MA42066B1 - Root lift system with movable fuselage wing - Google Patents

Root lift system with movable fuselage wing

Info

Publication number
MA42066B1
MA42066B1 MA42066A MA42066A MA42066B1 MA 42066 B1 MA42066 B1 MA 42066B1 MA 42066 A MA42066 A MA 42066A MA 42066 A MA42066 A MA 42066A MA 42066 B1 MA42066 B1 MA 42066B1
Authority
MA
Morocco
Prior art keywords
aircraft
order
fuselage wing
lift system
root
Prior art date
Application number
MA42066A
Other languages
French (fr)
Other versions
MA42066A1 (en
Inventor
Hicham Mahfad
Original Assignee
Hicham Mahfad
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Hicham Mahfad filed Critical Hicham Mahfad
Priority to MA42066A priority Critical patent/MA42066B1/en
Priority to PCT/MA2019/000001 priority patent/WO2019164385A1/en
Publication of MA42066A1 publication Critical patent/MA42066A1/en
Publication of MA42066B1 publication Critical patent/MA42066B1/en

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.

MA42066A 2018-02-23 2018-02-23 Root lift system with movable fuselage wing MA42066B1 (en)

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 MA42066A1 (en) 2019-12-31
MA42066B1 true 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)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114715380A (en) * 2022-04-20 2022-07-08 中国航空发动机研究院 Morphing aircraft and driving method thereof

Family Cites Families (17)

* Cited by examiner, † Cited by third party
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.
CA2761317A1 (en) 2009-05-05 2010-11-11 Aerostar Aircraft Corporation Aircraft winglet design having a compound curve profile
BR112012013602A2 (en) 2009-12-10 2017-03-01 Univ Johannesburg Witwatersrand aircraft wing set.
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

Also Published As

Publication number Publication date
MA42066A1 (en) 2019-12-31
WO2019164385A1 (en) 2019-08-29
WO2019164385A8 (en) 2020-02-20

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