WO1994026373A1 - Toy airplane - Google Patents

Toy airplane Download PDF

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Publication number
WO1994026373A1
WO1994026373A1 PCT/ES1994/000044 ES9400044W WO9426373A1 WO 1994026373 A1 WO1994026373 A1 WO 1994026373A1 ES 9400044 W ES9400044 W ES 9400044W WO 9426373 A1 WO9426373 A1 WO 9426373A1
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WO
WIPO (PCT)
Prior art keywords
hole
fuselage
counterweights
counterweight
assembly
Prior art date
Application number
PCT/ES1994/000044
Other languages
Spanish (es)
French (fr)
Inventor
Ezequiel Navarro Campos
Enrique Perez Campos
Original Assignee
Ezequiel Navarro Campos
Enrique Perez Campos
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 Ezequiel Navarro Campos, Enrique Perez Campos filed Critical Ezequiel Navarro Campos
Priority to EP94914421A priority Critical patent/EP0654290A1/en
Priority to AU66804/94A priority patent/AU6680494A/en
Publication of WO1994026373A1 publication Critical patent/WO1994026373A1/en

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Classifications

    • AHUMAN NECESSITIES
    • A63SPORTS; GAMES; AMUSEMENTS
    • A63HTOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
    • A63H27/00Toy aircraft; Other flying toys

Definitions

  • the present invention consists of improvements introduced in the assembly of toy airplanes, based on their components, whose main purpose lies in the fact of allowing to modify the flight characteristics, in depending on the number and place of counterweights that are available in a series of accommodations provided in the fuselage of the aircraft.
  • Another additional object of the invention is to allow different combinations between fuselages and wings, varying the aesthetics, and also the way of flight of the plane, according to the user's taste.
  • the removable airplanes of the type of those that are constituted by laminar portions only allow a combination of their elements, which establishes that only a structure of them and a single form of flight can be obtained, whose characteristics can be varied very slightly
  • the invention determines the possibility of mounting different wings in different fuselages, allowing the choice of the structure of the plane, while on the fuselages a series of housings are provided in which it is capable of being housed differently.
  • Counterweights whose shape and location allow modifying the flight conditions of the plane.
  • the corresponding grooves are provided on the fuselages of the plane that allow the assembly of the wings.
  • a hole is provided, centered and in its anterior area, followed by a plurality of small semicircular holes facing both sides of the groove.
  • a hole is provided on the wings that is arranged in correspondence with the hole
  • SUBSTITUTED SHEET included in the front part of the grooving, to allow the introduction of a counterweight.
  • One of the counterweights is constituted by a spherical body that is capable of including a perimetric groove; for its introduction in the holes provided in the "nose" of the plane and in the front part of the groove in which the wings are included.
  • annular counterweight that is arranged in the small semicircular holes provided on both sides of the groove in which the wings are included, thus leaving the annular counterweight, attached to the upper or lower part of the wing.
  • weights can be introduced in bars of different lengths that are arranged attached to the upper or lower part of the wing.
  • spherical counterweights are likely to be introduced into a quadrangular sheath equipped with a through hole for incorporation into the fuselage; for which the holes in the fuselage have a quadrangular shape, so that the counterweight is perfectly hidden.
  • Figure ia.- Shows an elevation view of a possible fuselage compatible with the rest of the elements, in which the different grooves and holes that allow the introduction of the different weights and wings are provided.
  • Figure 2a Shows an elevation view of another fuselage design, compatible in everything with that of the previous figure.
  • Figure 3a Shows a plan view of a possible wing structure to be driven on the fuselages of the previous figures.
  • Figure 4a Shows a plan view of another plane or wing to be mounted on the seals of figures la and 2.
  • FIGS 5a, 6a and 7a Show different embodiments of wings to be mounted on the rear of the fuselage of the plane.
  • Figure 8a Shows a sectional view of a possible spherical counterweight provided with a perimeter rail.
  • Figure 9a Shows an elevation and front view of the counterweight similar to that of a drop of water.
  • Figure loa.- Shows a prespective view of a quadrangular cover for the incorporation of counterweights
  • Figure lia.- Shows an elevation view of an annular counterweight.
  • Figure 12a Shows a perspective view of a possible embodiment in which a spherical counterweight, the annular counterweight and the quadrangular sleeve are used.
  • the invention at hand refers to the assembly of toy airplanes, of the type that are constituted from laminar portions.
  • the invention contemplates the possibility of using two fuselages 1 and 2, slightly different, but compatible with each other, for which they include the grooves 3 and 4 of inclusion of the different wings.
  • the fuselages 1 and 2 are provided in the area corresponding to the "nose" of a hole 5, preferably circular, following which another irregularly shaped hole 6 is provided that resembles a drop of water, in which The narrow area is slightly arched and runs along the bottom of the fuselages 1 and 2.
  • a new hole 7 is provided, which is arranged in correspondence with the hole 10 provided in the wings 9 and 11.
  • the invention has a series of counterweights, one of which is constituted by a spherical body 16 capable of including a perimeter groove 22, to allow its introduction into holes 5 and / or 7.
  • the invention has a counterweight 17 in the form of a drop of water curved in its narrowest part, which is capable of being introduced into the irregular hole 6 which has the same shape.
  • counterweight 17 has a channel
  • SUBSTITUTED SHEET perimeter 18 that facilitates its introduction into the housing 6 indicated above.
  • the invention has an annular counterweight 21 that is arranged in the small semicircular holes 8, being attached to the upper or lower part of the wing 9 or 11.
  • the spherical counterweights 16 are capable of being introduced into a quadrangular sheath 19 provided with a through hole 20, which is constituted of the same material as that of the aircraft, which is preferably made of a soft and flexible material, preventing it from breaking. , or damage the surfaces or objects that could impact when launched by the user, which determines that the aircraft of the invention can be used inside the user's own home, preventing the objects introduced therein can suffer damage
  • FIG. 12 A possible embodiment is shown in Figure 12, in which a counterweight 16 provided inside a quadrangular sheath 19 has been included, which in turn has been introduced inside the hole 5. Furthermore, in this An embodiment of the annular counterweight 21 is provided in the upper part of the wing 20.

