GB201610959D0 - Winglet - Google Patents
WingletInfo
- Publication number
- GB201610959D0 GB201610959D0 GBGB1610959.7A GB201610959A GB201610959D0 GB 201610959 D0 GB201610959 D0 GB 201610959D0 GB 201610959 A GB201610959 A GB 201610959A GB 201610959 D0 GB201610959 D0 GB 201610959D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- winglet
- 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.)
- Withdrawn
Links
Classifications
-
- 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
-
- 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
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
- B64C23/06—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices
- B64C23/065—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips
- B64C23/069—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips using one or more wing tip airfoil devices, e.g. winglets, splines, wing tip fences or raked wingtips
-
- 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
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1610959.7A GB2551708A (en) | 2016-06-23 | 2016-06-23 | Winglet |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1610959.7A GB2551708A (en) | 2016-06-23 | 2016-06-23 | Winglet |
Publications (2)
Publication Number | Publication Date |
---|---|
GB201610959D0 true GB201610959D0 (en) | 2016-08-10 |
GB2551708A GB2551708A (en) | 2018-01-03 |
Family
ID=56891539
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1610959.7A Withdrawn GB2551708A (en) | 2016-06-23 | 2016-06-23 | Winglet |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2551708A (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2577294A (en) | 2018-09-20 | 2020-03-25 | Airbus Operations Gmbh | A wing tip device |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8544800B2 (en) * | 2005-07-21 | 2013-10-01 | The Boeing Company | Integrated wingtip extensions for jet transport aircraft and other types of aircraft |
WO2015050617A2 (en) * | 2013-07-15 | 2015-04-09 | Design Intelligence Incorporated, LLC | Unmanned aerial vehicle (uav) with inter-connecting wing sections |
CN103625634B (en) * | 2013-12-17 | 2015-10-21 | 中国航天空气动力技术研究院 | A kind of winglet device of detachable adjustable inclination angle |
-
2016
- 2016-06-23 GB GB1610959.7A patent/GB2551708A/en not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
GB2551708A (en) | 2018-01-03 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |