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GB2458663A - Radome for a radar pressurised horn antenna - Google Patents

Radome for a radar pressurised horn antenna Download PDF

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Publication number
GB2458663A
GB2458663A GB0805484A GB0805484A GB2458663A GB 2458663 A GB2458663 A GB 2458663A GB 0805484 A GB0805484 A GB 0805484A GB 0805484 A GB0805484 A GB 0805484A GB 2458663 A GB2458663 A GB 2458663A
Authority
GB
United Kingdom
Prior art keywords
radome
horn
frame
film
radome according
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.)
Granted
Application number
GB0805484A
Other versions
GB0805484D0 (en
GB2458663B (en
Inventor
Anne Fuller
Sang Tu
Mike Tyrrell
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.)
Thales Holdings UK PLC
Original Assignee
Thales Holdings UK PLC
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 Thales Holdings UK PLC filed Critical Thales Holdings UK PLC
Priority to GB0805484.3A priority Critical patent/GB2458663B/en
Publication of GB0805484D0 publication Critical patent/GB0805484D0/en
Publication of GB2458663A publication Critical patent/GB2458663A/en
Application granted granted Critical
Publication of GB2458663B publication Critical patent/GB2458663B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/42Housings not intimately mechanically associated with radiating elements, e.g. radome
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/42Housings not intimately mechanically associated with radiating elements, e.g. radome
    • H01Q1/422Housings not intimately mechanically associated with radiating elements, e.g. radome comprising two or more layers of dielectric material
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q13/00Waveguide horns or mouths; Slot antennas; Leaky-waveguide antennas; Equivalent structures causing radiation along the transmission path of a guided wave
    • H01Q13/02Waveguide horns

Landscapes

  • Details Of Aerials (AREA)

Abstract

A radome for a pressurised horn 4 of a radar antenna comprises a fluoropolymer film 6 whose periphery is supported by a closed cell rigid foam plastics frame 7, 8. The said film 6 may be made of fluronated ethylene propylene FEP and may have a thickness of 0.1 to 0.5 mm. The frame 7, 8 may be formed with two flat surfaces between which the periphery of the film 6 may be sandwiched and secured into place by an epoxy resin adhesive. The frame 7, 8 may be made of a closed cell foam plastic material such as polymethacrylimide PMI with good flame-inhibiting properties. The frame 7, 8 may have a polygonal opening which conforms to that of a polyhedral horn. The radome may hermetically seal the mouth of the horn of a radar pressurized horn antenna, typically operating with a transmission power level of 1.5 to 2 kW, which is suitable for aircraft applications.