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  • Toys (AREA)

Abstract

The toy airplane is comprised of laminar parts which are provided with a plurality of differentiated regular and irregular orifices and grooves for receiving and setting in place said laminar parts as well as the corresponding counterweights which modify the flight characteristics of the airplane, one of said counterweights being comprised of a spherical body which has a peripheral groove which may be provided with additional counterweights and which, in its turn, may be introduced in a sheath passing through an orifice of the fuselage.

Description

AVIONES DE JUGUETE TOY AIRPLANES
D E S C R I P C I Ó ND E S C R I P C I Ó N
OBJETO DE LA INVENCIÓNOBJECT OF THE INVENTION
La presente invención, tal y como lo expresa el enunciado de esta memoria descriptiva, consiste en perfecionamientos introducidos en el armado de aviones de juguete, a partir de sus componentes, cuyo objeto principal reside en el hecho de permitir modificr las características de vuelo, en función del número y lugar de contrapesos que se dispongan en una serie de alojamientos previstos en el fuselaje del avión.The present invention, as expressed in the statement of this specification, consists of improvements introduced in the assembly of toy airplanes, based on their components, whose main purpose lies in the fact of allowing to modify the flight characteristics, in depending on the number and place of counterweights that are available in a series of accommodations provided in the fuselage of the aircraft.
Otro objeto adicional de la invención, consiste en permitir realizar distintas combinaciones entre fuselajes y alas, variando la estética, e igualmente la forma de vuelo del avión, según el gusto del usuario.Another additional object of the invention is to allow different combinations between fuselages and wings, varying the aesthetics, and also the way of flight of the plane, according to the user's taste.
ANTECEDENTES DE LA INVENCIÓNBACKGROUND OF THE INVENTION
Convencionalmente, los aviones desmontables del tipo de los que están constituidos por porciones laminares, sólo permiten una combinación de sus elementos, lo que establece que sólo pueda obtenerse una estructura de los mismos y una única forma de vuelo, cuyas características puedan ser variadas muy ligeramenteConventionally, the removable airplanes of the type of those that are constituted by laminar portions, only allow a combination of their elements, which establishes that only a structure of them and a single form of flight can be obtained, whose characteristics can be varied very slightly
Esto determina una limitación en cuanto a su uso y diseño.This determines a limitation in terms of its use and design.
Además, el material utilizado en la fabricación de dichos aviones, impide el uso de los mismos en el interiorIn addition, the material used in the manufacture of these aircraft prevents their use inside
HOJA SUSTITUIDA de una vivienda, dado que al impactar contra un objeto existe una cierta probabilidad de que éste pueda resultar dañado, lo que constituye un inconveniente y una limitación en su uso.SUBSTITUTED SHEET of a dwelling, since when hitting an object there is a certain probability that it may be damaged, which constitutes an inconvenience and a limitation in its use.
DESCRIPCIÓN DE LA INVENCIÓNDESCRIPTION OF THE INVENTION
Para resolver los invonvenientes anteriormente indicados, la invención determina la posibilidad de montaje de distintas alas en distintos fuselajes, permitiéndose elegir la estructura del avión, al mismo tiempo que sobre los fuselajes se han previsto una serie de alojamientos en los que es susceptible de albergarse distintos contrapesos, cuya forma y ubicación permiten modificar las condiciones de vuelo del avión.In order to solve the aforementioned drawbacks, the invention determines the possibility of mounting different wings in different fuselages, allowing the choice of the structure of the plane, while on the fuselages a series of housings are provided in which it is capable of being housed differently. Counterweights, whose shape and location allow modifying the flight conditions of the plane.
