JPH03264356A - Method for internal repairing of parabolic antenna made of frp having honeycomb structure - Google Patents

Method for internal repairing of parabolic antenna made of frp having honeycomb structure

Info

Publication number
JPH03264356A
JPH03264356A JP2064640A JP6464090A JPH03264356A JP H03264356 A JPH03264356 A JP H03264356A JP 2064640 A JP2064640 A JP 2064640A JP 6464090 A JP6464090 A JP 6464090A JP H03264356 A JPH03264356 A JP H03264356A
Authority
JP
Japan
Prior art keywords
resin
frp
moisture
blind holes
repairing
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
Application number
JP2064640A
Other languages
Japanese (ja)
Inventor
Akio Shibata
昭男 柴田
Hiroshi Yamazaki
弘 山崎
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.)
Mitsubishi Heavy Industries Ltd
Choryo Engineering Co Ltd
Original Assignee
Mitsubishi Heavy Industries Ltd
Choryo Engineering Co Ltd
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 Mitsubishi Heavy Industries Ltd, Choryo Engineering Co Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP2064640A priority Critical patent/JPH03264356A/en
Publication of JPH03264356A publication Critical patent/JPH03264356A/en
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C73/00Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D
    • B29C73/02Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D using liquid or paste-like material
    • B29C73/025Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D using liquid or paste-like material fed under pressure
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C73/00Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D
    • B29C73/24Apparatus or accessories not otherwise provided for
    • B29C73/26Apparatus or accessories not otherwise provided for for mechanical pretreatment
    • B29C2073/268Apparatus or accessories not otherwise provided for for mechanical pretreatment for drilling holes in the area to be repaired
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00Other particular articles
    • B29L2031/60Multitubular or multicompartmented articles, e.g. honeycomb
    • B29L2031/608Honeycomb structures

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Laminated Bodies (AREA)
  • Aerials With Secondary Devices (AREA)

Abstract

PURPOSE:To easily perform repairing in low cost by making small diameter blind holes in a damaged part at two places and evacuating the blind holes to remove moisture therein and injecting a low viscosity unsaturated polyester resin or epoxy resin in the blind holes to cure the same under pressure. CONSTITUTION:At first, the surface of blind holes reaching FRP 14 are made in the surface of the FRP of a released area 22 at two places of the upper and lower end parts thereof by an electric drill and a vacuum pump 29 is operated to remove the moisture in the released area. As an injection resin for repairing, a low viscosity solventless type unsaturated polyester resin having good adhesiveness to a honeycomb structure and FRP is selected. Next, load is applied to the plunger of an injector by the hand and the vacuum pump 29 is operated to discharge the moisture in the released area to the outside through an upper end tube 24 and the released part is filled with the synthetic resin 31 for repairing. Further, an iron plate is placed on the released area as load 36 to return the dimension expanded in the thickness direction by the injection resin to the original dimension and allowed to stand overnight at room temp. to perfectly cure the resin.

Description

【発明の詳細な説明】 〔産業上の利用分野〕 本発明は、船舶、陸上のアンテナとして使用されている
ハニカム構造FRP製ノくラボラアンテナの内部補修方
法に関する。
DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to a method for repairing the interior of a honeycomb-structured FRP antenna used as an antenna on a ship or on land.

〔従来の技術〕[Conventional technology]

第3図斜視図に示すようなハニカム構造FRP製パラボ
ラ状アンテナは、屋外に露出しているので日光による紫
外線及び降雨による水分に曝され、また海上にあっては
海水からの海塩粒子等の影響を受けるので、第4図断面
図に示すように、大気に直接接触する表FiFRP11
から、水分と塩分等が次第に内部へ浸透し、その結果、
例えば上層ハニカム13とその下のFRP14の間から
一部が剥離し、空洞を生じてアンテナの機能に支障を来
たすことがある。
As the honeycomb structure FRP parabolic antenna shown in the perspective view of Figure 3 is exposed outdoors, it is exposed to ultraviolet rays from sunlight and moisture from rain, and when it is on the sea, it is exposed to sea salt particles from seawater. Therefore, as shown in the cross-sectional view in Figure 4, the table FiFRP11 that is in direct contact with the atmosphere
From there, moisture and salt gradually penetrate into the interior, and as a result,
For example, a portion of the upper honeycomb 13 and the FRP 14 below may peel off, creating a cavity and interfering with the function of the antenna.

