JP2948435B2 - Method of forming composite material blade - Google Patents

Method of forming composite material blade

Info

Publication number
JP2948435B2
JP2948435B2 JP5136593A JP5136593A JP2948435B2 JP 2948435 B2 JP2948435 B2 JP 2948435B2 JP 5136593 A JP5136593 A JP 5136593A JP 5136593 A JP5136593 A JP 5136593A JP 2948435 B2 JP2948435 B2 JP 2948435B2
Authority
JP
Japan
Prior art keywords
mold
resin
molding
composite material
blade
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.)
Expired - Lifetime
Application number
JP5136593A
Other languages
Japanese (ja)
Other versions
JPH06239296A (en
Inventor
拓郎 山田
秀光 小林
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.)
JISEDAI KOKUKI KIBAN GIJUTSU KENKYUSHO KK
Original Assignee
JISEDAI KOKUKI KIBAN GIJUTSU KENKYUSHO KK
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 JISEDAI KOKUKI KIBAN GIJUTSU KENKYUSHO KK filed Critical JISEDAI KOKUKI KIBAN GIJUTSU KENKYUSHO KK
Priority to JP5136593A priority Critical patent/JP2948435B2/en
Publication of JPH06239296A publication Critical patent/JPH06239296A/en
Application granted granted Critical
Publication of JP2948435B2 publication Critical patent/JP2948435B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【産業上の利用分野】この発明は、レジンインジェクシ
ョン成形法を用いた複合材ブレードの成形方法の改良に
係り、樹脂を注入する工程途中で型の締めつけを緩めて
からさらに樹脂を注入する工程を取り入れることによ
り、金型キャビティー面を正確に転写させ、表面の微細
なひけの発生を防止して、高精度な表面形状を有する複
合材ブレードを得る成形方法に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an improvement in a method for forming a composite material blade using a resin injection molding method. The present invention relates to a molding method for accurately transferring a mold cavity surface, preventing the occurrence of fine sink marks on the surface, and obtaining a composite material blade having a highly accurate surface shape.

【0002】[0002]

【従来の技術】航空機用プロペラ・ブレード、ターボフ
ァン・ブレード、ヘリコプタ・ブレード、一般産業用回
転翼などのブレードは、従来の金属製に代えてFRP等
の複合材で製作される場合がある。複合材ブレードの成
形方法には、一般にブレードの腹面を成形する型と背面
を成形する型の間に、表面に強化繊維を取りつけたブレ
ードインサートを入れて該型を絞めつけ、熱硬化性樹脂
を注入しながら余剰の樹脂を排出口より流出させたの
ち、必要な温度に加熱しあるいはさらに所要時間保持し
て、樹脂を固化させて成形するレジンインジェクション
成形法が採用されている。
2. Description of the Related Art Blades such as propeller blades for aircraft, turbofan blades, helicopter blades, and general industrial rotor blades are sometimes made of composite materials such as FRP instead of conventional metals. In the method of molding a composite material blade, generally, a blade insert having reinforcing fibers attached to the surface is inserted between a mold for molding the abdominal surface of the blade and a mold for molding the back surface, and the mold is squeezed, and a thermosetting resin is formed. A resin injection molding method is employed in which excess resin is allowed to flow out of an outlet while being injected, and then heated to a required temperature or further maintained for a required time to solidify and mold the resin.

【0003】[0003]

【発明が解決しようとする課題】従来の成形方法では、
樹脂の注入を終わった時点と樹脂が硬化収縮する時点で
樹脂の入る容積が同じであるため、硬化収縮が発生する
と成形品表面が金型キャビティーから剥離するのでキャ
ビティー面を転写することができず、表面に微細なひけ
が発生し、外観が悪くなる問題があった。
In the conventional molding method,
Since the volume of the resin is the same at the end of the resin injection and at the time the resin cures and shrinks, when the cure shrinkage occurs, the surface of the molded product separates from the mold cavity, so the cavity surface can be transferred. However, there was a problem that fine sink marks occurred on the surface and the appearance deteriorated.

