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 PDFInfo
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- 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
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- wings
- tubes
- plane
- circular
- airplane
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/10—Shape of wings
- B64C3/16—Frontal aspect
-
- 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
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Toys (AREA)
- Road Paving Structures (AREA)
Abstract
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)
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 |
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ES201200764A ES2438009B1 (en) | 2012-07-12 | 2012-07-12 | Airplane wings with stabilizer tubes |
Publications (2)
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ES2438009A1 true ES2438009A1 (en) | 2014-01-15 |
ES2438009B1 ES2438009B1 (en) | 2014-10-28 |
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ES201200764A Active ES2438009B1 (en) | 2012-07-12 | 2012-07-12 | Airplane wings with stabilizer tubes |
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Cited By (3)
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)
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 |
-
2012
- 2012-07-12 ES ES201200764A patent/ES2438009B1/en active Active
Patent Citations (7)
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)
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) |
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Publication number | Publication date |
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ES2438009B1 (en) | 2014-10-28 |
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