RU2015109128A - Конструкционный материал для изготовления элементов конструкции, топливного бака, основного крыла и летательного аппарата - Google Patents
Конструкционный материал для изготовления элементов конструкции, топливного бака, основного крыла и летательного аппарата Download PDFInfo
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- RU2015109128A RU2015109128A RU2015109128A RU2015109128A RU2015109128A RU 2015109128 A RU2015109128 A RU 2015109128A RU 2015109128 A RU2015109128 A RU 2015109128A RU 2015109128 A RU2015109128 A RU 2015109128A RU 2015109128 A RU2015109128 A RU 2015109128A
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- structural
- fuel tank
- structural elements
- main wing
- elements according
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- 239000002828 fuel tank Substances 0.000 title claims abstract 7
- 239000004035 construction material Substances 0.000 title 1
- 239000000463 material Substances 0.000 claims abstract 12
- 229920000049 Carbon (fiber) Polymers 0.000 claims abstract 6
- 239000004917 carbon fiber Substances 0.000 claims abstract 6
- 239000011159 matrix material Substances 0.000 claims abstract 4
- 239000004033 plastic Substances 0.000 claims abstract 3
- 229920003023 plastic Polymers 0.000 claims abstract 3
- 239000004918 carbon fiber reinforced polymer Substances 0.000 claims abstract 2
- 239000000446 fuel Substances 0.000 claims abstract 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims abstract 2
- 239000012779 reinforcing material Substances 0.000 claims abstract 2
- 239000002990 reinforced plastic Substances 0.000 abstract 1
Classifications
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- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
- C08J5/00—Manufacture of articles or shaped materials containing macromolecular substances
- C08J5/04—Reinforcing macromolecular compounds with loose or coherent fibrous material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/02—Tanks
- B64D37/04—Arrangement thereof in or on aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/02—Tanks
- B64D37/06—Constructional adaptations thereof
- B64D37/08—Internal partitioning
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
- C08J5/00—Manufacture of articles or shaped materials containing macromolecular substances
- C08J5/04—Reinforcing macromolecular compounds with loose or coherent fibrous material
- C08J5/0405—Reinforcing macromolecular compounds with loose or coherent fibrous material with inorganic fibres
- C08J5/042—Reinforcing macromolecular compounds with loose or coherent fibrous material with inorganic fibres with carbon fibres
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
- C08J7/00—Chemical treatment or coating of shaped articles made of macromolecular substances
- C08J7/04—Coating
- C08J7/0427—Coating with only one layer of a composition containing a polymer binder
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
- C08J7/00—Chemical treatment or coating of shaped articles made of macromolecular substances
- C08J7/04—Coating
- C08J7/044—Forming conductive coatings; Forming coatings having anti-static properties
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/34—Tanks constructed integrally with wings, e.g. for fuel or water
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/02—Lightning protectors; Static dischargers
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
- C08J2300/00—Characterised by the use of unspecified polymers
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
- C08J2363/00—Characterised by the use of epoxy resins; Derivatives of epoxy resins
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
- C08J2367/00—Characterised by the use of polyesters obtained by reactions forming a carboxylic ester link in the main chain; Derivatives of such polymers
- C08J2367/06—Unsaturated polyesters
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
- C08J2400/00—Characterised by the use of unspecified polymers
- C08J2400/12—Polymers characterised by physical features, e.g. anisotropy, viscosity or electrical conductivity
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
- C08J7/00—Chemical treatment or coating of shaped articles made of macromolecular substances
- C08J7/04—Coating
-
- 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
-
- 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]
- Y10T428/31511—Of epoxy ether
-
- 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]
- Y10T428/31786—Of polyester [e.g., alkyd, etc.]
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Polymers & Plastics (AREA)
- Organic Chemistry (AREA)
- Medicinal Chemistry (AREA)
- Health & Medical Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Manufacturing & Machinery (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Inorganic Chemistry (AREA)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
- Laminated Bodies (AREA)
- Reinforced Plastic Materials (AREA)
- Moulding By Coating Moulds (AREA)
- Coating Of Shaped Articles Made Of Macromolecular Substances (AREA)
Abstract
1. Конструкционный материал для конструкций, содержащий:пластик, армированный углеродным волокном, в котором армирующий материал включает в себя углеродные волокна, а матрица включает в себя пластик;материал для защиты поверхности, обладающий низкой вязкостью, которому придана электропроводность за счет нанесения пластика, армированного углеродным волокном, на поверхность, на которой выступают окончания углеродных волокон.2. Конструкционный материал для элементов конструкции по п. 1, в котором матрице придана электропроводность.3. Конструкционный материал для элементов конструкции по п. 1, в котором удельное объемное сопротивление составляет 0,5 Ом·см и менее.4. Топливный бак, включающий в себя конструкционный материал для элементов конструкции по любому из пп. 1-3, в котором на поверхность, обращенную внутрь топливного бака, где хранится топливо, нанесен материал для защиты поверхности.5. Основное крыло, включающее в себя топливный бак по п. 4, который представляет собой элемент конструкции.6. Летательный аппарат, включающий в себя основное крыло по п. 5.
