GB201704787D0 - Foldable aerodynamic structure with slewing bearing - Google Patents
Foldable aerodynamic structure with slewing bearingInfo
- Publication number
- GB201704787D0 GB201704787D0 GBGB1704787.9A GB201704787A GB201704787D0 GB 201704787 D0 GB201704787 D0 GB 201704787D0 GB 201704787 A GB201704787 A GB 201704787A GB 201704787 D0 GB201704787 D0 GB 201704787D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- slewing bearing
- aerodynamic structure
- foldable aerodynamic
- foldable
- slewing
- 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- Withdrawn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
- 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
- B64C23/072—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 the wing tip airfoil devices being moveable in their entirety
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/40—Varying angle of sweep
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/56—Folding or collapsing to reduce overall dimensions of aircraft
-
- 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
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Rolling Contact Bearings (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1704787.9A GB2560900A (en) | 2017-03-27 | 2017-03-27 | Foldable aerodynamic structure with slewing bearing |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1704787.9A GB2560900A (en) | 2017-03-27 | 2017-03-27 | Foldable aerodynamic structure with slewing bearing |
Publications (2)
Publication Number | Publication Date |
---|---|
GB201704787D0 true GB201704787D0 (en) | 2017-05-10 |
GB2560900A GB2560900A (en) | 2018-10-03 |
Family
ID=58687809
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1704787.9A Withdrawn GB2560900A (en) | 2017-03-27 | 2017-03-27 | Foldable aerodynamic structure with slewing bearing |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2560900A (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11254412B2 (en) | 2019-03-29 | 2022-02-22 | The Boeing Company | Foldable raked wing tips having aerodynamic devices |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3279721A (en) * | 1964-10-30 | 1966-10-18 | Boeing Co | Bearing arrangement for variable sweep wing aircraft |
DE1481541C3 (en) * | 1966-12-22 | 1975-09-04 | Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen | Bearing for an aircraft wing that can be pivoted about a vertical axis |
FR1531596A (en) * | 1967-05-23 | 1968-07-05 | Dassault Avions | Connection device between the fuselage and the movable wings of a variable-geometry airplane |
FR1569233A (en) * | 1967-07-05 | 1969-05-30 | ||
DE1935920A1 (en) * | 1969-07-15 | 1971-05-27 | Messerschmitt Boelkow Blohm | Storage facility |
US8708286B2 (en) * | 2012-06-21 | 2014-04-29 | The Boeing Company | Swing tip assembly rotation joint |
US9296471B2 (en) * | 2013-10-06 | 2016-03-29 | The Boeing Company | Swing wing tip system, assembly and method with dual load path structure |
GB2539497A (en) * | 2015-06-19 | 2016-12-21 | Airbus Operations Ltd | A Rotational Joint For An Aircraft Folding Wing |
US9856910B2 (en) * | 2015-11-30 | 2018-01-02 | Roller Bearing Company Of America, Inc. | Self-lubricated thrust bearing for a hinged aircraft wing |
-
2017
- 2017-03-27 GB GB1704787.9A patent/GB2560900A/en not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
GB2560900A (en) | 2018-10-03 |
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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) |