しかしながら、現状では適当な補修方法がないため、支
障を起したものは新品と取り替えているので、例えば船
舶の場合、非常にコストが高く、また納入までに半年も
かかるという問題がある。
However, as there is currently no suitable repair method, defective items are replaced with new ones, which in the case of ships, for example, is extremely costly and takes half a year to deliver.

〔発明が解決しようとする課題〕[Problem to be solved by the invention]

これは、パラボラアンテナの内部剥離の補修には、下記
のような問題があるからである。
This is because repairing internal peeling of a parabolic antenna has the following problems.

(1)アンテナ内部の剥離箇所の範囲を外部からいかに
して確かめるか? (2)剥離箇所に水分が入っていることが多く、その水
分は接着を阻害するので、いかにしてその水分を除去す
るか? (3)剥離箇所は、−例を挙げると、第4図の上層ハニ
カム13とその下のFRP14の間が約111mの薄い
厚みであり、また横方向に広がっているため、剥離箇所
を接着させる補修用注入樹脂としては粘度が低く、また
アンテナを構成しているハニカムや FRPとの接着性が良いこと、更に、アンテナの構造上
、無溶剤型が条件となる故、このような特性の樹脂をい
かにして入手するか? (4)補修用注入樹脂をいかにして損傷部分に注入する
か? 本発明はこのような事情に鑑みて提案されたもので、低
コストで容易に修理することのできる経済的なハニカム
構造FRP製パラボラアンテナの内部補修方法を提供す
ることにある。
(1) How can we confirm the extent of the peeling inside the antenna from the outside? (2) Moisture is often present in the peeled area, and this moisture inhibits adhesion, so how can this moisture be removed? (3) The peeled area is - For example, the area between the upper layer honeycomb 13 and the FRP 14 below in Figure 4 is thin, about 111 m, and spreads laterally, so the peeled area must be bonded. As an injection resin for repairs, it has low viscosity and good adhesion to the honeycomb and FRP that make up the antenna.Furthermore, due to the structure of the antenna, a solvent-free type is required, so a resin with such characteristics is used. How do I get it? (4) How to inject repair injection resin into the damaged area? The present invention has been proposed in view of the above circumstances, and it is an object of the present invention to provide an economical method for repairing the inside of a honeycomb structure FRP parabolic antenna that can be easily repaired at low cost.

〔課題を解決するための手段〕[Means to solve the problem]

そのために本発明者は、前記各問題点をそれぞれ下記の
ような手段で解決した。
To this end, the inventors of the present invention solved each of the above-mentioned problems by the following means.

(1)  ハンマーを使用し、ハンマー打診時の発生音
によって損傷範囲を確定した。
(1) A hammer was used, and the damage area was determined by the sound produced during hammer percussion.

(2)水分乾燥用として、互いに離れた小径盲穴を2箇
所開け、次に一方の盲穴に真空ポンプを連結し、損傷部
分の真空引きによって内部の水分を吸引し、また減圧乾
燥することで、水分を除去した。
(2) For drying moisture, make two small diameter blind holes separated from each other, then connect a vacuum pump to one of the blind holes, draw a vacuum on the damaged area to suck out the moisture inside, and then dry under reduced pressure. The water was removed.

(3)実験によって、低粘度で、またハニカムとFRP
との接着性が良く、更に無溶剤型の樹脂を選定し採用し
た。
(3) Experiments have shown that with low viscosity, honeycomb and FRP
We selected a solvent-free resin that has good adhesion to the material.

