ES2438009A1 - Plane wings with stabilizer tubes (Machine-translation by Google Translate, not legally binding) - Google Patents

Plane wings with stabilizer tubes (Machine-translation by Google Translate, not legally binding) Download PDF

Info

Publication number
ES2438009A1
ES2438009A1 ES201200764A ES201200764A ES2438009A1 ES 2438009 A1 ES2438009 A1 ES 2438009A1 ES 201200764 A ES201200764 A ES 201200764A ES 201200764 A ES201200764 A ES 201200764A ES 2438009 A1 ES2438009 A1 ES 2438009A1
Authority
ES
Spain
Prior art keywords
wings
tubes
plane
circular
airplane
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.)
Granted
Application number
ES201200764A
Other languages
Spanish (es)
Other versions
ES2438009B1 (en
Inventor
Fº JAVIER PORRAS VILA
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to ES201200764A priority Critical patent/ES2438009B1/en
Publication of ES2438009A1 publication Critical patent/ES2438009A1/en
Application granted granted Critical
Publication of ES2438009B1 publication Critical patent/ES2438009B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/10Shape of wings
    • B64C3/16Frontal aspect
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/08Aircraft not otherwise provided for having multiple wings

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Toys (AREA)
  • Road Paving Structures (AREA)

Abstract

The airplane wings, with stabilizing tubes, are characterized by having a different form to the usual wings that extend perpendicularly from the fuselage of the plane. They are boxes (2) or (5), which can acquire different forms, -quared, parallelepiped or circular-, which are filled with multiple tubes (3). At the ends of the wings (2) other larger tubes (4) will have a stabilizing function. In this way, the airplane will work as if it had as many wings as floors of tubes (3) there are in the boxes (2), which allows the plane to have a very slow descent when its engines do not work. (Machine-translation by Google Translate, not legally binding)

Description

ALAS DE A VIÓN CON TUBOS ESTABILIZADORES WINGS OF A VIÓN WITH STABILIZING TUBES

OBJETIVO DE LA INVENCIÓN OBJECTIVE OF THE INVENTION

El objetivo de la presente invención es el de conseguir una mayor estabilidad y una mayor sustentación en el vuelo de un avión, que impedirá que pueda caer en vertical, ya que, cuando el aire en contra de la caída, que entra por los tubitos huecos y múltiples (3) que forman las cajas (2) de las alas, empujará hacia arriba sobre la cara superior de estos tubitos (3), -porque las alas siempre están inclinadas algunos grados hacia arriba-, con lo cual, el avión funcionará como si tuviese varias alas, tantas como pisos de tubitos (3) tengan las cajas (2) de las alas .. Aún sin motor, -o, con un motor averiado-, el avión podría planear con total tranquilidad, en un descenso muy lento, tanto como tubitos huecos podamos poner en las alas (2), o, -tal como se observa también en la figura nO 2-, en las alas circulares (5) que envuelven el fuselaje de la nave. Con estos tubitos (3), y, estas alas múltiples (2, 4, 5), podemos construir un avión que no podrá caer con facilidad, salvo sabot~e o accidente casual con otro objeto volante. The objective of the present invention is to achieve greater stability and greater lift in the flight of an airplane, which will prevent it from falling vertically, since, when the air against the fall, which enters through the hollow tubes and multiple (3) that form the boxes (2) of the wings, will push up on the upper face of these tubes (3), -because the wings are always tilted a few degrees up-, with which, the plane will work as if it had several wings, as many as tube floors (3) have the boxes (2) of the wings .. Even without an engine, -or, with a broken engine-, the plane could plan with total peace of mind, in a very low descent Slow, as much as hollow tubes we can put on the wings (2), or, - as can also be seen in figure 2 - 2, on the circular wings (5) that surround the fuselage of the ship. With these tubes (3), and, these multiple wings (2, 4, 5), we can build an airplane that cannot fall easily, except sabot ~ e or casual accident with another flying object.

ANTECEDENTES DE LA INVENCIÓN BACKGROUND OF THE INVENTION

No conozco antecedente alguno de esta invención. I do not know any background of this invention.

