WO2014133636A3 - Hybrid continuous fiber chopped fiber polymer composite structure - Google Patents
Hybrid continuous fiber chopped fiber polymer composite structure Download PDFInfo
- Publication number
- WO2014133636A3 WO2014133636A3 PCT/US2013/074992 US2013074992W WO2014133636A3 WO 2014133636 A3 WO2014133636 A3 WO 2014133636A3 US 2013074992 W US2013074992 W US 2013074992W WO 2014133636 A3 WO2014133636 A3 WO 2014133636A3
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- composite structure
- polymer composite
- hybrid continuous
- chopped fiber
- fiber
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—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
- B32B5/02—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 structural features of a fibrous or filamentary layer
- B32B5/024—Woven fabric
-
- 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
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/06—Fibrous reinforcements only
- B29C70/08—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
- B29C70/081—Combinations of fibres of continuous or substantial length and short fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—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
- B32B5/22—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
- 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
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/141—Shape, i.e. outer, aerodynamic form
- F01D5/142—Shape, i.e. outer, aerodynamic form of the blades of successive rotor or stator blade-rows
- F01D5/143—Contour of the outer or inner working fluid flow path wall, i.e. shroud or hub contour
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/141—Shape, i.e. outer, aerodynamic form
- F01D5/146—Shape, i.e. outer, aerodynamic form of blades with tandem configuration, split blades or slotted blades
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/282—Selecting composite materials, e.g. blades with reinforcing filaments
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/748—Machines or parts thereof not otherwise provided for
- B29L2031/7504—Turbines
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
- B32B2260/02—Composition of the impregnated, bonded or embedded layer
- B32B2260/021—Fibrous or filamentary layer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
- B32B2260/04—Impregnation, embedding, or binder material
- B32B2260/046—Synthetic resin
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/02—Synthetic macromolecular fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/02—Synthetic macromolecular fibres
- B32B2262/0276—Polyester fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/101—Glass fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/106—Carbon fibres, e.g. graphite fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/542—Shear strength
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/544—Torsion strength; Torsion stiffness
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/546—Flexural strength; Flexion stiffness
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/558—Impact strength, toughness
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2605/00—Vehicles
- B32B2605/18—Aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/02—Hub construction
- B64C11/14—Spinners
-
- 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
- F05D2250/00—Geometry
- F05D2250/20—Three-dimensional
- F05D2250/23—Three-dimensional prismatic
- F05D2250/232—Three-dimensional prismatic conical
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/603—Composites; e.g. fibre-reinforced
-
- 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
Abstract
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201380068021.0A CN104870180B (en) | 2012-12-27 | 2013-12-13 | Hybrid continuous fiber chopped fiber polymer composite structure |
CA2896684A CA2896684A1 (en) | 2012-12-27 | 2013-12-13 | Hybrid continuous fiber chopped fiber polymer composite structure |
EP13870397.0A EP2938484A2 (en) | 2012-12-27 | 2013-12-13 | Hybrid continuous fiber chopped fiber polymer composite structure |
BR112015015563A BR112015015563A2 (en) | 2012-12-27 | 2013-12-13 | aircraft engine component |
