JP5547819B2 - 航空機の着陸装置構造のロッカアームなどの蝶着された構造のアームを作成する方法 - Google Patents
航空機の着陸装置構造のロッカアームなどの蝶着された構造のアームを作成する方法 Download PDFInfo
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- JP5547819B2 JP5547819B2 JP2012549288A JP2012549288A JP5547819B2 JP 5547819 B2 JP5547819 B2 JP 5547819B2 JP 2012549288 A JP2012549288 A JP 2012549288A JP 2012549288 A JP2012549288 A JP 2012549288A JP 5547819 B2 JP5547819 B2 JP 5547819B2
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- 239000012783 reinforcing fiber Substances 0.000 claims description 20
- 239000011347 resin Substances 0.000 claims description 20
- 229920005989 resin Polymers 0.000 claims description 20
- 238000000034 method Methods 0.000 claims description 16
- 239000013256 coordination polymer Substances 0.000 claims 1
- 239000000835 fiber Substances 0.000 description 12
- 239000002131 composite material Substances 0.000 description 10
- 238000004519 manufacturing process Methods 0.000 description 7
- 239000006096 absorbing agent Substances 0.000 description 4
- 238000009940 knitting Methods 0.000 description 4
- 239000000463 material Substances 0.000 description 4
- 230000035939 shock Effects 0.000 description 4
- 238000002347 injection Methods 0.000 description 3
- 239000007924 injection Substances 0.000 description 3
- 239000000243 solution Substances 0.000 description 3
- 229920000049 Carbon (fiber) Polymers 0.000 description 2
- 239000004917 carbon fiber Substances 0.000 description 2
- 230000000295 complement effect Effects 0.000 description 2
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 239000004744 fabric Substances 0.000 description 2
- 230000036961 partial effect Effects 0.000 description 2
- 230000000379 polymerizing effect Effects 0.000 description 2
- 230000003014 reinforcing effect Effects 0.000 description 2
- 238000004804 winding Methods 0.000 description 2
- 240000001549 Ipomoea eriocarpa Species 0.000 description 1
- 235000005146 Ipomoea eriocarpa Nutrition 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 230000002238 attenuated effect Effects 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 230000027455 binding Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 238000005553 drilling Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 230000000670 limiting effect Effects 0.000 description 1
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 230000000284 resting effect Effects 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 239000004753 textile Substances 0.000 description 1
Images
Classifications
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- 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
- B29C70/68—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
- B29C70/72—Encapsulating inserts having non-encapsulated projections, e.g. extremities or terminal portions of electrical components
-
- 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
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
-
- 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
- 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
- B29L2031/75—Shafts
-
- 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
- F16C2326/00—Articles relating to transporting
- F16C2326/43—Aeroplanes; Helicopters
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Moulding By Coating Moulds (AREA)
- Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
- Gears, Cams (AREA)
Description
航空機の着陸装置構造のような蝶着された構造のアームを作成する方法であって、
このアームは、縦方向に延びる本体を具備し、本体から半径方向に突出するヨークのような接合部分を含み、
この方法は、
− 接合部分を担持する基部を含む挿入体を作成する段階と、
− 挿入体の基部を組み合わせるマンドレルを、挿入体の基部の外面部分によってこのマンドレルの外表面部分の境界が定められるように作成する段階と、
− マンドレルの周囲においてその全長にわたって、強化繊維の1又は複数の層を、層のそれぞれが覆うことなく各層を貫通する接合部分を有するように適用する段階と、
− 強化繊維の1又は複数の層内に、これらの層の基部の外面との接触領域のレベルで、樹脂を注入する段階と、
− 強化繊維の層と挿入体の基部とを固く結合させるように樹脂を重合させる段階と、
を含む方法を提供する。
Claims (5)
- 航空機の着陸装置構造である蝶着された構造のアームを作成する方法であって、
このアームは、縦方向(AP;BP;CP)に延びる本体(30;130;230)を具備し、本体から半径方向に突出する接合部分(13;113;213)を含み、
この方法は、
− 接合部分を担持する基部(12;212)を含む挿入体(11;211)を作成する段階と、
− 挿入体の基部を組み合わせるマンドレル(10;110)を、挿入体の基部の外面(17;217)部分によってこのマンドレルの外表面部分の境界が定められるように作成する段階と、
− マンドレルの周囲においてその全長にわたって、強化繊維の1又は複数の層を、層のそれぞれが覆うことなく各層を貫通する接合部分(13;113;213)を有するように適用する段階と、
− 強化繊維の1又は複数の層(31;131;231)内に、基部の外面(17;217)とのこれらの層(31)の接触領域(32)のレベルで、樹脂を注入する段階と、
− 強化繊維の層と挿入体の基部とを固く結合させるように樹脂を重合させる段階と、
を含む、
方法。 - 基部(12;212)が全体的に筒形状である、
請求項1に記載の方法。 - マンドレル(10;110)が、少なくとも1つのスリーブ(23,24)と共に基部の外面(17;217)と沿うように形成される、
請求項1又は請求項2に記載の方法。 - シールされた連結部(25,26)が基部(12;212)と各スリーブ(23,24)との間に作成される、
請求項3に記載の方法。 - 筒形状基部(12;212)は、本体(30;130;230)の内壁において力を分配するようにされた傾斜した形状の縦方向断面(19,20)を有する、
請求項4に記載の方法。
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1050416 | 2010-01-22 | ||
FR1050416A FR2955524B1 (fr) | 2010-01-22 | 2010-01-22 | Procede de fabrication d'un bras pour structure articulee tel qu'un balancier equipant une structure d'atterrisseu d'aeronef. |
PCT/EP2011/000200 WO2011088992A1 (fr) | 2010-01-22 | 2011-01-19 | Procede de fabrication d'un bras pour structure articulee tel qu'un balancier equipant une structure d'atterrisseur d'aeronef |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2013517180A JP2013517180A (ja) | 2013-05-16 |
JP5547819B2 true JP5547819B2 (ja) | 2014-07-16 |
Family
ID=42668293
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2012549288A Active JP5547819B2 (ja) | 2010-01-22 | 2011-01-19 | 航空機の着陸装置構造のロッカアームなどの蝶着された構造のアームを作成する方法 |
Country Status (9)
Country | Link |
---|---|
US (1) | US20130062012A1 (ja) |
EP (1) | EP2525965B1 (ja) |
JP (1) | JP5547819B2 (ja) |
CN (1) | CN102770262B (ja) |
BR (1) | BR112012017999A2 (ja) |
CA (1) | CA2787271C (ja) |
FR (1) | FR2955524B1 (ja) |
RU (1) | RU2521644C2 (ja) |
WO (1) | WO2011088992A1 (ja) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2978935B1 (fr) * | 2011-08-09 | 2013-08-23 | Messier Bugatti Dowty | Procede de fabrication d'une piece structurale en materiau composite comprenant une chape double orientee radialement |
CN106313583B (zh) * | 2015-06-18 | 2018-07-13 | 余永元 | 附加有固定件的轮椅复合材质骨架之成型方法及其制品 |
EP3202557B1 (en) * | 2016-02-08 | 2021-02-17 | Crompton Technology Group Limited | Strut comprising composite cylinder with a mid-strut fitting |
DE102016208115A1 (de) * | 2016-05-11 | 2017-11-16 | Contitech Mgw Gmbh | Verfahren zur Herstellung eines Ladeluftrohres |
US10272991B2 (en) * | 2016-06-23 | 2019-04-30 | Goodrich Corporation | Metallic composite joint |
US10556673B2 (en) * | 2016-06-27 | 2020-02-11 | Goodrich Corporation | Manufacturing method of polymer composite/metal load transfer joint for landing gear |
DE102017203477A1 (de) | 2017-03-03 | 2018-09-06 | Aktiebolaget Skf | Kompositformstück |
US10527086B2 (en) | 2017-06-30 | 2020-01-07 | Crompton Technology Group Limited | Strut comprising composite cylinder with a mid-strut fitting |
CN110126300A (zh) * | 2019-05-05 | 2019-08-16 | 宜兴市新立织造有限公司 | 一种采用三维编织的复合材料起落架及其制备方法 |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
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CA1076090A (en) * | 1977-03-08 | 1980-04-22 | Societe Anonyme Dite: Messier-Hispano-Bugatti | Retractable fuselage mounted undercarriage |
US4248062A (en) * | 1979-10-05 | 1981-02-03 | Shakespeare Company | Drive shaft assembly and method for making same |
JPS5950216A (ja) * | 1982-09-16 | 1984-03-23 | Honda Motor Co Ltd | 繊維強化合成樹脂製駆動軸とその製造方法 |
US4973372A (en) * | 1984-08-29 | 1990-11-27 | Allied-Signal Inc. | Method of making a tie-bar with internal lubrication |
US4704918A (en) * | 1985-02-19 | 1987-11-10 | Kamatics Corporation | Composite material force or motion transmitting member |
JPH0587115A (ja) * | 1991-09-25 | 1993-04-06 | Toyota Motor Corp | 動力伝達軸の製造方法 |
JP3292350B2 (ja) * | 1994-09-30 | 2002-06-17 | 東レ株式会社 | プロペラシャフトおよびその製造方法 |
US5908261A (en) * | 1997-08-06 | 1999-06-01 | Amsted Industries Incorporated | Turnbuckle and method of making a turnbuckle |
US6116113A (en) * | 1997-08-13 | 2000-09-12 | Maclean-Fogg Company | Composite link |
RU12101U1 (ru) * | 1999-06-17 | 1999-12-16 | Государственный космический научно-производственный центр им.М.В.Хруничева | Убирающееся шасси самолета |
US20050252244A1 (en) * | 2003-04-09 | 2005-11-17 | Fred Heldoorn | Method, system and apparatus for a takeout holder and insert |
FR2887601B1 (fr) * | 2005-06-24 | 2007-10-05 | Snecma Moteurs Sa | Piece mecanique et procede de fabrication d'une telle piece |
RU2370413C2 (ru) * | 2007-04-26 | 2009-10-20 | Открытое акционерное общество "Центральная компания Финансово-промышленной группы "Российский авиационный консорциум" | Основная опора шасси самолета |
FR2932409B1 (fr) * | 2008-06-13 | 2013-04-12 | Messier Dowty Sa | Procede de fabrication d'une piece structurale en materiau composite a matrice organique, piece obtenue. |
-
2010
- 2010-01-22 FR FR1050416A patent/FR2955524B1/fr active Active
-
2011
- 2011-01-19 WO PCT/EP2011/000200 patent/WO2011088992A1/fr active Application Filing
- 2011-01-19 RU RU2012136117/05A patent/RU2521644C2/ru not_active IP Right Cessation
- 2011-01-19 BR BR112012017999A patent/BR112012017999A2/pt not_active IP Right Cessation
- 2011-01-19 CN CN201180006718.6A patent/CN102770262B/zh active Active
- 2011-01-19 US US13/574,327 patent/US20130062012A1/en not_active Abandoned
- 2011-01-19 EP EP11701617.0A patent/EP2525965B1/fr active Active
- 2011-01-19 JP JP2012549288A patent/JP5547819B2/ja active Active
- 2011-01-19 CA CA2787271A patent/CA2787271C/fr active Active
Also Published As
Publication number | Publication date |
---|---|
RU2521644C2 (ru) | 2014-07-10 |
CN102770262B (zh) | 2015-08-05 |
WO2011088992A1 (fr) | 2011-07-28 |
BR112012017999A2 (pt) | 2016-05-03 |
JP2013517180A (ja) | 2013-05-16 |
EP2525965B1 (fr) | 2018-04-25 |
FR2955524A1 (fr) | 2011-07-29 |
CA2787271A1 (fr) | 2011-07-28 |
CA2787271C (fr) | 2015-10-27 |
US20130062012A1 (en) | 2013-03-14 |
CN102770262A (zh) | 2012-11-07 |
EP2525965A1 (fr) | 2012-11-28 |
FR2955524B1 (fr) | 2014-01-31 |
RU2012136117A (ru) | 2014-02-27 |
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