DESCRIPCIÓN DE LA INVENCIÓN DESCRIPTION OF THE INVENTION

Las Alas de avión, con tubos estabilizadores, son cajas (2) rellenas de tubitos múltiples Airplane wings, with stabilizer tubes, are boxes (2) filled with multiple tubes

(3) que pueden adquirir varias formas distintas. Una de ellas (2), es la de las alas habituales en uff-avión, que se: extienden en perpendicular a su fuselaje. En los extremos de las alas (2), se pondrán otros tubos grandes (4) que tendrán una función estabilizadora. La otra forma de la caja, -ver figura nO 2-, será circular (5), y, también estará formada por tubitos múltiples (3), que envolverán el fuselaje del avión y lo recorrerán de principio a fin. Los tubitos múltiples (3), pueden, también, aumentar el equilibrio y la estabilidad del avión, lo que puede permitir que se mantenga en vuelo en las mejores condiciones posibles cuando el clima sea adverso. Y, cuando las condiciones son favorables, viene a funcionar como un protector anti-caída en la medida en que, mientras el avión tenga movimiento de avance, el aire entrará por los huecos de los tubos (3), y, ofrecerá una sustentación mucho mayor que la que ofrecen unas alas convencionales, ya que los distintos "pisos" que se forman con estos tubitos (3) de las alas (2), vienen a funcionar como varias alas superpuestas. Esto (3) that they can acquire several different forms. One of them (2), is the one of the usual wings in uff-plane, that extend: perpendicular to its fuselage. At the ends of the wings (2), other large tubes (4) will be placed that will have a stabilizing function. The other shape of the box, see figure # 2-, will be circular (5), and will also be formed by multiple tubes (3), which will wrap the fuselage of the plane and travel it from beginning to end. Multiple tubes (3), can also increase the balance and stability of the aircraft, which can allow it to remain in flight in the best possible conditions when the weather is adverse. And, when the conditions are favorable, it comes to work as an anti-fall protector to the extent that, as long as the plane has forward movement, the air will enter through the holes in the tubes (3), and, it will offer a lot of support greater than that offered by conventional wings, since the different "floors" that are formed with these tubes (3) of the wings (2), come to function as several overlapping wings. This

La forma de la caja (2) de estos tubitos múltiples (3) puede variar, y, puede, también, situarse por encima, o, por debajo de las alas, o, situarse en una especie de ala adicional que va sobre las alas, -formando así una especie de parapente .. Fecha de la invención: (08.08.09). The shape of the box (2) of these multiple tubes (3) can vary, and, also, can be located above, or, below the wings, or, placed in a kind of additional wing that goes over the wings , thus forming a kind of paraglider. Date of the invention: (08.08.09).

un descenso muy lento, o, que descienda a ser un seguro anti-caída oastante a very slow descent, or, that descends to be an oastante anti-fall insurance

DESCRIPCIÓN DE LAS FIGURAS Figura nO 1: Vista en perspectiva de un avión (1) cuyas alas (2) están formadas por unas cajas llenas de tubos huecos y múltiples. DESCRIPTION OF THE FIGURES Figure 1: Perspective view of an airplane (1) whose wings (2) are formed by boxes filled with hollow and multiple tubes.

Figura n° 2: Vista frontal de un avión (1) que, además de las alas (2) formadas por tubitos múltiples y huecos, tiene, en los extremos de las alas (2), unos tubos huecos (4), grandes. Alrededor del cuerpo del avión, se observan, además, unas alas circulares (5), formadas, también, por tubitos huecos (3), -como los de las alas (2)-, y, que, -aunque no se aprecia en la figura-, dejarían libre el espacio destinado a las ventanillas de los pasajeros. Figure 2: Front view of an airplane (1) that, in addition to the wings (2) formed by multiple and hollow tubes, has, at the ends of the wings (2), large hollow tubes (4). Around the body of the plane, there are also circular wings (5), also formed by hollow tubes (3), -like those of the wings (2) -, and, which, although not seen in the figure-, they would free the space destined to the passenger windows.

Figuras n° 1-2: Figures 1-2:

1) Avión 2) Alas en forma de cajas de tubitos huecos 3) Tubitos huecos de las Alas 4) Tubos huecos grandes 5) Afas circulares éon tubito s huecos 1) Airplane 2) Wings in the form of hollow tube boxes 3) Hollow Wings tubes 4) Large hollow tubes 5) Circular tubes in hollow tubes

DESCRIPa6NDEUNMODODEREALI~a6NPREFERmO DESCRIPTION 6 NDEUNMODODEREALI ~ a6NPREFERmO

Las Alas de avión, con tubos estabilizadores, están caracterizadas por ser unas cajas (1) que sobresalen en perpendicular del fuselaje del avión, y, que están formadas por tubitos (3) longitudinales y cuadrados o rectangulares que recorren todo su espacio interior. Esta disposición permite que las alas (2) se constituyan en alas múltiples, ya que cada fila de tubitos (3) funcionará como un ala distinta, ya que el aire que recorra su interior, en todo su recorrido, tropezará contra la pared superior del tubito (3) correspondiente, empujándola hacia arriba y consolidando la función sustentadora del avión. En los extremos de estas alas The airplane wings, with stabilizer tubes, are characterized by being boxes (1) that protrude perpendicularly from the fuselage of the aircraft, and, which are formed by longitudinal and square or rectangular tubes (3) that run throughout its interior space. This arrangement allows the wings (2) to be constituted into multiple wings, since each row of tubes (3) will function as a different wing, since the air that travels inside, throughout its path, will stumble against the upper wall of the corresponding tube (3), pushing it up and consolidating the supporting function of the plane. At the ends of these wings

