RU2016129734A - Способ и устройство для производства профилированных элементов жесткости из композитного слоистого материала с уменьшенным образованием складок - Google Patents
Способ и устройство для производства профилированных элементов жесткости из композитного слоистого материала с уменьшенным образованием складок Download PDFInfo
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- stiffener
- pressing device
- composite laminate
- inner radius
- parts
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- 239000002131 composite material Substances 0.000 title claims 9
- 238000000034 method Methods 0.000 title claims 7
- 230000015572 biosynthetic process Effects 0.000 title claims 2
- 230000003247 decreasing effect Effects 0.000 title 1
- 239000000463 material Substances 0.000 title 1
- 238000003825 pressing Methods 0.000 claims 13
- 239000003351 stiffener Substances 0.000 claims 13
- 230000006835 compression Effects 0.000 claims 3
- 238000007906 compression Methods 0.000 claims 3
- 238000000465 moulding Methods 0.000 claims 2
- 238000005452 bending Methods 0.000 claims 1
- 239000000835 fiber Substances 0.000 claims 1
- 238000004519 manufacturing process Methods 0.000 claims 1
Classifications
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- 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
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/0007—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding involving treatment or provisions in order to avoid deformation or air inclusion, e.g. to improve surface quality
- B32B37/0015—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding involving treatment or provisions in order to avoid deformation or air inclusion, e.g. to improve surface quality to avoid warp or curl
-
- 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
- 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
- B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
- B29C53/02—Bending or folding
-
- 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
- B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
- B29C53/80—Component parts, details or accessories; Auxiliary operations
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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
- B29C70/04—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
- B29C70/28—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
-
- 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
- B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-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
- B29C70/28—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
- B29C70/549—Details of caul plates, e.g. materials or shape
-
- 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
- B29C70/56—Tensioning reinforcements before or during shaping
-
- 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
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/10—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the pressing technique, e.g. using action of vacuum or fluid pressure
- B32B37/1018—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the pressing technique, e.g. using action of vacuum or fluid pressure using only vacuum
-
- 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
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/14—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers
- B32B37/144—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers using layers with different mechanical or chemical conditions or properties, e.g. layers with different thermal shrinkage, layers under tension during bonding
-
- 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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/18—Spars; Ribs; Stringers
-
- 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
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/001—Profiled members, e.g. beams, sections
-
- 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
- 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
- B29L2031/7502—Supports, machine frames or beds, worktables
-
- 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
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- 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)
- Composite Materials (AREA)
- Chemical & Material Sciences (AREA)
- Aviation & Aerospace Engineering (AREA)
- Textile Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Transportation (AREA)
- Fluid Mechanics (AREA)
- Physics & Mathematics (AREA)
- Quality & Reliability (AREA)
- Moulding By Coating Moulds (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
Claims (25)
1. Способ изготовления профилированного элемента жесткости из композитного слоистого материала, включающий
сборку по существу плоской заготовки композитного слоистого материала;
формование заготовки композитного слоистого материала по существу с получением прямолинейного элемента жесткости, имеющего необходимую форму поперечного сечения;
формование профиля в элементе жесткости, имеющем внутренний радиус и внешний радиус; и
уменьшение деформации сжатия на внутреннем радиусе во время формования профиля.
2. Способ по п. 1, согласно которому сборка заготовки композитного слоистого материала включает укладку частей слоя препрега, каждая из которых обладает ориентацией волокон под углом 0°.
3. Способ по п. 2, согласно которому укладка частей слоя препрега включает их перекрытие.
4. Способ по п. 1, согласно которому формование профиля в элементе жесткости включает:
размещение прямолинейного элемента жесткости на криволинейной поверхности приспособления,
размещение устройства прессования на прямолинейном элементе жесткости и
использование устройства прессования для прессования элемента жесткости с упором в криволинейную поверхность приспособления.
5. Способ по п. 4, согласно которому уменьшение деформации сжатия на внутреннем радиусе включает увеличение деформации растяжения на внешнем радиусе устройства прессования.
6. Способ по п. 5, согласно которому увеличение деформации растяжения на внешнем радиусе устройства прессования выполнено посредством образования набора щелей во внешнем радиусе устройства прессования.
7. Способ по п. 4, согласно которому
уменьшение деформации сжатия на внутреннем радиусе элемента жесткости из композитного слоистого материала выполнено посредством использования устройства прессования для приложения силы натяжения к внешним концевым частям элемента жесткости из композитного слоистого материала.
8. Устройство для формования профилированного элемента жесткости из композитного слоистого материала, содержащее
профилированное устройство прессования, выполненное с возможностью формования и прессования элемента жесткости из композитного слоистого материала с упором в криволинейную поверхность приспособления, причем
устройство прессования имеет кривизну, превышающую кривизну поверхности приспособления.