【0004】この発明は、レジンインジェクション成形
法を用いた複合材ブレードの成形方法において、金型キ
ャビティー面を正確に転写させ、表面の微細なひけの発
生を防止して、高精度な表面形状を有する複合材ブレー
ドを得る成形方法の提供を目的としている。
[0004] The present invention relates to a method of forming a composite material blade using a resin injection molding method, wherein a mold cavity surface is accurately transferred to prevent the occurrence of fine sink marks on the surface, thereby achieving a highly accurate surface shape. It is an object of the present invention to provide a forming method for obtaining a composite material blade having the following.

【0005】[0005]

【課題を解決するための手段】この発明は、ブレードの
腹面を成形する型と背面を成形する型の間に、表面に強
化繊維を取りつけたブレードインサートを入れて該型を
絞めつけ、熱硬化性樹脂を注入したのち固化させるレジ
ンインジェクション成形法を用いた複合材ブレードの成
形方法において、腹面型と背面型の合わせ面にシーラン
トを挟んで型締めし、樹脂を注入しながら余剰の樹脂を
排出口より流出させ、その後、型の締めつけを緩めてか
らさらに樹脂を注入し、注入停止後に樹脂を硬化させ型
締めを行うことを特徴とする複合材ブレードの成形方法
である。
SUMMARY OF THE INVENTION According to the present invention, a blade insert having reinforcing fibers attached to the surface thereof is inserted between a mold for molding the abdominal surface of the blade and a mold for molding the back surface thereof, and the mold is squeezed and heat-cured. In a method of forming a composite material blade using a resin injection molding method in which a reactive resin is injected and then solidified, a sealant is sandwiched between the mating surfaces of the abdominal surface type and the back type with a sealant interposed therebetween, and excess resin is discharged while injecting the resin. This is a method of forming a composite material blade, characterized in that the resin is discharged from an outlet, the mold is loosened, the resin is further injected, the resin is hardened after the injection is stopped, and the mold is clamped.

【0006】詳述すると、以下の工程を特徴としてい
る。 1)腹面型と背面型の合わせ面にシーラントを挟んで型
締めして硬化させる。 2)ブレードインサートを装填して型を締める。 3)金型と同温度に保持された熱硬化性樹脂を型内に注
入し、排出口からオーバーフローさせる。 4)型締めを隙間換算で0.1mm乃至0.5mm程度
緩める。 5)樹脂を更に注入する。 6)注入を停止し、樹脂を硬化させる。 7)型内の樹脂の圧力が低下し始める時点を含んだタイ
ミングでゆっくりと元通り型締めする。 8)硬化させる。
Specifically, the following steps are characterized. 1) The mold is clamped with a sealant between the mating surfaces of the abdominal surface type and the back type to cure. 2) Load the blade insert and tighten the mold. 3) The thermosetting resin kept at the same temperature as the mold is injected into the mold and overflows from the outlet. 4) Loosen the mold clamping by about 0.1 mm to 0.5 mm in terms of gap. 5) Inject resin further. 6) Stop the injection and cure the resin. 7) The mold is slowly re-closed at the timing including the time when the pressure of the resin in the mold starts to decrease. 8) Cure.

【0007】[0007]

【作用】この発明による複合材ブレードの成形方法の作
用を図面に基いて詳述する。図1のA,Bはこの発明に
よる複合材ブレードの成形方法の工程を示す成形用型の
断面説明図である。図2はこの発明による複合材ブレー
ドの成形方法の工程を示す成形用型の斜視説明図であ
る。成形装置の成形用型1には樹脂注入口2及び排出口
3を設けてあり、樹脂注入口2には樹脂圧送タンクから
の注入管で連結し、排出口3には導管を介して樹脂溜め
容器と連結した構成からなる。
The operation of the method for forming a composite material blade according to the present invention will be described in detail with reference to the drawings. FIGS. 1A and 1B are cross-sectional views of a molding die showing steps of a method for molding a composite material blade according to the present invention. FIG. 2 is a perspective explanatory view of a molding die showing steps of a method for molding a composite material blade according to the present invention. A resin injection port 2 and a discharge port 3 are provided in a molding die 1 of the molding apparatus. The resin injection port 2 is connected to an injection pipe from a resin pressure feeding tank, and the discharge port 3 is connected to a resin reservoir via a conduit. It is configured to be connected to a container.