Description

RADOME
This invention relates to a radome suitable for a pressurised horn of a radar antenna.
High power radar antennae for aircraft typically comprise a polyhedral, e.g. octagonal section, horn sealed hermetically at its mouth by a radome, the horn being pressurised and filled with an inert gas such as nitrogen. The radome necessarily absorbs some of [lie fflicrowave radiation transmittcd by the antenna, and its materia! has to withstand high temperatures as a result of the microwave absorption. It has been difficult to find a suitable radome which can withstand typical fluid pressures of a pressurised horn whilst resisting burning from the microwave absorption.
The invention provides a radome for a pressurised horn of a radar antenna, comprising a fluoropolymer film whose periphery is supported by a closed cell rigid foam plastics frame.
A preferred embodiment of the invention will now be described, by way of example only, with reference to the accompanying drawings, in which: Figure 1 is a perspective view, including a separate and enlarged view of a portion, of a high power, high-pressure horn radome installed in an airborne radar antenna, embodying the present invention; Figure 2 is an axial longitudinal cross-section through the dome of the radar antenna of Figure I, taken along the line 2-2 of Figure 3; Figure 3 is a front elevation of the dome of Figure 2; and Figure 4 is a perspective view of the dome of Figures 2 and 3.
A radar antenna suitable for airborne use and capable of high power transmission is shown in Figure 1. The radar antenna I comprises a dish 2 and a transmitting and receiving portion 3, which is also shown to an enlarged scale in Figure I. The transmitting arid receiving portion 3 comprises a metal wave-guide of rectangular section for microwave communication with a dome 4, which is shown in greater detail in Figures 2 to 4.
The dome 4 is hermetically sealed to the external atmosphere and, in use, is filled with an inert gas such as nitrogen which must be dry. The differential pressure can be of the order of one atmosphere, although we have discovered in tests that a horn embodying the invention can withstand over two atmospheres.
The mean transmission power of the radar is typically in the range of 1.5-2 kW.
The horn 4 comprises a wafl 5 which, as shown more clearly in Figure 4, is polyhedral, and octagonal in cross-section. This shape sets up desirable vertical and horizontal polarisations to give a well-defined power distribution across the horn, but it will be appreciated that this particular shape is not essential to the present invention.
The mouth of the horn 4 is planar, as shown in Figure 2, and its generally polyhedral outer surface is enlarged near its mouth so as to provide flat surfaces 9 parallel to the horn axis, for supporting a radome 12 as shown in Figure 2.
The radonie 12 comprises a membrane or film 6 of fluorinated ethylene propylene, FEP, which in this example is 0.254 mm thick but which could be in the range of 0.1 to 0.5 mm, preferably 0.2 to 0.3 mm. The membrane 6 has a peripheral shape, in this example octagonal, to conform to the mouth of the horn 4. FEP has been found to have satisfactory mechanical properties as well as the ability to bond well to a support frame 7, 8. It can be made stronger and thinner than the radome materials of existing structures, and as a result it can withstand high power microwave radiation without degrading or burning. This was surprising in view of its reputation as being rather brittle.
The membrane is gripped between flat opposed surfaces of two components 7, 8 of a frame. The axially inward component 7 of the frame has an internal surface 9 which fits closely over, and is bonded by adhesive to the external surface of the mouth of the horn 4 as shown in Figure 2. The axially outward component 8 of the frame has a frusto-conical surface 10 with the same half angle as the conical horn wall 5. The flat surfaces of the frame components 7, 8 which face each other cover the same area of the periphery of the membrane 6, but on opposite sides of the membrane, as shown in Figure 2. A groove 11 is cut into the exterior of the opposed surfaces of the frame components 7, 8, so that the groove follows the peripheral edge of the membrane 6.
An epoxy resin adhesive, preferably Araldite (registered trade mark) bonds the surfaces of the periphery of the membrane 6 to the opposed flat surfaces of the frame components 7, 8, and the adhesive also fills the groove 11 and is flush with the external flat surface othe frame 7, 8 as shown in Figure 2.
To minimise the risk of electric discharge within the horn, the internal surfaces are smooth, and the surface is uninterrupted as it tapers outwardly from the wall 5 of the horn to the wall 10 of the radome. The risk of discharge is also minimised by the presence of the inert gas.
The frame 7,8 is of a closed cell rigid foam plastics material, which in this case is based on polymethacrylirnide, PM1. PMI is described for example in US Patent 5698605 and in WO/2003/078514, and it is known to have the ability to bond to epoxy adhesives, as well as to have good flame-inhibiting properties. By sandwiching the membrane 6 between the two frame components 7, 8, the arrangement has good mechanical strength and the ability to withstand changes in pressure and also shock from acceleration, without tearing and without breaking the adhesive bond.
It will be appreciated that all internal faces of the horn and the radome are to be free from adhesive.
The external surfaces of the radome are free from paint, but the horn is painted with an epoxy resin enamel.

Claims (15)