(4)注入樹脂の注入方法は上記(2)で開けた2つの
盲穴を再使用し、一方の盲穴から樹脂を加圧注入すると
ともに、他方の盲穴を真空ポンプに連結し、その真空引
きによって注入速度を早め、余剰の樹脂が排出した時、
樹脂の注入を終了とした。
(4) The resin injection method reuses the two blind holes drilled in (2) above, injects the resin under pressure through one blind hole, and connects the other blind hole to a vacuum pump. The injection speed is accelerated by vacuuming, and when the excess resin is discharged,
The injection of resin was completed.

〔作用〕[Effect]

このような方法によれば、下記の作用が行われる。 According to such a method, the following effects are performed.

(1)内部損傷箇所の検査は、外部から視認することは
できないが、ハンマーでアンテナ表層を軽く叩き、その
際の発生音によって損傷範囲を判別する。この方法によ
れば、内部剥離部は打診時の発生音が良好部に比較して
低いことから、その剥離範囲が判明し、その補修範囲を
限定することができる。
(1) Although internal damage cannot be visually confirmed from the outside, the damage area can be determined by tapping the surface of the antenna with a hammer and listening to the sound generated. According to this method, since the internal peeling part generates a lower sound when percussing than the good part, the peeling range can be determined and the repair range can be limited.

(2)  アンテナを構成しているFRPII。(2) FRPII that constitutes the antenna.

工4とハニカム13.15の材質は有機系合成樹脂のポ
リエステル樹脂又はエポキシ樹脂であることから、剥離
箇所に入っている水分を除去するため、アンテナ本体を
加熱し乾燥する方法はこれらの合成樹脂の劣化を招くた
め好ましくないので、加熱に代えて常温で乾燥ができる
真空減圧による乾燥法について検討した結果、支障なく
水分の乾燥ができた。
Since the material of No. 4 and Honeycomb No. 13.15 is organic synthetic resin such as polyester resin or epoxy resin, the method of heating and drying the antenna body in order to remove the moisture that has entered the peeled area is to use these synthetic resins. Therefore, we investigated a drying method using vacuum depressurization, which allows drying at room temperature instead of heating, and as a result, we were able to dry the moisture without any problems.

(3)補修用注入樹脂がアンテナの剥離箇所、例えば第
4図に示す上層ハニカム13とその下のFRP 14の
間に注入されると、硬化後、剥離箇所の両面つまり上層
ハニカム13とその下のFRP14を全面的接着する作
用がある。
(3) When the repair injection resin is injected into the peeled part of the antenna, for example between the upper layer honeycomb 13 and the FRP 14 below it as shown in FIG. It has the effect of bonding the entire FRP 14.

(4)真空法は補修用樹脂の注入速度が速く、また充填
精度も高いことが判明した。
(4) It was found that the vacuum method allows for faster injection of repair resin and also has higher filling accuracy.

〔実施例〕〔Example〕

本発明を船舶に搭載され内部の剥離が発見されたハニカ
ム構造FRP製パラボラアンテナ(おわん形)直径2.
5mのものに適用した一実施例を図面について説明する
と、第1図は内部損傷部分の水分除去手段を示す説明図
、第2図は損傷部分への樹脂の注入手段を示す説明図で
ある。
A honeycomb structure FRP parabolic antenna (bowl shape) diameter 2.
An example applied to a 5 m long product will be explained with reference to the drawings. FIG. 1 is an explanatory diagram showing a means for removing moisture from an internally damaged part, and FIG. 2 is an explanatory diagram showing a means for injecting resin into the damaged part.

上図において、第3〜4図と同一の符番はそれぞれ第3
〜4図と同一の部材を示し、まずハンマー打診法によっ
て剥離箇所を検査した結果、剥離面積は直径が約300
mであることが判明し、また深さ方向はハンマー打診音
から、第4図に示した上層ハニカム13とその下のFR
P14の間であることも判明した。
In the above diagram, the same numbers as in Figures 3 and 4 are number 3.
~ Figure 4 shows the same member, and as a result of inspecting the peeled area using the hammer percussion method, the peeled area was approximately 300 mm in diameter.
m, and from the hammer percussion sound in the depth direction, the upper honeycomb 13 and the FR below it as shown in FIG.
It was also found that it was between P14.

