CN102317154B - 一种复合结构桁架的方法与系统 - Google Patents

一种复合结构桁架的方法与系统 Download PDF

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Publication number
CN102317154B
CN102317154B CN200880014861.8A CN200880014861A CN102317154B CN 102317154 B CN102317154 B CN 102317154B CN 200880014861 A CN200880014861 A CN 200880014861A CN 102317154 B CN102317154 B CN 102317154B
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CN
China
Prior art keywords
flange
web
spar
rib
chord member
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
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CN200880014861.8A
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English (en)
Chinese (zh)
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CN102317154A (zh
Inventor
R·L·库里莎
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Boeing Co
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Boeing Co
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Publication of CN102317154A publication Critical patent/CN102317154A/zh
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Publication of CN102317154B publication Critical patent/CN102317154B/zh
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/18Spars; Ribs; Stringers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/18Spars; Ribs; Stringers
    • B64C3/187Ribs
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10Methods of surface bonding and/or assembly therefor
    • Y10T156/1089Methods of surface bonding and/or assembly therefor of discrete laminae to single face of additional lamina
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49616Structural member making
    • Y10T29/49622Vehicular structural member making
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
CN200880014861.8A 2007-04-05 2008-03-29 一种复合结构桁架的方法与系统 Expired - Fee Related CN102317154B (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US11/697,162 US8490362B2 (en) 2007-04-05 2007-04-05 Methods and systems for composite structural truss
US11/697,162 2007-04-05
PCT/US2008/058799 WO2008124352A1 (en) 2007-04-05 2008-03-29 Methods and systems for composite structural truss

Publications (2)

Publication Number Publication Date
CN102317154A CN102317154A (zh) 2012-01-11
CN102317154B true CN102317154B (zh) 2015-09-09

Family

ID=39688780

Family Applications (1)

Application Number Title Priority Date Filing Date
CN200880014861.8A Expired - Fee Related CN102317154B (zh) 2007-04-05 2008-03-29 一种复合结构桁架的方法与系统

Country Status (6)

Country Link
US (2) US8490362B2 (enExample)
EP (1) EP2139761B1 (enExample)
JP (1) JP5475639B2 (enExample)
CN (1) CN102317154B (enExample)
ES (1) ES2622680T3 (enExample)
WO (1) WO2008124352A1 (enExample)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9903848B2 (en) * 2008-12-30 2018-02-27 Sikorsky Aircraft Corporation Non-destructive inspection method with objective evaluation
EP2330294B1 (en) * 2009-12-02 2013-01-16 Bladena ApS Reinforced airfoil shaped body
DE102010043850A1 (de) * 2010-11-12 2012-05-16 Airbus Operations Gmbh Strukturelement für ein Luft- und/oder Raumfahrzeug und Verfahren zum Herstellen eines derartigen Strukturelementes
US10907609B2 (en) * 2014-07-15 2021-02-02 Ge Renewable Technologies Apparatus and method for modifying a geometry of a turbine part
CA2857297C (en) * 2014-07-21 2021-08-17 Alstom Renewable Technologies Apparatus and method for modifying a geometry of a turbine part
US9610728B2 (en) 2014-07-18 2017-04-04 The Boeing Company Apparatus and methods for bonding laminate structures
CN104554704B (zh) * 2015-01-27 2016-09-28 新誉集团有限公司 可横向组装的大展弦比机翼结构及其组装方法
ES2705124T3 (es) * 2015-09-29 2019-03-21 Airbus Operations Sl Costilla de composite para una caja de torsión de aeronave y procedimiento de fabricación de la misma
ES2808671T3 (es) 2016-04-11 2021-03-01 Asco Ind Nv Dispositivo hipersustentador
US10286998B2 (en) * 2016-05-05 2019-05-14 The Boeing Company Mechanical fastening system and associated structural assembly and method
EP3498591A1 (en) 2017-12-13 2019-06-19 AIRBUS HELICOPTERS DEUTSCHLAND GmbH A composite truss beam with a sandwich web
EP3590824B1 (en) * 2018-07-06 2021-06-23 Airbus Operations, S.L. Method for manufacturing the trailing edge ribs and the bearing ribs of trailing edges of aircraft lifting surfaces
CN111056047B (zh) * 2018-10-17 2021-07-30 哈尔滨工业大学 基于形状记忆聚合物复合材料的桁架式可收展太空舱
US11046420B2 (en) * 2019-10-23 2021-06-29 The Boeing Company Trailing edge flap having a waffle grid interior structure
US20210316343A1 (en) * 2020-04-09 2021-10-14 Imperial Systems, Inc. Fume Hood Having Structurally Integrated Components
CN113733595B (zh) * 2021-08-30 2022-06-14 北京航空航天大学 一种全包裹式复合材料泡沫夹芯翼肋加工方法
US12157572B2 (en) * 2021-08-31 2024-12-03 The Boeing Company Method of making a control surface
US11987353B2 (en) 2022-04-19 2024-05-21 The Boeing Company Thermoplastic skin panels, torque box and method
US20240066762A1 (en) * 2022-08-29 2024-02-29 The Boeing Company Curing Composites Out-Of-Autoclave Using Induction Heating with Smart Susceptors
US12286221B2 (en) * 2022-10-04 2025-04-29 The Boeing Company Tubular wing structures and methods of manufacture
US12431835B1 (en) * 2023-03-28 2025-09-30 Fushun Ma Aerodynamic solar cell system