(2) en forma de caja con tubitos (3), se pondrán unos tubos estabilizadores más grandes (4), cuya forma podrá ser rectangular, cuadrada, triangular, circular, etc .., cuya función será la de aumentar la estabilidad del avión en su marcha. Las alas (2) pueden adquirir también otra forma distinta (5), o bien, se pueden añadir a las anteriores. Este otro tipo de alas (5) también forman una caja llena de tubitos (3) en su interior, pero que, en esta ocasión, tienen forma circular (5) y envuelven al fuselaje del avión, dejando libre, tan sólo, la zona de las ventanillas laterales. Estas alas circulares (5), también, se extienden longitudinalmente a todo 10 largo del avión. (2) in the form of a box with tubes (3), larger stabilizer tubes (4) will be placed, whose shape may be rectangular, square, triangular, circular, etc., whose function will be to increase the stability of the aircraft in its march. The wings (2) can also acquire a different form (5), or they can be added to the previous ones. This other type of wings (5) also form a box full of tubes (3) inside, but which, on this occasion, have a circular shape (5) and wrap the fuselage of the plane, leaving only the area free of the side windows. These circular wings (5), too, extend longitudinally along the entire length of the plane.

Claims (1)

REIVINDICACIONES 1) Alas de avión, con íubos estabilizadores, caracterizadas por ser unas cajas (1) que sobresalen en perpendicular del fusel~e de] avión, y, que están formadas por tubitos (3) longitudinales y cuadrados o rectangulares que recorren todo su espacio interior. En los extremos de estas alas (2) en forma de c~a con tubitos (3), se pondrán unos tubos estabilizadores más grandes (4), cuya forma podrá ser rectangular, cuadrada, triangular, circular, etc ... 2) Alas de avión, con tubos estabilizadores, según reivindicación primera, caracterizada por el hecho de que las alas (2) pueden adquirir ahora otra forma distinta (5), o bien, se pueden añadir a las anteriores. Este otro tipo de alas (5) también forman una caja llena de tubitos   1) Airplane wings, with stabilizing icons, characterized by being boxes (1) that protrude perpendicularly from the aircraft gun, and, which are formed by longitudinal and square or rectangular tubes (3) that run throughout their space inside. At the ends of these wings (2) in the form of c ~ a with tubes (3), larger stabilizer tubes (4) will be placed, whose shape may be rectangular, square, triangular, circular, etc ... 2) Airplane wings, with stabilizer tubes, according to claim one, characterized in that the wings (2) can now acquire a different shape (5), or they can be added to the previous ones. This other type of wings (5) also form a box full of tubes (3) en su interior, pero que, en esta ocasión, tienen forma circular (5) y envuelven al fuselaje del avión, dejando libre, tan sólo, la zona de las ventanillas laterales. Estas alas circulares (5), también, se extienden longitudinalmente a todo lo largo del avión. (3) inside, but which, on this occasion, have a circular shape (5) and wrap the fuselage of the plane, leaving only the area of the side windows free. These circular wings (5), too, extend longitudinally along the entire length of the plane. \ 3 \ 3 5 Figura n° 2 5 Figure 2
ES201200764A 2012-07-12 2012-07-12 Airplane wings with stabilizer tubes Active ES2438009B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
ES201200764A ES2438009B1 (en) 2012-07-12 2012-07-12 Airplane wings with stabilizer tubes

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES201200764A ES2438009B1 (en) 2012-07-12 2012-07-12 Airplane wings with stabilizer tubes

Publications (2)

Publication Number Publication Date
ES2438009A1 true ES2438009A1 (en) 2014-01-15
ES2438009B1 ES2438009B1 (en) 2014-10-28

Family

ID=49912577

Family Applications (1)

Application Number Title Priority Date Filing Date
ES201200764A Active ES2438009B1 (en) 2012-07-12 2012-07-12 Airplane wings with stabilizer tubes

Country Status (1)

Country Link
ES (1) ES2438009B1 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2546705R1 (en) * 2014-03-25 2015-10-13 Fº JAVIER PORRAS VILA Airplane with groups of fins above and below the fuselage and wings
ES2547361R1 (en) * 2014-04-04 2015-11-12 Fº JAVIER PORRAS VILA Helicopter with finned structure on lever radius and fins on propellers
ES2606943A1 (en) * 2015-09-25 2017-03-28 Fº JAVIER PORRAS VILA Airplane with anti-fall tubes, with diaphragm and fins (Machine-translation by Google Translate, not legally binding)

