NL6903311A - - Google Patents
Info
- Publication number
- NL6903311A NL6903311A NL6903311A NL6903311A NL6903311A NL 6903311 A NL6903311 A NL 6903311A NL 6903311 A NL6903311 A NL 6903311A NL 6903311 A NL6903311 A NL 6903311A NL 6903311 A NL6903311 A NL 6903311A
- Authority
- NL
- Netherlands
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)
- Tires In General (AREA)
- Toys (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR958702A FR1388089A (fr) | 1963-12-27 | 1963-12-27 | Avion à configuration variable |
| FR142393A FR94080E (fr) | 1963-12-27 | 1968-03-05 | Avion a configuration variable. |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| NL6903311A true NL6903311A (enExample) | 1969-09-09 |
Family
ID=8646998
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| NL6903311A NL6903311A (enExample) | 1963-12-27 | 1969-03-04 |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US3572617A (enExample) |
| DE (1) | DE1909835A1 (enExample) |
| FR (1) | FR94080E (enExample) |
| GB (1) | GB1251698A (enExample) |
| NL (1) | NL6903311A (enExample) |
Families Citing this family (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1307990A (en) * | 1969-05-27 | 1973-02-21 | British Aircraft Corp Ltd | Variable-geometry aircraft |
| US3680816A (en) * | 1969-12-29 | 1972-08-01 | Mc Donnell Douglas Corp | Aircraft having auxiliary airfoils |
| IL39260A (en) * | 1972-04-21 | 1975-06-25 | Bouchnik J | Detachable cabin aircraft |
| DE9201272U1 (de) * | 1992-02-03 | 1992-03-26 | Gebr. Schulte GmbH & Co KG, 5768 Sundern | Rohrträgersystem |
| 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 |
| AT413977B (de) * | 2002-07-29 | 2006-07-15 | Firooz Kita | Luft- und raumfahrzeug |
| JP4171913B2 (ja) * | 2004-04-13 | 2008-10-29 | 独立行政法人 宇宙航空研究開発機構 | 低ブーム特性と低抵抗特性を両立する可変前進翼超音速航空機 |
| US7216835B2 (en) * | 2005-02-25 | 2007-05-15 | Northrop Grumman Corporation | Aircraft with extendable leading edge of fuselage and wings |
| US7246770B2 (en) * | 2005-02-25 | 2007-07-24 | Northrop Grumman Corporation | Aircraft with rotatable leading edge of fuselage and wings |
| US7204454B2 (en) * | 2005-02-25 | 2007-04-17 | Northrop Grumman Corporation | Aircraft with articulated leading edge of fuselage and wings |
| EP2239195A1 (en) | 2009-04-06 | 2010-10-13 | Airbus Deutschland GmbH | Center fuselage bellows |
| US9296471B2 (en) * | 2013-10-06 | 2016-03-29 | The Boeing Company | Swing wing tip system, assembly and method with dual load path structure |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3104082A (en) * | 1961-11-16 | 1963-09-17 | Edward C Polhamus | Variable sweep aircraft wing |
| FR1388089A (fr) * | 1963-12-27 | 1965-02-05 | Aviation Louis Breguet Sa | Avion à configuration variable |
| DE1481572A1 (de) * | 1966-02-10 | 1969-03-20 | Hamburger Flugzeugbau Gmbh | Flugzeug,insbesondere UEberschallflugzeug,mit Ausgleich der Neutralpunktwanderung |
-
1968
- 1968-03-05 FR FR142393A patent/FR94080E/fr not_active Expired
-
1969
- 1969-02-21 GB GB1251698D patent/GB1251698A/en not_active Expired
- 1969-02-26 US US802380A patent/US3572617A/en not_active Expired - Lifetime
- 1969-02-27 DE DE19691909835 patent/DE1909835A1/de active Pending
- 1969-03-04 NL NL6903311A patent/NL6903311A/xx unknown
Also Published As
| Publication number | Publication date |
|---|---|
| GB1251698A (enExample) | 1971-10-27 |
| DE1909835A1 (de) | 1969-10-02 |
| FR94080E (fr) | 1969-06-27 |
| US3572617A (en) | 1971-03-30 |