JP4705175B2 - 複合材料コネクティングロッドの作製方法 - Google Patents
複合材料コネクティングロッドの作製方法 Download PDFInfo
- Publication number
- JP4705175B2 JP4705175B2 JP2008541781A JP2008541781A JP4705175B2 JP 4705175 B2 JP4705175 B2 JP 4705175B2 JP 2008541781 A JP2008541781 A JP 2008541781A JP 2008541781 A JP2008541781 A JP 2008541781A JP 4705175 B2 JP4705175 B2 JP 4705175B2
- Authority
- JP
- Japan
- Prior art keywords
- fibers
- weft
- fiber
- rows
- pattern
- 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.)
- Expired - Fee Related
Links
- 239000002131 composite material Substances 0.000 title claims description 13
- 238000004519 manufacturing process Methods 0.000 title claims description 6
- 239000000835 fiber Substances 0.000 claims abstract description 87
- 239000004744 fabric Substances 0.000 claims abstract description 24
- 238000000034 method Methods 0.000 claims abstract description 14
- 239000011347 resin Substances 0.000 claims abstract description 6
- 229920005989 resin Polymers 0.000 claims abstract description 6
- 239000011295 pitch Substances 0.000 claims description 17
- 238000004804 winding Methods 0.000 claims description 5
- 230000000379 polymerizing effect Effects 0.000 claims 1
- 238000005520 cutting process Methods 0.000 abstract description 3
- 229920000049 Carbon (fiber) Polymers 0.000 abstract description 2
- 239000004917 carbon fiber Substances 0.000 abstract description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 abstract description 2
- 239000000463 material Substances 0.000 abstract 1
- 238000005304 joining Methods 0.000 description 3
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000006116 polymerization reaction Methods 0.000 description 1
- 238000009958 sewing Methods 0.000 description 1
- 238000001721 transfer moulding Methods 0.000 description 1
Images
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
- 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
- B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
- B29C70/545—Perforating, cutting or machining during or after 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
- 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
- B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
- B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
- B29C70/22—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure
- B29C70/222—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure the structure being shaped to form a three dimensional configuration
-
- 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
- B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
- B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
- B29C70/24—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least three directions forming a three dimensional structure
-
- D—TEXTILES; PAPER
- D03—WEAVING
- D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
- D03D11/00—Double or multi-ply fabrics not otherwise provided for
-
- D—TEXTILES; PAPER
- D03—WEAVING
- D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
- D03D25/00—Woven fabrics not otherwise provided for
- D03D25/005—Three-dimensional woven fabrics
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C7/00—Connecting-rods or like links pivoted at both ends; Construction of connecting-rod heads
- F16C7/02—Constructions of connecting-rods with constant length
- F16C7/026—Constructions of connecting-rods with constant length made of fibre reinforced resin
-
- 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
- B29C70/48—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 and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding [RTM], e.g. by vacuum
-
- 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
- B29L2031/7488—Cranks
-
- 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
- Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
- Y10T156/10—Methods of surface bonding and/or assembly therefor
- Y10T156/1052—Methods of surface bonding and/or assembly therefor with cutting, punching, tearing or severing
- Y10T156/1062—Prior to assembly
Landscapes
- Engineering & Computer Science (AREA)
- Textile Engineering (AREA)
- Mechanical Engineering (AREA)
- Composite Materials (AREA)
- Chemical & Material Sciences (AREA)
- General Engineering & Computer Science (AREA)
- Woven Fabrics (AREA)
- Moulding By Coating Moulds (AREA)
- Metal Extraction Processes (AREA)
- Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
- Superconductors And Manufacturing Methods Therefor (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
Description
Claims (9)
- 互いに滑ることが可能なように重ね合わせて結合された複数の1次層(N1、...、N7)から構成される複合繊維布帛から、対向する2つの縁部(112)を有するパターン(110)を切り抜く工程と、前記1次層が互いに滑って前記2つの縁部に面取り形状を付与するように、前記パターンをチューブに巻く工程と、面取り形状の前記縁部を重ね合わせて接合する工程とを含む、複合材料コネクティングロッドの作製方法。
- 前記パターンを、
・第1に、前記布帛の厚さ方向(E)にそれぞれ延在する少なくとも8つの列(C1〜C8)にまとめられており、かつ、所定ピッチ(P)で間隔が空けられた、少なくとも3本の重なり合う横糸繊維を有する列(C2、C4、C6、C8)と、同じピッチ(P)で間隔が空けられた、少なくとも4本の重なり合う横糸繊維を有する列(C1、C3、C5、C7)との間で交互する互い違いの配置で配設されている、少なくとも28本の横糸繊維(1〜28)であって、少なくとも7つの1次層(N1〜N7)を画定するように延在する少なくとも28本の横糸繊維(1〜28)と、
・第2に、前記横糸繊維方向にオフセットしている少なくとも4つの平行な面(P1、P2、P3、P4)に配設されている、少なくとも12本の縦糸繊維(29〜40)であって、各面が、これらの面のそれぞれに次のように配置された3本の重なり合う平行な縦糸繊維、すなわち
・4つの横糸繊維列(C1、C3、C5、C7)の最上部の横糸繊維(1、8、15、22)を、先の列から少なくとも2ピッチ(P)分間隔の空いた4つの横糸繊維列(C5、C7、C1、C3)の中間上部の横糸繊維(16、23、2、9)と繋ぎ、最初の列から少なくとも4ピッチ(P)分間隔の空いた4つの横糸繊維列(C1、C3、C5、C7)の上端の横糸繊維(1、8、15、22)の上に戻る、第1の縦糸繊維(番号がそれぞれ29、32、35、38)と、
・4つの横糸繊維列(C1、C3、C5、C7)の中間上部の横糸繊維(2、9、16、23)を、先の列から少なくとも2ピッチ(P)分間隔の空いた4つの横糸繊維列(C5、C7、C1、C3)の中間下部の横糸繊維(17、24、3、10)と繋ぎ、最初の列から少なくとも4ピッチ(P)分間隔の空いた4つの横糸繊維列(C1、C3、C5、C7)の中間上部の横糸繊維(2、9、16、23)の上に戻る、第2の縦糸繊維(番号がそれぞれ30、33、36、39)と、
・4つの横糸繊維列(C1、C3、C5、C7)の中間下部の横糸繊維(3、10、17、24)を、先の列から少なくとも2ピッチ(P)分間隔の空いた4つの横糸繊維列(C5、C7、C1、C3)の最下部の横糸繊維(18、25、4、11)と繋ぎ、最初の列から少なくとも4ピッチ(P)分間隔の空いた4つの横糸繊維列(C1、C3、C5、C7)の中間下部の横糸繊維(3、10、17、24)の上に戻る、第3の縦糸繊維(番号がそれぞれ31、34、37、40)と、
を含み、平行な縦糸繊維(29、30、31;32、33、34;35、36、37;38、39、40)の位置が、ある面から他の面に1ピッチ(P)分長手方向にオフセットしている、少なくとも12本の縦糸繊維(29〜40)と
から構成される基本織りを含む布帛から切り抜く、請求項1に記載の方法。 - 前記パターンが対称軸(114)を有し、前記1次層が、前記対称軸に沿って延在する横糸繊維を有するように、前記パターンを前記布帛から切り抜く、請求項2に記載の方法。
- 前記パターンをチューブに形成したときに対面することになる少なくとも2つの延長部(113)を有するように、前記パターンを切り抜く、請求項1に記載の方法。
- 前記延長部における前記1次層(N1、...、N7)を互いに分離させ、複合繊維布帛の中間層(116)を前記1次層の間に滑り込ませる、請求項4に記載の方法。
- 前記中間層が、前記延長部において前記1次層を形成する横糸繊維に対して斜めに配向した繊維を有する、請求項5に記載の方法。
- 前記1次層及び前記中間層を通して横断繊維(117)を挿入する、請求項5に記載の方法。
- 樹脂を注入し重合した後に、前記延長部に穴を開けて、連結フォークの突出部(104)を形成する、請求項5に記載の方法。
- 開けられた前記穴にリングの対(120)を取り付ける、請求項8に記載の方法。
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0511847 | 2005-11-23 | ||
FR0511847A FR2893683B1 (fr) | 2005-11-23 | 2005-11-23 | Procede de fabrication d'une bielle en materiau composite |
PCT/FR2006/002505 WO2007060306A1 (fr) | 2005-11-23 | 2006-11-10 | Procede de fabrication d'une bielle en materiau composite |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2009516608A JP2009516608A (ja) | 2009-04-23 |
