JPH02291703A - Radar dome made of fiber reinforced plastic - Google Patents
Radar dome made of fiber reinforced plasticInfo
- Publication number
- JPH02291703A JPH02291703A JP1112099A JP11209989A JPH02291703A JP H02291703 A JPH02291703 A JP H02291703A JP 1112099 A JP1112099 A JP 1112099A JP 11209989 A JP11209989 A JP 11209989A JP H02291703 A JPH02291703 A JP H02291703A
- Authority
- JP
- Japan
- Prior art keywords
- fabric
- layers
- radar dome
- woven
- warps
- 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
Links
- 229920002430 Fibre-reinforced plastic Polymers 0.000 title claims description 3
- 239000011151 fibre-reinforced plastic Substances 0.000 title claims description 3
- 239000004744 fabric Substances 0.000 claims abstract description 27
- 239000003822 epoxy resin Substances 0.000 claims abstract description 8
- 229920000647 polyepoxide Polymers 0.000 claims abstract description 8
- 239000002985 plastic film Substances 0.000 abstract description 5
- 229920006255 plastic film Polymers 0.000 abstract description 5
- 239000005060 rubber Substances 0.000 abstract description 3
- 238000003475 lamination Methods 0.000 abstract 1
- 238000000465 moulding Methods 0.000 description 7
- 238000010586 diagram Methods 0.000 description 6
- 238000004519 manufacturing process Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 3
- 238000010438 heat treatment Methods 0.000 description 3
- 229920005989 resin Polymers 0.000 description 3
- 239000011347 resin Substances 0.000 description 3
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 2
- 239000000835 fiber Substances 0.000 description 2
- 239000003365 glass fiber Substances 0.000 description 2
- 238000010030 laminating Methods 0.000 description 2
- 230000002093 peripheral effect Effects 0.000 description 2
- AZBAQHIVVLQMFX-UHFFFAOYSA-N 4-(2,4-dimethylphenyl)-5-methyl-1,3-thiazol-2-amine Chemical compound S1C(N)=NC(C=2C(=CC(C)=CC=2)C)=C1C AZBAQHIVVLQMFX-UHFFFAOYSA-N 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000012778 molding material Substances 0.000 description 1
- 229920001225 polyester resin Polymers 0.000 description 1
- 239000004645 polyester resin Substances 0.000 description 1
- 239000000377 silicon dioxide Substances 0.000 description 1
- 210000004894 snout Anatomy 0.000 description 1
- 229920001187 thermosetting polymer Polymers 0.000 description 1
- 230000037303 wrinkles Effects 0.000 description 1
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Landscapes
- Moulding By Coating Moulds (AREA)
- Details Of Aerials (AREA)
Abstract
Description
【発明の詳細な説明】
〔産業上の利用分野〕
本発明は、航空機等に装着される繊維強化プラスチック
製レーダドームに関する。DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to a fiber-reinforced plastic radar dome mounted on an aircraft or the like.
従来の航空機等の先端に装着されるレーダドームは、第
5図に示すように先端部かはソ゛半球状で後方向に向っ
てテーパ状に広がった形状をなしており、内部には受信
機02が装着されている。As shown in Figure 5, the conventional radar dome attached to the tip of an aircraft has a hemispherical tip that tapers toward the rear, and a receiver is installed inside. 02 is installed.
上記レーダドーム01は要求される電気性能から、ガラ
ス繊維,シリカ繊維等を強化材とした複合材料の積層構
造もしくはサンドインチ構造品が広く適用されている。Due to the required electrical performance, the radar dome 01 has a laminated structure or a sandwich structure made of a composite material reinforced with glass fiber, silica fiber, etc., and is widely used.
