[go: up one dir, main page]

RU2011118500A - Система и способ для формирования подкрепляющего элемента за одно целое с многослойным металловолокнистым листом - Google Patents

Система и способ для формирования подкрепляющего элемента за одно целое с многослойным металловолокнистым листом Download PDF

Info

Publication number
RU2011118500A
RU2011118500A RU2011118500/11A RU2011118500A RU2011118500A RU 2011118500 A RU2011118500 A RU 2011118500A RU 2011118500/11 A RU2011118500/11 A RU 2011118500/11A RU 2011118500 A RU2011118500 A RU 2011118500A RU 2011118500 A RU2011118500 A RU 2011118500A
Authority
RU
Russia
Prior art keywords
layer
metal layer
extreme inner
additional layer
inner metal
Prior art date
Application number
RU2011118500/11A
Other languages
English (en)
Other versions
RU2501710C2 (ru
Inventor
Дейвид П. ХЕК (US)
Дейвид П. ХЕК
Лорен Дж. СТРАМ (US)
Лорен Дж. СТРАМ
Original Assignee
Дзе Боинг Компани (Us)
Дзе Боинг Компани
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=41528523&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=RU2011118500(A) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Дзе Боинг Компани (Us), Дзе Боинг Компани filed Critical Дзе Боинг Компани (Us)
Publication of RU2011118500A publication Critical patent/RU2011118500A/ru
Application granted granted Critical
Publication of RU2501710C2 publication Critical patent/RU2501710C2/ru

Links

Classifications

    • 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
    • B64C1/12—Construction or attachment of skin panels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K20/00—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
    • B23K20/12—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating the heat being generated by friction; Friction welding
    • 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
    • B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/06—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using friction, e.g. spin welding
    • 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
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B15/043—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of metal
    • 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
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/14—Layered products comprising a layer of metal next to a 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
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/20—Layered products comprising a layer of metal comprising aluminium or copper
    • 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
    • B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/02—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by features of form at particular places, e.g. in edge regions
    • B32B3/08—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by features of form at particular places, e.g. in edge regions characterised by added members at particular parts
    • 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
    • B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/26—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer
    • B32B3/30—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer characterised by a layer formed with recesses or projections, e.g. hollows, grooves, protuberances, ribs
    • 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
    • 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
    • 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
    • B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/04—Interconnection of layers
    • B32B7/12—Interconnection of layers using interposed adhesives or interposed materials with bonding properties
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2101/00—Articles made by soldering, welding or cutting
    • B23K2101/001—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
    • 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
    • B32B2307/30—Properties of the layers or laminate having particular thermal properties
    • 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
    • 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
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/70—Other properties
    • B32B2307/718—Weight, e.g. weight per square meter
    • 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
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/12347—Plural layers discontinuously bonded [e.g., spot-weld, mechanical fastener, etc.]
    • 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
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/12375—All metal or with adjacent metals having member which crosses the plane of another member [e.g., T or X cross section, etc.]
    • 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
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/1241—Nonplanar uniform thickness or nonlinear uniform diameter [e.g., L-shape]
    • 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
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/12444—Embodying fibers interengaged or between layers [e.g., paper, etc.]
    • 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
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/31504—Composite [nonstructural laminate]
    • Y10T428/31678—Of metal

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)

Abstract

1. Цельная конструкция, включающая в себя: ! - многослойный металловолокнистый лист, содержащий неметаллические и металлические слои и крайний внутренний металлический слой; и ! - по меньшей мере один добавочный слой, присоединенный к крайнему внутреннему металлическому слою путем сварки трением с перемешиванием. ! 2. Цельная конструкция по п.1, в которой неметаллические и металлические слои расположены с чередованием. ! 3. Цельная конструкция по п.1, в которой добавочный слой выполнен из металлического материала. ! 4. Цельная конструкция по п.1, в которой добавочный слой выполнен в виде удлиненной полосы. ! 5. Цельная конструкция по п.1, в которой добавочный слой представляет собой несколько добавочных слоев, в том числе первый добавочный слой, присоединенный к крайнему внутреннему металлическому слою. ! 6. Способ изготовления цельной конструкции, характеризующийся следующими стадиями: ! - подготавливают многослойный металловолокнистый лист, содержащий неметаллические и металлические слои и по меньшей мере один крайний внутренний металлический слой; ! - к крайнему внутреннему металлическому слою присоединяют путем сварки трением с перемешиванием по меньшей мере один добавочный слой с получением сварного полуфабриката. ! 7. Способ по п.6, характеризующийся тем, что крайний внутренний металлический слой и добавочный слой образуют между собой границу раздела, и для присоединения добавочного слоя к крайнему внутреннему металлическому слою путем сварки трением с перемешиванием ориентируют палец поперек границы раздела, так что палец входит в добавочный слой, и вращают палец в процессе его перемещения вдоль границ

Claims (13)

1. Цельная конструкция, включающая в себя:
- многослойный металловолокнистый лист, содержащий неметаллические и металлические слои и крайний внутренний металлический слой; и
- по меньшей мере один добавочный слой, присоединенный к крайнему внутреннему металлическому слою путем сварки трением с перемешиванием.
2. Цельная конструкция по п.1, в которой неметаллические и металлические слои расположены с чередованием.
3. Цельная конструкция по п.1, в которой добавочный слой выполнен из металлического материала.
4. Цельная конструкция по п.1, в которой добавочный слой выполнен в виде удлиненной полосы.
5. Цельная конструкция по п.1, в которой добавочный слой представляет собой несколько добавочных слоев, в том числе первый добавочный слой, присоединенный к крайнему внутреннему металлическому слою.
6. Способ изготовления цельной конструкции, характеризующийся следующими стадиями:
- подготавливают многослойный металловолокнистый лист, содержащий неметаллические и металлические слои и по меньшей мере один крайний внутренний металлический слой;
- к крайнему внутреннему металлическому слою присоединяют путем сварки трением с перемешиванием по меньшей мере один добавочный слой с получением сварного полуфабриката.
7. Способ по п.6, характеризующийся тем, что крайний внутренний металлический слой и добавочный слой образуют между собой границу раздела, и для присоединения добавочного слоя к крайнему внутреннему металлическому слою путем сварки трением с перемешиванием ориентируют палец поперек границы раздела, так что палец входит в добавочный слой, и вращают палец в процессе его перемещения вдоль границы раздела с образованием сварного соединения.
8. Способ по п.6, характеризующийся тем, что добавочный слой представляет собой несколько добавочных слоев, в том числе первый добавочный слой, причем добавочные слои последовательно присоединяют к первому добавочному слою путем сварки трением с перемешиванием.
9. Способ по п.6, характеризующийся тем, что сварной полуфабрикат подвергают механической обработке с формированием по меньшей мере одного подкрепляющего элемента.
10. Способ изготовления цельной конструкции, характеризующийся следующими стадиями:
- подготавливают заготовку;
- к заготовке присоединяют путем сварки трением с перемешиванием по меньшей мере один добавочный слой с получением сварного полуфабриката;
- сварной полуфабрикат подвергают механической обработке для формирования внешней поверхности крайнего внутреннего металлического слоя многослойного металловолокнистого листа;
- на внешнюю поверхность крайнего внутреннего металлического слоя укладывают неметаллические и металлические слои с получением многослойного металловолокнистого листа;
- сварной полуфабрикат подвергают механической обработке для формирования внутренней поверхности крайнего внутреннего металлического слоя;
- сварной полуфабрикат подвергают механической обработке с формированием по меньшей мере одного подкрепляющего элемента, образующего единое целое с крайним внутренним металлическим слоем.
11. Цельная конструкция, включающая в себя:
- многослойный металловолокнистый лист, содержащий неметаллические и металлические слои и по меньшей мере один крайний внутренний металлический слой; и
- по меньшей мере один подкрепляющий элемент, выполненный за одно целое с крайним внутренним металлическим слоем.
12. Способ изготовления цельной конструкции, характеризующийся следующими стадиями:
- подготавливают заготовку;
- подвергают заготовку механической обработке для формирования внешней поверхности крайнего внутреннего металлического слоя многослойного металловолокнистого листа;
- на внешнюю поверхность крайнего внутреннего металлического слоя укладывают неметаллические и металлические слои с получением многослойного металловолокнистого листа;
- подвергают заготовку механической обработке для формирования внутренней поверхности крайнего внутреннего металлического слоя и по меньшей мере одного подкрепляющего элемента.
13. Способ по п.12, характеризующийся тем, что механическую обработку заготовки для формирования внутренней поверхности выполняют перед механической обработкой заготовки для формирования внешней поверхности.
RU2011118500/11A 2008-10-10 2009-10-09 Система и способ для формирования подкрепляющего элемента за одно целое с многослойным металловолокнистым листом RU2501710C2 (ru)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US12/249,740 US8678267B2 (en) 2008-10-10 2008-10-10 System and method for integrally forming a stiffener with a fiber metal laminate
US12/249,740 2008-10-10
PCT/US2009/060102 WO2010042782A1 (en) 2008-10-10 2009-10-09 System and method for integrally forming a substructure element with a fiber metal laminate

