CN204991956U - Machine that satisfies radar and IR homing head simultaneous working carries multiwindow antenna house - Google Patents
Machine that satisfies radar and IR homing head simultaneous working carries multiwindow antenna house Download PDFInfo
- Publication number
- CN204991956U CN204991956U CN201520701671.0U CN201520701671U CN204991956U CN 204991956 U CN204991956 U CN 204991956U CN 201520701671 U CN201520701671 U CN 201520701671U CN 204991956 U CN204991956 U CN 204991956U
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- multiwindow
- radome
- infrared
- radar
- antenna house
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Abstract
The utility model provides a machine that satisfies radar and IR homing head simultaneous working carries multiwindow antenna house, pass through the ripples district including passing through ripples district, infrared window district and non -, pass through the ripples and distinguish the curved surface that is rectangle, be located one side of multiwindow antenna house, the infrared window position is in the front portion of multiwindow antenna house, including infrared glass, yielding rubber and aluminum metal alloy frame, infrared glass and damping rubber suit are on aluminum metal alloy frame, and aluminum metal alloy frame is pre -buried to be advanced in the multiwindow antenna house, the non - is passed through the ripples district and is adopted glass fiber cloth reinforcing epoxy resin combined material. Compared with the prior art, the utility model discloses can solve current antenna house and pass through the unsatisfied requirement of ripples rate, and can not carry out synthetic aperture radar and the experimental technical problem of infrared automatic target identification simultaneously, guarantee effectively that the warpout carrier band flies going on smoothly of experimental task.
Description
Technical field
The utility model relates to a kind of radome.
Background technology
Airborne band flies test and implements on diploma aircraft, utilizes the mounting panel of diploma aircraft belly to install fixed radar antenna and infrared seeker.But the radome of existing diploma aircraft belly is curved surface honeycomb sandwich construction, and wave transmission rate does not meet the demands, and does not have infrared window, can not meet the condition that radar and infrared target seeker works simultaneously.
Summary of the invention
The technical problems to be solved in the utility model is: provide a kind of airborne multiwindow radome simultaneously tested for radar and infrared target seeker, solve existing radome wave transmission rate not meet the demands, and the technical problem of radar and infrared automatic target detection test can not be carried out simultaneously.
The utility model solves the technical scheme that its technical problem adopts:
For the airborne multiwindow radome that radar and infrared target seeker is tested simultaneously, it is characterized in that: comprise wave transparent district, infrared window mouth region and non-wave transparent district; Described wave transparent district is rectangle curve form, is positioned at the side of multiwindow radome; Described infrared window district is positioned at the front portion of multiwindow radome, comprises infrared glass, yielding rubber and aluminum alloy frame; Infrared glass and vibration isolation rubber are sleeved on aluminum alloy frame, and aluminum alloy frame is nuzzled in multiwindow radome in advance; Non-wave transparent district adopts glass fabric reinforced epoxy based composites.
Preferably, described wave transparent district adopts glass fabric reinforced epoxy based composites as inside and outside covering, and centre is honeycombed paper sandwich.
Preferably, for ensureing the rigidity of multiwindow radome, the ring rib of more than two is set in radome cover body.
Preferably, for gaining in strength, surrounding's layout one deck glass-reinforced plastic material of described aluminum alloy frame.
Preferably, described infrared window mouth region arranges two or more at airborne multiwindow radome.
Compared with prior art, the utility model can solve existing radome wave transmission rate and not meet the demands, and can not carry out the technical problem of radar and infrared automatic target detection test simultaneously, effectively ensure that airborne band flies carrying out smoothly of test mission.
Accompanying drawing explanation
In order to be illustrated more clearly in the utility model embodiment or technical scheme of the prior art, be briefly described to the accompanying drawing used required in embodiment or description of the prior art below, apparently, accompanying drawing in the following describes is embodiments more of the present utility model, for those of ordinary skill in the art, under the prerequisite not paying creative work, other accompanying drawing can also be obtained according to these accompanying drawings.
Fig. 1 is structural representation of the present utility model.
Embodiment
For making the object of the utility model embodiment, technical scheme and advantage clearly, below in conjunction with the accompanying drawing in the utility model embodiment, technical scheme in the utility model embodiment is clearly and completely described, obviously, described embodiment is the utility model part embodiment, instead of whole embodiments.Based on the embodiment in the utility model, those of ordinary skill in the art are not making the every other embodiment obtained under creative work prerequisite, all belong to the scope of the utility model protection.
As shown in Figure 1 be a kind of airborne multiwindow radome simultaneously worked for radar and infrared target seeker, comprise wave transparent district 1, infrared window mouth region 234 and non-wave transparent district 5; Shown in figure is two-dimensional projection's schematic diagram of radome, and the curve form of radome of the present invention is consistent with radome of the prior art; Described wave transparent district 1 is rectangle curve form, is positioned at the side of multiwindow radome; Described infrared window mouth region 234 is positioned at the front portion of multiwindow radome, comprises infrared glass 2, yielding rubber 3 and aluminum alloy frame 4; Infrared glass 2 and vibration isolation rubber 3 are sleeved on aluminum alloy frame 4, and aluminum alloy frame 4 is nuzzled in multiwindow radome in advance.For ensureing the intensity of radome, non-wave transparent district 5 adopts glass fabric reinforced epoxy based composites.The utility model can solve existing radome wave transmission rate and not meet the demands, and can not carry out the technical problem of radar and infrared automatic target detection test simultaneously, effectively ensure that airborne band flies carrying out smoothly of test mission.