次に、内部剥離部分内の水分乾燥は、第1図に示すよう
に、下記手順で行った。
Next, as shown in FIG. 1, the moisture in the inner peeled portion was dried by the following procedure.

まず、剥離箇所22について、FRP表面の上端部と下
端部の2箇所に、電気ドリルにて、第4図に示したFR
P14に達する直径5uの盲穴を開け、続いてこれらの
2箇所の盲穴に外径5flで長さ20mmのポリエチレ
ンの上端チューブ24.下端チューブ23を差し込む。
First, regarding the peeling location 22, use an electric drill to drill the FR as shown in FIG.
A blind hole with a diameter of 5u reaching P14 is made, and then a polyethylene upper end tube 24. with an outer diameter of 5 fl and a length of 20 mm is inserted into these two blind holes. Insert the lower end tube 23.

上端チューブ24と下端チューブ23はそれぞれアンテ
ナ表面から外れないようにするため市販のシリコーンシ
ーラントでその周囲をシールしたのち接着した。
The upper end tube 24 and the lower end tube 23 were each sealed with a commercially available silicone sealant around their peripheries to prevent them from coming off the antenna surface, and then bonded together.

下端チューブ23の上端には更にビニルホース25.シ
リカゲル27を入れた透明のアクリル製容器26を順次
連ぎ、透明のアクリル製容器26の上端開口はビニルホ
ース28を経て真空ポンプ29に連結したのち、真空ポ
ンプ29を稼動し、真空減圧法により剥離内の水分を除
去した。
A vinyl hose 25 is further attached to the upper end of the lower end tube 23. Transparent acrylic containers 26 filled with silica gel 27 are successively connected, and the upper end opening of the transparent acrylic containers 26 is connected to a vacuum pump 29 via a vinyl hose 28. Then, the vacuum pump 29 is operated, and the vacuum decompression method is applied. The water inside the peel was removed.

この方法によると、シリカゲル27が真空乾燥を行った
当初、青色から赤色へ変色し、アンテナ内部に水分が含
まれていることが判ったが、真空乾燥を続けることによ
り、やがてシリカゲル27を新品のものと取り替えても
赤色に変色せず、これによりアンテナ内部の水分が除去
され乾燥していることが確認された。
According to this method, when the silica gel 27 was first vacuum-dried, it changed color from blue to red, indicating that moisture was contained inside the antenna. Even after replacing it with a new one, it did not turn red, confirming that the moisture inside the antenna had been removed and it was dry.

更に、注入樹脂については、後記する試験により確認さ
れた低粘度でハニカム及びFRPとの接着性も良く、か
つ無溶剤型の不飽和ポリエステル樹脂例えばケミフレー
クプライマーP−0,5M(東洋ゴム工業■製)を選定
し、注入樹脂の注入は第2図に示す手段で、下記手順で
行った。
Furthermore, the injection resin has a low viscosity and good adhesion to honeycomb and FRP as confirmed by the tests described below, and is a solvent-free unsaturated polyester resin such as Chemiflake Primer P-0.5M (Toyo Rubber Industries ■). The injection resin was injected using the means shown in FIG. 2 in accordance with the following procedure.

まず、上端チューブ24をビニルホース28を介して、
真空ポンプ29を連結し、次に、下端チューブ23の垂
直方向にビニルホース33を介して補修用合成樹脂31
を入れた圧大器外筒32 (例えば100cc注射器)
と圧大器内筒34を連結する。次に、圧大器内筒34と
して、100 cc注射器のプランジャーに手で荷重を
加えるとともに、真空ポンプ29を稼動させることによ
り、剥離部内部の空気が上端チューブ24を経由して外
へ排出され、引き続きその跡へ補修用合成樹脂31を犀
τた。その際、補修用合成樹脂31の終了は上端チュー
ブ24から余剰の樹脂が排出されることで確認できる。
First, connect the upper end tube 24 through the vinyl hose 28,
A vacuum pump 29 is connected, and then a repair synthetic resin 31 is connected to the lower end tube 23 via a vinyl hose 33 in the vertical direction.
(e.g. 100cc syringe)
and the compressor inner cylinder 34 are connected. Next, by manually applying a load to the plunger of a 100 cc syringe as the compressor inner cylinder 34 and operating the vacuum pump 29, the air inside the peeling section is discharged to the outside via the upper end tube 24. Then, a synthetic resin 31 for repair was applied to the spot. At this time, completion of the repair synthetic resin 31 can be confirmed by the discharge of excess resin from the upper end tube 24.