【0008】まず、型1a,1bの合わせ面にシリコン
シーラント4を適量塗布し、テフロン・フィルムで覆っ
成形用型1を締めきり硬化させる。成形用型1を開い
てテフロン・フィルムを除去し、キャビティー1cに強
化繊維11で覆ったブレードインサート10を装着し
て、成形用型1を規定どうりのトルクで締め切る。樹脂
は硬化剤を主剤と混合して圧送タンクに入れ金型と同じ
温度に保持する。成形に際し、樹脂圧送タンクのピスト
ンを押しげて、タンク内の樹脂を注入管を経由して注入
口2より成形用型1内に注入する。樹脂はキャビティー
1cの壁とブレードインサート10の隙間を流れるが、
隙間は補強繊維11で充たされているので強化繊維11
に浸透するようにゆっくりと流れる。
First, an appropriate amount of a silicone sealant 4 is applied to the mating surfaces of the molds 1a and 1b, covered with a Teflon film, and the molding mold 1 is tightened and cured. The mold 1 is opened, the Teflon film is removed, the blade insert 10 covered with the reinforcing fiber 11 is mounted in the cavity 1c, and the mold 1 is closed with a specified torque. The resin is prepared by mixing a curing agent with the base material, placing the mixture in a pressure feed tank, and maintaining the same temperature as the mold. At the time of molding, the piston of the resin pressure feeding tank is pushed down, and the resin in the tank is injected into the molding die 1 from the injection port 2 via the injection pipe. The resin flows through the gap between the wall of the cavity 1c and the blade insert 10,
Since the gap is filled with the reinforcing fibers 11, the reinforcing fibers 11
Flows slowly to penetrate

【0009】上記の樹脂圧送時に、型締めを隙間換算で
0.1mm程度緩めて、注入を続け、型締めの緩みによ
り生じる容積増分を樹脂で充たす(図1のA参照)。次
いで、注入を停止し、注入口2を閉じ、排出口3を開い
たままで、硬化温度に昇温して保持する。排出管内の樹
脂が型の方へ吸い込まれる時点近傍にタイミングを合わ
せて型締めをゆっくりと進め、図1のBに示す如く、最
終的に正規位置にまで型締めして、その後樹脂を硬化さ
せる。
At the time of the resin pressure feeding, the mold clamping is loosened by about 0.1 mm in terms of a gap, the injection is continued, and the volume increment caused by the loosening of the mold clamping is filled with the resin (see FIG. 1A). Next, the injection is stopped, the injection port 2 is closed, and the discharge port 3 is kept open, and the temperature is raised to the curing temperature and held. The mold clamping is slowly advanced in time with the timing at which the resin in the discharge pipe is sucked into the mold, and finally the mold is clamped to a proper position as shown in FIG. 1B, and then the resin is cured. .