Preferably, described wave transparent district 1 adopts glass fabric reinforced epoxy based composites as inside and outside covering, and centre is honeycombed paper sandwich.The large I in wave transparent district 1 may inswept scope be determined according to the overall dimension of radar antenna, carry position and wave beam.For ensureing the rigidity of multiwindow radome, the ring rib 6 of more than two is set in radome cover body.For gaining in strength, surrounding's layout one deck glass-reinforced plastic material of described aluminum alloy frame 4.Preferably, described infrared window mouth region 234 arranges two or more at airborne multiwindow radome.
Last it is noted that above embodiment is only in order to illustrate the technical solution of the utility model, be not intended to limit; Although be described in detail the utility model with reference to previous embodiment, those of ordinary skill in the art is to be understood that: it still can be modified to the technical scheme described in foregoing embodiments, or carries out equivalent replacement to wherein portion of techniques feature; And these amendments or replacement, do not make the essence of appropriate technical solution depart from the spirit and scope of each embodiment technical scheme of the utility model.
Claims (5)
1. meet the airborne multiwindow radome that radar and infrared target seeker works simultaneously, it is characterized in that: comprise wave transparent district (1), infrared window mouth region (234) and non-wave transparent district (5);
Described wave transparent district (1) is rectangle curve form, is positioned at the side of multiwindow radome;
Described infrared window mouth region (234) is positioned at the front portion of multiwindow radome, comprises infrared glass (2), yielding rubber (3) and aluminum alloy frame (4); Infrared glass (2) and vibration isolation rubber (3) are sleeved on aluminum alloy frame (4), and aluminum alloy frame (4) is nuzzled in multiwindow radome in advance;
Non-wave transparent district (5) adopts glass fabric reinforced epoxy based composites.
2. a kind of airborne multiwindow radome meeting radar and infrared target seeker and work simultaneously as claimed in claim 1, it is characterized in that: wherein said wave transparent district (1) adopts glass fabric reinforced epoxy based composites as inside and outside covering, and centre is honeycombed paper sandwich.
3. a kind of airborne multiwindow radome meeting radar and infrared target seeker and work simultaneously as claimed in claim 1 or 2, is characterized in that: the ring rib (6) arranging more than two in radome cover body.
4. a kind of airborne multiwindow radome meeting radar and infrared target seeker and work simultaneously as claimed in claim 3, is characterized in that: surrounding's layout one deck glass-reinforced plastic material of wherein said aluminum alloy frame (4).
5. a kind of airborne multiwindow radome meeting radar and infrared target seeker and work simultaneously as claimed in claim 4, is characterized in that: wherein said infrared window mouth region (234) arranges two or more at airborne multiwindow radome.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520701671.0U CN204991956U (en) | 2015-09-10 | 2015-09-10 | Machine that satisfies radar and IR homing head simultaneous working carries multiwindow antenna house |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520701671.0U CN204991956U (en) | 2015-09-10 | 2015-09-10 | Machine that satisfies radar and IR homing head simultaneous working carries multiwindow antenna house |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204991956U true CN204991956U (en) | 2016-01-20 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520701671.0U Expired - Fee Related CN204991956U (en) | 2015-09-10 | 2015-09-10 | Machine that satisfies radar and IR homing head simultaneous working carries multiwindow antenna house |
Country Status (1)
| Country | Link |
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| CN (1) | CN204991956U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2019039860A (en) * | 2017-08-28 | 2019-03-14 | 豊田合成株式会社 | Radio wave transmission cover |
| CN109489501A (en) * | 2017-09-12 | 2019-03-19 | 江西洪都航空工业集团有限责任公司 | A kind of Nonopaque type target seeker protective cover |
| CN112408990A (en) * | 2019-08-20 | 2021-02-26 | 山东工业陶瓷研究设计院有限公司 | Ceramic wave-transmitting material matched with infrared material in performance, antenna housing and preparation method |
| CN113394561A (en) * | 2021-06-10 | 2021-09-14 | 中国科学院空天信息创新研究院 | Ultra-wideband antenna cover for multiband synthetic aperture radar antenna and test method |
| CN117154398A (en) * | 2023-09-25 | 2023-12-01 | 南京玻璃纤维研究设计院有限公司 | High-temperature-resistant radome and preparation method thereof |
-
2015
- 2015-09-10 CN CN201520701671.0U patent/CN204991956U/en not_active Expired - Fee Related
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2019039860A (en) * | 2017-08-28 | 2019-03-14 | 豊田合成株式会社 | Radio wave transmission cover |
| CN109489501A (en) * | 2017-09-12 | 2019-03-19 | 江西洪都航空工业集团有限责任公司 | A kind of Nonopaque type target seeker protective cover |
| CN112408990A (en) * | 2019-08-20 | 2021-02-26 | 山东工业陶瓷研究设计院有限公司 | Ceramic wave-transmitting material matched with infrared material in performance, antenna housing and preparation method |
| CN112408990B (en) * | 2019-08-20 | 2023-05-02 | 山东工业陶瓷研究设计院有限公司 | Ceramic wave-transmitting material matched with infrared material in performance, radome and preparation method |
| CN113394561A (en) * | 2021-06-10 | 2021-09-14 | 中国科学院空天信息创新研究院 | Ultra-wideband antenna cover for multiband synthetic aperture radar antenna and test method |
| CN113394561B (en) * | 2021-06-10 | 2022-12-23 | 中国科学院空天信息创新研究院 | Ultra-wideband antenna cover for multiband synthetic aperture radar antenna and test method |
| CN117154398A (en) * | 2023-09-25 | 2023-12-01 | 南京玻璃纤维研究设计院有限公司 | High-temperature-resistant radome and preparation method thereof |
| CN117154398B (en) * | 2023-09-25 | 2024-04-19 | 南京玻璃纤维研究设计院有限公司 | High-temperature-resistant radome and preparation method thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160120 Termination date: 20160910 |