RU2002110770A - A method of manufacturing composite large blades - Google Patents
A method of manufacturing composite large bladesInfo
- Publication number
- RU2002110770A RU2002110770A RU2002110770/12A RU2002110770A RU2002110770A RU 2002110770 A RU2002110770 A RU 2002110770A RU 2002110770/12 A RU2002110770/12 A RU 2002110770/12A RU 2002110770 A RU2002110770 A RU 2002110770A RU 2002110770 A RU2002110770 A RU 2002110770A
- Authority
- RU
- Russia
- Prior art keywords
- blades
- polymerization
- manufacturing composite
- overpressure
- autoclave
- Prior art date
Links
- 239000002131 composite material Substances 0.000 title claims 2
- 238000004519 manufacturing process Methods 0.000 title claims 2
- 238000006116 polymerization reaction Methods 0.000 claims 3
- 239000011230 binding agent Substances 0.000 claims 1
- 239000011152 fibreglass Substances 0.000 claims 1
- 238000007789 sealing Methods 0.000 claims 1
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2002110770A RU2219058C1 (en) | 2002-04-22 | 2002-04-22 | Method of manufacture of composite large-sized blades |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2002110770A RU2219058C1 (en) | 2002-04-22 | 2002-04-22 | Method of manufacture of composite large-sized blades |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2002110770A true RU2002110770A (en) | 2003-10-27 |
RU2219058C1 RU2219058C1 (en) | 2003-12-20 |
Family
ID=32066327
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2002110770A RU2219058C1 (en) | 2002-04-22 | 2002-04-22 | Method of manufacture of composite large-sized blades |
Country Status (1)
Country | Link |
---|---|
RU (1) | RU2219058C1 (en) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB0614087D0 (en) * | 2006-07-14 | 2006-08-23 | Airbus Uk Ltd | Composite manufacturing method |
GB0712553D0 (en) | 2007-06-29 | 2007-08-08 | Airbus Uk Ltd | Composite panel stiffener |
GB0712549D0 (en) | 2007-06-29 | 2007-08-08 | Airbus Uk Ltd | Improvements in elongate composite structural members |
GB0712552D0 (en) | 2007-06-29 | 2007-08-08 | Airbus Uk Ltd | Elongate composite structural members and improvements therein |
DE102007062872A1 (en) * | 2007-12-28 | 2009-07-09 | Airbus Deutschland Gmbh | Method for producing a profile from fiber composite material |
GB0813161D0 (en) | 2008-07-18 | 2008-08-27 | Airbus Uk Ltd | Ramped stiffener and apparatus and method for forming the same |
GB0813149D0 (en) | 2008-07-18 | 2008-08-27 | Airbus Uk Ltd | Ramped stiffener and apparatus and method for forming the same |
GB0813146D0 (en) * | 2008-07-18 | 2008-08-27 | Airbus Uk Ltd | Ramped stiffener and apparatus and method for forming the same |
US10357922B2 (en) * | 2016-01-07 | 2019-07-23 | The Boeing Company | Edge breathers for composite products |
RU2678814C1 (en) * | 2017-09-14 | 2019-02-01 | Закрытое акционерное общество "Завод экспериментального машиностроения Ракетно-космической корпорации "Энергия" имени С.П. Королева" | Multi-layered structures manufacturing method |
-
2002
- 2002-04-22 RU RU2002110770A patent/RU2219058C1/en not_active IP Right Cessation
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