JP7161989B2 - 保護フィルム - Google Patents
保護フィルム Download PDFInfo
- Publication number
- JP7161989B2 JP7161989B2 JP2019516473A JP2019516473A JP7161989B2 JP 7161989 B2 JP7161989 B2 JP 7161989B2 JP 2019516473 A JP2019516473 A JP 2019516473A JP 2019516473 A JP2019516473 A JP 2019516473A JP 7161989 B2 JP7161989 B2 JP 7161989B2
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- JP
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- Prior art keywords
- protective film
- carrier layer
- carrier
- fibers
- layer
- Prior art date
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Images
Classifications
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- B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
- B32B5/26—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
- B32B5/275—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary characterised by one woven fabric layer next to a non-woven fabric layer
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- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08K—Use of inorganic or non-macromolecular organic substances as compounding ingredients
- C08K3/00—Use of inorganic substances as compounding ingredients
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- C—CHEMISTRY; METALLURGY
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- C—CHEMISTRY; METALLURGY
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- C08K—Use of inorganic or non-macromolecular organic substances as compounding ingredients
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Description
本明細書で使用する場合、
「不織」は、機械的、化学的、熱的、又は溶媒手段及びこれらの組み合わせによって達成される、繊維の結合若しくは連結、又はその両方によって製造されるテキスタイル構造を指し;
「織物」は、少なくとも2組のストランドが、通常は互いに直角に、所定のインターレースパターンに従って、かつ少なくとも1組は布地の長手方向に沿う軸に平行になるように織り合わされたときに作製される構造を指し;
「z軸」は、保護フィルムの平面に対して垂直な方向を指す。
例示的な保護フィルムが図1に示されており、本明細書において、符号100により表されている。保護フィルム100は、多層化されており、互いに反対側にある第1及び第2の主表面104、106を有する導電体102を含む。導体102は、第1のキャリア層112と第2のキャリア層114の間に配置される。選択した実施形態において、第1及び第2のキャリア層112、114は繊維質である。ここに示すように、第1及び第2のキャリア層112、114はそれぞれ織物材料を含む。
上記のように、提供された保護フィルムは、1つ以上の導体を含む。導体は、任意の好適な導電性材料、典型的には金属で作製され得る。一例として、導体は、保護フィルムが屈曲して非平面状の表面になじむことができる十分に薄い金属箔であってもよい。
本明細書に開示される保護フィルムは、導電性である1つ以上のキャリア層を含む。導電性を提供するため、本明細書に開示されるキャリア層は、複数の導電性繊維を含み得る。いくつかの実施形態では、導電性繊維は、導電性材料を均一に含む。代替的な実施形態では、導電性繊維は、非導電性繊維材料上に配置された導電性外層を含む。
有用な硬質化可能な組成物としては、硬化性熱硬化組成物が挙げられる。本明細書で使用する場合、「硬化性熱硬化組成物」は、架橋反応を起こすことができる化合物を指す。適切な開始剤及び/又は触媒を硬化性熱硬化組成物に含めることで、組成物が、例えば、加熱又は化学線(例えば、可視光又は紫外光)照射時に架橋できるようにすることができる。
任意に、保護フィルムは、好ましくは導電性である個別の部位を示す表面を含んでもよい。
°F:華氏温度
℃:摂氏温度
cm:センチメートル
gsm:グラム毎平方センチメートル
mg:ミリグラム
mil:10-3インチ
μm:マイクロメートル
mm:ミリメートル
mOhms/□:ミリオーム/スクエア
kPa:キロパスカル
psi:ポンド/平方インチ
rpm:毎分回転数
体積%:体積パーセント
重量%:重量パーセント