更に、荷重36として20kgの鉄板、砂入の袋等を剥
離箇所の表面に乗せて、注入樹脂により膨張した厚み方
向の寸法を元の寸法に戻したのち、室温で1晩、放置す
ると完全に樹脂硬化した。なお、剥離箇所の面積が小さ
いときは、真空ポンプ29と荷重36は使用せずに修理
を行うことができる。
Furthermore, as a load 36, a 20 kg iron plate, a bag containing sand, etc. is placed on the surface of the peeled area, and after returning the dimension in the thickness direction expanded by the injected resin to its original size, the resin is completely removed by leaving it at room temperature overnight. Hardened. Note that when the area of the peeled part is small, the repair can be performed without using the vacuum pump 29 and the load 36.

室温で1晩放置後、第2図に示す荷重36を取り外し、
ハンマー打診法によって剥離部分を調査した結果、全面
とも樹脂が充填されており、本施工方法が満足すべきも
のであることが確認できた。またアンテナとしての機能
も回復していることが確認された。
After leaving it at room temperature overnight, remove the load 36 shown in Figure 2,
As a result of investigating the peeled parts using the hammer percussion method, the entire surface was filled with resin, confirming that this construction method was satisfactory. It was also confirmed that its function as an antenna had been restored.

最後に注入樹脂とアンテナ本体樹脂との接着性試験結果
について述べると、 ■、試験規格: 接着剤試験方法JISK6850に準 拠した。
Finally, the results of the adhesion test between the injected resin and the antenna body resin are as follows: (1) Test standard: Adhesive test method JIS K6850 was followed.

■、試験要領: 下記手順で、接着性試験を行った。■、Test guidelines: An adhesion test was conducted according to the following procedure.

(1)実施例で使用するFRPと同種のエポキシ樹脂(
ボンドEセント(コ ニシ■製))及びガラス繊維(平織。
(1) Epoxy resin of the same type as FRP used in the examples (
Bond E Cent (manufactured by Konishi ■)) and glass fiber (plain weave.

日東紡績#@)を使用して、巾12im×長さ100m
x厚み5mのFRP 板2枚を作製した。
Using Nitto Boseki #@), width 12im x length 100m
x Two FRP boards with a thickness of 5 m were produced.

(2)次に、片面の端面から長さ12+nの部分まで2
枚とも、注入樹脂とし て選定した不飽和ポリエステル樹脂 ケミフレークプライマーP−05M (東洋ゴム工業■製)を約0.3 m厚みに塗布し、続
いてこの塗布した2 枚を互いに貼り合せ、室温で24 Hr放装し硬化させ、せん断接着用 試験片とした。なお、試験片は3役 作製した。
(2) Next, from the end face of one side to the part of length 12 + n
Both sheets were coated with unsaturated polyester resin Chemiflake Primer P-05M (manufactured by Toyo Tire & Rubber Industries, Ltd.) selected as the injection resin to a thickness of about 0.3 m, and then the two coated sheets were pasted together and heated at room temperature. This was cured for 24 hours to obtain a shear adhesive test piece. Note that three test pieces were prepared.

■、試験結果: (3)引張速度5 tm / 5hinで引張試験機(
島津オートグラフS−500)に よるせん断接着力を測定した結果、 10kgf/ad、  l 2kgf/ci、  I 
3kgf/cdの値が得られ、良好な接着性を示した。
■, Test results: (3) Tensile testing machine (with tensile speed 5tm/5hin)
The results of measuring the shear adhesive force using Shimadzu Autograph S-500) were: 10 kgf/ad, l 2 kgf/ci, I
A value of 3 kgf/cd was obtained, indicating good adhesion.

