FR444080A - Airplane - Google Patents
AirplaneInfo
- Publication number
- FR444080A FR444080A FR444080A FR444080DA FR444080A FR 444080 A FR444080 A FR 444080A FR 444080 A FR444080 A FR 444080A FR 444080D A FR444080D A FR 444080DA FR 444080 A FR444080 A FR 444080A
- Authority
- FR
- France
- Prior art keywords
- airplane
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C17/00—Aircraft stabilisation not otherwise provided for
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE444080X | 1911-05-21 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR444080A true FR444080A (en) | 1912-10-09 |
Family
ID=1485086
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR444080A Expired FR444080A (en) | 1911-05-21 | 1912-05-21 | Airplane |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR444080A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6722615B2 (en) * | 2001-04-09 | 2004-04-20 | Fairchild Dornier Gmbh | Wing tip extension for a wing |
US8944386B2 (en) | 2011-06-09 | 2015-02-03 | Aviation Partners, Inc. | Split blended winglet |
US9033282B2 (en) | 2010-07-14 | 2015-05-19 | Airbus Operations Limited | Wing tip device |
US9302766B2 (en) | 2008-06-20 | 2016-04-05 | Aviation Partners, Inc. | Split blended winglet |
US9381999B2 (en) | 2008-06-20 | 2016-07-05 | C. R. Bard, Inc. | Wing tip with optimum loading |
-
1912
- 1912-05-21 FR FR444080A patent/FR444080A/en not_active Expired
Cited By (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6722615B2 (en) * | 2001-04-09 | 2004-04-20 | Fairchild Dornier Gmbh | Wing tip extension for a wing |
US9302766B2 (en) | 2008-06-20 | 2016-04-05 | Aviation Partners, Inc. | Split blended winglet |
US10589846B2 (en) | 2008-06-20 | 2020-03-17 | Aviation Partners, Inc. | Split blended winglet |
US10252793B2 (en) | 2008-06-20 | 2019-04-09 | Aviation Partners, Inc. | Split blended winglet |
US10005546B2 (en) | 2008-06-20 | 2018-06-26 | Aviation Partners, Inc. | Split blended winglet |
US9381999B2 (en) | 2008-06-20 | 2016-07-05 | C. R. Bard, Inc. | Wing tip with optimum loading |
US9193445B2 (en) | 2010-07-14 | 2015-11-24 | Airbus Operations Limited | Wing tip device |
US9199727B2 (en) | 2010-07-14 | 2015-12-01 | Airbus Operations Limited | Wing tip device |
US9033282B2 (en) | 2010-07-14 | 2015-05-19 | Airbus Operations Limited | Wing tip device |
US11851164B2 (en) | 2010-07-14 | 2023-12-26 | Airbus Operations Limited | Wing tip device |
US9434470B2 (en) | 2011-06-09 | 2016-09-06 | Aviation Partners, Inc. | Split spiroid |
US9580170B2 (en) | 2011-06-09 | 2017-02-28 | Aviation Partners, Inc. | Split spiroid |
US9038963B2 (en) | 2011-06-09 | 2015-05-26 | Aviation Partners, Inc. | Split spiroid |
US10106247B2 (en) | 2011-06-09 | 2018-10-23 | Aviation Partners, Inc. | Split blended winglet |
US10377472B2 (en) | 2011-06-09 | 2019-08-13 | Aviation Partners, Inc. | Wing tip with winglet and ventral fin |
US8944386B2 (en) | 2011-06-09 | 2015-02-03 | Aviation Partners, Inc. | Split blended winglet |
US10787246B2 (en) | 2011-06-09 | 2020-09-29 | Aviation Partners, Inc. | Wing tip with winglet and ventral fin |
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