CCGF:導電性コーティングされたガラスフレーク、商品名「CONDUCT-O-FIL SG15F35」でPotters Industries(Valley Forge,Pennsylvania)から入手。
CG-1400:ジシアンジアミド、商品名「AMICURE CG-1400」でAir Products and Chemicals,Incorporated(Allentown,Pennsylvania)から入手可能。
CNC:8gsmの銅-ニッケル-炭素不織スクリム、商品名「20444A」でTechnical Fibre Products,LLC(Newburgh,New York)から入手。
DER-330:低粘度液体エポキシ樹脂は、エピクロロヒドリンとビスフェノールAとの反応生成物であり、商品名「D.E.R.330」でDow Chemical Company(Midland,Michigan)から入手。
DER-6508:イソシアネート変性2官能性エポキシ樹脂、商品名「DER-6508」でDow Chemical Companyから入手。
DF-1:高分子、非シリコーンの流動添加剤、商品名「DYNOADD F-1」でDynea Oy(Helsinki,Finland)から入手可能。
ECF:57~175gsmのエキスパンド銅箔、商品名「AEROMESH」でBenmetal GmbH(Seigen,Germany)から入手。
EPON SU-8:約8の平均エポキシド基官能性を有するエポキシノボラック樹脂、商品名「EPON SU-8」でMomentive Specialty Chemicals(Houston,Texas)から入手可能。
GL-104:104gsmのガラスクロス、JPS Composite Materials Corporation(Anderson,South Carolina)から入手。
MEK:メチルエチルケトン
MPK:メチルプロピルケトン
MX-257:濃度37%のコアシェルゴム強靭化剤をビスフェノールAベースの液体エポキシ樹脂に配合、商品名「MX-257」としてKaneka North America,LLC.から入手可能。
MY-9634:多官能エポキシ樹脂、商品名「ARALDITE MY-9634」でHuntsman Corporation(Woodlands,Texas)から入手可能。
OPT-10:10gsmのガラススクリム、商品名「OPTIMAT 20103A」でTechnical Fibre Products,LLCから入手可能。
P2353U:一方向エポキシプリプレグ、商品名「TORAY P2353U 19 152」でToray Industries,Inc.から入手可能。
PCDI:35:60:5重量部のポリカルボジイミド:MEK:シクロヘキサノン
PG-7:銅-フタロシアニン顔料、商品名「VYNAMON GREEN 600734」でHeucotech Ltd.(Fairless Hills,Pennsylvania)から入手可能。
RA-95:ビスフェノールAエポキシ樹脂変性カルボキシル末端ブタジエン-アクリロニトリルエラストマー、商品名「HYPOX RA-95」でCVC Specialty Chemicals Inc.(Moorestown,New Jersey)から入手可能。
R-960:ルチル二酸化チタン顔料、商品名「TI-PURE R-960」でE.I.du DuPont de Nemours and Company(Wilmington,Delaware)から入手可能。
SD-3:変性ヘクトライト粘土、商品名「BENTONE SD-3」でElementis Specialities(Hightown,New Jersey)から入手可能。
TS-720:処理済みヒュームドシリカ、商品名「CAB-O-SIL TS-720」でCabot Corporation(Billerica,Massachusetts)から入手可能。
U-52:芳香族置換尿素(4,4’-メチレンビス(フェニルジメチル尿素)、商品名「OMICURE U-52」でCVC Specialty Chemicals Inc.(Moorestown,New Jersey)から入手可能。
ミルベース
70°F(21.1℃)の温度で、14.32グラムのDER-330、0.77グラムのSD-3、0.47グラムのPG-7、2.33グラムのR-960、4.40グラムのCG-1400及び0.23グラムのU-52を、遊星ミル(モデル「SPEED MIXER DA 400 FV」、Synergy Devices Limited(Buckinghamshire,United Kingdom)から入手可能)で使用するために設計されたプラスチックカップに入れた。このカップを遊星ミキサー内に配置し、2分間、2200rpmで混合した。この混合物を3ロールミルに3回かけて、脇に置いておいた。
12.99グラムのMX-257、3.05グラムのMY-9634、0.67グラムのDF-1、4.328グラムのRA-95、1.48グラムのTS-720、16.06グラムのミルベース、0.6グラムのDF-1及び5.7グラムのPCDIをカップに添加した。混合物を遊星ミキサーに戻し、混合を2,000rpmで更に1分間継続した。混合物を手動で掻き取って遊星ミルに戻し、全ての成分が均一に分散されるまで約1分間混合した。
50グラムのAC-1に32.0グラムのCCGF及び11.4グラムのMEKを添加した。混合物を遊星ミキサーに戻し、混合を2,000rpmで更に1分間継続した。混合物を手動で掻き取って遊星ミルに戻し、全ての成分が均一に分散されるまで約1分間混合した。導電性コーティングされたガラスフレークの濃度は38顔料体積%であった。
CCGF及びMEKの量をそれぞれ39.0グラム及び13.0グラムに増やして、AC-2調製の手順を繰り返した。導電性コーティングされたガラスフレークの濃度は43顔料体積%であった。
CCGF及びMEKの量をそれぞれ39.0グラム及び13.0グラムに増やして、AC-2調製の手順を繰り返した。導電性コーティングされたガラスフレークの濃度は48顔料体積%であった。
AC-1の調製に関して全般的に記載した手順を、CNCスクリムをOPT-10及びGL-104ガラススクリムで置き換えて、繰り返した。