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1706996A (en) * 1927-03-31 1929-03-26 Edmund B Carns Beam or girder
GB462904A (en) * 1935-09-14 1937-03-15 Richard Vogt Improvements in spars for the wings of aircraft
US2233969A (en) * 1938-12-30 1941-03-04 Bell Aircraft Corp Pressed wing rib
US2392818A (en) * 1940-11-18 1946-01-15 Lockheed Aircraft Corp Double skin sheet metal structural element
US5100713A (en) * 1989-06-06 1992-03-31 Toray Industries, Inc. Reinforcing woven fabric and preformed material, fiber reinforced composite material and beam using it

Family Cites Families (59)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1682202A (en) * 1928-08-28 vaughn
US582527A (en) 1897-05-11 Dominic golden
US1429600A (en) 1918-11-21 1922-09-19 American Balsa Company Inc Beam structure
US1343707A (en) * 1918-11-25 1920-06-15 Edmund B Carns Aircraft
US1372478A (en) * 1919-10-15 1921-03-22 Bradley Parker Richardson Method of fireproofing aircraft parts
US1571239A (en) * 1923-02-17 1926-02-02 Firm Dornier Metallbauten Gmbh Metal girder for light metal structures
US1840643A (en) * 1925-07-11 1932-01-12 Ford Motor Co Airplane
US1769005A (en) * 1927-07-29 1930-07-01 Glenn L Martin Co Airplane-wing structure
US1796654A (en) * 1927-11-07 1931-03-17 Hermann Otto Metallic aeroplane wing
US1887627A (en) * 1931-05-26 1932-11-15 Finger Salo Cyrus Method and means of fabricating structures of metal and nonmetallic materials
US2029645A (en) * 1933-12-18 1936-02-04 Stran Steel Corp Structural element
US2097597A (en) * 1935-08-19 1937-11-02 Pavlecka John Cellular structure
US2102095A (en) * 1936-04-20 1937-12-14 Joseph R Salzman Airplane
US2122698A (en) * 1936-05-16 1938-07-05 Rafter Machine Company Beam and the like for building construction
US2098676A (en) * 1936-05-16 1937-11-09 Rafter Machine Company Beam and the like for building construction
US2092472A (en) * 1936-12-04 1937-09-07 Rafter Machine Company Stud and rafter
US2129624A (en) * 1936-12-04 1938-09-06 Rafter Machine Company Stud and rafter
US2396625A (en) * 1941-03-26 1946-03-12 Budd Edward G Mfg Co Aircraft structure
US2389917A (en) * 1941-10-16 1945-11-27 Frederic A Leisen Aircraft structure
US2386019A (en) * 1943-01-28 1945-10-02 Budd Edward G Mfg Co Truss structure and parts thereof
US2514607A (en) * 1946-02-07 1950-07-11 Dravo Corp Truss construction
US2589193A (en) 1946-11-29 1952-03-11 Goodyear Aircraft Corp Airfoil, and particularly helicopter blade
US3901465A (en) 1974-03-05 1975-08-26 Lawrence J Deangelis Variable-area variable incidence wing and aircraft incorporating same
GB1534697A (en) 1975-03-27 1978-12-06 Heath Charles William Model aircraft wing construction jig
US4002116A (en) 1975-05-09 1977-01-11 Jack N. Schmitt Apparatus for forming trusses
US4051289A (en) 1976-04-12 1977-09-27 General Electric Company Composite airfoil construction
US4120065A (en) 1977-12-15 1978-10-17 Eugene W. Sivachenko Lightweight modular, truss-deck bridge system
US4223053A (en) 1978-08-07 1980-09-16 The Boeing Company Truss core panels
US4481703A (en) 1980-02-25 1984-11-13 Rockwell International Corporation Method of making rib structures for an airfoil
US4452657A (en) * 1982-09-15 1984-06-05 The Boeing Company Composite integral web stiffening method
US4671470A (en) 1985-07-15 1987-06-09 Beech Aircraft Corporation Method for fastening aircraft frame elements to sandwich skin panels covering same using woven fiber connectors
US4887406A (en) * 1987-12-31 1989-12-19 Saia Wilburn H F Structural member for buildings
JPH03123798U (enExample) * 1990-03-30 1991-12-16
US5332178A (en) 1992-06-05 1994-07-26 Williams International Corporation Composite wing and manufacturing process thereof
GB9215827D0 (en) 1992-07-24 1992-09-09 British Aerospace A lightning shield
CA2077429C (en) * 1992-09-02 1999-03-30 Ernest R. Bodnar Roll formed metal member
US5375324A (en) 1993-07-12 1994-12-27 Flowind Corporation Vertical axis wind turbine with pultruded blades
US5632940A (en) 1994-03-29 1997-05-27 Whatley; Bradford L. Method of making an integrally stiffened article
RU2116934C1 (ru) 1997-05-06 1998-08-10 Акционерное общество "Центр перспективных разработок акционерного общества "Центральный научно-исследовательский институт специального машиностроения" Нервюра из композиционных материалов (варианты) и устройство для изготовления ее плоской реберно-ячеистой структуры
JP2000006893A (ja) * 1998-06-23 2000-01-11 Fuji Heavy Ind Ltd 複合材翼構造
DE19922295C1 (de) 1999-05-14 2000-07-27 Eurocopter Deutschland Unterbodenstruktur einer Rumpfzelle eines Luftfahrzeuges
US6513757B1 (en) 1999-07-19 2003-02-04 Fuji Jukogyo Kabushiki Kaisha Wing of composite material and method of fabricating the same
JP4316059B2 (ja) * 1999-08-06 2009-08-19 富士重工業株式会社 複合材翼の製造方法
US6889937B2 (en) 1999-11-18 2005-05-10 Rocky Mountain Composites, Inc. Single piece co-cure composite wing
US6655633B1 (en) 2000-01-21 2003-12-02 W. Cullen Chapman, Jr. Tubular members integrated to form a structure
JP4416900B2 (ja) 2000-03-10 2010-02-17 富士重工業株式会社 複合材パネルおよびその製造方法
FR2817608B1 (fr) * 2000-12-04 2004-11-05 Eads Airbus Sa Poutre composite a initiateur de rupture integre et fuselage d'aeronef integrant de telles poutres
US6638466B1 (en) 2000-12-28 2003-10-28 Raytheon Aircraft Company Methods of manufacturing separable structures
JP4545339B2 (ja) * 2001-04-05 2010-09-15 富士重工業株式会社 複合材翼およびその製造方法
US6945727B2 (en) 2002-07-19 2005-09-20 The Boeing Company Apparatuses and methods for joining structural members, such as composite structural members
CA2404320C (en) * 2002-09-30 2005-02-08 Ernest R. Bodnar Steel stud with openings and edge formations and method
CA2456321A1 (en) 2003-01-30 2004-07-30 Martin Bureau Laminated polymer composite material
US7587877B2 (en) * 2003-10-28 2009-09-15 Best Joist Inc Cold-formed steel joists
US20060032702A1 (en) 2004-07-29 2006-02-16 Oshkosh Truck Corporation Composite boom assembly
GB0426944D0 (en) * 2004-12-08 2005-01-12 Airbus Uk Ltd A trussed structure
US7387277B2 (en) * 2004-12-29 2008-06-17 The Boeing Company Aircraft wing composed of composite and metal panels
FI118761B (fi) * 2006-02-09 2008-03-14 Patria Aerostructures Oy Ilma-aluksen siipi, kiinnitysjärjestely sekä välituki
JP4657189B2 (ja) * 2006-11-02 2011-03-23 本田技研工業株式会社 飛行機の翼構造
US7575194B2 (en) 2006-11-30 2009-08-18 The Boeing Company Apparatuses and methods for joining composite members and other structural members in aircraft wing boxes and other structures

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1706996A (en) * 1927-03-31 1929-03-26 Edmund B Carns Beam or girder
GB462904A (en) * 1935-09-14 1937-03-15 Richard Vogt Improvements in spars for the wings of aircraft
US2233969A (en) * 1938-12-30 1941-03-04 Bell Aircraft Corp Pressed wing rib
US2392818A (en) * 1940-11-18 1946-01-15 Lockheed Aircraft Corp Double skin sheet metal structural element
US5100713A (en) * 1989-06-06 1992-03-31 Toray Industries, Inc. Reinforcing woven fabric and preformed material, fiber reinforced composite material and beam using it

Also Published As

Publication number Publication date
EP2139761A1 (en) 2010-01-06
US20080245928A1 (en) 2008-10-09
JP5475639B2 (ja) 2014-04-16
US8490362B2 (en) 2013-07-23
US20130276310A1 (en) 2013-10-24
CN102317154A (zh) 2012-01-11
ES2622680T3 (es) 2017-07-07
US8677717B2 (en) 2014-03-25
EP2139761B1 (en) 2017-01-18
JP2010523397A (ja) 2010-07-15
WO2008124352A1 (en) 2008-10-16

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Granted publication date: 20150909

Termination date: 20210329

CF01 Termination of patent right due to non-payment of annual fee