JP4705175B2 true JP4705175B2 (ja) | 2011-06-22 |
Family
ID=36570864
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2008541781A Expired - Fee Related JP4705175B2 (ja) | 2005-11-23 | 2006-11-10 | 複合材料コネクティングロッドの作製方法 |
Country Status (13)
Country | Link |
---|---|
US (1) | US7704429B2 (ja) |
EP (1) | EP1954475B1 (ja) |
JP (1) | JP4705175B2 (ja) |
CN (1) | CN101309792B (ja) |
AT (1) | ATE432812T1 (ja) |
BR (1) | BRPI0618905A2 (ja) |
CA (1) | CA2630763C (ja) |
DE (1) | DE602006007165D1 (ja) |
ES (1) | ES2325967T3 (ja) |
FR (1) | FR2893683B1 (ja) |
PL (1) | PL1954475T3 (ja) |
RU (1) | RU2379185C1 (ja) |
WO (1) | WO2007060306A1 (ja) |
Families Citing this family (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2907475B1 (fr) * | 2006-10-18 | 2008-12-05 | Messier Dowty Sa Sa | Tissu composite 3d |
FR2918134B1 (fr) * | 2007-06-28 | 2009-09-18 | Eads Europ Aeronautic Defence | Bielle structurale en materiau composite et procede de realisation d'une bielle en materiau composite |
FR2932410B1 (fr) * | 2008-06-11 | 2010-05-28 | Aircelle Sa | Procede de fabrication d'une piece a corps creux en materiau composite |
FR2932408B1 (fr) * | 2008-06-11 | 2010-05-28 | Aircelle Sa | Preforme destinee a former une piece mecanique structurante creuse |
US8940214B2 (en) * | 2008-06-27 | 2015-01-27 | Airbus Operations S.L. | Method for the manufacture of one or more pairs of components in composite material |
FR2945847B1 (fr) * | 2009-05-20 | 2011-12-02 | Messier Dowty Sa | Procede de fabrication d'une bielle en materiau composite et bielle obtenue par la mise en oeuvre dudit procede. |
EP2266788A1 (fr) * | 2009-06-26 | 2010-12-29 | Bd Invent S.A. | Procédé de fabrication de bielles composites et bielles obtenues selon le procédé |
FR2953160A1 (fr) * | 2009-11-30 | 2011-06-03 | Messier Dowty Sa | Procede de fabrication d'une bielle en materiau composite integrant une chape renforcee |
FR2953443B1 (fr) * | 2009-12-08 | 2013-08-23 | Messier Dowty Sa | Procede de fabrication d'une bielle en materiau composite comprenant une surepaisseur localisee |
FR2957844B1 (fr) * | 2010-03-26 | 2012-05-18 | Messier Dowty Sa | Procede de fabrication d'un organe mecanique en materiau composite ayant une tenue mecanique accrue en traction-compression et en flexion |
FR2978695B1 (fr) * | 2011-08-01 | 2013-08-23 | Messier Bugatti Dowty | Procede de fabrication d'une piece structurale generalement triangulaire en materiau composite |
FR2978696B1 (fr) * | 2011-08-01 | 2013-08-23 | Messier Bugatti Dowty | Bielle en materiau composite ayant une tenue mecanique augmentee |
FR2993022B1 (fr) * | 2012-07-03 | 2015-02-20 | Aircelle Sa | Outil de frettage de pieces mecaniques et procede de frettage utilisant un tel outil |
BE1021537B1 (fr) * | 2012-10-11 | 2015-12-09 | Bd Invent S.A. | Bielle monobloc |
DE102013002893A1 (de) * | 2013-02-20 | 2014-08-21 | Diehl Aircabin Gmbh | Hybridbauteil und Herstellungsverfahren |
DE102013212571A1 (de) | 2013-06-28 | 2014-07-31 | Audi Ag | Verfahren zur Verbindung von Teil-Preforms |
DE102015120635A1 (de) * | 2015-03-02 | 2016-09-08 | Koki Technik Transmission Systems Gmbh | Verwendung eines Faserverbundwerkstoffs zur Herstellung einer Schaltgabel |
KR101824301B1 (ko) | 2015-06-30 | 2018-02-01 | 연세대학교 산학협력단 | 표면 기능성 복합 코팅막 및 이의 제조 방법 |