   ゛ 〔発明の効果〕 従来は、新品への取り替えは非常に高価であるのみな−
らず、納期が数か月必要であったが、本発明による補修
方法により数日間で補修ができ、またその補修費用も新
品の価格の数%台と安価であり、アンテナの機能も十分
に回復できた。
[Effect of the invention] Conventionally, replacing with a new product was extremely expensive.
However, with the repair method of the present invention, the repair can be done in a few days, and the repair cost is only a few percent of the new price, and the antenna functions sufficiently. I was able to recover.

要するに本発明によれば、まず、ハニカム構造FRP製
パラボラアンテナの内部の一部が剥がれた破損部分の互
いに離れた2箇所にそれぞれ小径盲穴を開け、一方の盲
穴から真空引きにより破損部分内部の水分乾燥を行い、
次にこの盲穴から補修用樹脂として低粘度の不飽和ポリ
エステル樹脂又はエポキシ樹脂を注入するとともに、他
方の盲穴から上記樹脂の流出を確認後、内部に充填され
た樹脂が硬化するまで上記アンテナの反射面を原反射面
と同一面となるように加圧することにより、低コストで
容易に修理することのできる経済的なハニカム構造FR
P製パラボラアンテナの内部補修方法を得るから、本発
明は産業上極めて有益なものである。
In short, according to the present invention, first, small-diameter blind holes are made in two separate locations in a damaged part of a honeycomb structure FRP parabolic antenna where a part of the inside has peeled off, and vacuum is drawn from one blind hole to inside the damaged part. The water is dried,
Next, inject a low-viscosity unsaturated polyester resin or epoxy resin as a repair resin through this blind hole, and after confirming that the resin has flowed out from the other blind hole, wait until the resin filled inside is cured. An economical honeycomb structure FR that can be easily repaired at low cost by applying pressure so that the reflective surface is flush with the original reflective surface.
The present invention is extremely useful industrially because it provides a method for repairing the inside of a parabolic antenna made of P.

【図面の簡単な説明】[Brief explanation of drawings]

第1図は本発明を船舶用パラボラアンテナに適用した一
実施例における内部損傷部の水分除去手段を示す説明図
、第2図は損傷部分への樹脂の注入手段を示す説明図で
ある。 第3図は公知のパラボラ状アンテナの全体斜視図、第4
図は第3図のパラボラ状アンテナ(おわん形〉の断面を
示す部分拡大図である。 10・・・方向可変用支持枠、11・・・表層FRP、
12・・・受発信用ワイヤ、13・・・上層ハニカム、
14・・・FRP、15・・・下層ハニカム、21・・
・アンテナ本体、22・・・アンテナ内部の剥離箇所、
23・・・下端チューブ、24・・・上端チューブ、2
5・・・ビニルホース、26・・・アクリル製容器、2
7・・・シリカゲル、28・・・ビニルホース、29・
・・真空ポンプ、31・・・補修用合成樹脂、32・・
・圧入器外筒、33・・・ビニルホース、34・・・圧
入器内筒、35・・・加圧手段、36・・・荷重。
FIG. 1 is an explanatory view showing means for removing moisture from an internally damaged part in an embodiment in which the present invention is applied to a parabolic antenna for ships, and FIG. 2 is an explanatory view showing means for injecting resin into the damaged part. Figure 3 is an overall perspective view of a known parabolic antenna;
The figure is a partially enlarged view showing a cross section of the parabolic antenna (bowl-shaped) shown in Fig. 3. 10... Direction variable support frame, 11... Surface layer FRP,
12... Wire for receiving and transmitting, 13... Upper layer honeycomb,
14...FRP, 15...Lower honeycomb, 21...
・Antenna body, 22...Peeling part inside the antenna,
23...Lower end tube, 24...Upper end tube, 2
5... Vinyl hose, 26... Acrylic container, 2
7...Silica gel, 28...Vinyl hose, 29.
...Vacuum pump, 31...Synthetic resin for repair, 32...
- Press fitter outer cylinder, 33... Vinyl hose, 34... Press fitter inner cylinder, 35... Pressurizing means, 36... Load.

