FR1003096A - Perfectionnements aux surfaces alaires à revêtement mobile ou déformable - Google Patents
Perfectionnements aux surfaces alaires à revêtement mobile ou déformableInfo
- Publication number
- FR1003096A FR1003096A FR1003096DA FR1003096A FR 1003096 A FR1003096 A FR 1003096A FR 1003096D A FR1003096D A FR 1003096DA FR 1003096 A FR1003096 A FR 1003096A
- Authority
- FR
- France
- Prior art keywords
- mobile
- wing surfaces
- deformable coating
- deformable
- coating
- 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
- B64C3/30—Wings comprising inflatable structural components
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1003096T | 1946-12-04 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1003096A true FR1003096A (fr) | 1952-03-13 |
Family
ID=9562676
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1003096D Expired FR1003096A (fr) | 1946-12-04 | 1946-12-04 | Perfectionnements aux surfaces alaires à revêtement mobile ou déformable |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR1003096A (fr) |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2932470A (en) * | 1955-05-24 | 1960-04-12 | Chance Vought Aircraft Inc | Variable contour airfoil |
US2960281A (en) * | 1957-03-20 | 1960-11-15 | Snecma | Control device for the air intake of a jet propulsion unit |
US3128966A (en) * | 1964-04-14 | Alvarez-calderon | ||
US3139248A (en) * | 1961-06-15 | 1964-06-30 | Alvarez-Calderon Alberto | Variable geometry system and apparatus for aircraft |
US3188021A (en) * | 1963-04-17 | 1965-06-08 | Boeing Co | Boundary layer control system utilizing a collapsible duct positioned in a control surface |
US3195836A (en) * | 1962-04-16 | 1965-07-20 | Alvarez-Calderon Alberto | High lift slotted flap |
US3203647A (en) * | 1961-12-06 | 1965-08-31 | Alvarez-Calderon Alberto | High lift fdaps for aircraft wings |
US3711039A (en) * | 1970-10-26 | 1973-01-16 | Boeing Co | Pneumatic leading edge flap for an aircraft wing |
US4585192A (en) * | 1983-03-30 | 1986-04-29 | British Aerospace Public Limited Company | Leading edge arrangements for aircraft wings |
US6047923A (en) * | 1995-01-13 | 2000-04-11 | Trimbach Turbine, Ltd. | Aircraft having multiple fuselages |
EP3156323A1 (fr) * | 2015-10-15 | 2017-04-19 | Airbus Operations S.L. | Profil aérodynamique pour un bord d'attaque |
-
1946
- 1946-12-04 FR FR1003096D patent/FR1003096A/fr not_active Expired
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3128966A (en) * | 1964-04-14 | Alvarez-calderon | ||
US2932470A (en) * | 1955-05-24 | 1960-04-12 | Chance Vought Aircraft Inc | Variable contour airfoil |
US2960281A (en) * | 1957-03-20 | 1960-11-15 | Snecma | Control device for the air intake of a jet propulsion unit |
US3139248A (en) * | 1961-06-15 | 1964-06-30 | Alvarez-Calderon Alberto | Variable geometry system and apparatus for aircraft |
US3203647A (en) * | 1961-12-06 | 1965-08-31 | Alvarez-Calderon Alberto | High lift fdaps for aircraft wings |
US3195836A (en) * | 1962-04-16 | 1965-07-20 | Alvarez-Calderon Alberto | High lift slotted flap |
US3188021A (en) * | 1963-04-17 | 1965-06-08 | Boeing Co | Boundary layer control system utilizing a collapsible duct positioned in a control surface |
US3711039A (en) * | 1970-10-26 | 1973-01-16 | Boeing Co | Pneumatic leading edge flap for an aircraft wing |
US4585192A (en) * | 1983-03-30 | 1986-04-29 | British Aerospace Public Limited Company | Leading edge arrangements for aircraft wings |
US6047923A (en) * | 1995-01-13 | 2000-04-11 | Trimbach Turbine, Ltd. | Aircraft having multiple fuselages |
EP3156323A1 (fr) * | 2015-10-15 | 2017-04-19 | Airbus Operations S.L. | Profil aérodynamique pour un bord d'attaque |
US10322793B2 (en) | 2015-10-15 | 2019-06-18 | Airbus Operations S.L. | Leading edge for an airfoil |
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