SE361856B - - Google Patents
Info
- Publication number
- SE361856B SE361856B SE17579/69A SE1757969A SE361856B SE 361856 B SE361856 B SE 361856B SE 17579/69 A SE17579/69 A SE 17579/69A SE 1757969 A SE1757969 A SE 1757969A SE 361856 B SE361856 B SE 361856B
- Authority
- SE
- Sweden
Links
Classifications
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transmission Devices (AREA)
- Chairs For Special Purposes, Such As Reclining Chairs (AREA)
- Sealing Devices (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE1816065A DE1816065C3 (de) | 1968-12-20 | 1968-12-20 | Flugzeug mit um Hochachsen schwenkbaren Tragflügeln |
Publications (1)
Publication Number | Publication Date |
---|---|
SE361856B true SE361856B (xx) | 1973-11-19 |
Family
ID=5716932
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE17579/69A SE361856B (xx) | 1968-12-20 | 1969-12-19 |
Country Status (5)
Country | Link |
---|---|
US (1) | US3645477A (xx) |
DE (1) | DE1816065C3 (xx) |
FR (1) | FR2026750B1 (xx) |
GB (1) | GB1265584A (xx) |
SE (1) | SE361856B (xx) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3968946A (en) * | 1975-03-31 | 1976-07-13 | The Boeing Company | Extendable aerodynamic fairing |
US4206893A (en) * | 1978-09-27 | 1980-06-10 | The Boeing Company | Seal closure for slot in engine mounting strut |
US5282591A (en) * | 1992-12-21 | 1994-02-01 | The United States Of America As Represented By The Secretary Of The Navy | Active vortex control for a high performance wing |
EP2239195A1 (en) | 2009-04-06 | 2010-10-13 | Airbus Deutschland GmbH | Center fuselage bellows |
GB201018185D0 (en) | 2010-10-28 | 2010-12-08 | Airbus Operations Ltd | Wing tip device attachment apparatus and method |
US9296471B2 (en) * | 2013-10-06 | 2016-03-29 | The Boeing Company | Swing wing tip system, assembly and method with dual load path structure |
US11319054B2 (en) * | 2018-05-31 | 2022-05-03 | Airbus Operations Gmbh | Wing arrangement for an aircraft |
US11370526B2 (en) * | 2018-05-31 | 2022-06-28 | Airbus Operations Gmbh | Latching device for a wing arrangement for an aircraft |
CN110550187A (zh) * | 2018-06-01 | 2019-12-10 | 空中客车德国运营有限责任公司 | 用于飞行器的机翼装置和飞行器 |
EP3587252A1 (en) * | 2018-06-28 | 2020-01-01 | Airbus Operations GmbH | Arresting system for arresting a first aircraft component relative to a second aircraft component |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1515159A (fr) * | 1967-01-17 | 1968-03-01 | Dassault Avions | Dispositif d'obturateur mobile entre voilure et structure fixe pour avions ou aérodynes à géométrie variable |
-
1968
- 1968-12-20 DE DE1816065A patent/DE1816065C3/de not_active Expired
-
1969
- 1969-12-16 GB GB1265584D patent/GB1265584A/en not_active Expired
- 1969-12-18 US US886088A patent/US3645477A/en not_active Expired - Lifetime
- 1969-12-19 SE SE17579/69A patent/SE361856B/xx unknown
- 1969-12-22 FR FR6944418A patent/FR2026750B1/fr not_active Expired
Also Published As
Publication number | Publication date |
---|---|
DE1816065A1 (de) | 1970-08-13 |
FR2026750B1 (xx) | 1974-02-01 |
DE1816065C3 (de) | 1974-07-25 |
US3645477A (en) | 1972-02-29 |
FR2026750A1 (xx) | 1970-09-18 |
GB1265584A (xx) | 1972-03-01 |
DE1816065B2 (de) | 1973-11-29 |