JP6567530B2 - フライホイール格納アセンブリのための管状格納パーツおよびそれを製造するための方法 - Google Patents
フライホイール格納アセンブリのための管状格納パーツおよびそれを製造するための方法 Download PDFInfo
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Description
構造材料の第一層のための鋼鉄ストリップを選択する工程であって、ここで、鋼鉄は、低合金高強度鋼、ベイナイト鋼、TWIP鋼グレード、および中から高炭素鋼から成る群より選択される工程、
1つ以上の連続した層の各々のための材料のストリップまたはウェブを、アルミニウム、アルミニウム合金、繊維材料、および合金鋼から成る材料の群より選択する工程、ならびに
第一層および1つ以上の連続した層のストリップをらせん状に巻いて、そのようにして形成された管状格納パーツの内側壁が、第一層の構造材料によって形成されるようにする工程、
を含む。
図面では、構造材料の最内第一層2を有する格納ケースの例のマンドレル1上への製造が示され、ここで、第一構造層は、適切な伸び、強度、および靭性の性能を示すS900、S960、高強度ベイナイト鋼、またはその他の高炭素鋼などの高強度高靭性鋼ストリップの層である。
Claims (11)
- フライホイール格納アセンブリのための管状格納パーツであって、
前記管状格納パーツは、異なる材料の層から構成されており、
前記管状格納パーツの前記異なる材料の層は、互いの上にらせん状に巻かれた連続層であり、
前記連続層は、構造材料の第一層および1つまたは2つ以上の異なる材料から構成される1以上の連続した層を含み、
前記管状格納パーツの内側壁は、前記第一層の前記構造材料によって形成されており、
前記構造材料の前記第一層が、鋼鉄ストリップであり、
前記鋼鉄は、低合金高強度鋼、ベイナイト鋼 TWIPグレード、および中から高炭素鋼から成る群より選択され
前記1以上の連続した層が、アルミニウム、アルミニウム合金、繊維材料、および合金鋼から成る材料の群より選択される1つ以上の材料のストリップまたはウェブから作製され、
前記第一層、および前記連続した層の各々が、前記管状格納パーツの2つ以上の巻き付けターンに及んでいることを特徴とする、フライホイール格納アセンブリのための管状格納パーツ。 - 前記繊維材料が、アラミド繊維、ナイロン繊維、ガラス繊維、炭素繊維、鋼鉄繊維を含む、請求項1に記載の格納パーツ。
- 前記繊維材料が、硬化された樹脂中に埋め込まれている、請求項1または2に記載の格納パーツ。
- 繊維材料の層内において、前記繊維を、互いに対して異なる縦糸および横糸配向であるグループとして備える、請求項1〜3のいずれか一項に記載の格納パーツ。
- 前記1以上の連続した層が、波形金属を含む金属層を備える、請求項1〜4のいずれか一項に記載の格納パーツ。
- 前記波形によって形成される空隙が、相変化材料によって充填されて、破片エネルギー吸収が高められる、請求項5に記載の格納パーツ。
- 請求項1〜6のいずれか一項に記載の管状格納パーツおよび末端部材を備える、フライホイール格納アセンブリであって、
前記管状格納パーツは、前記末端部材の両側に刻まれた溝部に取り付けられる、フライホイール格納アセンブリ。 - フライホイール格納アセンブリのための管状格納パーツを製造するための方法であって、前記方法は:
構造材料の第一層のための鋼鉄ストリップを選択する工程であって、前記鋼鉄は、低合金高強度鋼、ベイナイト鋼、TWIP鋼グレード、および中から高炭素鋼から成る群より選択される工程、
1以上の連続した層の各々のための材料のストリップまたはウェブを、アルミニウム、アルミニウム合金、繊維材料、および合金鋼から成る材料の群より選択する工程、ならびに
前記第一層および前記1以上の連続した層の前記ストリップをらせん状に巻いて、こうして形成された管状格納パーツの内側壁が、前記第一層の前記構造材料によって形成されるようにする工程、
を含み、
前記第一層、および前記連続した層の各々が、前記管状格納パーツの2つ以上の巻き付けターンに及んでいる、フライホイール格納アセンブリのための管状格納パーツを製造するための方法。 - 前記1以上の連続した層の1つ以上が、硬化性樹脂で含浸された繊維材料を含み、および前記らせん状に巻かれた層が、硬化操作を受ける、請求項8に記載の方法。
- 前記硬化操作が、前記第一層および順に続く層を巻いて管状格納パーツとした後に行われる、請求項9に記載の方法。
- 前記繊維材料が、連続湿式積層プロセス(continual wet layup processes)を用いて含浸され、硬化される、請求項9または10に記載の方法。
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PCT/EP2014/002303 WO2015036088A1 (en) | 2013-09-11 | 2014-08-22 | Tubular containment part for a flywheel containment assembly and method for manufacturing same |
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EP (1) | EP3043992B1 (ja) |
JP (1) | JP6567530B2 (ja) |
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US2870236A (en) * | 1957-03-21 | 1959-01-20 | Monsanto Chemicals | Electrical devices containing alkyl beta-alkoxypropionates |
US3176618A (en) * | 1961-06-14 | 1965-04-06 | Hexcel Products Inc | Rocket motor construction and fabrication process |
US3264536A (en) * | 1964-07-20 | 1966-08-02 | Union Carbide Corp | Capacitor with a polyarylene polyether dielectric |
US3695966A (en) * | 1970-05-05 | 1972-10-03 | Frederick S Kuhns | Method of manufacturing furniture fabrication cores |
US3964341A (en) * | 1974-03-18 | 1976-06-22 | The Johns Hopkins University | Multi-ring filament rotor |
US5285699A (en) * | 1988-12-07 | 1994-02-15 | Board Of Regents, University Of Texas System | Reinforced composite flywheels and shafts |
DE4111712A1 (de) * | 1991-04-10 | 1992-10-22 | Emitec Emissionstechnologie | Elektrisch leitfaehiger wabenkoerper |
US5466503A (en) * | 1992-05-07 | 1995-11-14 | Milliken Research Corporation | Energy absorption of a high tenacity fabric during a ballistic event |
FR2748964B1 (fr) * | 1996-05-23 | 1998-08-07 | Castagner Bernard | Equipement tubulaire en materiaux composites realises par enroulement de tissus desequilibres en trame sur un mandrin compressible |
JPH10193467A (ja) | 1997-01-09 | 1998-07-28 | Sekisui Chem Co Ltd | 樹脂複合管の製造方法 |
US6044726A (en) * | 1997-06-30 | 2000-04-04 | Lockheed Martin Energy Research Corporation | Optimum rotationally symmetric shells for flywheel rotors |
US6203924B1 (en) * | 1998-02-24 | 2001-03-20 | The Regents Of The University Of Californaia | Lightweight flywheel containment |
US7111522B2 (en) | 2004-02-26 | 2006-09-26 | Honeywell International, Inc. | Energy storage flywheel system containment vessel |
CN101127465B (zh) * | 2007-07-26 | 2010-12-01 | 严密 | 磁悬浮飞轮储能系统 |
GB2469657B (en) * | 2009-04-22 | 2013-09-25 | Williams Hybrid Power Ltd | Flywheel assembly |
US8932002B2 (en) | 2010-12-03 | 2015-01-13 | Hamilton Sundstrand Corporation | Air turbine starter |
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US20160223051A1 (en) | 2016-08-04 |
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