Claims (12)
- 複数の導電性金属化繊維を含む第1のキャリア層;
10マイクロメートルから40マイクロメートルの厚さを有する有孔金属箔を含む金属層;及び
複数の導電性金属化繊維を含む第2のキャリア層、という順序で複数の層を含み、前記第1及び第2のキャリア層のそれぞれが、硬質化可能な組成物で少なくとも部分的に充填された空隙体積を有し、
それによってz軸方向に沿って導電性を示す、保護フィルム。 - 複数の繊維を含む第3のキャリア層と、
複数の繊維を含む第4のキャリア層と、を更に含み、前記第1のキャリア層、金属層、及び第2のキャリア層は、集合的に前記第3のキャリア層と第4のキャリア層との間に介在し、前記第3及び第4のキャリア層のそれぞれが、硬質化可能な組成物で少なくとも部分的に充填された空隙体積を有する、請求項1に記載の保護フィルム。 - 10マイクロメートルから40マイクロメートルの厚さを有する有孔金属箔を含む第1の金属層;
複数の導電性金属化繊維を含むキャリア層;及び
10マイクロメートルから40マイクロメートルの厚さを有する有孔金属箔を含む第2の金属層、という順序で複数の層を含み、前記キャリア層が硬質化可能な組成物で少なくとも部分的に充填されており、
それによってz軸方向に沿って導電性を示す、保護フィルム。 - 前記有孔金属箔がエキスパンドメタル箔を含む、請求項1~3のいずれか一項に記載の保護フィルム。
- 1つ以上の金属層が、硬質化可能な組成物で少なくとも部分的に充填された空隙体積を有する、請求項1~4のいずれか一項に記載の保護フィルム。
- 1つ以上のキャリア層が、織物材料、不織材料、又は複数の連続繊維を含む、請求項1~5のいずれか一項に記載の保護フィルム。
- 前記第1及び第2のキャリア層が織物材料を含み、前記第3及び第4のキャリア層が不織材料を含む、請求項2に記載の保護フィルム。
- 少なくとも1つのキャリア層が、金属コーティングされているガラス、炭素、ナイロン、又はポリエステル繊維を含む、請求項1~7のいずれか一項に記載の保護フィルム。
- 各硬質化可能な組成物がエポキシ樹脂を含む、請求項1~8のいずれか一項に記載の保護フィルム。
- 前記キャリア層及び前記金属層のうちの1つ以上が、熱可塑性ポリマーで少なくとも部分的に充填されている、請求項1~9のいずれか一項に記載の保護フィルム。
- 前記熱可塑性ポリマーが、ポリフッ化ビニリデン、テトラフルオロエチレン-ヘキサフルオロプロピレン-フッ化ビニリデン、ヘキサフルオロプロピレン-テトラフルオロエチレン-エチレンフルオロエラストマー、ポリウレタン、ポリエーテルエーテルケトン又はこれらの組み合わせから選択される、請求項10に記載の保護フィルム。
- 結合又は硬化の前に、炭素繊維複合材又はガラス繊維複合材上に配置された請求項1~11のいずれか一項に記載の保護フィルムを含む、プリプレグ物品。
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US20210367416A1 (en) | 2018-06-07 | 2021-11-25 | 3M Innovative Properties Company | Lightning strike protection film |
CN113195215B (zh) | 2018-12-21 | 2024-01-19 | 3M创新有限公司 | 纤维增强复合材料铺设 |
KR20210126586A (ko) * | 2019-02-13 | 2021-10-20 | 세키스이가가쿠 고교가부시키가이샤 | 적층 시트 |
FR3106774A1 (fr) * | 2020-02-05 | 2021-08-06 | Airbus Operations (S.A.S.) | Procédé de fabrication d’une pièce en matériau composite comportant au moins une étape de détection de morceaux de film de protection |
US11504925B2 (en) | 2020-06-18 | 2022-11-22 | Spirit Aerosystems, Inc. | Lightning strike protection surfacer and method of manufacturing the same |
KR102516090B1 (ko) * | 2021-05-13 | 2023-04-03 | 한국항공우주산업 주식회사 | 낙뢰 보호 기능이 적용된 복합재 및 그 제조방법 |
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- 2017-09-25 EP EP17784726.6A patent/EP3519176A1/en active Pending
- 2017-09-25 WO PCT/US2017/053202 patent/WO2018063970A1/en unknown
- 2017-09-25 US US16/323,486 patent/US11745468B2/en active Active
- 2017-09-25 CN CN201780058302.6A patent/CN109789662A/zh active Pending
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EP3519176A1 (en) | 2019-08-07 |
JP2019534809A (ja) | 2019-12-05 |
BR112019005772A2 (pt) | 2019-06-11 |
US11745468B2 (en) | 2023-09-05 |
US20210283883A1 (en) | 2021-09-16 |
WO2018063970A1 (en) | 2018-04-05 |
CN109789662A (zh) | 2019-05-21 |
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