JP2014524373A - パネル及びそのための処理法 - Google Patents
パネル及びそのための処理法 Download PDFInfo
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- JP2014524373A JP2014524373A JP2014526061A JP2014526061A JP2014524373A JP 2014524373 A JP2014524373 A JP 2014524373A JP 2014526061 A JP2014526061 A JP 2014526061A JP 2014526061 A JP2014526061 A JP 2014526061A JP 2014524373 A JP2014524373 A JP 2014524373A
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- JP
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- Prior art keywords
- panel
- processing method
- preform
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- abradable
- 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.)
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C44/00—Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles
- B29C44/02—Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles for articles of definite length, i.e. discrete articles
- B29C44/04—Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles for articles of definite length, i.e. discrete articles consisting of at least two parts of chemically or physically different materials, e.g. having different densities
- B29C44/0446—Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles for articles of definite length, i.e. discrete articles consisting of at least two parts of chemically or physically different materials, e.g. having different densities by increasing the density locally by compressing part of the foam while still in the mould
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C44/00—Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles
- B29C44/02—Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles for articles of definite length, i.e. discrete articles
- B29C44/08—Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles for articles of definite length, i.e. discrete articles using several expanding or moulding steps
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C44/00—Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles
- B29C44/34—Auxiliary operations
- B29C44/3484—Stopping the foaming reaction until the material is heated or re-heated
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C44/00—Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles
- B29C44/34—Auxiliary operations
- B29C44/36—Feeding the material to be shaped
- B29C44/46—Feeding the material to be shaped into an open space or onto moving surfaces, i.e. to make articles of indefinite length
- B29C44/50—Feeding the material to be shaped into an open space or onto moving surfaces, i.e. to make articles of indefinite length using pressure difference, e.g. by extrusion or by spraying
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C48/00—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
- B29C48/001—Combinations of extrusion moulding with other shaping operations
- B29C48/0011—Combinations of extrusion moulding with other shaping operations combined with compression moulding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C48/00—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
- B29C48/001—Combinations of extrusion moulding with other shaping operations
- B29C48/0012—Combinations of extrusion moulding with other shaping operations combined with shaping by internal pressure generated in the material, e.g. foaming
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
- F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
- F01D11/122—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part with erodable or abradable material
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
- F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
- F01D11/122—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part with erodable or abradable material
- F01D11/125—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part with erodable or abradable material with a reinforcing structure
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
- F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29B—PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
