CA2829899C - Joint pour ailes faites de materiaux composites - Google Patents
Joint pour ailes faites de materiaux composites Download PDFInfo
- Publication number
- CA2829899C CA2829899C CA2829899A CA2829899A CA2829899C CA 2829899 C CA2829899 C CA 2829899C CA 2829899 A CA2829899 A CA 2829899A CA 2829899 A CA2829899 A CA 2829899A CA 2829899 C CA2829899 C CA 2829899C
- Authority
- CA
- Canada
- Prior art keywords
- inboard
- outboard
- stringer
- wing
- chord
- 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.)
- Active
Links
- 239000002131 composite material Substances 0.000 title claims description 18
- 235000012149 noodles Nutrition 0.000 claims abstract description 80
- 238000000034 method Methods 0.000 claims description 28
- 230000000712 assembly Effects 0.000 claims description 7
- 238000000429 assembly Methods 0.000 claims description 7
- 238000009966 trimming Methods 0.000 claims description 6
- 238000004519 manufacturing process Methods 0.000 description 8
- 239000000463 material Substances 0.000 description 8
- 239000004918 carbon fiber reinforced polymer Substances 0.000 description 3
- 239000000835 fiber Substances 0.000 description 3
- 239000011800 void material Substances 0.000 description 3
- 230000008901 benefit Effects 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 239000000945 filler Substances 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 239000011152 fibreglass Substances 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical class C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000008520 organization Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 238000009419 refurbishment Methods 0.000 description 1
- 235000013599 spices Nutrition 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
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
- B64C1/26—Attaching the wing or tail units or stabilising surfaces
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/18—Spars; Ribs; Stringers
- B64C3/182—Stringers, longerons
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/26—Construction, shape, or attachment of separate skins, e.g. panels
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Connection Of Plates (AREA)
Abstract
Un joint pour ailes comprend une première plaque de serrage, une seconde plaque de serrage et un ensemble panneau daile, lensemble panneau daile constitué dun longeron connecté à un revêtement daile, une partie de lensemble panneau daile étant fixée entre la première plaque de serrage et la seconde plaque de serrage, dans laquelle le longeron de la partie de lensemble panneau daile fixé entre la première plaque de serrage et la seconde plaque de serrage est taillé afin dexposer un flotteur.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CA2829899A CA2829899C (fr) | 2013-10-10 | 2013-10-10 | Joint pour ailes faites de materiaux composites |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CA2829899A CA2829899C (fr) | 2013-10-10 | 2013-10-10 | Joint pour ailes faites de materiaux composites |
Publications (2)
Publication Number | Publication Date |
---|---|
CA2829899A1 CA2829899A1 (fr) | 2015-04-10 |
CA2829899C true CA2829899C (fr) | 2017-07-04 |
Family
ID=52824825
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA2829899A Active CA2829899C (fr) | 2013-10-10 | 2013-10-10 | Joint pour ailes faites de materiaux composites |
Country Status (1)
Country | Link |
---|---|
CA (1) | CA2829899C (fr) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110406658B (zh) * | 2019-08-08 | 2024-07-23 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | 一种机翼机身连接接头及飞机 |
US11214349B2 (en) | 2019-09-24 | 2022-01-04 | The Boeing Company | Stringers for aircraft skin structures and related methods |
US11718047B2 (en) | 2019-12-12 | 2023-08-08 | The Boeing Company | Flyaway stringer end caps |
US11806948B2 (en) * | 2019-12-12 | 2023-11-07 | The Boeing Company | Method of forming flyaway stringer end caps |
US11858661B2 (en) | 2022-02-10 | 2024-01-02 | The Boeing Company | Method of manufacturing an assembly having a nominal thickness skin panel |
CN115214872A (zh) * | 2022-06-17 | 2022-10-21 | 航天特种材料及工艺技术研究所 | 一种复合材料主承载梁及整体成型方法 |
-
2013
- 2013-10-10 CA CA2829899A patent/CA2829899C/fr active Active
Also Published As
Publication number | Publication date |
---|---|
CA2829899A1 (fr) | 2015-04-10 |
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