JP7199940B2 - 複合材料製航空機用部品およびその製造方法 - Google Patents
複合材料製航空機用部品およびその製造方法 Download PDFInfo
- Publication number
- JP7199940B2 JP7199940B2 JP2018226503A JP2018226503A JP7199940B2 JP 7199940 B2 JP7199940 B2 JP 7199940B2 JP 2018226503 A JP2018226503 A JP 2018226503A JP 2018226503 A JP2018226503 A JP 2018226503A JP 7199940 B2 JP7199940 B2 JP 7199940B2
- Authority
- JP
- Japan
- Prior art keywords
- composite material
- laminate
- aircraft
- manufacturing
- reinforcing fibers
- 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.)
- Active
Links
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
- B29D99/00—Subject matter not provided for in other groups of this subclass
- B29D99/0003—Producing profiled members, e.g. beams
-
- 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
- B29C70/28—Shaping operations therefor
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
- B29C70/34—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
- B29C70/342—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation using isostatic pressure
-
- 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
- B29C70/28—Shaping operations therefor
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
- B29C70/46—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/061—Frames
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/064—Stringers; Longerons
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2307/00—Use of elements other than metals as reinforcement
- B29K2307/04—Carbon
-
- 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
- B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
- B29L2031/3076—Aircrafts
- B29L2031/3082—Fuselages
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C2001/0054—Fuselage structures substantially made from particular materials
- B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
-
- 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
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Transportation (AREA)
- Moulding By Coating Moulds (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
Priority Applications (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2018226503A JP7199940B2 (ja) | 2018-12-03 | 2018-12-03 | 複合材料製航空機用部品およびその製造方法 |
| PCT/JP2019/046789 WO2020116343A1 (ja) | 2018-12-03 | 2019-11-29 | 複合材料製航空機用部品およびその製造方法 |
| EP19893392.1A EP3892549A4 (en) | 2018-12-03 | 2019-11-29 | AIRCRAFT COMPONENT MADE OF COMPOSITE MATERIAL AND PROCESS FOR THEIR MANUFACTURE |
| US17/337,416 US12168525B2 (en) | 2018-12-03 | 2021-06-03 | Composite-material aircraft part and method of manufacturing same |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2018226503A JP7199940B2 (ja) | 2018-12-03 | 2018-12-03 | 複合材料製航空機用部品およびその製造方法 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2020090110A JP2020090110A (ja) | 2020-06-11 |
| JP2020090110A5 JP2020090110A5 (enExample) | 2022-01-06 |
| JP7199940B2 true JP7199940B2 (ja) | 2023-01-06 |
Family
ID=70975121
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2018226503A Active JP7199940B2 (ja) | 2018-12-03 | 2018-12-03 | 複合材料製航空機用部品およびその製造方法 |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US12168525B2 (enExample) |
| EP (1) | EP3892549A4 (enExample) |
| JP (1) | JP7199940B2 (enExample) |
| WO (1) | WO2020116343A1 (enExample) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP7149151B2 (ja) | 2018-10-03 | 2022-10-06 | 川崎重工業株式会社 | 複合材料製航空機用部品およびその製造方法 |
| JP7240559B2 (ja) | 2020-03-31 | 2023-03-15 | 川崎重工業株式会社 | 航空機部品の中間生成品の製造方法および航空機部品 |
| JP2021183586A (ja) | 2020-05-22 | 2021-12-02 | 武田薬品工業株式会社 | 複素環化合物 |
| CN119928300B (zh) * | 2023-11-03 | 2025-11-21 | 上海交通大学 | 碳纤维复合材料无人机螺旋桨组件与机身翼肋一体成型结构及工艺 |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2010023449A (ja) | 2008-07-24 | 2010-02-04 | Toray Ind Inc | 繊維強化プラスチックの製造方法 |
| JP2015143007A (ja) | 2013-12-03 | 2015-08-06 | ザ・ボーイング・カンパニーTheBoeing Company | ハイブリッド積層体及び成形複合構造体 |
| WO2016043156A1 (ja) | 2014-09-19 | 2016-03-24 | 東レ株式会社 | 切込プリプレグおよび切込プリプレグシート |
| JP2016508900A (ja) | 2013-01-07 | 2016-03-24 | ザ・ボーイング・カンパニーTheBoeing Company | 輪郭に合致した積層構造体を製作するための方法及び装置 |
| JP2017008258A (ja) | 2015-06-25 | 2017-01-12 | 三菱レイヨン株式会社 | 繊維強化複合材料 |