JP2015550446A JP2016511291A (en) | 2012-12-27 | 2013-12-13 | Hybrid continuous fiber-chopped fiber polymer composite structure |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/728,880 US20140186166A1 (en) | 2012-12-27 | 2012-12-27 | Hybrid Continuous Fiber Chopped Fiber Polymer Composite Structure |
US13/728,880 | 2012-12-27 |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2014133636A2 WO2014133636A2 (en) | 2014-09-04 |
WO2014133636A3 true WO2014133636A3 (en) | 2014-11-20 |
Family
ID=51017391
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US2013/074992 WO2014133636A2 (en) | 2012-12-27 | 2013-12-13 | Hybrid continuous fiber chopped fiber polymer composite structure |
Country Status (7)
Country | Link |
---|---|
US (1) | US20140186166A1 (en) |
EP (1) | EP2938484A2 (en) |
JP (1) | JP2016511291A (en) |
CN (1) | CN104870180B (en) |
BR (1) | BR112015015563A2 (en) |
CA (1) | CA2896684A1 (en) |
WO (1) | WO2014133636A2 (en) |
Families Citing this family (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2986580B1 (en) * | 2012-02-08 | 2014-02-28 | Safran | ROTOR REVOLUTION PIECE OF AERONAUTICAL TURBOMACHINE |
US20140186166A1 (en) * | 2012-12-27 | 2014-07-03 | General Electric Company | Hybrid Continuous Fiber Chopped Fiber Polymer Composite Structure |
WO2014120123A2 (en) * | 2013-01-29 | 2014-08-07 | United Technologies Corporation | Thermoplastic nosecone for a turbine engine |
US9481448B2 (en) * | 2013-03-11 | 2016-11-01 | Rolls-Royce Corporation | Aerodynamic fairings secondarily attached to nosecone |
FR3010442B1 (en) * | 2013-09-09 | 2015-10-09 | Snecma | REDUCED MONOBLOC DRAWING DISK IN WAVE FOOT, PREFERABLY FOR AIRCRAFT TURBOMACHINE BLOWER |
EP3058199B1 (en) * | 2013-10-15 | 2021-06-30 | Raytheon Technologies Corporation | Compression molded fiber reinforced fan case ice panel |
EP2915953B1 (en) * | 2014-03-03 | 2019-01-16 | Rolls-Royce Corporation | Spinner for a gas turbine engine |
US10472048B2 (en) * | 2014-12-02 | 2019-11-12 | United Technologies Corporation | Gas turbine engine spinner |
CN105298685A (en) * | 2014-12-23 | 2016-02-03 | 丁义存 | Turbofan type vehicle engine |
US9777593B2 (en) | 2015-02-23 | 2017-10-03 | General Electric Company | Hybrid metal and composite spool for rotating machinery |
CN106555675B (en) * | 2015-09-30 | 2018-07-10 | 中国航发商用航空发动机有限责任公司 | Fan inlet cone and aviation turbofan engine gas handling system |
WO2017081655A1 (en) * | 2015-11-11 | 2017-05-18 | Sabic Global Technologies B.V. | Composite-plastic hybrid engine cover and process for making the same |
US10183421B2 (en) | 2016-09-16 | 2019-01-22 | General Electric Company | Molding method |
US10583913B2 (en) * | 2017-03-14 | 2020-03-10 | General Electric Company | Stud push out mount for a turbine engine spinner assembly having a spinner push out stud joint connecting through a counterbore of a spinner bolt hole |
US10677090B2 (en) * | 2017-05-10 | 2020-06-09 | General Electric Company | Component having co-bonded composite and metal rings and method of assembling same |
US10746031B2 (en) * | 2017-07-18 | 2020-08-18 | Rolls-Royce Corporation | Annulus filler |
FR3071765B1 (en) * | 2017-10-03 | 2020-11-20 | Safran Ceram | COMPOSITE MATERIAL REALIZATION OF A FLOW MIXER LOBE STRUCTURE |
US11078839B2 (en) * | 2018-01-22 | 2021-08-03 | Rolls-Royce Corporation | Composite nosecone |
US20190285028A1 (en) * | 2018-03-16 | 2019-09-19 | Mra Systems, Llc. | Thrust reverser cascade |
EP3597928A1 (en) * | 2018-07-16 | 2020-01-22 | Rolls-Royce plc | Fan unit for a turbofan engine comprising vortex-generating elements |
US11261825B2 (en) * | 2018-09-24 | 2022-03-01 | Rohr, Inc. | Thermoplastic acoustic blocker door |
FR3089891B1 (en) * | 2018-12-18 | 2020-11-27 | Stelia Aerospace | MODULAR DASHBOARD |
US11421538B2 (en) | 2020-05-12 | 2022-08-23 | Rolls-Royce Corporation | Composite aerofoils |
US11506083B2 (en) | 2020-06-03 | 2022-11-22 | Rolls-Royce Corporalion | Composite liners for turbofan engines |
US11773732B2 (en) * | 2021-04-21 | 2023-10-03 | General Electric Company | Rotor blade with protective layer |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2008115301A2 (en) * | 2007-01-23 | 2008-09-25 | The Boeing Company | Composite laminate having a damping interlayer and method of making the same |
US20090023647A1 (en) * | 1998-07-24 | 2009-01-22 | Cardiovascular Biotherapeutics, Inc. | Method of producing biologically active human acidic fibroblast growth factor and its use in promoting angiogenesis |
