CA2824727C - Extremite d'aile a rabattement horizontal - Google Patents
Extremite d'aile a rabattement horizontal Download PDFInfo
- Publication number
- CA2824727C CA2824727C CA2824727A CA2824727A CA2824727C CA 2824727 C CA2824727 C CA 2824727C CA 2824727 A CA2824727 A CA 2824727A CA 2824727 A CA2824727 A CA 2824727A CA 2824727 C CA2824727 C CA 2824727C
- Authority
- CA
- Canada
- Prior art keywords
- wing
- unfixed
- drop
- rotating
- link
- 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
- 230000007704 transition Effects 0.000 claims abstract description 38
- 238000000034 method Methods 0.000 claims description 89
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- 230000004044 response Effects 0.000 claims description 5
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- 238000010586 diagram Methods 0.000 description 15
- 238000004519 manufacturing process Methods 0.000 description 13
- 238000013461 design Methods 0.000 description 10
- 239000000463 material Substances 0.000 description 5
- 238000005728 strengthening Methods 0.000 description 4
- 238000012546 transfer Methods 0.000 description 4
- 238000012423 maintenance Methods 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- 239000003381 stabilizer Substances 0.000 description 3
- 230000001419 dependent effect Effects 0.000 description 2
- 230000005484 gravity Effects 0.000 description 2
- 230000010354 integration Effects 0.000 description 2
- 230000008520 organization Effects 0.000 description 2
- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000004917 carbon fiber Substances 0.000 description 1
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- 238000005461 lubrication Methods 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 238000009419 refurbishment Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
Classifications
-
- 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
- Y02T50/10—Drag reduction
Landscapes
- Tires In General (AREA)
- Toys (AREA)
- Transmission Devices (AREA)
Abstract
Il existe un besoin pour un aéronef qui peut tirer avantage dune longue envergure alaire en cours de vol et dune envergure alaire réduite à un aéroport. On propose un appareil dun aéronef qui comprend une aile comprenant des parties fixes et non fixes reliées de manière amovible. La partie non fixée comprend une partie rotative qui tourne entre des positions de vol et rabattues, et une partie abaissée mobile à un emplacement qui débloque la partie rotative et fournit un espace pour les parties fixes et non fixes à plier. Une articulation permet une rotation de la partie non fixe par rapport à la partie fixe autour dun axe de rotation qui est : vertical, sensiblement perpendiculaire à laile et/ou sensiblement parallèle à un axe de lacet. Un premier élément supporte la partie non fixe et connecte les parties non fixes et fixes; et une extension de rail sinsère dans un rail, et supporte et guide lélément dans des positions de vol et rabattues, et une transition entre les positions.
Applications Claiming Priority (6)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US201261720351P | 2012-10-30 | 2012-10-30 | |
| US13/664,416 | 2012-10-30 | ||
| US13/664,416 US10538307B2 (en) | 2011-10-01 | 2012-10-30 | Hinged raked wing tip |
| US61/720,351 | 2012-10-30 | ||
| US13/964,072 | 2013-08-10 | ||
| US13/964,072 US9296469B2 (en) | 2011-10-01 | 2013-08-10 | Horizontal folding wingtip |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CA2824727A1 CA2824727A1 (fr) | 2014-04-30 |
| CA2824727C true CA2824727C (fr) | 2018-01-02 |
Family
ID=50605969
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA2824727A Expired - Fee Related CA2824727C (fr) | 2012-10-30 | 2013-08-23 | Extremite d'aile a rabattement horizontal |
Country Status (1)
| Country | Link |
|---|---|
| CA (1) | CA2824727C (fr) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB201520289D0 (en) | 2015-11-18 | 2015-12-30 | Airbus Operations Ltd | An actuation assembly with a track and follower for use in moving a wing tip device on an aircraft wing |
-
2013
- 2013-08-23 CA CA2824727A patent/CA2824727C/fr not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| CA2824727A1 (fr) | 2014-04-30 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| EEER | Examination request |
Effective date: 20140716 |
|
| MKLA | Lapsed |
Effective date: 20220823 |