MA42066A1 - Root lift system with movable fuselage wing - Google Patents
Root lift system with movable fuselage wingInfo
- Publication number
- MA42066A1 MA42066A1 MA42066A MA42066A MA42066A1 MA 42066 A1 MA42066 A1 MA 42066A1 MA 42066 A MA42066 A MA 42066A MA 42066 A MA42066 A MA 42066A MA 42066 A1 MA42066 A1 MA 42066A1
- Authority
- MA
- Morocco
- Prior art keywords
- aircraft
- order
- fuselage wing
- lift system
- root
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/08—Aircraft not otherwise provided for having multiple wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C5/00—Stabilising surfaces
- B64C5/08—Stabilising surfaces mounted on, or supported by, wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C5/00—Stabilising surfaces
- B64C5/10—Stabilising surfaces adjustable
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Toys (AREA)
Abstract
Système hypersustentateur installé sur les avions au niveau de l'emplanture. Il est constitué de deux redresseurs de flux d'emplanture qui permettent d'augmenter les forces de portance des ailes, d'une nouvelle aile de fuselage qui fourni une force de portance supplémentaire à l'ensemble de l'avion dans le but de réduire l'envergure totale de l'avion et améliorer ses performances aérodynamiques. En plus, l'aile de fuselage est rendue mobile, elle peut se déplacer vers l'avant ou vers l'arrière, afin de contrôler et optimiser le centrage de l'avion durant toutes les phases du vol, dans le but d'améliorer les performances de l'avion et réaliser d'importantes économies en carburant.High lift system installed on airplanes at root level. It consists of two root flow straighteners which increase the lift forces of the wings, a new fuselage wing which provides additional lift force to the entire aircraft in order to reduce the overall wingspan of the aircraft and improve its aerodynamic performance. In addition, the fuselage wing is made mobile, it can move forwards or backwards, in order to control and optimize the centering of the aircraft during all phases of the flight, in order to improve aircraft performance and achieve significant fuel savings.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
MA42066A MA42066B1 (en) | 2018-02-23 | 2018-02-23 | Root lift system with movable fuselage wing |
PCT/MA2019/000001 WO2019164385A1 (en) | 2018-02-23 | 2019-01-08 | Wing root flap system with mobile fuselage wing |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
MA42066A MA42066B1 (en) | 2018-02-23 | 2018-02-23 | Root lift system with movable fuselage wing |
Publications (2)
Publication Number | Publication Date |
---|---|
MA42066A1 true MA42066A1 (en) | 2019-12-31 |
MA42066B1 MA42066B1 (en) | 2020-03-31 |
Family
ID=65234615
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
MA42066A MA42066B1 (en) | 2018-02-23 | 2018-02-23 | Root lift system with movable fuselage wing |
Country Status (2)
Country | Link |
---|---|
MA (1) | MA42066B1 (en) |
WO (1) | WO2019164385A1 (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114715380B (en) * | 2022-04-20 | 2024-07-02 | 中国航空发动机研究院 | Variant aircraft and driving method thereof |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1803805A (en) | 1930-09-20 | 1931-05-05 | Edward H Lanier | Aeroplane |
US2910254A (en) * | 1955-07-27 | 1959-10-27 | Razak Charles Kenneth | Boundary layer control apparatus relating to aircraft |
US2927749A (en) | 1956-11-02 | 1960-03-08 | Walter T Brownell | Airfoil wing root fillet |
US4598885A (en) | 1979-03-05 | 1986-07-08 | Waitzman Simon V | Airplane airframe |
FR2761658B1 (en) * | 1997-04-04 | 1999-07-23 | Pierre Mignet | DEVICE FOR CONTROLLING GOVERNORS OF AN AIRCRAFT AND AIRCRAFT EQUIPPED WITH THIS DEVICE |
DE19719922C1 (en) | 1997-05-13 | 1998-11-12 | Daimler Benz Aerospace Airbus | Device for influencing a root flow |
ITFI20030043A1 (en) | 2003-02-19 | 2004-08-20 | Aldo Frediani | TWO-LEVEL WINGS AIRCRAFT WITH HIGH STATIC STABILITY |
US20080203233A1 (en) | 2007-02-23 | 2008-08-28 | Schmidt Willard H | Flueted aircraft wing |
US7744038B2 (en) | 2007-06-15 | 2010-06-29 | The Boeing Company | Controllable winglets |
FR2936490B1 (en) * | 2008-09-30 | 2011-05-20 | Airbus France | AIRCRAFT HAS AT LEAST TWO MOTORS |
FR2941915B1 (en) | 2009-02-12 | 2013-05-10 | Airbus France | AIRCRAFT WITH TWO PAIRS OF WINGS |
ES2377637B1 (en) * | 2009-04-07 | 2013-02-28 | Airbus Operations, S.L. | PLANE WITH ALAR CONFIGURATION IN LAMBDA BOX. |
US9120562B2 (en) | 2009-05-05 | 2015-09-01 | Aerostar Aircraft Corporation | Aircraft winglet design having a compound curve profile |
RU2558415C2 (en) | 2009-12-10 | 2015-08-10 | Юниверсити Оф Зе Витватерсранд, Йоханнесбург | Method of concentrated vortex reduction and aircraft wing tip used to this end |
GB201011843D0 (en) | 2010-07-14 | 2010-09-01 | Airbus Operations Ltd | Wing tip device |
US8936219B2 (en) | 2012-03-30 | 2015-01-20 | The Boeing Company | Performance-enhancing winglet system and method |
US9452825B2 (en) | 2013-04-19 | 2016-09-27 | The Boeing Company | Winglet attach fitting for attaching a split winglet to a wing |
-
2018
- 2018-02-23 MA MA42066A patent/MA42066B1/en unknown
-
2019
- 2019-01-08 WO PCT/MA2019/000001 patent/WO2019164385A1/en active Application Filing
Also Published As
Publication number | Publication date |
---|---|
WO2019164385A1 (en) | 2019-08-29 |
WO2019164385A8 (en) | 2020-02-20 |
MA42066B1 (en) | 2020-03-31 |
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