【0010】この発明において、型の合わせ面に介在さ
せるシリコンシーラント4は型を緩めた時に合わせ面に
できる隙間を埋め、ここを樹脂が優先的に流れてしまう
のを防止している。また、ブレードインサートへの樹脂
の含浸は残留気泡等困難な問題を有するため、まず正規
位置に締め切った状態で含浸を完了させて、欠陥の発生
を防止している。さらに、樹脂は主剤に硬化剤を混合済
みのものを圧送タンクで型の温度と同じになるまで温め
て保持することにより、型内全域で硬化が同時進行し
て、型の締めこみの効果が全域に及ぶようにしている。
型の締め込みはゆっくりと行うことにより粘度の上昇し
た樹脂を大きな反力を発生させることなく流動させ、余
剰の樹脂の排出を図っている。従って、樹脂を注入する
工程途中で型の締めつけを緩めてからさらに樹脂を注入
する工程を取り入れることにより、型締めの緩みにより
生じる容積増分を樹脂で充たすことができ、金型キャビ
ティー面を正確に転写させ、表面の微細なひけの発生を
防止して、高精度な表面形状を有する複合材ブレードを
得ることができる。
In the present invention, the silicone sealant 4 interposed between the mating surfaces of the molds fills gaps formed in the mating surfaces when the mold is loosened, thereby preventing the resin from flowing preferentially there. In addition, impregnation of the resin into the blade insert has a difficult problem such as residual air bubbles. Therefore, impregnation is first completed in a state where the blade insert is closed at a regular position, thereby preventing generation of defects. In addition, the resin is pre-mixed with a curing agent and heated and held in the pressure feed tank until the temperature becomes the same as that of the mold. It covers the whole area.
By slowly tightening the mold, the resin whose viscosity has increased is caused to flow without generating a large reaction force, thereby discharging excess resin. Therefore, by loosening the mold during the resin injection process and introducing the resin injection process further, the volume increase caused by the loose mold can be filled with the resin, and the mold cavity surface can be accurately measured. The composite material blade having a highly accurate surface shape can be obtained by preventing the occurrence of fine sink marks on the surface.

【0011】[0011]

【実施例】図2に示す上述のこの発明による成形装置を
用いて、強化繊維に炭素繊維、樹脂にエポキシ樹脂を用
いて複合材ブレードの成形を行った。この際に、成形用
型のキャビティー面には予め鏡面仕上げを施しておき、
樹脂を注入する工程途中で型の締めつけを緩めてからさ
らに樹脂を注入し、型締めの緩みにより生じる容積増分
を樹脂で充たしたのち、型の締め込みをはゆっくりと行
い、その後樹脂を硬化させた。成形を完了した複合材ブ
レードは、その表層部に微細ひけの発生が全くなく、ま
た表面形状は鏡面仕上げと同等の精度で成形されている
ことを確認した。
EXAMPLE Using a molding apparatus according to the present invention described above and shown in FIG. 2, a composite material blade was molded using carbon fiber as the reinforcing fiber and epoxy resin as the resin. At this time, the cavity surface of the mold is mirror-finished in advance,
After loosening the mold in the process of injecting the resin, inject more resin, fill the volume increase caused by loosening of the mold with the resin, tighten the mold slowly, then cure the resin Was. It was confirmed that the composite material blade which had been formed had no fine sink marks on its surface layer, and that the surface shape was formed with the same precision as mirror finish.

【0012】[0012]

【発明の効果】この発明は、ブレードの腹面を成形する
型と背面を成形する型の間に、表面に強化繊維を取りつ
けたブレードインサートを入れて該型を絞めつけ、熱硬
化性樹脂を注入したのち固化させるレジンインジェクシ
ョン成形法を用いた複合材ブレードの成形方法におい
て、腹面型と背面型の合わせ面にシーラントを挟んで型
締めし、樹脂を注入する工程途中で型の締めつけを緩め
てからさらに樹脂を注入し、ブレード成形品表面の微細
ひけ部に樹脂を補給できるので型の良好な転写性が得ら
れ、型内面を美麗な鏡面に仕上げておけば、成形品の表
面もこれに倣わせることができるという利点があり、高
精度な表面形状を有する複合材ブレードを得ることがで
きる。
According to the present invention, a blade insert having reinforcing fibers attached to the surface is inserted between a mold for molding the abdominal surface of the blade and a mold for molding the back surface, the mold is squeezed, and a thermosetting resin is injected. Then, in the method of molding a composite material blade using the resin injection molding method of solidifying, the mold is clamped with a sealant between the mating surface of the abdominal mold and the back mold, and the mold is loosened during the resin injection process. In addition, resin can be injected and resin can be replenished to the fine sink marks on the blade molded product surface, so good mold transferability can be obtained.If the inner surface of the mold is finished to a beautiful mirror surface, the surface of the molded product will follow this There is an advantage that it is possible to obtain a composite material blade having a highly accurate surface shape.

