FR752680A - Improvements to airplanes - Google Patents
Improvements to airplanesInfo
- Publication number
- FR752680A FR752680A FR752680DA FR752680A FR 752680 A FR752680 A FR 752680A FR 752680D A FR752680D A FR 752680DA FR 752680 A FR752680 A FR 752680A
- Authority
- FR
- France
- Prior art keywords
- airplanes
- 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
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/385—Variable incidence wings
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR752680T | 1932-06-28 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR752680A true FR752680A (en) | 1933-09-28 |
Family
ID=9159524
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR752680D Expired FR752680A (en) | 1932-06-28 | 1932-06-28 | Improvements to airplanes |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR752680A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2584666A (en) * | 1944-03-11 | 1952-02-05 | George E Bockrath | Aircraft gust alleviating control means |
EP2860100A1 (en) * | 2013-10-09 | 2015-04-15 | The Boeing Company | Aircraft wing-to-fuselage joint with active suspension and method |
-
1932
- 1932-06-28 FR FR752680D patent/FR752680A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2584666A (en) * | 1944-03-11 | 1952-02-05 | George E Bockrath | Aircraft gust alleviating control means |
EP2860100A1 (en) * | 2013-10-09 | 2015-04-15 | The Boeing Company | Aircraft wing-to-fuselage joint with active suspension and method |
US9399508B2 (en) | 2013-10-09 | 2016-07-26 | The Boeing Company | Aircraft wing-to-fuselage joint with active suspension and method |
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