Claims (1)

【特許請求の範囲】 まず、ハニカム構造FRP製パラボラアン テナの内部の一部が剥がれた破損部分の互いに離れた2
箇所にそれぞれ小径盲穴を開け、一方の盲穴から真空引
きにより破損部分内部の水分乾燥を行い、次にこの盲穴
から補修用樹脂として低粘度の不飽和ポリエステル樹脂
又はエポキシ樹脂を注入するとともに、他方の盲穴から
上記樹脂の流出を確認後、内部に充填された樹脂が硬化
するまで上記アンテナの反射面を原反射面と同一面とな
るように加圧することを特徴とするハニカム構造FRP
製パラボラアンテナの内部補修方法。
[Claims] First, two parts of the damaged part of the honeycomb structure FRP parabolic antenna separated from each other are separated from each other.
A small diameter blind hole is made in each location, and the water inside the damaged part is dried by vacuuming through one blind hole. Next, a low viscosity unsaturated polyester resin or epoxy resin is injected as a repair resin through this blind hole. , after confirming the outflow of the resin from the other blind hole, pressurization is applied so that the reflective surface of the antenna becomes flush with the original reflective surface until the resin filled inside is cured.
How to repair the inside of a manufactured parabolic antenna.
JP2064640A 1990-03-15 1990-03-15 Method for internal repairing of parabolic antenna made of frp having honeycomb structure Pending JPH03264356A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2064640A JPH03264356A (en) 1990-03-15 1990-03-15 Method for internal repairing of parabolic antenna made of frp having honeycomb structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2064640A JPH03264356A (en) 1990-03-15 1990-03-15 Method for internal repairing of parabolic antenna made of frp having honeycomb structure

Publications (1)

Publication Number Publication Date
JPH03264356A true JPH03264356A (en) 1991-11-25

Family

ID=13264071

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2064640A Pending JPH03264356A (en) 1990-03-15 1990-03-15 Method for internal repairing of parabolic antenna made of frp having honeycomb structure

Country Status (1)

Country Link
JP (1) JPH03264356A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0839635A1 (en) * 1996-11-01 1998-05-06 British Aerospace Public Limited Company Repair of composite laminates
JP2006187897A (en) * 2005-01-04 2006-07-20 Fuji Heavy Ind Ltd Defective part repairing method of composite material
JP2006305750A (en) * 2005-04-26 2006-11-09 Fuji Heavy Ind Ltd Reinforcing method of honeycomb sandwich panel and repairing method of honeycomb sandwich panel
JP2009512570A (en) * 2005-09-29 2009-03-26 エアバス・フランス Method for penetration repair of a composite structure with three skins and two core layers
JP2012175638A (en) * 2011-02-24 2012-09-10 Mitsubishi Electric Corp Manufacturing method of antenna reflector, and antenna reflector
US9387636B2 (en) 2013-03-28 2016-07-12 Mitsubishi Aircraft Corporation Method and apparatus for repairing honeycomb core sandwich panel

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0839635A1 (en) * 1996-11-01 1998-05-06 British Aerospace Public Limited Company Repair of composite laminates
JP2006187897A (en) * 2005-01-04 2006-07-20 Fuji Heavy Ind Ltd Defective part repairing method of composite material
JP2006305750A (en) * 2005-04-26 2006-11-09 Fuji Heavy Ind Ltd Reinforcing method of honeycomb sandwich panel and repairing method of honeycomb sandwich panel
JP2009512570A (en) * 2005-09-29 2009-03-26 エアバス・フランス Method for penetration repair of a composite structure with three skins and two core layers
JP2012175638A (en) * 2011-02-24 2012-09-10 Mitsubishi Electric Corp Manufacturing method of antenna reflector, and antenna reflector
US9387636B2 (en) 2013-03-28 2016-07-12 Mitsubishi Aircraft Corporation Method and apparatus for repairing honeycomb core sandwich panel

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