FR2998264A1 - Device for doubling lift of e.g. civil aircraft, has two additional wings attached to aircraft for doubling surface of wings to double lift of aircraft caused by flow of air on surface of wings, where wings bear additional reactors - Google Patents

Device for doubling lift of e.g. civil aircraft, has two additional wings attached to aircraft for doubling surface of wings to double lift of aircraft caused by flow of air on surface of wings, where wings bear additional reactors Download PDF

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Publication number
FR2998264A1
FR2998264A1 FR1203085A FR1203085A FR2998264A1 FR 2998264 A1 FR2998264 A1 FR 2998264A1 FR 1203085 A FR1203085 A FR 1203085A FR 1203085 A FR1203085 A FR 1203085A FR 2998264 A1 FR2998264 A1 FR 2998264A1
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FR
France
Prior art keywords
wings
aircraft
lift
doubling
additional
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.)
Withdrawn
Application number
FR1203085A
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French (fr)
Inventor
Said Mahmoud Mohamed
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Individual
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Individual
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Publication date
Application filed by Individual filed Critical Individual
Priority to FR1203085A priority Critical patent/FR2998264A1/en
Publication of FR2998264A1 publication Critical patent/FR2998264A1/en
Withdrawn legal-status Critical Current

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/04—Aircraft not otherwise provided for having multiple fuselages or tail booms

Abstract

The device has two additional wings attached to an aircraft for doubling a surface of wings to double a lift of the aircraft, where the wings bear additional reactors. The lift of the aircraft is caused by flow of air on the surface of the wings to produce depression above the wings. The wings are provided toward center of the aircraft to produce a large takeoff and landing angle.

Description

Description Le but de cette invention est de doubles la portance pour l'avion La portance pour un avion '').5 41.Cz. Ve.S = mass volumique d'air /m2) 6 cz= coefficient de portance V = vitesse d'écoulement de l'air sur les surfaces des ailes (m/ sec ) La surface S qui représente la surface des ailes et par doubler cette surface S on peut doubler la portance. Actuellement l'on agrandi cette surface sur les 2 ailes elles mêmes mais avec e) cette invention on va agrandir la surface en doublant le nombre des ailes. Les 2 ailes supplémentaires vont porter des réacteurs supplémentaires aussi. Et pour doubler la surface S il faut ajouter 2 autres ailes pour l'avion soit un avion avec 4 ailes (pas 2 comme maintenant) fig.Description The purpose of this invention is to double the lift for the aircraft. The lift for an aircraft.) 41.Cz. Ve.S = air mass density / m2) 6 cz = lift coefficient V = air flow velocity on the wing surfaces (m / sec) The S surface which represents the wing surface and double this surface can be doubled lift. Currently this area is enlarged on the 2 wings themselves but with e) this invention we will enlarge the surface by doubling the number of wings. The 2 extra wings will carry additional reactors too. And to double the surface S must be added 2 other wings for the plane is a plane with 4 wings (not 2 as now) fig.

1 La portance est causée par l'écoulement d'air sur les ailes qui produit la dépression au-dessus des 2 ails et en produisant cet écoulement sur 4 ailes, la portance sera doublée. La résultante aérodynamique sera doublée aussi. R= 0.5. gUe, \fi e; 2-0 Le centre de gravite de l'avion sera au milieu entre les 4 ailes. L'avion sera porté par 4 forces à la place de 2 actuellement. L'atterrissage et le décollage de l'avion avec 4 ailes sera plus stable qu'avec 2 ailes et le vol palier sera rapide a obtenir parce que le gouverne de profondeur pour décollage et atterrissage par l'axe central de tangage de vol sera plus facile. 2-5 Les 2 ailes se trouvent actuellement vers le centre de l'avion qui produit un grand angle de décollage et atterrissage mais les 4 ailes qui se trouvent a un tiers de devant et arrière du avion va réduire cette angle considérablement. Les 4 ailes permettent d'agrandir la longueur de l'avion donc le volume et pour un avion du même volume les ailes 3 0 Cette idée été appliquée pour certains hélicoptères américains par ajouter un deuxième rotor pour double la portance de hélicoptères Cet invention est applicable pour les avions cargo et civils1 The lift is caused by the airflow on the wings that produces the depression above the 2 garlic and producing this flow on 4 wings, the lift will be doubled. The aerodynamic result will be doubled too. R = 0.5. gue, \ fi e; 2-0 The center of gravity of the aircraft will be in the middle between the 4 wings. The plane will be carried by 4 forces instead of 2 currently. The landing and takeoff of the aircraft with 4 wings will be more stable than with 2 wings and the landing flight will be quick to obtain because the elevator for takeoff and landing by the central axis of pitching flight will be more easy. 2-5 The two wings are currently in the center of the aircraft, which produces a large take-off and landing angle, but the four wings at one-third from the front and rear of the aircraft will reduce this angle considerably. The 4 wings allow to enlarge the length of the aircraft so the volume and for an aircraft of the same volume the wings 3 0 This idea was applied for some American helicopters by adding a second rotor for double the lift of helicopters This invention is applicable for cargo and civil aircraft