上記レーダドームOlの製作方法を第6図により説明す
ると、ガラス繊維等の織物にエポキシ樹脂.ポリエステ
ル樹脂等の熱硬化性樹脂を含浸させ、一般にプリブレグ
と称される成形素材03(以下プリプレグと称す)とし
、同プリプレグ03にしわや折重ね部ができないように
切れ目05を入れながら成形型040表面に注意深く所
要の厚さになるまで積層した後、プラスチックフィルム
06で覆い、オートクレーフ等の加圧加熱装置を用いて
成形していた。The manufacturing method of the above-mentioned radar dome Ol is explained with reference to FIG. 6. The manufacturing method is as follows: epoxy resin is applied to a fabric such as glass fiber. A thermosetting resin such as polyester resin is impregnated to form a molding material 03 (hereinafter referred to as prepreg), which is then molded into a mold 040 while making cuts 05 to prevent wrinkles or folded portions from forming in the prepreg 03. After carefully laminating the layers on the surface to a desired thickness, they were covered with plastic film 06 and molded using a pressure heating device such as an autoclave.
従来のレーダドームにおいては、プリプレグがあまり伸
縮しないために、プリブレグを切断し、切断面をつき合
せ、もしくは重ね合わせて成形型になしませていく必要
があった。このため、当該部位における板厚の局部的変
化や材料の電気定数の局部的変化により、レーダドーム
としての電波的性能に悪影響を与えていた。また製品中
に繊維の切断部が存在するため、強度的にも不利であっ
た。In conventional radar domes, the prepreg does not expand or contract very much, so it was necessary to cut the prepreg and match or overlap the cut surfaces to form a mold. For this reason, local changes in the plate thickness and electric constants of the material at these locations adversely affect the radio wave performance of the radar dome. Furthermore, since there were cut portions of fibers in the product, it was also disadvantageous in terms of strength.
本発明は、かかる事情に鑑みてなされたものであって、
織物の切断部を成形品中に存在させることなくレーダド
ームを製作し、機械的強度並びに電波的性能が良好なレ
ーダドームを提供しようとするものである。The present invention has been made in view of such circumstances, and
The present invention aims to manufacture a radar dome without having cut portions of fabric in the molded product, and to provide a radar dome with good mechanical strength and radio wave performance.
本発明のレーダドームは、多層をなす縦糸とそれぞれ一
層おきの上記縦糸の各層に主として織り込まれ縦糸複数
本に1本の割合で縦糸の隣接する他の層の糸と交差する
横糸よりなりエポキシ樹脂等が含浸され伸縮性を有する
多層織物よりなることを特徴としている。The radome of the present invention is made of epoxy resin consisting of multi-layered warp threads and weft threads that are mainly woven into each layer of the warp threads and intersect with threads of other layers adjacent to the warp threads at a rate of one warp thread for every plurality of warp threads. It is characterized by being made of a stretchable multilayer fabric impregnated with
上記において、多層織物はエボキシ樹脂等が含浸され、
成型治具の表面に積層された後、オートクレープ等によ
り加圧加熱され樹脂が硬化して、レーダドームを形成す
る。In the above, the multilayer fabric is impregnated with epoxy resin etc.
After being laminated on the surface of a molding jig, the resin is heated under pressure using an autoclave or the like to harden and form a radar dome.
上記多層織物は、横糸が一層おきに織り込まれ中間層と
の結合度合が弱く伸縮性があるために成型治具の表面に
よくなじみ、切れ目を入れることなく成型治具に密着さ
せることができる。The multilayer fabric has weft yarns woven every other layer, has a weak bond with the intermediate layer, and is stretchable, so it fits well on the surface of the molding jig and can be brought into close contact with the molding jig without making cuts.
上記により、織物の切断面のつき合せ部もしくは重ね合
わせ部のないレーダードームとしたため、当該部位で発
現する電気定数の局部変化が防止でき、レーダドームの
電波性能の向上とともに機械的強度の向上を図ることが
できた。As a result of the above, the radar dome is created without the abutting or overlapping parts of the cut surfaces of the fabric, making it possible to prevent local changes in the electrical constant that occur at the relevant parts, improving the radio wave performance of the radar dome as well as its mechanical strength. I was able to figure it out.
本発明の一実施例を第1図に示す。 An embodiment of the present invention is shown in FIG.