  1. CLAIMS: I. A radome for a pressurised horn of a radar antenna, comprising a fluoropolymer film whose periphery is supported by a closed cell rigid foam plastics frame.
  2. 2. A radome according to Claim 1, in which the film has a thickness of 0.1 to 0.5 mm.
  3. 3. A radome according to Claim 3, in which the film has a thickness of 0.2 to 0.3 ni m.
  4. 4. A radome according to any preceding claim, in which the frame comprises two components with flat surfaces facing each other and gripping therebetween the periphery of the film.
  5. 5. A radorne according to any preceding claim, in which the fluoropolymer comprises fluorinated ethylene propylene.
  6. 6. A radome according to any preceding claim, in which the frame has a polygonal opening to conform to a polyhedral horn.
  7. 7. A radome according to any preceding claim, comprising a layer of adhesive bonding the periphery of the film to the frame.
  8. 8. A radome according to Claim 4, comprising a layer of adhesive bonding each surface of the periphery of the film to the flat surface of the respective frame component.
  9. 9. A radon-ic according to Claim 7 or 8, in which the adhesive is an epoxy resin.
  10. 10. A radome according to any preceding claim, in which the plastics frame is of a closed cell foam.
  11. 11. A radome according to Claim 10, in which the closed cell foam comprises polym ethacryli m ide.
  12. 12. A pressurisable horn for a radar antenna, comprising a radome according to any preceding claim hermetically sealing its mouth.
  13. 13. A radar comprising a pressurisable horn according to Claim 12.
  14. 14. An hermetically sealed, pressurised radar horn having a radome according to any ofClaims Ito II.
  15. 15. A radome substantially as described herein with reference to Figures 2 to 4 of the accompanying drawings.AMENDMENTS TO THE CLAIMS HAVE BEEN FILED AS FOLLOWS: 1. A radome for a pressurised horn of a radar antenna, comprising a fluoropolymer film whose periphery is supported by a closed cell rigid foam plastics frame.2. A radome according to Claim 1, in which the film has a thickness of 0.1 to 0.5 mm.3. A radome according to Claim 2, in which the film has a thickness of 0.2 to 0.3 mm.4. A radome according to any preceding claim, in which the frame comprises two components with flat surfaces facing each other and gripping therebetween the periphery of the film.5. A radome according to any preceding claim, in which the fluoropolymer comprises fluorinated ethylene propylene.6. A radome according to any preceding claim, in which the frame has a polygonal ::::. opening to conform to a polyhedral horn.7. A radome according to any preceding claim, comprising a layer of adhesive * S., bonding the periphery of the film to the frame. *.SS::*. 8. A radome according to Claim 4, comprising a layer of adhesive bonding each I...surface of the periphery of the film to the flat surface of the respective frame component.9. A radome according to Claim 7 or 8, in which the adhesive is an epoxy resin.10. A radome according to any preceding claim, in which the plastics frame is of a closed cell foam.11. A radome according to Claim 10, in which the closed cell foam comprises polymethacrylimide.12 A pressurisable horn for a radar antenna, comprising a radome according to any preceding claim hermetically sealing its mouth.13. A radar comprising a pressurisable horn according to Claim 12.14. An hermetically sealed, pressurised radar horn having a radome according to any of Claims Ito ii.15. A radome substantially as described herein with reference to Figures 2 to 4 of the accompanying drawings.
GB0805484.3A 2008-03-26 2008-03-26 Radome Active GB2458663B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB0805484.3A GB2458663B (en) 2008-03-26 2008-03-26 Radome

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB0805484.3A GB2458663B (en) 2008-03-26 2008-03-26 Radome

Publications (3)

Publication Number Publication Date
GB0805484D0 GB0805484D0 (en) 2008-04-30
GB2458663A true GB2458663A (en) 2009-09-30
GB2458663B GB2458663B (en) 2012-11-21

Family

ID=39386773

Family Applications (1)

Application Number Title Priority Date Filing Date
GB0805484.3A Active GB2458663B (en) 2008-03-26 2008-03-26 Radome

Country Status (1)

Country Link
GB (1) GB2458663B (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107046173A (en) * 2017-04-20 2017-08-15 哈尔滨哈玻拓普复合材料有限公司 A composite material pressure-resistant structure rectome and its manufacturing method
CN110698715A (en) * 2019-10-16 2020-01-17 浙江中科恒泰新材料科技有限公司 Radiation crosslinking polymethacrylimide foam and preparation method thereof
US20200381814A1 (en) * 2019-06-03 2020-12-03 Space Exploration Technologies Corp. Antenna apparatus having radome spacing
US12334630B2 (en) 2021-11-09 2025-06-17 Space Exploration Technologies Corp. Radome assembly having nodeless cells
US12374772B2 (en) 2021-11-09 2025-07-29 Space Exploration Technologies Corp. User terminal housing