- B29B11/00—Making preforms
- B29B11/06—Making preforms by moulding the material
- B29B11/10—Extrusion moulding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C48/00—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
- B29C48/03—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor characterised by the shape of the extruded material at extrusion
- B29C48/07—Flat, e.g. panels
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2280/00—Materials; Properties thereof
- F05B2280/40—Organic materials
- F05B2280/4007—Thermoplastics
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
- F05C2225/00—Synthetic polymers, e.g. plastics; Rubber
- F05C2225/08—Thermoplastics
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/20—Manufacture essentially without removing material
- F05D2230/23—Manufacture essentially without removing material by permanently joining parts together
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/4932—Turbomachine making
Abstract
【選択図】図1
Description
12 シュラウドアセンブリ
13 回転可能ブレード
13A 半径方向ギャップ
14 プロファイルド表面
16 支持構造
18 ボンドライン
20 反対表面
22 第1密度ゾーン
24 第2密度ゾーン
26 円周方向ライン
30 押出機システム
32 押出機
34 押出ダイ
36 液体混合タンク
38 個別送達システム
40 個別送達システム
42 ホッパ
44 ホッパ
46 機械デバイス
48 真空ポンプ
50 連続フォーム(押出形成体)
52 コンベア
54 プレス装置
56 モールド
58 モールド半体
60 モールドキャビティ
62 プレフォーム
62A 薄い区画
62B 厚い区画
64 モールド
66 キャビティ
68 モールド半体
70A 領域
70B 領域
72 リブ
74 フローチャンネル
Claims (20)
- パネルを製作するための処理法であって、
膨張可能発泡材料の構成素材を部分硬化済み調合済み高分子材料とするように連続式に調合する連続形成装置内に膨張可能発泡材料の構成素材を導入する工程と、
連続形成装置の連続形成方向に対する横断方向で一定の断面形状を有する連続フォームが製作されるように連続形成装置によって調合済み高分子材料を連続的に形成する工程と、
プレフォームが製作されるように連続フォームの一部分を変形する工程と、さらに
プレフォームの膨張及びパネルの製作をさせるようにプレフォームを制限体積内部で硬化させる工程と、
を含む処理法。 - 前記プレフォームは連続フォームと異なる断面形状を有する、請求項1に記載の処理法。
- 前記制限体積によってパネルのゾーンに対して異なる密度を有させている、請求項1に記載の処理法。
- 前記制限体積によってパネルのゾーンに対して異なる密度及び厚さを有させている、請求項1に記載の処理法。
- 前記連続形成装置は押出装置である、請求項1に記載の処理法。
- 前記膨張可能発泡材料の構成素材は押出装置の内部で組み合わされる液体と固体の構成素材から成る、請求項5に記載の処理法。
- 前記変形工程はモールド内で実行されている、請求項1に記載の処理法。
- 前記硬化工程はモールド内で実行されておりかつ前記制限体積はモールド内部のモールドキャビティである、請求項1に記載の処理法。
- 前記パネルはアブレイダブルパネルである、請求項1に記載の処理法。
- アブレイダブルパネルをターボファンエンジンのファン区画内にシュラウドアセンブリの一部として据え付ける工程をさらに含む請求項9に記載の処理法。
- 請求項1に記載の処理法によって製作されたパネル。
- ターボファンエンジンのファン区画内にアブレイダブルシールを形成するために一体に組み上げるように適合させたアブレイダブルパネルを製作するための処理法であって、
膨張可能発泡材料の構成素材を部分硬化済み調合済み高分子材料とするように連続式に調合する押出装置内に膨張可能発泡材料の構成素材を導入する工程と、
押出装置の連続形成方向に対する横断方向で一定の断面形状を有する連続フォームが製作されるように押出装置によって調合済み高分子材料を連続的に形成する工程と、
連続フォームと異なる断面形状を有するプレフォームが製作されるように連続フォームの一部分を変形する工程と、さらに
パネルの少なくとも2つのゾーンに異なる密度を有させるような制限体積内部でプレフォームの膨張及びパネルの製作をさせるようにプレフォームを硬化させる工程と、
を含む処理法。 - 前記制限体積によってパネルのゾーンに対して異なる密度及び厚さを有させている、請求項12に記載の処理法。
- 前記膨張可能発泡材料の構成素材は押出装置の内部で組み合わされる液体と固体の構成素材から成る、請求項12に記載の処理法。
- 前記変形工程はモールド内で実行されている、請求項12に記載の処理法。
- 前記硬化工程はモールド内で実行されておりかつ前記制限体積はモールド内部のモールドキャビティである、請求項12に記載の処理法。
- 前記モールドキャビティは、プレフォームのより薄い区画がプレフォームのより厚い区画と比べてより大きく膨張するようなサイズ設定とし、その結果としてパネルのより薄い区画から製作された第1のゾーンにパネルのより厚い区画から製作された第2のゾーンと比べてより低い密度を有させている、請求項16に記載の処理法。
- 前記膨張可能発泡材料の構成素材はエポキシ樹脂系、ポリブタジエン、少なくとも1つのファイバ材料及び少なくとも1つの起泡剤から成る、請求項12に記載の処理法。
- アブレイダブルパネルをターボファンエンジンのファン区画内にシュラウドアセンブリの一部として据え付ける工程をさらに含む請求項12に記載の処理法。
- 請求項12に記載の処理法によって製作されたパネル。
Applications Claiming Priority (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201161524218P | 2011-08-16 | 2011-08-16 | |
US61/524,218 | 2011-08-16 | ||
US13/334,616 US9421703B2 (en) | 2011-08-16 | 2011-12-22 | Panels and processes therefor |
US13/334,616 | 2011-12-22 | ||
PCT/US2012/049688 WO2013025385A1 (en) | 2011-08-16 | 2012-08-06 | Panels and processes therefor |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2014524373A true JP2014524373A (ja) | 2014-09-22 |
JP6085602B2 JP6085602B2 (ja) | 2017-02-22 |
Family
ID=47711572
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2014526061A Expired - Fee Related JP6085602B2 (ja) | 2011-08-16 | 2012-08-06 | パネル及びそのための処理法 |
Country Status (7)
Country | Link |
---|---|
US (1) | US9421703B2 (ja) |
EP (1) | EP2744637A1 (ja) |
JP (1) | JP6085602B2 (ja) |
CN (1) | CN104039523B (ja) |
CA (1) | CA2844624A1 (ja) |
DE (1) | DE112012003380T5 (ja) |
WO (1) | WO2013025385A1 (ja) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2014120117A1 (en) * | 2013-01-29 | 2014-08-07 | United Technologies Corporation | Blade rub material |