Claims (2)

REVENDICATIONS1) Dispositif pour doubler la portance de l'avion caractérisé en ce qu'il comporte d'ajouter 2 ailes supplémentaires donc un avion de 4 ailes Fig. 1CLAIMS1) Device for doubling the lift of the aircraft characterized in that it comprises adding 2 additional wings so a plane of 4 wings Fig. 1 2) Dispositif selon la revendication 1 caractérisé en ce que les 2 ailes supplémentaires portent des réacteurs supplémentaires2) Device according to claim 1 characterized in that the two additional wings carry additional reactors
FR1203085A 2012-11-16 2012-11-16 Device for doubling lift of e.g. civil aircraft, has two additional wings attached to aircraft for doubling surface of wings to double lift of aircraft caused by flow of air on surface of wings, where wings bear additional reactors Withdrawn FR2998264A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1203085A FR2998264A1 (en) 2012-11-16 2012-11-16 Device for doubling lift of e.g. civil aircraft, has two additional wings attached to aircraft for doubling surface of wings to double lift of aircraft caused by flow of air on surface of wings, where wings bear additional reactors

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1203085A FR2998264A1 (en) 2012-11-16 2012-11-16 Device for doubling lift of e.g. civil aircraft, has two additional wings attached to aircraft for doubling surface of wings to double lift of aircraft caused by flow of air on surface of wings, where wings bear additional reactors

Publications (1)

Publication Number Publication Date
FR2998264A1 true FR2998264A1 (en) 2014-05-23

Family

ID=47501332

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1203085A Withdrawn FR2998264A1 (en) 2012-11-16 2012-11-16 Device for doubling lift of e.g. civil aircraft, has two additional wings attached to aircraft for doubling surface of wings to double lift of aircraft caused by flow of air on surface of wings, where wings bear additional reactors

Country Status (1)

Country Link
FR (1) FR2998264A1 (en)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2339338A (en) * 1941-12-18 1944-01-18 Karlik Charles Double wing airplane
DE4323020A1 (en) * 1993-07-09 1995-01-19 Hausser Fritz Karl Aircraft having two pairs of wings
EP0857648A2 (en) * 1997-02-05 1998-08-12 Anatoli J. Prof. Dr. Vassiliev Aircraft for passengers and freight
DE10041030A1 (en) * 2000-08-22 2002-10-17 Akram Soleman Fire fighting aircraft has four tilting wings all of same size
BRPI0706140A2 (en) * 2007-09-21 2009-05-12 Galvao Francisco Leme multi-floor fuselage tandem biplane
JP2011162173A (en) * 2010-02-13 2011-08-25 Am Creation:Kk Vertical takeoff and landing airplane

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2339338A (en) * 1941-12-18 1944-01-18 Karlik Charles Double wing airplane
DE4323020A1 (en) * 1993-07-09 1995-01-19 Hausser Fritz Karl Aircraft having two pairs of wings
EP0857648A2 (en) * 1997-02-05 1998-08-12 Anatoli J. Prof. Dr. Vassiliev Aircraft for passengers and freight
DE10041030A1 (en) * 2000-08-22 2002-10-17 Akram Soleman Fire fighting aircraft has four tilting wings all of same size
BRPI0706140A2 (en) * 2007-09-21 2009-05-12 Galvao Francisco Leme multi-floor fuselage tandem biplane
JP2011162173A (en) * 2010-02-13 2011-08-25 Am Creation:Kk Vertical takeoff and landing airplane

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Effective date: 20140731