JPH01309402A - Antenna laminated in composite member - Google Patents
Antenna laminated in composite memberInfo
- Publication number
- JPH01309402A JPH01309402A JP481888A JP481888A JPH01309402A JP H01309402 A JPH01309402 A JP H01309402A JP 481888 A JP481888 A JP 481888A JP 481888 A JP481888 A JP 481888A JP H01309402 A JPH01309402 A JP H01309402A
- Authority
- JP
- Japan
- Prior art keywords
- antenna element
- aircraft
- composite member
- glass cloth
- cloth layer
- 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.)
- Pending
Links
- 239000002131 composite material Substances 0.000 title claims abstract description 18
- 239000011888 foil Substances 0.000 claims abstract description 9
- 229910052751 metal Inorganic materials 0.000 claims description 9
- 239000002184 metal Substances 0.000 claims description 9
- 239000004744 fabric Substances 0.000 abstract description 8
- 239000011521 glass Substances 0.000 abstract description 7
- 229910052782 aluminium Inorganic materials 0.000 abstract description 5
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 abstract description 5
- 230000006866 deterioration Effects 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/36—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like adapted to receive antennas or radomes
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (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、例えば航空機及び車両等に適用される複合材
中に積層されたアンテナに関する。DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to an antenna laminated in a composite material, which is applied to, for example, aircraft and vehicles.
航空機及び車両においては、近年複合材で製作された部
分にアンテナを組込むことがよく行なわれるが、この場
合従来はアンテナエレメントとして、アルミニウム等の
金属を用い、これを複合材で製作された部分の外面に貼
り付けていた。In recent years, it has become common for aircraft and vehicles to incorporate antennas into parts made of composite materials.In this case, conventionally, metals such as aluminum were used as the antenna element, and this was used as a part of the parts made of composite materials. It was attached to the outside.
従来の複合材部分の外面に貼り付けられたアンテナは航
空機等の外観を損ない商品価値を低下させ、また重量増
加となり、経年劣化しやすかった。Conventional antennas attached to the outer surface of composite parts spoil the appearance of aircraft, reduce commercial value, increase weight, and are prone to deterioration over time.
ある。be.
本発明は、航空機等の一部を構成する外側の複合材と内
側の複合材の間に金属箔または金属メツシュよりなるア
ンテナエレメントを備えた。The present invention includes an antenna element made of metal foil or metal mesh between an outer composite material and an inner composite material that constitute a part of an aircraft or the like.
上記において、アンテナエレメントは外側の複合材によ
ってお＼われ、外部に露出し２ていない。In the above, the antenna element is covered by an outer composite material and is not exposed to the outside.
上記により、アンテナエレメントは外部に露出していな
いため航空機等の外観を損なうことがなくなり、徒だア
ンテナエレメントは外側の複合材によって支持され保護
されるため重量が軽減され、経年劣化も殆んどしなくな
った。As a result of the above, the antenna element is not exposed to the outside, so it does not spoil the appearance of the aircraft, etc., and the useless antenna element is supported and protected by the outer composite material, reducing its weight, and almost no deterioration over time. I no longer do it.
不発明の一実施例を第１図および第２図に示す。 An embodiment of the invention is shown in FIGS. 1 and 2.
第１図および第２図に示す本実施例は、航空機の外板Ｃ
に取付けられだバルジＡ前方の複合アルミ箔製のアンテ
ナエレメント１を備えており、同アンテナエレメント１
は図示しでいないアンテナ給電線が接続されている。The present embodiment shown in FIG. 1 and FIG.
It is equipped with an antenna element 1 made of composite aluminum foil in front of the bulge A, which is attached to the antenna element 1.
is connected to an antenna feed line (not shown).
上記において、アンテナエレメント１は外側のカラスク
ロス層２によっておＸわれ、外部に露出していない。In the above, the antenna element 1 is covered by the outer crow cloth layer 2 and is not exposed to the outside.
上記により、アンテナエレメント１は、外部に露出して
いないため航空機の外観を損なうことがなくなり、また
アンテナエレメント１は外側のガラスクロス１−２によ
って支持され保護されるため重量が軽減され、経年劣化
も殆んどしなくなった。As a result of the above, the antenna element 1 is not exposed to the outside, so it does not spoil the appearance of the aircraft, and the antenna element 1 is supported and protected by the outer glass cloth 1-2, so its weight is reduced and it deteriorates over time. I almost no longer do it.
なお上記不実施例の製作には、成形用木型上に外１ｊ１
１１のガラスクロス層２を形成させた後、所定の形状に
切断されたアルミ箔を展張し、更にその上に内０！Ｉｆ
のガラスクロス層３を二層に成形させる。まだ、本実施
例ではアンテナエレメントとじてアルミ箔を用いている
が、他の金属になる金属箔または金属メッシュとするこ
ともできる。In addition, to manufacture the above-mentioned non-example, place 1j1 on the wooden mold for molding.
After forming the glass cloth layer 2 of No. 11, aluminum foil cut into a predetermined shape is spread, and furthermore, U0! If
The glass cloth layer 3 is formed into two layers. In this embodiment, aluminum foil is used to close the antenna element, but other metal foil or metal mesh may also be used.
本発明は、航空機等の一部を構成する外側の複合側と内
側の複合材の間に金属箔寸だは金属メツシュよりなるア
ンテナエレメントを配設することによって、航空機等の
外的を損なうことがなくなり、重量が軽減され、まだ経
年劣化も殆んどしなくなった。The present invention prevents damage to the exterior of an aircraft, etc. by disposing an antenna element made of metal foil or metal mesh between the outer composite side and the inner composite material that constitute a part of the aircraft, etc. The weight has been reduced, and there is almost no deterioration over time.
第１図は本発明の一実施例の説明図、第２図は第１図の
■−■矢視図である。
１・・・アンテナエレメント、
２．３・・・ガラスクロス層。FIG. 1 is an explanatory diagram of an embodiment of the present invention, and FIG. 2 is a view taken along arrows -■ in FIG. 1... Antenna element, 2.3... Glass cloth layer.
Claims (1)
の間に金属箔または金属メッシュよりなるアンテナエレ
メントを備えたことを特徴とする複合材中に積層された
アンテナ。An antenna laminated in a composite material, characterized in that an antenna element made of metal foil or metal mesh is provided between an outer composite material and an inner composite material constituting a part of an aircraft or the like.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP481888A JPH01309402A (en) | 1988-01-14 | 1988-01-14 | Antenna laminated in composite member |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP481888A JPH01309402A (en) | 1988-01-14 | 1988-01-14 | Antenna laminated in composite member |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH01309402A true JPH01309402A (en) | 1989-12-13 |
Family
ID=11594308
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP481888A Pending JPH01309402A (en) | 1988-01-14 | 1988-01-14 | Antenna laminated in composite member |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH01309402A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2009542523A (en) * | 2006-07-12 | 2009-12-03 | エアバス フランス | Aircraft front leg storage compartment |
-
1988
- 1988-01-14 JP JP481888A patent/JPH01309402A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2009542523A (en) * | 2006-07-12 | 2009-12-03 | エアバス フランス | Aircraft front leg storage compartment |
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