Para conseguir estos objetivos, sobre los fuselajes del avión se han previsto los ranurados correspondientes que posibiitan el armado de las alas.In order to achieve these objectives, the corresponding grooves are provided on the fuselages of the plane that allow the assembly of the wings.
Además, sobre los fuselajes se incluye, en la zona correspondiente al "morro" , un orificio a continuación del cual se ha previsto otro orificio de forma irregular, cuya estructura asemeja a la de una gota de agua en la que su zona estrecha es ligeramente arqueada y discurre por la parte inferior swk fuselaje.In addition, on the fuselages there is included, in the area corresponding to the "nose", a hole following which another irregularly shaped hole is provided, whose structure resembles that of a drop of water in which its narrow area is slightly arched and runs along the bottom swk fuselage.
En la zona correspondiente a la ranura en la que se ubican las alas o planos, se ha previsto, centradamente y en su zona anterior, un orificio al que siguen una pluralidad de pequeños orificios semicirculares enfrentados a ambos lados de la ranura.In the area corresponding to the groove in which the wings or planes are located, a hole is provided, centered and in its anterior area, followed by a plurality of small semicircular holes facing both sides of the groove.
Igualmente, en las alas se ha previsto un orificio que queda dispuesto en correspondencia con el orificioLikewise, a hole is provided on the wings that is arranged in correspondence with the hole
HOJA SUSTITUIDA incluido en la parte anterior del ranurado, para permitir la introducción de un contrapeso.SUBSTITUTED SHEET included in the front part of the grooving, to allow the introduction of a counterweight.
Uno de los contrapesos está constituido por un cuerpo esférico que es susceptible de incluir una ranura perimétrica; para su introducción en los orificios previstos en el "morro" del avión y en la parte delantera del ranurado en el que se incluyen las alas.One of the counterweights is constituted by a spherical body that is capable of including a perimetric groove; for its introduction in the holes provided in the "nose" of the plane and in the front part of the groove in which the wings are included.
Además, existe un contrapeso anular que se dispone en los pequeños orificios semicirculares previstos a ambos lados de la ranura en la que se incluyen las alas, quedando así el contrapeso anular, adosado a la parte superior o inferior del ala.In addition, there is an annular counterweight that is arranged in the small semicircular holes provided on both sides of the groove in which the wings are included, thus leaving the annular counterweight, attached to the upper or lower part of the wing.
Igualmente, en los pequeños orificios se pueden introducir unos contrapesos en barra de distinta longitud que quedan dispuestos adosados a la parte superior o inferior del ala.Likewise, in the small holes, weights can be introduced in bars of different lengths that are arranged attached to the upper or lower part of the wing.
Por otro lado existe un contrapeso en forma de gota de agua, curvada por su parte más estrecha, para su inclusión en el orificio de la misma forma previsto en el fuselaje.On the other hand there is a counterweight in the form of a drop of water, curved by its narrowest part, for inclusion in the hole in the same way provided in the fuselage.
Cabe indicar que los contrapesos esféricos son susceptibles de ser introducidos en una funda cuadrangular dotada de un orificio pasante para su incorporación al fuselaje; para lo que los orificios del fuselaje presentan una forma cuadrangular, al objeto de que el contrapeso quede perfectamente oculto.It should be noted that spherical counterweights are likely to be introduced into a quadrangular sheath equipped with a through hole for incorporation into the fuselage; for which the holes in the fuselage have a quadrangular shape, so that the counterweight is perfectly hidden.