Publications (2)

Publication Number Publication Date
RU2011118500A true RU2011118500A (ru) 2012-11-20
RU2501710C2 RU2501710C2 (ru) 2013-12-20

Family

ID=41528523

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2011118500/11A RU2501710C2 (ru) 2008-10-10 2009-10-09 Система и способ для формирования подкрепляющего элемента за одно целое с многослойным металловолокнистым листом

Country Status (4)

Country Link
US (2) US8678267B2 (ru)
EP (1) EP2344378B2 (ru)
RU (1) RU2501710C2 (ru)
WO (1) WO2010042782A1 (ru)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8100316B2 (en) * 2008-05-29 2012-01-24 Airbus Operations Gmbh Method for joining aircraft fuselage elements by friction stir welding (fsw)
US8678267B2 (en) 2008-10-10 2014-03-25 The Boeing Company System and method for integrally forming a stiffener with a fiber metal laminate
US8141764B1 (en) 2010-04-06 2012-03-27 United Launch Alliance, Llc Friction stir welding apparatus, system and method
US8123104B1 (en) 2010-04-06 2012-02-28 United Launch Alliance, Llc Friction welding apparatus, system and method
US7866532B1 (en) 2010-04-06 2011-01-11 United Launch Alliance, Llc Friction stir welding apparatus, system and method
EP2543499A1 (en) * 2011-07-06 2013-01-09 LM Wind Power A/S Wind turbine blade comprising metal filaments and carbon fibres and a method of manufacturing thereof
US20150360317A1 (en) * 2013-01-22 2015-12-17 University Of Utah Research Foundation Friction Spot Welding and Friction Seam Welding
US20140315040A1 (en) * 2013-04-19 2014-10-23 Sikorsky Aircraft Corporation Integrally formed stiffener
CN105339125B (zh) * 2013-06-26 2018-10-12 伊苏瓦尔肯联铝业 通过线性摩擦焊接获得的改进的结构元件
US10407755B2 (en) 2014-01-08 2019-09-10 United Technologies Corporation Solid-state method for forming an alloy
DE102014101907A1 (de) * 2014-02-14 2015-08-20 Thyssenkrupp Ag Metallblech mit lokaler metallischer Verstärkung und Verfahren zu dessen Herstellung
US9376013B2 (en) 2014-08-05 2016-06-28 KIRCHHOFF Van-Rob Automotive Composite fuel tank support
US9708065B2 (en) 2015-04-07 2017-07-18 The Boeing Company Crown cabin configuration for an aircraft
US10889067B1 (en) * 2015-04-13 2021-01-12 Lockheed Martin Corporation Tension-wound solid state additive manufacturing
US10279423B2 (en) 2016-08-17 2019-05-07 The Boeing Company Apparatuses and methods for fabricating metal matrix composite structures
US11273622B2 (en) 2016-12-14 2022-03-15 The Boeing Company Stiffening elements that comprise integral current flowpaths
US11014337B2 (en) 2016-12-14 2021-05-25 The Boeing Company Laminate structures comprising fiber-reinforced thermoplastic prepreg plies
US11077644B2 (en) 2016-12-14 2021-08-03 The Boeing Company Material systems and methods of manufacturing material systems
CN108312665B (zh) * 2018-02-06 2020-06-16 哈尔滨工业大学 多级结构Ti-Al-Cf层状复合材料的制备方法
TWI682822B (zh) * 2018-07-16 2020-01-21 國立中正大學 摩擦攪拌積層製造方法
DE102018212156A1 (de) * 2018-07-20 2020-01-23 Technische Universität Ilmenau Verfahren zum Beschichten eines Werkstücks, Werkstück, Beschichtungsmaschine, und Verwendung eines Reibschweißgeräts
CN109175669A (zh) * 2018-09-17 2019-01-11 上海航天设备制造总厂有限公司 一种摩擦点焊增材制造方法
CN109226959B (zh) * 2018-10-26 2020-08-25 同济大学 一种纤维增强金属基复合板材及其预处理方法
AU2022246294A1 (en) * 2021-03-22 2023-10-05 Commonwealth Scientific And Industrial Research Organisation Method for forming a metal matrix composite structure
EP4438272A1 (en) * 2023-03-31 2024-10-02 Airbus Operations GmbH Friction stir welding method and device, as well as workpiece comprising a butt weld seam