US20100124494A1 (en) * | 2008-11-19 | 2010-05-20 | Graham Howarth | Integrated inlet design |
US20140186166A1 (en) * | 2012-12-27 | 2014-07-03 | General Electric Company | Hybrid Continuous Fiber Chopped Fiber Polymer Composite Structure |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4576857A (en) * | 1983-03-14 | 1986-03-18 | E. I. Du Pont De Nemours And Company | Melt-fusible polyimides |
US5252160A (en) * | 1990-11-15 | 1993-10-12 | Auto Air Composites, Inc. | Method of manufacturing a metal/composite spinner cone |
US5200252A (en) * | 1992-07-20 | 1993-04-06 | Davidson Textron Inc. | Reinforced fastening boss and method for making the same |
JP3303410B2 (en) * | 1993-04-02 | 2002-07-22 | 石川島播磨重工業株式会社 | Manufacturing method of resin parts |
JPH10166380A (en) * | 1996-12-06 | 1998-06-23 | Senshin Zairyo Riyou Gas Jienereeta Kenkyusho:Kk | Molding of resin blade part |
US6869558B2 (en) * | 1997-12-18 | 2005-03-22 | Thermoplastic Composite Designs, Inc. | Thermoplastic molding process and apparatus |
JP2002161703A (en) * | 2000-11-27 | 2002-06-07 | Mitsubishi Heavy Ind Ltd | Blade and manufacturing method of the blade |
US7070725B2 (en) * | 2003-02-25 | 2006-07-04 | Mathson Industries | Method of making part having insert assembly |
US7960674B2 (en) * | 2005-06-28 | 2011-06-14 | Hexcel Corporation | Aerospace articles made from quasi-isotropic chopped prepreg |
US20090165924A1 (en) * | 2006-11-28 | 2009-07-02 | General Electric Company | Method of manufacturing cmc articles having small complex features |
US7883737B2 (en) * | 2008-03-18 | 2011-02-08 | General Electric Company | Methods allowing for visual inspection of coated components for erosion damage |
US7897249B2 (en) * | 2008-10-07 | 2011-03-01 | The Boeing Company | Composite material structure with interlayer electrical conductance |
BR112012004110A2 (en) * | 2009-08-26 | 2016-03-15 | Bayer Materialscience Ag | fiber-reinforced polyurethane molded part with three-dimensional relief structures |
US8449260B2 (en) * | 2009-10-30 | 2013-05-28 | General Electric Company | Composite load-bearing rotating ring and process therefor |
GB201005053D0 (en) * | 2010-03-26 | 2010-05-12 | Rolls Royce Plc | A gas turbine engine nose cone |
US20120108132A1 (en) * | 2010-10-28 | 2012-05-03 | General Electric Company | Composite Compositions |
GB201020230D0 (en) * | 2010-11-30 | 2011-01-12 | Rolls Royce Plc | Nose cone assembly |
JP5844967B2 (en) * | 2010-12-13 | 2016-01-20 | 三菱レイヨン株式会社 | Fiber-reinforced thermoplastic resin molded article and method for producing the same |
-
2012
- 2012-12-27 US US13/728,880 patent/US20140186166A1/en not_active Abandoned
-
2013
- 2013-12-13 CA CA2896684A patent/CA2896684A1/en not_active Abandoned
- 2013-12-13 JP JP2015550446A patent/JP2016511291A/en active Pending
- 2013-12-13 EP EP13870397.0A patent/EP2938484A2/en not_active Withdrawn
- 2013-12-13 WO PCT/US2013/074992 patent/WO2014133636A2/en active Application Filing
- 2013-12-13 BR BR112015015563A patent/BR112015015563A2/en not_active IP Right Cessation
- 2013-12-13 CN CN201380068021.0A patent/CN104870180B/en not_active Expired - Fee Related
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20090023647A1 (en) * | 1998-07-24 | 2009-01-22 | Cardiovascular Biotherapeutics, Inc. | Method of producing biologically active human acidic fibroblast growth factor and its use in promoting angiogenesis |
WO2008115301A2 (en) * | 2007-01-23 | 2008-09-25 | The Boeing Company | Composite laminate having a damping interlayer and method of making the same |
US20100124494A1 (en) * | 2008-11-19 | 2010-05-20 | Graham Howarth | Integrated inlet design |
WO2010059301A2 (en) * | 2008-11-19 | 2010-05-27 | General Electric Company | Integrated inlet design |
US20140186166A1 (en) * | 2012-12-27 | 2014-07-03 | General Electric Company | Hybrid Continuous Fiber Chopped Fiber Polymer Composite Structure |
Also Published As
Publication number | Publication date |
---|---|
CA2896684A1 (en) | 2014-09-04 |
EP2938484A2 (en) | 2015-11-04 |
WO2014133636A2 (en) | 2014-09-04 |
CN104870180B (en) | 2017-03-22 |
BR112015015563A2 (en) | 2017-07-11 |
CN104870180A (en) | 2015-08-26 |
JP2016511291A (en) | 2016-04-14 |
US20140186166A1 (en) | 2014-07-03 |
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Legal Events
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