| US20170129207A1 (en) | 2014-07-03 | 2017-05-11 | Saab Ab | A composite article having multifunctional properties and method for its manufacture |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9278484B2 (en) * | 2008-04-17 | 2016-03-08 | The Boeing Company | Method and apparatus for producing contoured composite structures and structures produced thereby |
| CN104918770A (zh) * | 2012-12-19 | 2015-09-16 | 法孚机械加工系统股份有限公司 | 用于模制三维部件的工序 |
| FR3020780B1 (fr) | 2014-05-09 | 2017-01-13 | Airbus Operations Sas | Procede de fabrication d'une piece en materiau composite pour structure d'aeronef par pultrusion et cocuisson |
| US10596778B2 (en) * | 2015-04-13 | 2020-03-24 | Howard E. Crawford, III | Fiber-reinforced composite material |
| WO2017159567A1 (ja) * | 2016-03-16 | 2017-09-21 | 東レ株式会社 | 繊維強化プラスチックの製造方法および繊維強化プラスチック |
-
2018
- 2018-12-03 JP JP2018226503A patent/JP7199940B2/ja active Active
-
2019
- 2019-11-29 EP EP19893392.1A patent/EP3892549A4/en not_active Withdrawn
- 2019-11-29 WO PCT/JP2019/046789 patent/WO2020116343A1/ja not_active Ceased
-
2021
- 2021-06-03 US US17/337,416 patent/US12168525B2/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2010023449A (ja) | 2008-07-24 | 2010-02-04 | Toray Ind Inc | 繊維強化プラスチックの製造方法 |
| JP2016508900A (ja) | 2013-01-07 | 2016-03-24 | ザ・ボーイング・カンパニーTheBoeing Company | 輪郭に合致した積層構造体を製作するための方法及び装置 |
| JP2015143007A (ja) | 2013-12-03 | 2015-08-06 | ザ・ボーイング・カンパニーTheBoeing Company | ハイブリッド積層体及び成形複合構造体 |
| US20170129207A1 (en) | 2014-07-03 | 2017-05-11 | Saab Ab | A composite article having multifunctional properties and method for its manufacture |
| WO2016043156A1 (ja) | 2014-09-19 | 2016-03-24 | 東レ株式会社 | 切込プリプレグおよび切込プリプレグシート |
| JP2017008258A (ja) | 2015-06-25 | 2017-01-12 | 三菱レイヨン株式会社 | 繊維強化複合材料 |
Also Published As
| Publication number | Publication date |
|---|---|
| JP2020090110A (ja) | 2020-06-11 |
| US20210284317A1 (en) | 2021-09-16 |
| WO2020116343A1 (ja) | 2020-06-11 |
| EP3892549A4 (en) | 2022-08-17 |
| US12168525B2 (en) | 2024-12-17 |
| EP3892549A1 (en) | 2021-10-13 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JP7149151B2 (ja) | 複合材料製航空機用部品およびその製造方法 | |
| JP7199940B2 (ja) | 複合材料製航空機用部品およびその製造方法 | |
| EP2477799B1 (en) | Method of molding complex composite parts using pre-plied multi-directional continuous fiber laminate | |
| RU2697451C2 (ru) | Способ изготовления композитного изделия | |
| CA2693812C (en) | A method of manufacturing a curved element made of composite material | |
| RU2686894C2 (ru) | Изготовление пропитанной смолой цельной композитной фермовой конструкции | |
| JP2673566B2 (ja) | 複雑な複合材料物品を形成するための半ば剛固な工具及び方法 | |
| US20170274621A1 (en) | Fabrication of Composite Laminates Using Temporarily Stitched Preforms | |
| AU2005232257A1 (en) | Moulding materials | |
| EP2886311A1 (en) | Three-dimensional reuseable curing caul for use in curing integrated composite components and methods of making the same | |
| CN107521124A (zh) | 碳纤维双面板加筋结构件及其制造方法 | |
| JP7240559B2 (ja) | 航空機部品の中間生成品の製造方法および航空機部品 | |
| TW201919839A (zh) | 纖維強化塑膠及纖維強化塑膠之製造方法 | |
| US8715560B2 (en) | Method to control thickness in composite parts cured on closed angle tool | |
| EP2983899B1 (en) | Multi-component composite structures | |
| WO2019219662A1 (en) | Composite joint | |
| JPH04244839A (ja) | 炭素繊維強化複合材料の作製方法 | |
| GB2401081A (en) | Moulding material |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| A521 | Request for written amendment filed |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20211129 |
|
| A621 | Written request for application examination |
Free format text: JAPANESE INTERMEDIATE CODE: A621 Effective date: 20211129 |
|
| A131 | Notification of reasons for refusal |
Free format text: JAPANESE INTERMEDIATE CODE: A131 Effective date: 20220906 |
|
| A521 | Request for written amendment filed |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20221104 |
|
| TRDD | Decision of grant or rejection written | ||
| A01 | Written decision to grant a patent or to grant a registration (utility model) |
Free format text: JAPANESE INTERMEDIATE CODE: A01 Effective date: 20221122 |
|
| A61 | First payment of annual fees (during grant procedure) |
Free format text: JAPANESE INTERMEDIATE CODE: A61 Effective date: 20221221 |
|
| R150 | Certificate of patent or registration of utility model |
Ref document number: 7199940 Country of ref document: JP Free format text: JAPANESE INTERMEDIATE CODE: R150 |
|
| R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |