FR799840A - Aircraft wing with retractable auxiliary airfoil - Google Patents
Aircraft wing with retractable auxiliary airfoilInfo
- Publication number
- FR799840A FR799840A FR799840DA FR799840A FR 799840 A FR799840 A FR 799840A FR 799840D A FR799840D A FR 799840DA FR 799840 A FR799840 A FR 799840A
- Authority
- FR
- France
- Prior art keywords
- aircraft wing
- auxiliary airfoil
- retractable auxiliary
- retractable
- airfoil
- 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
- B64C3/54—Varying in area
- B64C3/546—Varying in area by foldable elements
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/54—Varying in area
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR799840T | 1935-12-24 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR799840A true FR799840A (en) | 1936-06-20 |
Family
ID=9237027
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR799840D Expired FR799840A (en) | 1935-12-24 | 1935-12-24 | Aircraft wing with retractable auxiliary airfoil |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR799840A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4140139A1 (en) * | 1991-12-05 | 1993-06-09 | Klaus Dipl.-Werkmeister 6600 Saarbruecken De Lellig | Aircraft which can be converted from biplane to monoplane - has short take-off and landing capability but high cruising speed |
US6138954A (en) * | 1998-08-17 | 2000-10-31 | Gaunt; John J. | Aircraft funnel slat system |
RU2812162C1 (en) * | 2023-11-17 | 2024-01-24 | Федеральное автономное учреждение "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского" (ФАУ "ЦАГИ") | Aircraft for local airlines |
-
1935
- 1935-12-24 FR FR799840D patent/FR799840A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4140139A1 (en) * | 1991-12-05 | 1993-06-09 | Klaus Dipl.-Werkmeister 6600 Saarbruecken De Lellig | Aircraft which can be converted from biplane to monoplane - has short take-off and landing capability but high cruising speed |
US6138954A (en) * | 1998-08-17 | 2000-10-31 | Gaunt; John J. | Aircraft funnel slat system |
RU2812162C1 (en) * | 2023-11-17 | 2024-01-24 | Федеральное автономное учреждение "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского" (ФАУ "ЦАГИ") | Aircraft for local airlines |
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