Family Cites Families (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4657171A (en) * 1985-06-13 1987-04-14 General Electric Company Repair of a member having a projection
US5207371A (en) * 1991-07-29 1993-05-04 Prinz Fritz B Method and apparatus for fabrication of three-dimensional metal articles by weld deposition
US5591363A (en) * 1995-03-02 1997-01-07 Westinghouse Electric Corporation Optimized welding technique for NiMoV rotors for high temperature applications
US5713507A (en) * 1996-03-21 1998-02-03 Rockwell International Corporation Programmable friction stir welding process
US5914055A (en) * 1996-11-18 1999-06-22 Tennessee Valley Authority Rotor repair system and technique
US5794338A (en) * 1997-04-04 1998-08-18 General Electric Company Method for repairing a turbine engine member damaged tip
GB9713209D0 (en) * 1997-06-20 1997-08-27 British Aerospace Friction welding metal components
US6118098A (en) * 1997-10-10 2000-09-12 Siemens Westinghouse Power Corporation Turbine rotor modernization and repair method
US6441338B1 (en) * 1999-04-19 2002-08-27 Joshua E. Rabinovich Rapid manufacturing of steel rule dies and other 3-dimensional products, apparatus, process and products
CA2383674A1 (en) * 1999-09-03 2001-03-15 Brian J. Dracup Friction stir welding as a rivet replacement technology
US6814823B1 (en) * 1999-09-16 2004-11-09 Solidica, Inc. Object consolidation through sequential material deposition
US6457629B1 (en) * 1999-10-04 2002-10-01 Solidica, Inc. Object consolidation employing friction joining
US6332272B1 (en) * 2000-01-07 2001-12-25 Siemens Westinghouse Power Corporation Method of repairing a turbine blade
RU2162189C1 (ru) * 2000-04-13 2001-01-20 Общество с ограниченной ответственностью "Транс-Прибор" Способ тепловой защиты, слоистая структура для его осуществления и защитный корпус из нее
US6582539B2 (en) * 2001-06-08 2003-06-24 Lockheed Martin Corporation Method for making large composite structures without use of an autoclave
EP1336469A1 (en) 2002-02-19 2003-08-20 Alenia Aeronautica S.P.A. Methods of manufacturing a stiffening element for an aircraft skin panel and a skin panel provided with the stiffening element
DE10301445B4 (de) * 2003-01-16 2005-11-17 Airbus Deutschland Gmbh Leichtbau-Strukturbauteil insbesondere für Flugzeuge und Verfahren zu seiner Herstellung
US7105205B2 (en) * 2003-03-28 2006-09-12 Research Foundation Of The State Of New York Densification of thermal spray coatings
US7090112B2 (en) * 2003-08-29 2006-08-15 The Boeing Company Method and sealant for joints
US8266800B2 (en) * 2003-09-10 2012-09-18 Siemens Energy, Inc. Repair of nickel-based alloy turbine disk
US7398911B2 (en) * 2003-12-16 2008-07-15 The Boeing Company Structural assemblies and preforms therefor formed by friction welding
CA2548369A1 (en) * 2004-01-05 2005-07-28 Airbus Deutschland Gmbh Fuselage
GB0412775D0 (en) * 2004-06-09 2004-07-07 Rolls Royce Plc Method of replacing damaged aerofoil
US7347351B2 (en) * 2004-08-18 2008-03-25 The Boeing Company Apparatus and system for unitized friction stir welded structures and associated method
US7628876B2 (en) * 2005-10-25 2009-12-08 Gm Global Technology Operations, Inc. Friction stir weld bonding of metal-polymer-metal laminates
DE102006031436B4 (de) * 2006-07-07 2012-12-06 Airbus Operations Gmbh Strukturelement, Verfahren zur Herstellung eines derartigen Strukturelements und Flugzeug mit einem derartigen Strukturelement
US7690164B2 (en) * 2006-12-05 2010-04-06 Lockheed Martin Corporation System, method, and apparatus for structural lug formed from a combination of metal and composite laminate materials
US8393574B2 (en) * 2006-12-22 2013-03-12 The Boeing Company Composite leg structure for a lightweight aircraft seat assembly
DE102007063608B4 (de) * 2007-05-23 2011-04-21 Airbus Operations Gmbh Verbund und Rumpfzellenabschnitt mit einem derartigen Verbund
US8678267B2 (en) 2008-10-10 2014-03-25 The Boeing Company System and method for integrally forming a stiffener with a fiber metal laminate