第1図に示す本実施例は、エポキシ樹脂等が含浸され積
層されてレーダドーム1の内側を形成する多層織物2、
同多層織物2の外周面に設けられたラバー製キャップ3
、および同キャソプ3の外周面に設けられたプラスチッ
クフィルム4を備えている。The present embodiment shown in FIG. 1 includes a multilayer fabric 2 impregnated with epoxy resin and laminated to form the inside of a radar dome 1;
A rubber cap 3 provided on the outer peripheral surface of the multilayer fabric 2
, and a plastic film 4 provided on the outer peripheral surface of the cassop 3.
上記において、多lm吻2は、第2図に示すように横糸
xI + x2 * ・・・・・・と縦糸YI.Yt
・・・・・・・よりなっている。上記縦糸)’l.)’
2,・・・・・・は、第2図のa−a断面,b−b断面
.・・団・l一l断面を表わす第3図(al. (b)
, −・・・・・, (/)に示すように多Fi(am
,b層,(1・旧・・)をなしており、横糸xI +
X2 + ・・・・・・は、それぞれ一層おきの縦糸
の各層(a層.C層.・・・・・・)に織り込まれ、と
きどき隣接する他の層の(b層,・・・・・・)の糸と
交羞している。In the above, the multi-lm snout 2 has the weft xI + x2 * . . . and the warp YI. Yt
It's more like... Warp above)'l. )'
2, . . . are the a-a cross section and the bb-b cross section in Fig. 2. ...Figure 3 (al. (b)) showing the cross section of the group
, −・・・・・・, As shown in (/), multi-Fi(am
, b layer, (1, old...), weft xI +
X2 +... is woven into each warp layer (layer a, layer C...), and is sometimes woven into each other layer (layer b,...) of the adjacent layer. ...) thread.
上記多層織物2を用いたレーダドーム1の成形は、まず
適当な離型処理が施された成型治具5の表面にエボキシ
樹脂等を含浸した上記多層織物2を積層する。同多層織
物2は、横糸が一層おきに織り込まれ中間層の結合度合
が弱く伸縮するために成型治具5へのなじみ性がよく、
切れ目を入れることなく成型治具5に密着させることが
できる。上記多層織物2の積層後は、表面の平滑性を得
るため、ほ\レーダドーム1の形状をなすラハー製のキ
ャソブ3を上記積層の表面に被せ、更にその表面をプラ
スチックフィルム4で覆い、オートクレープ等の加圧加
熱装置を用いて加圧加熱して樹脂を硬化させ、レーダド
ーム1としている。To mold the radar dome 1 using the multilayer fabric 2, first, the multilayer fabric 2 impregnated with epoxy resin or the like is laminated on the surface of a molding jig 5 that has been subjected to an appropriate mold release treatment. The multilayer fabric 2 has good compatibility with the molding jig 5 because the weft yarns are woven every other layer and the intermediate layer has a weak bond and expands and contracts.
It can be brought into close contact with the molding jig 5 without making cuts. After laminating the multilayer fabric 2, in order to obtain surface smoothness, a Laher cassob 3 in the shape of a radar dome 1 is placed over the laminated surface, and the surface is further covered with a plastic film 4. The resin is hardened by pressure heating using a pressure heating device such as a crepe to form the radome 1.
上記により、レーダドームは織物の切断部位、重ね合せ
部位がないため、電気的.強度的に優れたレーダドーム
となり、又表面が平滑で外観的にも良好なレーダドーム
が得られた。As a result of the above, the radar dome does not have any cutting or overlapping parts of the fabric, so it is electrically sensitive. A radar dome with excellent strength and a smooth surface and good appearance was obtained.
上記多層織物を用いたレーダドームの他の実施例を第4
図に示す。Another example of the radar dome using the above multilayer fabric is shown in the fourth example.
As shown in the figure.
第4図に示す本実施例においては、アウタスキン7とイ
ンナスキン8はエボキシ樹脂等が含浸され積層された上
記多層織物により形成され、上記アウタスキン7とイン
ナスキン8の間には−iにコア9と称される低密度材料
がはさみ込まれており、いわゆるサンドインチ構造のレ
ーダドームである。このレーダドームについても第1図
に示す上記一実施例と同様に製作することが可能であり
、同様の効果がある。In the present embodiment shown in FIG. 4, the outer skin 7 and the inner skin 8 are formed of the multilayer fabric impregnated with epoxy resin and laminated, and between the outer skin 7 and the inner skin 8 there is a core 9 at -i. The radar dome has a so-called sand-inch structure. This radar dome can also be manufactured in the same manner as the above embodiment shown in FIG. 1, and has the same effects.