A cotinuación para facilitar una mejor comprensión de esta memoria descriptiva y formando parte integrante de la misma, se acompaña una serie de figuras en las que conIn order to facilitate a better understanding of this descriptive report and being an integral part of it, a series of figures are accompanied in which
HOJA SUSTITUIDA carácter ilustrativo y no limitativo se ha representado el objeto de la invención.SUBSTITUTED SHEET Illustrative and non-limiting nature has been represented the object of the invention.
BREVE ENUNCIADO DE LAS FIGURASBRIEF STATEMENT OF THE FIGURES
Figura ia.- Muestra una vista en alzado de un posible fuselaje compatible con el resto de los elementos, en que se han previsto los distintos ranurados y orificios que facultan la introducción de los distintos contrapesos y alas.Figure ia.- Shows an elevation view of a possible fuselage compatible with the rest of the elements, in which the different grooves and holes that allow the introduction of the different weights and wings are provided.
Figura 2a.- Muestra una vista en alzado de otro diseño de fuselaje, compatible en todo con el de la figura anterior.Figure 2a.- Shows an elevation view of another fuselage design, compatible in everything with that of the previous figure.
Figura 3a.- Muestra una vista en planta de una posible estructura de ala a motar sobre los fuselajes de las figuras anteriores.Figure 3a.- Shows a plan view of a possible wing structure to be driven on the fuselages of the previous figures.
Figura 4a.- Muestra una vista en planta de otro plano o ala a montar sobre los fμselajes de las figuras la y 2 .Figure 4a.- Shows a plan view of another plane or wing to be mounted on the seals of figures la and 2.
Las figuras 5a, 6a y 7a., muestran distintas realizaciones de alas a montar sobre la parte trasera del fuselaje del avión.Figures 5a, 6a and 7a. Show different embodiments of wings to be mounted on the rear of the fuselage of the plane.
Figura 8a.- Muestra una vista seccionada de un posible contrapeso esférico dotado de un carril perimetral.Figure 8a.- Shows a sectional view of a possible spherical counterweight provided with a perimeter rail.
Figura 9a.- Muestra una vista en alzado y frontal del contrapeso en forma semejante a la de una gota de agua.Figure 9a.- Shows an elevation and front view of the counterweight similar to that of a drop of water.
Figura loa.- Muestra una vista en prespectiva de una funda cuadrangular de incorporación de contrapesosFigure loa.- Shows a prespective view of a quadrangular cover for the incorporation of counterweights
HOJA SUSTITUIDA esféricos .SUBSTITUTED SHEET spherical
Figura lia.- Muestra una vista en alzado de un contrapeso anular.Figure lia.- Shows an elevation view of an annular counterweight.
Figura 12a.- Muestra una vista en perspectiva de un posible ejemplo de realización en el que se utiliza un contrapeso esférico, el contrapeso anular y la funda cuadrangular.Figure 12a.- Shows a perspective view of a possible embodiment in which a spherical counterweight, the annular counterweight and the quadrangular sleeve are used.
DESCRIPCIÓN DE ÜNO O VARIOS EJEMPLOS DE REALIZACIÓN DE LA INVENCIÓNDESCRIPTION OF ÜNO OR VARIOUS EXAMPLES OF EMBODIMENT OF THE INVENTION
A continuación se realiza una descripción de la invención basada en las figuras anteriormente comentadas.Below is a description of the invention based on the figures mentioned above.
La invención que nos ocupa, se refiere al armado de aviones de juguete, del tipo de los que están constituidos a partir de porciones laminares.The invention at hand refers to the assembly of toy airplanes, of the type that are constituted from laminar portions.
Así, la invención contempla la posibilidad de utilizar dos fuselajes 1 y 2, ligeramente diferentes, pero compatibles entre sí, para lo que incluyen los ranurados 3 y 4 de inclusión de las distintas alas.Thus, the invention contemplates the possibility of using two fuselages 1 and 2, slightly different, but compatible with each other, for which they include the grooves 3 and 4 of inclusion of the different wings.