US10612407B2 (en) | 2013-02-28 | 2020-04-07 | United Technologies Corporation | Contoured blade outer air seal for a gas turbine engine |
US10036402B2 (en) * | 2014-05-14 | 2018-07-31 | United Technologies Corporation | Max phase reinforced polymer matrix composite abradables with enhanced thermal conductivity |
FR3100561B1 (fr) * | 2019-09-10 | 2023-01-20 | Safran Aircraft Engines | Fixation d’une virole acoustique a une enveloppe de carter pour une turbomachine d’aeronef |
US11970978B2 (en) | 2021-06-25 | 2024-04-30 | Rohr, Inc. | Acoustic panel and method of forming same |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5388959A (en) * | 1993-08-23 | 1995-02-14 | General Electric Company | Seal including a non-metallic abradable material |
JPH10100182A (ja) * | 1996-10-01 | 1998-04-21 | Tosoh Corp | ポリオレフィン樹脂ブロック状発泡体およびその製造方法 |
JP2003094473A (ja) * | 2001-09-20 | 2003-04-03 | Araco Corp | 発泡部を備えるプレス成形体の製造方法 |
JP2011042731A (ja) * | 2009-08-20 | 2011-03-03 | Nitto Denko Corp | 充填用発泡組成物および充填発泡部材 |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4478552A (en) | 1982-11-08 | 1984-10-23 | Thompson Stanley E | Method and apparatus for fan blade tip clearance |
JPH04135829A (ja) | 1990-09-28 | 1992-05-11 | Kansei Corp | 樹脂製品の成形法 |
US5660901A (en) | 1991-04-30 | 1997-08-26 | Dexter Corporation | Oriented expanded molded products |
US5234757A (en) | 1991-04-30 | 1993-08-10 | The Dexter Corporation | Expandable films and molded products therefrom |
US5401154A (en) * | 1993-05-26 | 1995-03-28 | Continental Structural Plastics, Inc. | Apparatus for compounding a fiber reinforced thermoplastic material and forming parts therefrom |
US5783272A (en) | 1993-08-10 | 1998-07-21 | Dexter Corporation | Expandable films and molded products therefrom |
US5665295A (en) * | 1994-08-04 | 1997-09-09 | Teijin Limited | Process for the production of composite molded article |
JP4135829B2 (ja) | 1998-10-22 | 2008-08-20 | コマツ工機株式会社 | インターナルクランクシャフトミラーのカッタ交換装置及びカッタ交換方法 |
JP4181278B2 (ja) | 1999-07-02 | 2008-11-12 | 株式会社ネオックスラボ | 中空構造物における中空室遮断具とその製造方法 |
IT1320370B1 (it) * | 2000-05-26 | 2003-11-26 | San Valeriano S P A | Pannello termoformato e procedimento per la sua produzione. |
WO2006060722A2 (en) | 2004-12-02 | 2006-06-08 | Panterra Engineered Plastics, Inc. | A method and apparatus for continuously producing discrete expanded thermoformable materials |
EP2202264B1 (fr) | 2008-12-24 | 2018-04-18 | Safran Aero Boosters SA | Procédé de fabrication par moulage d'un élément structurel de machine avec une surface abradable |
-
2011
- 2011-12-22 US US13/334,616 patent/US9421703B2/en active Active
-
2012
- 2012-08-06 CA CA2844624A patent/CA2844624A1/en not_active Abandoned
- 2012-08-06 DE DE112012003380.9T patent/DE112012003380T5/de not_active Withdrawn
- 2012-08-06 EP EP12746248.9A patent/EP2744637A1/en not_active Withdrawn
- 2012-08-06 JP JP2014526061A patent/JP6085602B2/ja not_active Expired - Fee Related
- 2012-08-06 CN CN201280039753.2A patent/CN104039523B/zh not_active Expired - Fee Related
- 2012-08-06 WO PCT/US2012/049688 patent/WO2013025385A1/en active Application Filing
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5388959A (en) * | 1993-08-23 | 1995-02-14 | General Electric Company | Seal including a non-metallic abradable material |
JPH10100182A (ja) * | 1996-10-01 | 1998-04-21 | Tosoh Corp | ポリオレフィン樹脂ブロック状発泡体およびその製造方法 |
JP2003094473A (ja) * | 2001-09-20 | 2003-04-03 | Araco Corp | 発泡部を備えるプレス成形体の製造方法 |
JP2011042731A (ja) * | 2009-08-20 | 2011-03-03 | Nitto Denko Corp | 充填用発泡組成物および充填発泡部材 |
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JP6085602B2 (ja) | 2017-02-22 |
US20130042475A1 (en) | 2013-02-21 |
EP2744637A1 (en) | 2014-06-25 |
DE112012003380T5 (de) | 2014-05-08 |
CA2844624A1 (en) | 2013-02-21 |
CN104039523A (zh) | 2014-09-10 |
US9421703B2 (en) | 2016-08-23 |
CN104039523B (zh) | 2017-06-09 |
WO2013025385A1 (en) | 2013-02-21 |
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