RU2678021C1 (ru) * | 2017-09-11 | 2019-01-22 | Государственное бюджетное образовательное учреждение высшего образования Московской области "Технологический университет" | Способ изготовления объемно армированного композиционного материала |
US10919256B2 (en) * | 2019-05-09 | 2021-02-16 | The Boeing Company | Composite structure having a variable gage and methods for forming a composite structure having a variable gage |
US10913215B2 (en) * | 2019-05-09 | 2021-02-09 | The Boeing Company | Composite structure having a variable gage and methods for forming a composite structure having a variable gage |
EP3859066B1 (en) * | 2020-02-03 | 2024-01-24 | STÄUBLI BAYREUTH GmbH | Weaving method and weft selector for implementing such a method |
FR3137012A1 (fr) | 2022-06-22 | 2023-12-29 | Safran Landing Systems | Renfort fibreux pour la fabrication d’une pièce composite destinée à être articulée avec d’autres pièces |
FR3137013A1 (fr) | 2022-06-22 | 2023-12-29 | Safran Landing Systems | Procédé de fabrication d’une pièce en matériau composite destinée à être articulée avec d’autres pièces |
FR3137014A1 (fr) | 2022-06-22 | 2023-12-29 | Safran Landing Systems | Renfort fibreux pour la fabrication d’une pièce composite destinée à être articulée avec d’autres pièces |
FR3152424A1 (fr) | 2023-09-04 | 2025-03-07 | Safran | Procédé de fabrication d’une préforme fibreuse pour pièce composite destinée à être articulée avec d’autres pièces |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3726340A1 (de) * | 1987-08-07 | 1989-02-16 | Sachs Systemtechnik Gmbh | Verfahren zur herstellung einer zug-druck-strebe mit krafteinleitungsaugen |
US5033514A (en) * | 1989-05-16 | 1991-07-23 | Sulzer Brothers Limited | Fiber reinforced plastic accelerating lever for a projectile loom |
JPH07290606A (ja) * | 1994-04-18 | 1995-11-07 | Aerospat Soc Natl Ind | 複合材料製の連結桿及びその製造方法 |
JPH09509107A (ja) * | 1993-08-06 | 1997-09-16 | ブランデンブルガー パテントフェルヴェルトゥングスゲゼルシャフト デス ビュールゲルリッヒェン レヒツ | 管状ライニングホース並びにその製造方法及び装置 |
JPH10219545A (ja) * | 1997-02-04 | 1998-08-18 | Soc Natl Etud Constr Mot Aviat <Snecma> | 構造用複合材料のための結合多層織物 |
Family Cites Families (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2884958A (en) * | 1956-05-18 | 1959-05-05 | Sr Leonard J Asselin | Rolled tube |
US3092148A (en) * | 1960-07-25 | 1963-06-04 | Smith Corp A O | Starting joints for continuous wound vessel |
GB1111995A (en) * | 1964-05-29 | 1968-05-01 | Sandvikens Jernverks Ab | Improvements in threaded drill rod elements |
US3386162A (en) * | 1966-02-28 | 1968-06-04 | Nooter Corp | Method of making a multi-layered vessel |
US3566925A (en) * | 1968-12-17 | 1971-03-02 | Mitsubishi Heavy Ind Ltd | Spiral multilayer pipe for pressure vessel |
US4023801A (en) * | 1974-09-24 | 1977-05-17 | Exxon Research And Engineering Company | Golf shaft and method of making same |
US4097626A (en) * | 1976-06-07 | 1978-06-27 | Grafalloy Corporation | Construction for a fiber reinforced shaft |
US4369742A (en) * | 1977-01-24 | 1983-01-25 | Piston Powered Products A Division Of Rw Technologies, Inc. | Connecting rod for internal combustion engine |
US4275122A (en) * | 1978-07-17 | 1981-06-23 | Gkn Transmissions Limited | Shaft and universal joint member assembly |
US4530379A (en) * | 1982-04-27 | 1985-07-23 | Hercules Incorporated | Filament wound interlaminate tubular attachment |