En el ejemplo de realización se ha contemplado la posibilidad de montar sobre el ranurado 3 dos alas diferentes la 9 y la 11, dotadas ambas del orificio 10 cuya función será explicada posteriormente.In the exemplary embodiment, the possibility of mounting on the groove 3 two different wings 9 and 11, both provided with the hole 10, whose function will be explained later, has been contemplated.
Igualmente, en el ejemplo de realización, se ha contemplado la posibilidad de montar en la ranura 4 tres alas diferentes 12, 14 y 15, estando la 12 dotada en sus extremos de unos rebajes para la introducción de unos planos 13.Similarly, in the exemplary embodiment, the possibility of mounting three different wings 12, 14 and 15 in the groove 4 has been contemplated, the 12 being provided at its ends with recesses for the introduction of planes 13.
HOJA SUSTITUIDA Por tanto, en el ejemplo de realización se utilizan dos fuselajes, dos tipos diferentes de alas delanteras y tres tipos diferentes de alas traseras, permitiéndose efectuar cualquier tipo de combinación entre los mismos.SUBSTITUTED SHEET Therefore, in the embodiment example two fuselages are used, two different types of front wings and three different types of rear wings, allowing any kind of combination to be made between them.
Además, los fuselajes 1 y 2 están dotados en la zona correspondiente al "morro" de un orificio 5, preferentemente circular, a continuación del cual se ha previsto otro orificio de forma irregular 6 que se asemeja a una gota de agua, en la que la zona estrecha es ligeramente arqueada y discurre por la parte inferior de los fuselajes 1 y 2.In addition, the fuselages 1 and 2 are provided in the area corresponding to the "nose" of a hole 5, preferably circular, following which another irregularly shaped hole 6 is provided that resembles a drop of water, in which The narrow area is slightly arched and runs along the bottom of the fuselages 1 and 2.
Además, en ambos fuselajes 1 y 2, y en la parte anterior y centradamente de la ranura 4, se ha previsto un nuevo orificio 7, que queda dispuesto en correspondencia con el orificio 10 previsto en las alas 9 y 11.In addition, in both fuselages 1 and 2, and in the front and centrally of the groove 4, a new hole 7 is provided, which is arranged in correspondence with the hole 10 provided in the wings 9 and 11.
A continuación del orificio 7, se incluye una pluralidad de pequeños orificios semicirculares 8 enfrentados ambos lados de la ranura 3.Following the hole 7, a plurality of small semicircular holes 8 facing both sides of the slot 3 is included.
Además, la invención cuenta con una serie de contrapesos, uno de los cuales está constituido por un cuerpo esférico 16 susceptible de incluir una ranura perimétrica 22, para permitir su introducción en los orificios 5 y/o 7.Furthermore, the invention has a series of counterweights, one of which is constituted by a spherical body 16 capable of including a perimeter groove 22, to allow its introduction into holes 5 and / or 7.
Además, la invención cuenta con un contrapeso 17 en forma de gota de agua curvada en su parte más estrecha, que es susceptible de ser introducido en el orificio irregular 6 que presenta su misma forma.In addition, the invention has a counterweight 17 in the form of a drop of water curved in its narrowest part, which is capable of being introduced into the irregular hole 6 which has the same shape.
Igualmente, el contrapeso 17 presenta un canalSimilarly, counterweight 17 has a channel
HOJA SUSTITUIDA perimétrico 18 que facilita su introducción en el alojamiento 6 anteriormente indicado.SUBSTITUTED SHEET perimeter 18 that facilitates its introduction into the housing 6 indicated above.
También, cabe indicar, que la invención cuenta con un contrapeso anular 21 que se dispone en los pequeños orificios semicirculares 8, quedando adosado a la parte superior o inferior del ala 9 o 11.Also, it should be noted that the invention has an annular counterweight 21 that is arranged in the small semicircular holes 8, being attached to the upper or lower part of the wing 9 or 11.