本発明のレーダドームは、多層をなす縦糸とそれぞれ一
層おきの上記縦糸の各層に主として織り込まれ複数本に
1本の割合で隣接する他の層の糸と交差し、伸縮性のあ
る多層織物を用いることによって、レーダードームは織
物のつぎ目や重ね合わせ部がないため、当該部位で発現
する電気定数の局部変化が防止でき、電波性能の向上が
図れ、更につぎ目がないため、機械的強度の向上も図る
ことができた。The radome of the present invention is made of a stretchable multilayer fabric, which is mainly woven into each layer of warp threads forming a multilayer structure, and intersects threads of other layers adjacent to each other at a ratio of one warp thread in each plurality of warp threads. By using a radar dome, there are no seams or overlapping parts of the fabric, so local changes in the electrical constant that occur in the area can be prevented, improving radio wave performance.Furthermore, since there are no seams, mechanical strength can be improved. We were also able to improve this.
第1図は本発明の一実施例の説明図、第2図は上記一実
施例に用いる多層織物の説明図、第3図は上記一実施例
に用いる多層織物の断面図、第4図は本発明の他の実施
例の説明図、第5図は従来の装置の説明図、第6図は従
来の装置の製造方法の説明図である。
1・・・レーダドーム、 2・・・多層織物、3・・・
ラバー製キャンプ、
4・・・プラスチックフィルム、
5・・・成型治具、 7・・・アウタスキン、8・・・
インナスキン、 9・・・コア。Fig. 1 is an explanatory diagram of one embodiment of the present invention, Fig. 2 is an explanatory diagram of a multilayer fabric used in the above embodiment, Fig. 3 is a sectional view of the multilayer fabric used in the above embodiment, and Fig. 4 is an explanatory diagram of the multilayer fabric used in the above embodiment. FIG. 5 is an explanatory diagram of another embodiment of the present invention, FIG. 5 is an explanatory diagram of a conventional device, and FIG. 6 is an explanatory diagram of a conventional method of manufacturing the device. 1... Radar dome, 2... Multilayer fabric, 3...
Rubber camp, 4... Plastic film, 5... Molding jig, 7... Outer skin, 8...
Inner skin, 9...core.
Claims (1)
主として織り込まれ縦糸複数本に1本の割合で縦糸の隣
接する他の層の糸と交差する横糸よりなりエポキシ樹脂
等が含浸され伸縮性を有する多層織物よりなることを特
徴とする繊維強化プラスチック製レーダドーム。It is made up of multi-layered warp threads and weft threads that are woven into each of the warp threads every other layer and intersect with the threads of other layers adjacent to the warp threads at a ratio of one warp thread to every other warp thread.It is impregnated with an epoxy resin and has elasticity. 1. A fiber-reinforced plastic radome characterized by being made of a multi-layered fabric.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP1112099A JP2500317B2 (en) | 1989-05-02 | 1989-05-02 | Fiber reinforced plastic radome |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP1112099A JP2500317B2 (en) | 1989-05-02 | 1989-05-02 | Fiber reinforced plastic radome |
Publications (2)
Publication Number | Publication Date |
---|---|
JPH02291703A true JPH02291703A (en) | 1990-12-03 |
JP2500317B2 JP2500317B2 (en) | 1996-05-29 |
Family
ID=14578104
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP1112099A Expired - Lifetime JP2500317B2 (en) | 1989-05-02 | 1989-05-02 | Fiber reinforced plastic radome |
Country Status (1)
Country | Link |
---|---|
JP (1) | JP2500317B2 (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2007296767A (en) * | 2006-05-01 | 2007-11-15 | Mitsubishi Heavy Ind Ltd | Molding method of structural member made of composite material and structural member made of composite material |
JP2010053479A (en) * | 2008-08-28 | 2010-03-11 | Mitsubishi Electric Corp | Fiber-reinforced woven cloth and radome using the same |
JP2010246929A (en) * | 2001-07-23 | 2010-11-04 | Daiwa:Kk | Carpet |
JP2011093329A (en) * | 2011-02-16 | 2011-05-12 | Mitsubishi Heavy Ind Ltd | Method for molding structural member formed of composite material |