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2576294A (en) * 1948-06-26 1951-11-27 Alexander D Geraci Airplane sustentation and control surface arrangement
FR1001944A (en) * 1946-07-04 1952-02-29 Jet aerodyne refinements
DE1121476B (en) * 1959-05-11 1962-01-04 Gen Electric Wing for supersonic speeds
DE2657714A1 (en) * 1976-12-20 1978-06-22 Reinhard Oster Aircraft wing with cascade configuration - has horizontal aerofoil section blades mounted in frame with wing section top and bottom members
WO1988005011A1 (en) * 1987-01-03 1988-07-14 Christian Taramasco Vertical take-off and landing aircraft
ES2174690A1 (en) * 1999-12-01 2002-11-01 Saiz Manuel Munoz Aircraft lift arrangement
WO2009093923A1 (en) * 2008-01-21 2009-07-30 Sergey Nikolaevich Afanasyev Aircraft

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1001944A (en) * 1946-07-04 1952-02-29 Jet aerodyne refinements
US2576294A (en) * 1948-06-26 1951-11-27 Alexander D Geraci Airplane sustentation and control surface arrangement
DE1121476B (en) * 1959-05-11 1962-01-04 Gen Electric Wing for supersonic speeds
DE2657714A1 (en) * 1976-12-20 1978-06-22 Reinhard Oster Aircraft wing with cascade configuration - has horizontal aerofoil section blades mounted in frame with wing section top and bottom members
WO1988005011A1 (en) * 1987-01-03 1988-07-14 Christian Taramasco Vertical take-off and landing aircraft
ES2174690A1 (en) * 1999-12-01 2002-11-01 Saiz Manuel Munoz Aircraft lift arrangement
WO2009093923A1 (en) * 2008-01-21 2009-07-30 Sergey Nikolaevich Afanasyev Aircraft

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2546705R1 (en) * 2014-03-25 2015-10-13 Fº JAVIER PORRAS VILA Airplane with groups of fins above and below the fuselage and wings
ES2547361R1 (en) * 2014-04-04 2015-11-12 Fº JAVIER PORRAS VILA Helicopter with finned structure on lever radius and fins on propellers
ES2606943A1 (en) * 2015-09-25 2017-03-28 Fº JAVIER PORRAS VILA Airplane with anti-fall tubes, with diaphragm and fins (Machine-translation by Google Translate, not legally binding)

Also Published As

Publication number Publication date
ES2438009B1 (en) 2014-10-28

Similar Documents

Publication Publication Date Title
ES2274502T3 (en) AIR INPUT STRUCTURE FOR AIRCRAFT ENGINE.
ES2438009A1 (en) Plane wings with stabilizer tubes (Machine-translation by Google Translate, not legally binding)
ES2633996T3 (en) Exhibition Package
BR102014020301B1 (en) Grille for an opening in a vehicle wall
ES2600655T3 (en) Hanging exhaust pipe support
ES2620628T3 (en) Resistant aircraft configuration to enter auger
ES2630527T3 (en) Adjustable rocket engine system
BRPI1008978A2 (en) cod tail tailed airplane and rear engine
BR102014002247A2 (en) ARM SUPPORT FOR A DOOR OF A VEHICLE CAR
ES2646715T3 (en) Ship of the type consisting of at least one receiving well of at least one missile launch container
ES2585737T3 (en) Facade Insulation System
ES2301359A1 (en) Sealing system for the gap existing between the fuselage and the elevator of an aircraft with orientable horizontal stabiliser
ES2884851T3 (en) A leading edge structure for an aircraft flow control system
ES2454365A2 (en) Gear-cone with line-shaped rods with successive folds (Machine-translation by Google Translate, not legally binding)
RU2012134565A (en) AIRCRAFT
ES2613360T3 (en) Structure of the front part of the box of a motor vehicle comprising two stringers whose front part can pivot in case of frontal collision
ES2734680T3 (en) Leading edge for an aerodynamic profile
ES2319492B1 (en) HELMET WITH REINFORCEMENT STRUCTURE.
ES2524765T3 (en) Device for positioning a drawer on drawer guides
ES2569194T3 (en) Protection device for protecting a fish caught with a hook and fishing system comprising said protection device
ES2681444T3 (en) Transport car
ES2608588T3 (en) Arrangement to accelerate the disintegration of turbulent trails in the short end part of an approach flight to an airstrip comprising the airstrip and a floor surface with a surface structure
CL2012000571A1 (en) Squeegee comprising a unitary body with a conical upper end and a first lower perimeter defining a central perforation, and a lower end comprising a plurality of outwardly extending grooves and a termination defining a second perimeter.
ES2661881T3 (en) Propeller blade for aircraft engine
RU2015151627A (en) AIRCRAFT

Legal Events

Date Code Title Description
FG2A Definitive protection

Ref document number: 2438009

Country of ref document: ES

Kind code of ref document: B1

Effective date: 20141028