Además, en dichos pequeños orificios semicirculares 8, se pueden introducir una serie de contrapesos en barra de distinta longitud, no representados en las figuras, por ser su estructura extremadamente sencilla.In addition, in said small semicircular holes 8, a series of bar weights of different lengths, not shown in the figures, can be introduced, since their structure is extremely simple.
Evidentemente, en los pequeños orificios semicirculares 8 existe la posibilidad de incluir contrapesos esféricos 16, cuyo diámetro se adapta al de la medida de los referidos pequeños orificios semicircularesObviously, in the small semicircular orifices 8 there is the possibility of including spherical weights 16, the diameter of which is adapted to the measure of the said small semicircular orifices.
8.8.
Los contrapesos esféricos 16, son susceptibles de ser introducidos en una funda cuadrangular 19 dotada de un orificio pasante 20, que está constituida del mismo material que el del avión, el cual está realizado preferentemente, en un material flexible y blando, impidiéndose que pueda romperse, o dañar las superficies u objetos contra los que pudiera impactar al ser lanzado por el usuario, lo que determina que los aviones de la invención puedan ser utilizados en el interior de la propia vivienda del usuario, evitando que los objetos en ella introducidos puedan sufrir daño alguno.The spherical counterweights 16 are capable of being introduced into a quadrangular sheath 19 provided with a through hole 20, which is constituted of the same material as that of the aircraft, which is preferably made of a soft and flexible material, preventing it from breaking. , or damage the surfaces or objects that could impact when launched by the user, which determines that the aircraft of the invention can be used inside the user's own home, preventing the objects introduced therein can suffer damage
Al permitirse la introducción de los contrapesos esféricos 16 en la funda 19, los anteriores quedan perfectamente ocultos y a juego con la estructura y materiales del avión.By allowing the introduction of spherical counterweights 16 in the sheath 19, the foregoing are perfectly hidden and match the structure and materials of the aircraft.
HOJA SUSTITUIDA Todos los elementos descritos, pueden ser montados de la forma en que desee el usuario, con lo que, por ejemplo, si únicamente se incluye un contrapeso en el orificio 5, el avión realizará un vuelo en picado, en tanto que si, por ejemplo, se utiliza un único contrapeso anular 21, el avión realizará un vuelo de planeo, por tanto, según la disposición de los distintos contrapesos se permite la variación de las características de vuelo del avión, con lo que el usuario puede experimentar, incluyendo los distintos contrapesos, de la forma deseada, distintas formas de vuelo.SUBSTITUTED SHEET All the elements described can be assembled in the way the user wishes, so that, for example, if only one counterweight is included in hole 5, the plane will take a plummeting flight, while if, for example , a single annular counterweight 21 is used, the plane will perform a gliding flight, therefore, according to the arrangement of the different weights the variation of the airplane's flight characteristics is allowed, with what the user can experience, including the different counterweights, in the desired way, different forms of flight.
En la figura 12 se ha representado un posible ejemplo de realización, en el que se ha incluido un contrapeso 16 previsto en el interior de una funda cuadrangular 19, que a su vez ha sido introducida en el interior del orificio 5. Además, en este ejemplo de realización se ha previsto la disposición de un contrapeso anular 21 en la parte superior del ala 20.A possible embodiment is shown in Figure 12, in which a counterweight 16 provided inside a quadrangular sheath 19 has been included, which in turn has been introduced inside the hole 5. Furthermore, in this An embodiment of the annular counterweight 21 is provided in the upper part of the wing 20.
HOJA SUSTITUIDA SUBSTITUTED SHEET