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

【図1】A,Bはこの発明による複合材ブレードの成形
方法の工程を示す成形用型の断面説明図である。
FIGS. 1A and 1B are cross-sectional explanatory views of a molding die showing steps of a method for molding a composite material blade according to the present invention.

【図2】この発明による複合材ブレードの成形方法の工
程を示す成形用型の斜視説明図である。
FIG. 2 is a perspective explanatory view of a molding die showing steps of a method of molding a composite material blade according to the present invention.

【符号の説明】[Explanation of symbols]

1 成形用型 1a,1b 型 1c キャビティー 2 注入口 3 排出口 4 シリコンシーラント 10 ブレードインサート 11 強化繊維 DESCRIPTION OF SYMBOLS 1 Mold 1a, 1b Mold 1c Cavity 2 Inlet 3 Outlet 4 Silicon sealant 10 Blade insert 11 Reinforcing fiber

───────────────────────────────────────────────────── フロントページの続き (58)調査した分野(Int.Cl.6,DB名) B64C 11/20 B64C 3/24 ──────────────────────────────────────────────────続 き Continued on the front page (58) Field surveyed (Int.Cl. 6 , DB name) B64C 11/20 B64C 3/24

Claims (1)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】 ブレードの腹面を成形する型と背面を成
形する型の間に、表面に強化繊維を取りつけたブレード
インサートを入れて該型を絞めつけ、熱硬化性樹脂を注
入したのち固化させるレジンインジェクション成形法を
用いた複合材ブレードの成形方法において、腹面型と背
面型の合わせ面にシーラントを挟んで型締めし、樹脂を
注入しながら余剰の樹脂を排出口より流出させ、その
後、型の締めつけを緩めてからさらに樹脂を注入し、注
入停止後に樹脂を硬化させ型締めを行うことを特徴とす
る複合材ブレードの成形方法。
1. A blade insert having reinforcing fibers attached to the surface thereof is inserted between a mold for molding the abdominal surface of the blade and a mold for molding the back surface, the mold is squeezed, and the thermosetting resin is injected and solidified. In the molding method of the composite material blade using the resin injection molding method, the mold is clamped with a sealant interposed between the mating surfaces of the abdominal mold and the back mold, and excess resin is allowed to flow out from the discharge port while injecting the resin, and then the mold is formed. A method of molding a composite material blade, in which the resin is further poured after loosening the resin, and after the injection is stopped, the resin is cured and the mold is clamped.
JP5136593A 1993-02-16 1993-02-16 Method of forming composite material blade Expired - Lifetime JP2948435B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP5136593A JP2948435B2 (en) 1993-02-16 1993-02-16 Method of forming composite material blade

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP5136593A JP2948435B2 (en) 1993-02-16 1993-02-16 Method of forming composite material blade

Publications (2)

Publication Number Publication Date
JPH06239296A JPH06239296A (en) 1994-08-30
JP2948435B2 true JP2948435B2 (en) 1999-09-13

Family

ID=12884922

Family Applications (1)

Application Number Title Priority Date Filing Date
JP5136593A Expired - Lifetime JP2948435B2 (en) 1993-02-16 1993-02-16 Method of forming composite material blade

Country Status (1)

Country Link
JP (1) JP2948435B2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20180031392A (en) * 2016-09-20 2018-03-28 다이텍연구원 Process Of Producing High―Tenacity Brading Tube Fraim Using Carbon Tow Fiber Prepreg

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20180031392A (en) * 2016-09-20 2018-03-28 다이텍연구원 Process Of Producing High―Tenacity Brading Tube Fraim Using Carbon Tow Fiber Prepreg

Also Published As

Publication number Publication date
JPH06239296A (en) 1994-08-30

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