FR2654483B1 (fr) * | 1989-11-13 | 1992-03-06 | Europ Propulsion | Bielle en materiau composite. |
US5093162A (en) * | 1990-04-30 | 1992-03-03 | Spalding & Evenflo Companies, Inc. | Large-tip composite golf shaft |
US5167742A (en) * | 1991-05-29 | 1992-12-01 | Westinghouse Electric Corp. | Method and device for producing a tapered scarf joint |
US5192384A (en) * | 1991-05-30 | 1993-03-09 | Kaiser Aerospace And Electronics Corporation | Methods for forming composite tubing having tapered ends |
US5352309A (en) * | 1991-08-05 | 1994-10-04 | Smith Fiberglas Products Inc. | Method for manufacturing pipe bells |
US5317828A (en) * | 1991-08-06 | 1994-06-07 | Shimano Inc. | Method of manufacturing a fishing rod |
US5281454A (en) * | 1991-08-16 | 1994-01-25 | Kaiser Aerospace & Electronics Corporation | Closed composite sections with bonded scarf joints |
US5624519A (en) * | 1992-05-29 | 1997-04-29 | Trek Bicycle, Corp. | Method making a composite bicycle frame using composite lugs |
US5280706A (en) * | 1992-06-25 | 1994-01-25 | Thiokol Corporation | Composite/metal hybrid rocket motor case and methods for manufacturing |
US5318742A (en) * | 1992-08-28 | 1994-06-07 | You Chin San | Method of making bicycle tubular frame of plastic composite material |
FR2705610B1 (fr) * | 1993-05-26 | 1995-08-11 | Aerospatiale | Procédé de fabrication de bielle en matériau composite monobloc par mise en place de fibres pré-imprégnées sur un mandrin extractible et bielle ainsi obtenue. |
FR2706354B1 (fr) * | 1993-06-14 | 1995-09-01 | Aerospatiale | Procédé de réalisation d'objets creux en matériau composite par bobinage-dépose au contact sur un mandrin expansible et objets ainsi obtenus. |
US5456405A (en) * | 1993-12-03 | 1995-10-10 | Quality Tubing Inc. | Dual bias weld for continuous coiled tubing |
US6036904A (en) * | 1994-04-18 | 2000-03-14 | Aerospatiale Societe Nationale Industrielle | Method of manufacturing a connecting rod made from composite material |
US6540954B1 (en) * | 1999-07-30 | 2003-04-01 | Resolute Racing Shells, Inc. | Process for fabricating a rowing shell |
DE20219281U1 (de) * | 2002-12-12 | 2004-04-15 | Liebherr-Werk Nenzing Ges.M.B.H., Nenzing | Kranausleger-Abspannelement |
-
2005
- 2005-11-23 FR FR0511847A patent/FR2893683B1/fr not_active Expired - Fee Related
-
2006
- 2006-11-10 EP EP06831105A patent/EP1954475B1/fr active Active
- 2006-11-10 WO PCT/FR2006/002505 patent/WO2007060306A1/fr active Application Filing
- 2006-11-10 CN CN2006800427941A patent/CN101309792B/zh active Active
- 2006-11-10 AT AT06831105T patent/ATE432812T1/de active
- 2006-11-10 RU RU2008125096/12A patent/RU2379185C1/ru not_active IP Right Cessation
- 2006-11-10 PL PL06831105T patent/PL1954475T3/pl unknown
- 2006-11-10 JP JP2008541781A patent/JP4705175B2/ja not_active Expired - Fee Related
- 2006-11-10 ES ES06831105T patent/ES2325967T3/es active Active
- 2006-11-10 CA CA2630763A patent/CA2630763C/fr active Active
- 2006-11-10 BR BRPI0618905-9A patent/BRPI0618905A2/pt not_active IP Right Cessation
- 2006-11-10 DE DE602006007165T patent/DE602006007165D1/de active Active
- 2006-11-13 US US11/559,141 patent/US7704429B2/en active Active
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3726340A1 (de) * | 1987-08-07 | 1989-02-16 | Sachs Systemtechnik Gmbh | Verfahren zur herstellung einer zug-druck-strebe mit krafteinleitungsaugen |