Claims

R E I V I N D I C A C I O N E S R E I V I N D I C A C I O N E S
l .- PERFECCIONAMIENTOS INTRODUCIDOS EN EL ARMADO DE AVIONES DE JUGUETE, A PARTIR DE SUS COMPONENTES, que siendo, dichos componentes del tipo de los que están constituidos por porciones laminares, cuyo fuselaje (1) y (2) está dotado de ranurados (3) y (4) para el armado de las alas; esencialmente se caracteriza porque el fuselaje (1) y (2) está dotado, en la zona correspondiente al "morro", de un orificio (5), preferentemente circular, a continuación del cual se incluye otro orificio irregular (6) , cuya forma asemeja la de una gota de agua en la que la zona estrecha es ligeramente arqueada y discurre por la parte inferior del fuselaje (1) y (2) , habiéndose previsto que en la ranura (3) de ubicación de las alas delanteras (9) y (11) , se haya incluido centradamente y en su zona anterior, un orificio (7) , preferentemente circular, al que sigue una pluralidad de pequeños orificios semicirculares (8) enfrentrados a ambos lados de la ranura (3) ; todo ello en orden a permitir la incorporación de una pluralidad de contrapesos (16) , (17) , (21) para modificar las características del vuelo del avión.l .- PERFECTING INTRODUCED IN THE ASSEMBLY OF TOY AIRPLANES, FROM ITS COMPONENTS, which being, said components of the type that are constituted by laminar portions, whose fuselage (1) and (2) are equipped with grooves (3 ) and (4) for wing assembly; essentially it is characterized in that the fuselage (1) and (2) is provided, in the area corresponding to the "nose", with a hole (5), preferably circular, following which another irregular hole (6) is included, whose shape resembles that of a drop of water in which the narrow area is slightly arched and runs along the bottom of the fuselage (1) and (2), having been provided in the groove (3) of the location of the front wings (9) and (11), a hole (7), preferably circular, which is followed by a plurality of small semicircular holes (8) facing both sides of the groove (3) has been included centrally and in its anterior zone; all in order to allow the incorporation of a plurality of counterweights (16), (17), (21) to modify the characteristics of the flight of the aircraft.
2a.- PERFECCIONAMIENTOS INTRODUCIDOS EN EL ARMADO DE AVIONES DE JUGUETE, A PARTIR DE SUS COMPONENTES, según reivindicación la, caracterizado porque uno de los contra¬ pesos está constituido por un cuerpo esférico (16) susceptible de incluir una ranura perimétrica (22) ; y con la particularidad de que cuenta con un contrapeso anular (21) que se dispone en los pequeños orificios semicirculares (8) , quedando adosado a la parte superior o inferior del ala (9) , (11) , habiéndose previsto que cuente contrapesos en barra, de distinta longitud, y con un contrapeso (17) en forma de gota de agua, curvada en su parte más estrecha, para su introducción en el orificio2a.- PERFECTIONS INTRODUCED IN THE ASSEMBLY OF TOY AIRPLANES, FROM THEIR COMPONENTS, according to claim la, characterized in that one of the counterweights is constituted by a spherical body (16) capable of including a perimeter groove (22); and with the particularity that it has an annular counterweight (21) that is arranged in the small semicircular orifices (8), being attached to the upper or lower part of the wing (9), (11), being provided that it has counterweights in bar, of different length, and with a counterweight (17) in the form of a drop of water, curved in its narrowest part, for its introduction into the hole
HOJA SUSTITUIDA irregular (6) de la misma forma.SUBSTITUTED SHEET irregular (6) in the same way.
3a.- PERFECCIONAMIENTOS INTRODUCIDOS EN EL ARMADO DE AVIONES DE JUGUETE, A PARTIR DE SUS COMPONENTES, según reivindicaciones anteriores, caracterizado porque los contrapesos esféricos son susceptibles de ser introducidos en una funda cuadrangular (19) dotada de un orificio pasante (20) para su incorporación a su fuselaje (1) y (2) ; para lo que los orificios (5) , (7) del fuselaje, son cuadrangulares, quedando el contrapeso perfectamente oculto.3a.- PERFECTIONS INTRODUCED IN THE ASSEMBLY OF TOY AIRPLANES, FROM THEIR COMPONENTS, according to previous claims, characterized in that the spherical counterweights are capable of being introduced into a quadrangular sheath (19) provided with a through hole (20) for its incorporation into its fuselage (1) and (2); for which the holes (5), (7) of the fuselage, are quadrangular, the counterweight being perfectly hidden.
HOJA SUSTITUIDA SUBSTITUTED SHEET
PCT/ES1994/000044 1993-05-07 1994-05-06 Toy airplane WO1994026373A1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
EP94914421A EP0654290A1 (en) 1993-05-07 1994-05-06 Toy airplane
AU66804/94A AU6680494A (en) 1993-05-07 1994-05-06 Toy airplane