Also Published As

Publication number Publication date
EP2344378A1 (en) 2011-07-20
US9027820B2 (en) 2015-05-12
EP2344378B2 (en) 2019-07-10
US20140220372A1 (en) 2014-08-07
RU2501710C2 (ru) 2013-12-20
US8678267B2 (en) 2014-03-25
WO2010042782A1 (en) 2010-04-15
EP2344378B1 (en) 2012-08-08
US20100092789A1 (en) 2010-04-15

Similar Documents

Publication Publication Date Title
RU2011118500A (ru) Система и способ для формирования подкрепляющего элемента за одно целое с многослойным металловолокнистым листом
US10363592B2 (en) Method for preparing metal composite plate strip by rolling
JP2019171857A5 (ru)
CN103878484B (zh) 一种层状双金属复合材料高效对接激光焊接方法
CN102679134B (zh) 一种钛钢复合板材及其制造方法
EP2492083A3 (en) Joint structure for fiber reinforced resin and metal, and joining method for fiber reinforced resin and metal
MY184340A (en) Method for producing a multi-layer large pipe
MX2019007147A (es) Procedimiento de fabricacion de un compuesto multicapa de metal-polimero soldable.
CN103350124A (zh) 一种输送石油天然气的直缝双金属复合焊管的制造方法
WO2010059528A3 (en) Method for downhole screen manufacturing
PH12015501719A1 (en) High strength thick steel plate for high heat input welding with excellent brittle crack arrestability and manufacturing method therefor
DK1827727T3 (da) Fremgangsmåde til fremstilling af et flerlagsrör
CN103269811A (zh) 具有提高的抗疲劳强度的挠性管及其制造方法
TW200722580A (en) Fabricating three-dimensional annular fiber structures
WO2008033882A3 (en) Aluminum clad steel composite for heat exchanger tubes and manifolds
CN108581378A (zh) 一种船体弯头连接管的制作方法
CN102861974A (zh) 一种不同强度及板厚桥梁钢组合的角接埋弧焊接方法
BR0316896A (pt) Conduto e método de fabricação do mesmo
RU2017120834A (ru) Нетканый звукопоглощающий рукав и способ его изготовления
JP2006517623A5 (ru)
CN207048691U (zh) 一种冶金式复合油井管
RU2010113479A (ru) Способ ремонта трещин металлоконструкций
RU2581527C2 (ru) Способ изготовления трехслойного ребристого строительного элемента
RU2015136362A (ru) Способ изготовления сварных стрингерных конструкций
CN104859196A (zh) 一种耐高温高强度铝合金板材