JP2011135223A (en) * | 2009-12-22 | 2011-07-07 | Kawasaki Heavy Ind Ltd | Radome for flying object |
JP2013504471A (en) * | 2009-09-09 | 2013-02-07 | エアロバイロメント,インコーポレイテッド | System and apparatus for a remotely operated unmanned aerial vehicle report suppression launcher having a portable RF transmissive launcher |
CN113799418A (en) * | 2021-08-23 | 2021-12-17 | 厦门大学 | Preparation method of intelligent composite material bolt, composite material bolt and use method |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103828124A (en) * | 2011-09-12 | 2014-05-28 | 帝斯曼知识产权资产管理有限公司 | Composite radome wall |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS6083826A (en) * | 1983-10-14 | 1985-05-13 | Mitsubishi Electric Corp | Preparation of frp redome |
-
1989
- 1989-05-02 JP JP1112099A patent/JP2500317B2/en not_active Expired - Lifetime
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS6083826A (en) * | 1983-10-14 | 1985-05-13 | Mitsubishi Electric Corp | Preparation of frp redome |
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2010246929A (en) * | 2001-07-23 | 2010-11-04 | Daiwa:Kk | Carpet |
JP2007296767A (en) * | 2006-05-01 | 2007-11-15 | Mitsubishi Heavy Ind Ltd | Molding method of structural member made of composite material and structural member made of composite material |
JP2010053479A (en) * | 2008-08-28 | 2010-03-11 | Mitsubishi Electric Corp | Fiber-reinforced woven cloth and radome using the same |
US10703506B2 (en) | 2009-09-09 | 2020-07-07 | Aerovironment, Inc. | Systems and devices for remotely operated unmanned aerial vehicle report-suppressing launcher with portable RF transparent launch tube |
JP2013504471A (en) * | 2009-09-09 | 2013-02-07 | エアロバイロメント,インコーポレイテッド | System and apparatus for a remotely operated unmanned aerial vehicle report suppression launcher having a portable RF transmissive launcher |
US9187184B2 (en) | 2009-09-09 | 2015-11-17 | Aerovironment, Inc. | Systems and devices for remotely operated unmanned aerial vehicle report-suppressing launcher with portable rf transparent launch tube |
US10124909B2 (en) | 2009-09-09 | 2018-11-13 | Aerovironment, Inc. | Systems and devices for remotely operated unmanned aerial vehicle report-suppressing launcher with portable RF transparent launch tube |
US10450089B2 (en) | 2009-09-09 | 2019-10-22 | Aerovironment, Inc. | Systems and devices for remotely operated unmanned aerial vehicle report-suppressing launcher with portable RF transparent launch tube |
US11319087B2 (en) | 2009-09-09 | 2022-05-03 | Aerovironment, Inc. | Systems and devices for remotely operated unmanned aerial vehicle report-suppressing launcher with portable RF transparent launch tube |
US11731784B2 (en) | 2009-09-09 | 2023-08-22 | Aerovironment, Inc. | Systems and devices for remotely operated unmanned aerial vehicle report-suppressing launcher with portable RF transparent launch tube |
JP2011135223A (en) * | 2009-12-22 | 2011-07-07 | Kawasaki Heavy Ind Ltd | Radome for flying object |
JP2011093329A (en) * | 2011-02-16 | 2011-05-12 | Mitsubishi Heavy Ind Ltd | Method for molding structural member formed of composite material |
CN113799418A (en) * | 2021-08-23 | 2021-12-17 | 厦门大学 | Preparation method of intelligent composite material bolt, composite material bolt and use method |
CN113799418B (en) * | 2021-08-23 | 2022-10-21 | 厦门大学 | Preparation method of intelligent composite material bolt, composite material bolt and use method |
Also Published As
Publication number | Publication date |
---|---|
JP2500317B2 (en) | 1996-05-29 |
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