BE438541A - - Google Patents
Info
- Publication number
- BE438541A BE438541A BE438541DA BE438541A BE 438541 A BE438541 A BE 438541A BE 438541D A BE438541D A BE 438541DA BE 438541 A BE438541 A BE 438541A
- Authority
- BE
- Belgium
- Prior art keywords
- deflector
- wing
- main patent
- question
- variants
- Prior art date
Links
- 230000000087 stabilizing Effects 0.000 claims description 5
- 230000000694 effects Effects 0.000 claims description 4
- 239000003381 stabilizer Substances 0.000 claims description 4
- 238000000926 separation method Methods 0.000 description 2
- 230000037250 Clearance Effects 0.000 description 1
- 235000004418 Durio kutejensis Nutrition 0.000 description 1
- 210000003462 Veins Anatomy 0.000 description 1
- 230000001133 acceleration Effects 0.000 description 1
- 230000035512 clearance Effects 0.000 description 1
- 238000002788 crimping Methods 0.000 description 1
- 230000001419 dependent Effects 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 239000010931 gold Substances 0.000 description 1
- 229910052737 gold Inorganic materials 0.000 description 1
- 210000000056 organs Anatomy 0.000 description 1
- 230000002441 reversible Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 230000003068 static Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
- B64C9/146—Adjustable control surfaces or members, e.g. rudders forming slots at an other wing location than the rear or the front
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
- B64C2009/143—Adjustable control surfaces or members, e.g. rudders forming slots comprising independently adjustable elements for closing or opening the slot between the main wing and leading or trailing edge flaps
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Air-Flow Control Members (AREA)
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE438541A true BE438541A (es) |
Family
ID=96732
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE438541D BE438541A (es) |
Country Status (1)
| Country | Link |
|---|---|
| BE (1) | BE438541A (es) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP3181444A1 (en) * | 2015-07-31 | 2017-06-21 | Airbus Operations Limited | A control surface for an aircraft |
| CN109305329A (zh) * | 2018-10-26 | 2019-02-05 | 上海歌尔泰克机器人有限公司 | 机翼、无人飞行器和机翼的加工方法 |
-
0
- BE BE438541D patent/BE438541A/fr unknown
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP3181444A1 (en) * | 2015-07-31 | 2017-06-21 | Airbus Operations Limited | A control surface for an aircraft |
| US10279888B2 (en) | 2015-07-31 | 2019-05-07 | Airbus Operations Limited | Control surface for an aircraft |
| CN109305329A (zh) * | 2018-10-26 | 2019-02-05 | 上海歌尔泰克机器人有限公司 | 机翼、无人飞行器和机翼的加工方法 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| EP0342069B1 (fr) | Vanne à clapet pour un aéronef | |
| EP3862261B1 (en) | An aircraft wing with a moveable wing tip device for load alleviation | |
| FR3065440B1 (fr) | Aeronef a voilure rhomboedrique a atterrissage vertical | |
| CA2901233C (fr) | Giravion muni d'un dispositif stabilisateur | |
| FR2859976A1 (fr) | Aile d'aeronef comportant au moins un volet deporteur et volet deporteur pour ladite aile | |
| FR2541231A1 (fr) | Montage de plans additionnels en bouts d'ailes | |
| FR2473466A1 (fr) | Avion a voilure fixe comportant des surfaces portantes placees en tandem | |
| FR2948628A1 (fr) | Avion a controle en lacet par trainee differentielle | |
| WO2015162399A1 (en) | An aircraft with a foldable wing tip device | |
| FR2521520A1 (fr) | Ailettes marginales a angles d'attaque variables | |
| EP1824731B1 (fr) | Procede pour ameliorer le pilotage en roulis d'un aeronef et aeronef mettent en oeuvre ce procede | |
| EP3647202B1 (fr) | Ensemble turbomachine d'aeronef comportant un capot articule | |
| EP3508416A1 (fr) | Elément aérodynamique d'un aéronef, pourvu d'un ensemble d'éléments protubérants | |
| EP1562091B1 (fr) | Procédé pour améliorer l'atterrissage d'un aéronef | |
| BE438541A (es) | ||
| EP1468909A1 (fr) | Volet rotatif et élément sustentateur muni d'un tel volet | |
| EP3495266A1 (fr) | Avion à configuration évolutive en vol | |
| EP0344048B1 (fr) | Vanne à ouverture autonome et aéronef comportant une telle vanne | |
| CA2270752C (fr) | Aeronef a efforts de voilure diminues | |
| FR2922192A1 (fr) | Aeronef a double fuselage. | |
| EP1112929B1 (fr) | Mât de suspension profilé de voilure d'aéronef | |
| FR3046133B1 (fr) | Cellule d'aeronef comprenant une porte s'ouvrant en translation rectiligne | |
| CA2500841C (fr) | Procede pour assurer la securite d'un aeronef volant horizontalement a faible vitesse | |
| FR2571021A1 (fr) | Dispositif pour la commande automatique d'un compensateur aerodynamique associe a une surface aerodynamique de commande d'un aeronef | |
| CA2489799C (fr) | Procede pour ameliorer la manoeuvrabilite d'un aeronef lors d'une ressource |