Claims (6)
1. Конструкционный материал для конструкций, содержащий:
пластик, армированный углеродным волокном, в котором армирующий материал включает в себя углеродные волокна, а матрица включает в себя пластик;
материал для защиты поверхности, обладающий низкой вязкостью, которому придана электропроводность за счет нанесения пластика, армированного углеродным волокном, на поверхность, на которой выступают окончания углеродных волокон.
2. Конструкционный материал для элементов конструкции по п. 1, в котором матрице придана электропроводность.
3. Конструкционный материал для элементов конструкции по п. 1, в котором удельное объемное сопротивление составляет 0,5 Ом·см и менее.
4. Топливный бак, включающий в себя конструкционный материал для элементов конструкции по любому из пп. 1-3, в котором на поверхность, обращенную внутрь топливного бака, где хранится топливо, нанесен материал для защиты поверхности.
5. Основное крыло, включающее в себя топливный бак по п. 4, который представляет собой элемент конструкции.
6. Летательный аппарат, включающий в себя основное крыло по п. 5.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2012224141 | 2012-10-09 | ||
JP2012-224141 | 2012-10-09 | ||
PCT/JP2013/077434 WO2014057960A1 (ja) | 2012-10-09 | 2013-10-09 | 構造体用構造材、燃料タンク、主翼及び航空機 |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2015109128A true RU2015109128A (ru) | 2016-12-10 |
RU2605716C2 RU2605716C2 (ru) | 2016-12-27 |
Family
ID=50477428
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2015109128/05A RU2605716C2 (ru) | 2012-10-09 | 2013-10-09 | Конструкционный материал для изготовления элементов конструкции, топливного бака, основного крыла и летательного аппарата |
Country Status (7)
Country | Link |
---|---|
US (1) | US9776732B2 (ru) |
JP (1) | JP5852255B2 (ru) |
CN (1) | CN104640913B (ru) |
BR (1) | BR112015006133A2 (ru) |
CA (1) | CA2885204C (ru) |
RU (1) | RU2605716C2 (ru) |
WO (1) | WO2014057960A1 (ru) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
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US20160196891A1 (en) * | 2014-09-26 | 2016-07-07 | The Boeing Company | Method for mitigating edge glow |
JP6580359B2 (ja) | 2015-03-31 | 2019-09-25 | 三菱重工業株式会社 | 構造体製造方法および構造体 |
US10472473B2 (en) * | 2015-05-26 | 2019-11-12 | The Boeing Company | Enhancing z-conductivity in carbon fiber reinforced plastic composite layups |
CN108367526A (zh) * | 2015-11-30 | 2018-08-03 | 塞特工业公司 | 用于复合结构的表面材料 |
US11745468B2 (en) | 2016-09-27 | 2023-09-05 | 3M Innovative Properties Company | Protection film |
CN109131904A (zh) * | 2018-09-28 | 2019-01-04 | 成都飞机工业(集团)有限责任公司 | 一种抗冲击的飞机整体油箱 |
US10913548B2 (en) | 2019-01-14 | 2021-02-09 | The Boeing Company | Metallic fittings for coupling composite ribs to skin panels of aircraft wings |
US11038334B2 (en) * | 2019-01-14 | 2021-06-15 | The Boeing Company | Aircraft wing composite ribs having electrical grounding paths |
CN111196733B (zh) * | 2020-01-09 | 2021-06-04 | 青岛理工大学 | 一种氧化致型形状记忆纤维及其制备方法和应用 |
JP2023073774A (ja) * | 2021-11-16 | 2023-05-26 | 三菱重工業株式会社 | 複合材料構造体及び複合材料構造体の製造方法 |
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US20160229552A1 (en) * | 2015-02-05 | 2016-08-11 | The Boeing Company | Intermetallic and composite metallic gap filler |
-
2013
- 2013-10-09 RU RU2015109128/05A patent/RU2605716C2/ru active
- 2013-10-09 US US14/434,553 patent/US9776732B2/en active Active
- 2013-10-09 BR BR112015006133A patent/BR112015006133A2/pt active Search and Examination
- 2013-10-09 JP JP2014540861A patent/JP5852255B2/ja active Active
- 2013-10-09 WO PCT/JP2013/077434 patent/WO2014057960A1/ja active Application Filing
- 2013-10-09 CA CA2885204A patent/CA2885204C/en active Active
- 2013-10-09 CN CN201380048718.1A patent/CN104640913B/zh not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
RU2605716C2 (ru) | 2016-12-27 |
US9776732B2 (en) | 2017-10-03 |
JPWO2014057960A1 (ja) | 2016-09-05 |
WO2014057960A1 (ja) | 2014-04-17 |
US20150274316A1 (en) | 2015-10-01 |
BR112015006133A2 (pt) | 2019-11-19 |
CA2885204C (en) | 2017-02-28 |
CA2885204A1 (en) | 2014-04-17 |
CN104640913A (zh) | 2015-05-20 |
CN104640913B (zh) | 2017-12-12 |
JP5852255B2 (ja) | 2016-02-03 |
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