9. Устройство по п. 8, в которому устройство прессования выполнено расширяемым и обеспечивающим приложение силы натяжения к элементу жесткости при формовании элемента жесткости с упором в поверхность приспособления.
10. Устройство по п. 9, в котором
устройство прессования имеет шляповидное поперечное сечение, имеющее часть в виде днища, пару частей в виде полок, пару частей в виде стенок, соединяющих часть в виде днища и части в виде полок, причем
часть в виде днища содержит набор отделенных друг от друга щелей.
11. Устройство по п. 8, в котором
устройство прессования содержит участок внутреннего радиуса и участок внешнего радиуса, причем
участок внутреннего радиуса содержит набор щелей, обеспечивающих возможность изгиба устройства прессования.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US14/876,475 | 2015-10-06 | ||
US14/876,475 US10399283B2 (en) | 2015-10-06 | 2015-10-06 | Method and device for producing contoured composite laminate stiffeners with reduced wrinkling |
Publications (2)
Publication Number | Publication Date |
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RU2016129734A true RU2016129734A (ru) | 2018-01-25 |
RU2727627C2 RU2727627C2 (ru) | 2020-07-22 |
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RU2016129734A RU2727627C2 (ru) | 2015-10-06 | 2016-07-20 | Способ и устройство для производства профилированных элементов жесткости из композитного слоистого материала с уменьшенным образованием складок |
Country Status (6)
Country | Link |
---|---|
US (1) | US10399283B2 (ru) |
EP (1) | EP3162544B1 (ru) |
CN (2) | CN106985488B (ru) |
ES (1) | ES2760944T3 (ru) |
PT (1) | PT3162544T (ru) |
RU (1) | RU2727627C2 (ru) |
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US20200254702A1 (en) * | 2019-02-07 | 2020-08-13 | The Boeing Company | Apparatus and method to tailor fiber distortion in composite parts |
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US7788784B2 (en) | 2006-10-17 | 2010-09-07 | The Boeing Company | Method of assembling composite structure |
FR2928295B1 (fr) | 2008-03-07 | 2017-12-08 | Duqueine Rhone Alpes | Procede et dispositif de moulage d'une piece courbe en materiau composite,et piece correspondante. |
DE102009029575B4 (de) | 2009-09-18 | 2011-06-22 | Airbus Operations GmbH, 21129 | Verfahren zur Versteifung eines Faserverbundbauteils und Anordnung zur Herstellung eines versteiften Faserverbundteils |
US8997642B2 (en) | 2011-08-08 | 2015-04-07 | The Boeing Company | Method for transporting, placing and compacting composite stiffeners |
US9931807B2 (en) | 2011-08-08 | 2018-04-03 | The Boeing Company | Flexible compactor with reinforcing spine |
FR2991624B1 (fr) | 2012-06-12 | 2015-03-06 | Airbus Operations Sas | Procede de realisation d'un profile courbe en materiau composite a partir d'une preforme rectiligne de nappes de fibres |
US9649809B2 (en) * | 2012-11-02 | 2017-05-16 | The Boeing Company | Wrinkle diffuser system for composites |
DE102014216160A1 (de) * | 2014-08-14 | 2016-02-18 | Airbus Operations Gmbh | Formkern, Verfahren und System zur Herstellung gekrümmter Verbundkomponenten |
-
2015
- 2015-10-06 US US14/876,475 patent/US10399283B2/en active Active
-
2016
- 2016-07-20 RU RU2016129734A patent/RU2727627C2/ru active
- 2016-07-21 EP EP16180509.8A patent/EP3162544B1/en active Active
- 2016-07-21 PT PT161805098T patent/PT3162544T/pt unknown
- 2016-07-21 ES ES16180509T patent/ES2760944T3/es active Active
- 2016-09-28 CN CN201610861728.2A patent/CN106985488B/zh active Active
- 2016-09-28 CN CN202010490777.6A patent/CN111619188B/zh active Active
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Publication number | Publication date |
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CN106985488B (zh) | 2020-06-30 |
RU2727627C2 (ru) | 2020-07-22 |
ES2760944T3 (es) | 2020-05-18 |
EP3162544A1 (en) | 2017-05-03 |
PT3162544T (pt) | 2019-11-25 |
CN106985488A (zh) | 2017-07-28 |
US10399283B2 (en) | 2019-09-03 |
US20170095983A1 (en) | 2017-04-06 |
CN111619188A (zh) | 2020-09-04 |
CN111619188B (zh) | 2022-02-08 |
EP3162544B1 (en) | 2019-09-04 |
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