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3201296A (en) * 1959-04-09 1965-08-17 Timothy J Kilduff Method of making a waveguide window
GB1296298A (en) * 1970-07-02 1972-11-15
GB1600668A (en) * 1977-10-05 1981-10-21 Endress Hauser Gmbh Co Microwave antennas
EP0303001A2 (en) * 1987-06-11 1989-02-15 IRTE S.p.A. Horn antenna
US5698605A (en) * 1996-02-22 1997-12-16 Roehm Gmbh Chemische Fabrik Flame-resistant polymethacrylimide foams
EP0814534A2 (en) * 1996-06-20 1997-12-29 Andrew A.G. Feed structure for antennas

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2989748A (en) * 1956-10-22 1961-06-20 Gen Bronze Corp Feed system for broad band antenna
JPS5341156A (en) * 1976-09-27 1978-04-14 Mitsubishi Electric Corp Horn antenna
DE4124011C1 (en) * 1991-07-19 1992-10-01 Philips Patentverwaltung Gmbh, 2000 Hamburg, De
JP2005026954A (en) * 2003-07-01 2005-01-27 Sharp Corp Radio wave receiving converter and antenna device

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3201296A (en) * 1959-04-09 1965-08-17 Timothy J Kilduff Method of making a waveguide window
GB1296298A (en) * 1970-07-02 1972-11-15
GB1600668A (en) * 1977-10-05 1981-10-21 Endress Hauser Gmbh Co Microwave antennas
EP0303001A2 (en) * 1987-06-11 1989-02-15 IRTE S.p.A. Horn antenna
US5698605A (en) * 1996-02-22 1997-12-16 Roehm Gmbh Chemische Fabrik Flame-resistant polymethacrylimide foams
EP0814534A2 (en) * 1996-06-20 1997-12-29 Andrew A.G. Feed structure for antennas

Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107046173B (en) * 2017-04-20 2020-04-24 哈尔滨哈玻拓普复合材料有限公司 Composite material voltage-resistant structure radome and manufacturing method thereof
CN107046173A (en) * 2017-04-20 2017-08-15 哈尔滨哈玻拓普复合材料有限公司 A composite material pressure-resistant structure rectome and its manufacturing method
US11600915B2 (en) 2019-06-03 2023-03-07 Space Exploration Technologies Corp. Antenna apparatus having heat dissipation features
US11652286B2 (en) 2019-06-03 2023-05-16 Space Exploration Technology Corp. Antenna apparatus having adhesive coupling
US20200381815A1 (en) * 2019-06-03 2020-12-03 Space Exploration Technologies Corp. Antenna apparatus housing and components for same
US12355148B2 (en) 2019-06-03 2025-07-08 Space Exploration Technologies Corp. Antenna apparatus having chassis portion
US11322833B2 (en) 2019-06-03 2022-05-03 Space Exploration Technologies Corp. Antenna apparatus having fastener system
US11509048B2 (en) 2019-06-03 2022-11-22 Space Exploration Technologies Corp. Antenna apparatus having antenna spacer
US12237575B2 (en) * 2019-06-03 2025-02-25 Space Explortion Technologies Corp. Antenna apparatus having radome spacing
US20200381814A1 (en) * 2019-06-03 2020-12-03 Space Exploration Technologies Corp. Antenna apparatus having radome spacing
US11843168B2 (en) 2019-06-03 2023-12-12 Space Exploration Technologies Corp. Antenna apparatus having antenna spacer
US12142826B2 (en) 2019-06-03 2024-11-12 Space Exploration Technologies Corp. Antenna apparatus having heat dissipation features
CN110698715A (en) * 2019-10-16 2020-01-17 浙江中科恒泰新材料科技有限公司 Radiation crosslinking polymethacrylimide foam and preparation method thereof
CN110698715B (en) * 2019-10-16 2022-03-18 浙江中科恒泰新材料科技有限公司 Radiation crosslinking polymethacrylimide foam and preparation method thereof
US12334630B2 (en) 2021-11-09 2025-06-17 Space Exploration Technologies Corp. Radome assembly having nodeless cells
US12374772B2 (en) 2021-11-09 2025-07-29 Space Exploration Technologies Corp. User terminal housing
US12463333B2 (en) 2021-11-09 2025-11-04 Space Exploration Technologies Corp. Radome assembly coupling with antenna assembly

Also Published As

Publication number Publication date
GB0805484D0 (en) 2008-04-30
GB2458663B (en) 2012-11-21

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