CN101516724B - 允许承受构件的自稳定加强肋 - Google Patents
允许承受构件的自稳定加强肋 Download PDFInfo
- Publication number
- CN101516724B CN101516724B CN2007800348380A CN200780034838A CN101516724B CN 101516724 B CN101516724 B CN 101516724B CN 2007800348380 A CN2007800348380 A CN 2007800348380A CN 200780034838 A CN200780034838 A CN 200780034838A CN 101516724 B CN101516724 B CN 101516724B
- Authority
- CN
- China
- Prior art keywords
- strengthening rib
- spike
- section
- web
- reinforced
- 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
Links
- 238000011084 recovery Methods 0.000 title abstract 2
- 239000003351 stiffener Substances 0.000 title abstract 2
- 238000005728 strengthening Methods 0.000 claims description 132
- 230000002787 reinforcement Effects 0.000 claims description 5
- 239000002131 composite material Substances 0.000 claims description 4
- 230000000087 stabilizing effect Effects 0.000 claims description 3
- 230000006835 compression Effects 0.000 abstract 1
- 238000007906 compression Methods 0.000 abstract 1
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 description 12
- 238000011105 stabilization Methods 0.000 description 7
- 230000005484 gravity Effects 0.000 description 6
- 230000000694 effects Effects 0.000 description 5
- 230000002459 sustained effect Effects 0.000 description 5
- 238000005452 bending Methods 0.000 description 4
- 239000000835 fiber Substances 0.000 description 4
- 239000000463 material Substances 0.000 description 4
- 238000009745 resin transfer moulding Methods 0.000 description 4
- 230000015572 biosynthetic process Effects 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 238000001746 injection moulding Methods 0.000 description 3
- 239000004744 fabric Substances 0.000 description 2
- 238000007667 floating Methods 0.000 description 2
- TVEXGJYMHHTVKP-UHFFFAOYSA-N 6-oxabicyclo[3.2.1]oct-3-en-7-one Chemical compound C1C2C(=O)OC1C=CC2 TVEXGJYMHHTVKP-UHFFFAOYSA-N 0.000 description 1
- 101100334009 Caenorhabditis elegans rib-2 gene Proteins 0.000 description 1
- 238000009954 braiding Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000002950 deficient Effects 0.000 description 1
- 230000013632 homeostatic process Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000000178 monomer Substances 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 238000002791 soaking Methods 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 239000003381 stabilizer Substances 0.000 description 1
Images
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
- B64C1/064—Stringers; Longerons
-
- 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
-
- 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
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24174—Structurally defined web or sheet [e.g., overall dimension, etc.] including sheet or component perpendicular to plane of web or sheet
Abstract
Description
Claims (10)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0653880 | 2006-09-21 | ||
FR0653880A FR2906218B1 (fr) | 2006-09-21 | 2006-09-21 | Raidisseur autostabilise autorisant une reprise d'elements |
PCT/FR2007/051855 WO2008034988A1 (fr) | 2006-09-21 | 2007-08-30 | Raidisseur autostabilise autorisant une reprise d'elements |
Publications (2)
Publication Number | Publication Date |
---|---|
CN101516724A CN101516724A (zh) | 2009-08-26 |
CN101516724B true CN101516724B (zh) | 2012-06-13 |
Family
ID=37917339
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN2007800348380A Expired - Fee Related CN101516724B (zh) | 2006-09-21 | 2007-08-30 | 允许承受构件的自稳定加强肋 |
Country Status (11)
Country | Link |
---|---|
US (1) | US8524352B2 (zh) |
EP (1) | EP2064113B1 (zh) |
JP (1) | JP5343004B2 (zh) |
CN (1) | CN101516724B (zh) |
AT (1) | ATE455035T1 (zh) |
BR (1) | BRPI0716904A2 (zh) |
CA (1) | CA2662849C (zh) |
DE (1) | DE602007004349D1 (zh) |
FR (1) | FR2906218B1 (zh) |
RU (1) | RU2434781C2 (zh) |
WO (1) | WO2008034988A1 (zh) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2953092B1 (fr) * | 2009-11-25 | 2011-12-16 | European Aeronautic Defence & Space Co Eads France | Raidisseur electro-structural en materiau composite |
DE102014107404A1 (de) * | 2014-05-26 | 2015-11-26 | Airbus Operations Gmbh | Druckschott für einen Flugzeugrumpf |
