * | 2010-05-17 | 2017-07-21 | 码科泰克公司 | Antenna house |
WO2013037811A1 (en) | 2011-09-12 | 2013-03-21 | Dsm Ip Assets B.V. | Composite radome wall |
WO2014057051A1 (en) | 2012-10-12 | 2014-04-17 | Dsm Ip Assets B.V. | Composite antiballistic radome walls and methods of making the same |
US10062962B2 (en) | 2012-10-12 | 2018-08-28 | Dsm Ip Assets B.V. | Composite antiballistic radome walls and methods of making the same |
WO2015000926A1 (en) | 2013-07-02 | 2015-01-08 | Dsm Ip Assets B.V. | Composite antiballistic radome walls and methods of making the same |
US10153546B2 (en) | 2013-07-02 | 2018-12-11 | Dsm Ip Assets B.V. | Composite antiballistic radome walls and methods of making the same |
US9985347B2 (en) | 2013-10-30 | 2018-05-29 | Commscope Technologies Llc | Broad band radome for microwave antenna |
Also Published As
Publication number | Publication date |
---|---|
GB8821741D0 (en) | 1989-09-13 |
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Legal Events
Date | Code | Title | Description |
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PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
17P | Request for examination filed |
Effective date: 19890919 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): DE ES FR GB IT SE |
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17Q | First examination report despatched |
Effective date: 19920730 |
|
RAP3 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: BRITISH AEROSPACE PUBLIC LIMITED COMPANY |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN |
|
18D | Application deemed to be withdrawn |
Effective date: 19940528 |