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
ES9301280U ES1024719Y (en) 1993-05-07 1993-05-07 IMPROVEMENTS INTRODUCED IN THE ASSEMBLY OF PLAYING AIRCRAFT, FROM ITS COMPONENTS.
ESU9301280 1993-05-07

Publications (1)

Publication Number Publication Date
WO1994026373A1 true WO1994026373A1 (en) 1994-11-24

Family

ID=8282138

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/ES1994/000044 WO1994026373A1 (en) 1993-05-07 1994-05-06 Toy airplane

Country Status (4)

Country Link
EP (1) EP0654290A1 (en)
AU (1) AU6680494A (en)
ES (1) ES1024719Y (en)
WO (1) WO1994026373A1 (en)

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR776303A (en) * 1933-10-13 1935-01-23 Improvements to gliders usable as toys or for advertising
US2599957A (en) * 1947-10-24 1952-06-10 Neville E Walker Miniature airplane with balancing weight
US2632282A (en) * 1949-02-21 1953-03-24 Philip B Johnson Toy glider and carrier
US3246425A (en) * 1962-12-17 1966-04-19 Carlton E Miller Aerial glider toy
US4203250A (en) * 1979-01-05 1980-05-20 The Hi-Flier Manufacturing Company Molded model airplane
US4642062A (en) * 1985-07-03 1987-02-10 Damon Corporation Nose weight for toy aircraft
US5176559A (en) * 1992-03-27 1993-01-05 Stephen Lane Toy glider

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR776303A (en) * 1933-10-13 1935-01-23 Improvements to gliders usable as toys or for advertising
US2599957A (en) * 1947-10-24 1952-06-10 Neville E Walker Miniature airplane with balancing weight
US2632282A (en) * 1949-02-21 1953-03-24 Philip B Johnson Toy glider and carrier
US3246425A (en) * 1962-12-17 1966-04-19 Carlton E Miller Aerial glider toy
US4203250A (en) * 1979-01-05 1980-05-20 The Hi-Flier Manufacturing Company Molded model airplane
US4642062A (en) * 1985-07-03 1987-02-10 Damon Corporation Nose weight for toy aircraft
US5176559A (en) * 1992-03-27 1993-01-05 Stephen Lane Toy glider

Also Published As

Publication number Publication date
EP0654290A1 (en) 1995-05-24
ES1024719Y (en) 1994-06-16
ES1024719U (en) 1993-09-01
AU6680494A (en) 1994-12-12

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