US9809297B2 (en) * | 2015-08-26 | 2017-11-07 | The Boeing Company | Structures containing stiffeners having transition portions |
US10220935B2 (en) * | 2016-09-13 | 2019-03-05 | The Boeing Company | Open-channel stiffener |
CN109263860A (zh) * | 2018-11-19 | 2019-01-25 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | 一种机翼翼梁及机翼 |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2642523A1 (de) * | 1976-09-22 | 1978-03-23 | Burkhart Dipl Ing Grob | Verfahren und vorrichtung zur herstellung eines flugzeugbauteils in profilverstaerkter schalenbauweise |
US4909655A (en) * | 1989-02-06 | 1990-03-20 | Grumman Aerospace Corporation | Interleaved tab assembly for connecting structural members |
US6173925B1 (en) * | 1998-04-16 | 2001-01-16 | Daimlerchrysler Ag | Skin-rib structure |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6513757B1 (en) * | 1999-07-19 | 2003-02-04 | Fuji Jukogyo Kabushiki Kaisha | Wing of composite material and method of fabricating the same |
JP4316067B2 (ja) * | 1999-09-30 | 2009-08-19 | 富士重工業株式会社 | 複合材翼およびその成形方法 |
SE517133C2 (sv) * | 2001-06-05 | 2002-04-16 | Saab Ab | Anordning för att stödja en skalyta i ett flygplansskrov |
JP4639551B2 (ja) * | 2001-08-10 | 2011-02-23 | 東レ株式会社 | Cfrp製スキン−ストリンガー構造部材の製造方法 |
DE10301445B4 (de) * | 2003-01-16 | 2005-11-17 | Airbus Deutschland Gmbh | Leichtbau-Strukturbauteil insbesondere für Flugzeuge und Verfahren zu seiner Herstellung |
-
2006
- 2006-09-21 FR FR0653880A patent/FR2906218B1/fr not_active Expired - Fee Related
-
2007
- 2007-08-30 JP JP2009528762A patent/JP5343004B2/ja not_active Expired - Fee Related
- 2007-08-30 AT AT07823754T patent/ATE455035T1/de not_active IP Right Cessation
- 2007-08-30 DE DE602007004349T patent/DE602007004349D1/de active Active
- 2007-08-30 CA CA2662849A patent/CA2662849C/fr not_active Expired - Fee Related
- 2007-08-30 BR BRPI0716904-3A patent/BRPI0716904A2/pt not_active IP Right Cessation
- 2007-08-30 EP EP07823754A patent/EP2064113B1/fr not_active Not-in-force
- 2007-08-30 US US12/438,252 patent/US8524352B2/en active Active
- 2007-08-30 CN CN2007800348380A patent/CN101516724B/zh not_active Expired - Fee Related
- 2007-08-30 RU RU2009114836/11A patent/RU2434781C2/ru not_active IP Right Cessation
- 2007-08-30 WO PCT/FR2007/051855 patent/WO2008034988A1/fr active Application Filing
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2642523A1 (de) * | 1976-09-22 | 1978-03-23 | Burkhart Dipl Ing Grob | Verfahren und vorrichtung zur herstellung eines flugzeugbauteils in profilverstaerkter schalenbauweise |
US4909655A (en) * | 1989-02-06 | 1990-03-20 | Grumman Aerospace Corporation | Interleaved tab assembly for connecting structural members |
US6173925B1 (en) * | 1998-04-16 | 2001-01-16 | Daimlerchrysler Ag | Skin-rib structure |
Also Published As
Publication number | Publication date |
---|---|
WO2008034988A1 (fr) | 2008-03-27 |
ATE455035T1 (de) | 2010-01-15 |
RU2434781C2 (ru) | 2011-11-27 |
DE602007004349D1 (de) | 2010-03-04 |
CA2662849C (fr) | 2014-09-23 |
JP5343004B2 (ja) | 2013-11-13 |
EP2064113A1 (fr) | 2009-06-03 |
US8524352B2 (en) | 2013-09-03 |
US20100297390A1 (en) | 2010-11-25 |
CA2662849A1 (fr) | 2008-03-27 |
RU2009114836A (ru) | 2010-10-27 |
EP2064113B1 (fr) | 2010-01-13 |
FR2906218B1 (fr) | 2009-05-15 |
FR2906218A1 (fr) | 2008-03-28 |
CN101516724A (zh) | 2009-08-26 |
JP2010504241A (ja) | 2010-02-12 |
BRPI0716904A2 (pt) | 2013-11-05 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C53 | Correction of patent of invention or patent application | ||
CB02 | Change of applicant information |
Address after: France Toulouse Applicant after: Airbus Operations S.A.S. Address before: France Toulouse Applicant before: Airbus France Address after: France Toulouse Applicant after: Airbus France Address before: France Toulouse Applicant before: Airbus France |
|
COR | Change of bibliographic data |
Free format text: CORRECT: APPLICANT; FROM: AIRBUS FRANCE TO: AIRBUS OPERATIONS GMBH |
|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20120613 Termination date: 20200830 |
|
CF01 | Termination of patent right due to non-payment of annual fee |