US5033514A (en) * | 1989-05-16 | 1991-07-23 | Sulzer Brothers Limited | Fiber reinforced plastic accelerating lever for a projectile loom |
JPH09509107A (ja) * | 1993-08-06 | 1997-09-16 | ブランデンブルガー パテントフェルヴェルトゥングスゲゼルシャフト デス ビュールゲルリッヒェン レヒツ | 管状ライニングホース並びにその製造方法及び装置 |
JPH07290606A (ja) * | 1994-04-18 | 1995-11-07 | Aerospat Soc Natl Ind | 複合材料製の連結桿及びその製造方法 |
JPH10219545A (ja) * | 1997-02-04 | 1998-08-18 | Soc Natl Etud Constr Mot Aviat <Snecma> | 構造用複合材料のための結合多層織物 |
Also Published As
Publication number | Publication date |
---|---|
BRPI0618905A2 (pt) | 2013-01-08 |
FR2893683A1 (fr) | 2007-05-25 |
DE602006007165D1 (de) | 2009-07-16 |
CA2630763A1 (fr) | 2007-05-31 |
EP1954475A1 (fr) | 2008-08-13 |
ATE432812T1 (de) | 2009-06-15 |
CN101309792A (zh) | 2008-11-19 |
US7704429B2 (en) | 2010-04-27 |
ES2325967T3 (es) | 2009-09-25 |
EP1954475B1 (fr) | 2009-06-03 |
FR2893683B1 (fr) | 2008-02-01 |
CA2630763C (fr) | 2011-01-04 |
JP2009516608A (ja) | 2009-04-23 |
US20070137778A1 (en) | 2007-06-21 |
WO2007060306A1 (fr) | 2007-05-31 |
PL1954475T3 (pl) | 2009-11-30 |
RU2379185C1 (ru) | 2010-01-20 |
CN101309792B (zh) | 2010-11-10 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JP4705175B2 (ja) | 複合材料コネクティングロッドの作製方法 | |
JP4705174B2 (ja) | 複合材料の構造要素、特にコネクティングロッドの上に、突出部を作製する方法 | |
EP1379716B1 (en) | Woven preform for structural joints | |
JP5659144B2 (ja) | パイ−プリフォームのための改良繊維構造 | |
JP6242348B2 (ja) | バイアス繊維を伴うパイ形プリフォーム | |
JP5547206B2 (ja) | 非直線状の脚を伴うパイ形プリフォームおよびその製造方法 | |
US6086968A (en) | Two- and three-dimensional shaped woven materials | |
ES2836214T3 (es) | Método para tejer sustratos con paredes laterales integrantes | |
JP5429779B2 (ja) | 複合構造を適用するための混合三次元織/積層支柱 | |
JP6150870B2 (ja) | 織式プリフォーム、繊維強化コンポジット、及びそれらの製造方法 | |
TWI604945B (zh) | 具一體偏軸加強件之編織預成形體 | |
BRPI0517154B1 (pt) | pré-forma tridimensional integralmente tecida e método para formar uma pré-forma tridimensional integralmente tecida | |
CN101321903A (zh) | 角件和利用纤维转移形成角件的方法 | |
ES2839298T3 (es) | Preformas con rellenos de espacios integrados | |
US20120049411A1 (en) | Method for manufacturing a composite material connecting rod | |
CN210827846U (zh) | 一种多层自体成型弹性杆空间曲面编织结构体系 | |
JP2657519B2 (ja) | 分岐部を有するバイアス織物及びその製造方法 | |
ITUA20164437A1 (it) | Telaio reticolare in carbonio o fibre composite per strutture leggere e procedimento per la sua realizzazione |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
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: 20110208 |
|
A61 | First payment of annual fees (during grant procedure) |
Free format text: JAPANESE INTERMEDIATE CODE: A61 Effective date: 20110310 |
|
R150 | Certificate of patent or registration of utility model |
Ref document number: 4705175 Country of ref document: JP Free format text: JAPANESE INTERMEDIATE CODE: R150 |
|
FPAY | Renewal fee payment (event date is renewal date of database) |
Free format text: PAYMENT UNTIL: 20140318 Year of fee payment: 3 |
|
S111 | Request for change of ownership or part of ownership |
Free format text: JAPANESE INTERMEDIATE CODE: R313111 |
|
FPAY | Renewal fee payment (event date is renewal date of database) |
Free format text: PAYMENT UNTIL: 20140318 Year of fee payment: 3 |
|
R350 | Written notification of registration of transfer |
Free format text: JAPANESE INTERMEDIATE CODE: R350 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
LAPS | Cancellation because of no payment of annual fees |