EP0840641B1 - Remote-controlled toy aircraft for use in a confined space, particularly a room - Google Patents
Remote-controlled toy aircraft for use in a confined space, particularly a room Download PDFInfo
- Publication number
- EP0840641B1 EP0840641B1 EP96927084A EP96927084A EP0840641B1 EP 0840641 B1 EP0840641 B1 EP 0840641B1 EP 96927084 A EP96927084 A EP 96927084A EP 96927084 A EP96927084 A EP 96927084A EP 0840641 B1 EP0840641 B1 EP 0840641B1
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- EP
- European Patent Office
- Prior art keywords
- aircraft
- toy
- aircraft according
- model
- toy aircraft
- 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.)
- Expired - Lifetime
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Classifications
-
- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63H—TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
- A63H27/00—Toy aircraft; Other flying toys
- A63H27/04—Captive toy aircraft
-
- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63H—TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
- A63H30/00—Remote-control arrangements specially adapted for toys, e.g. for toy vehicles
- A63H30/02—Electrical arrangements
Definitions
- the present invention relates to a toy plane able to fly by remote control in an enclosed space or protected from the wind, especially in a room.
- the room in which the plane can fly can be a room relatively small dimensions like a room an apartment or a house (living room, bedroom, bathroom etc.).
- Airplane toys are very popular with children especially when you can make them steal.
- the most elaborate are scale models reproducing the essential characteristics of a real airplane and which are remotely controlled by track over the air. They have a heat engine or electric to turn the propeller, a tank fuel or battery and control mechanism rudders and elevators. Engine and the control mechanism for the control surfaces are controlled thanks to a transmitter housed in a control box and a receiver installed on the aircraft. These models discounts are for teenagers or adults and in most cases you can hardly qualify as toys.
- radio controlled airplanes are relatively heavy and therefore fly at a relatively high speed. Those are must have outdoor planes. Any structural modification would only allow them transform into an interior cheek for a reduced space Nice than an apartment. The need to find open land considerably limits use of these planes.
- the present invention has been designed to provide a solution to this problem. It made it possible to design a flying machine easily usable.
- the remote-controlled and flying airplane according to the invention is intended for a child, which is the most likely case for this type of object, it is imperative that it is not dangerous, not only when he flies but also when the child manipulates it. This toy will also have to be robust to be able to resist impact and manipulation while remaining extremely light.
- the maximum speed at which the model plane must fly has been rated at 2 m / s.
- a child can easily control the flight of the airplane model.
- the connecting cable is not not intended to be stretched.
- the flight domain is therefore not not limited to the surface of a sphere as in the case of circular flight.
- the airplane model can evolve freely in all directions.
- the plane model To fly at such a low speed, the plane model must be very light. It is estimated that the wing loading of the aircraft model trailing the connecting cable should be ⁇ 1.5 g / dm 2 . We were able to obtain this low wing loading value because, the toy aircraft according to the invention being with connecting cable, there is no power source or radio control receiver carried on board the model. plane.
- Figure 1 shows the three elements essentials of the toy aircraft according to the invention: the airplane model 1, the control device 2 and the cable 3 ensuring the electrical connection between the model aircraft and the control device.
- the control device 2 comprises a battery 21 serving this source of electrical energy can be switched on by switch 22.
- a battery 21 serving this source of electrical energy can be switched on by switch 22.
- switch 22 To make the controller more attractive, we can give it the shape of a modern airplane steering wheel that is to say provide it with two handles 23 and 24 are attached to the central part 25 which comprises electrical and electronic control elements.
- On the left handle 23 is the control member 26 of the engine 11 of the airplane model driving the propeller 19.
- the control members 26 and 27 operate variable resistors or dimmers power electronics that can be found easily in trade. Terminal voltage of the motor must be adjustable from 0 to the maximum voltage. Voltage across the rudder actuator (which will be described later) must be adjustable between a negative maximum voltage value and a value positive of maximum voltage, this maximum voltage may be different from that supplying the engine.
- the two control members 26 and 27 are provided springs that bring them back to a neutral position correspond to 0 V in both cases.
- the electrical connection cable must be as light as possible and for that the electric wires that make it up should be as light as possible, therefore the finest possible. Intensity who runs through them must therefore be limited to a low value. It is therefore necessary, to have a sufficient power, to provide a voltage relatively large.
- the tension maximum power of the electric motor 11 can be 9 V while the control voltage of the actuator can vary between + 9 V and - 9 V.
- the electrical connection cable 3 must be flexible and very light so as not to hinder developments of the airplane model 1. A length of about 1.75 m seems well suited for operation in a medium-sized living room.
- a cable electric of this length and not weighing, feel them connection sockets which 0.6 g knows about 0.35 g / m.
- This cable is shown alone in Figure 2. It is composed of four conducting wires 31, 32, 33 and 34 0.1 mm in diameter, two wires being intended for power the electric motor and two wires being reserved for the rudder actuator. These wires are made of copper and are electrically insulated with a varnish. We can thus group them in the fold of a fold 35 made from a ribbon of plastic folded in half.
- Plastic tape used can be 4 mm wide for 10 or 12 ⁇ m thick which is a common thickness for manufacturers of plastic films. It is advantageous to use a little tearable plastic because lengthening a lot before rupture, for example the polyethylene or polypropylene.
- the cable is finished, device side control, by a connector with four contacts.
- Another four-way connector connects the cable to the model plane.
- This last connector can have a weight equal to or less than 0.1 g if chosen from certain minaturized connectors used in computer or mobile phone equipment.
- These connectors are preferably sized to allow easy disconnection at the slightest abnormal effort. This protects the electric cable and the constraints aircraft model mechanical too important.
- FIG. 3 represents an airplane model 1 in exploded view but with incomplete wings.
- its wingspan can be 45 cm, its length by 40 cm, the surface area of the wings by 4.5 dm 2 and its weight by 6 g.
- the electrical connection cable is attached to the airplane model by its connector, below the model and near its center of gravity.
- the powertrain 100 is made up electric motor 11, a propeller and a cone propeller 106.
- Motor 11 must have an excellent ratio power over weight. It can be a direct current with very powerful brushes and magnets (rare earth magnets). The consumption of this engine is around 200 mA at a voltage 7 V power supply.
- the powertrain must be able to lift two-thirds when stationary the weight of the aircraft, in this case 4 g, i.e. slightly less than twice the weight of the group motor-propellant.
- the motor can be of the type used in micro-mechanism and equipped with magnets at samarium-cobalt. Engines of this type are available for a weight of around 3.2 g. This weight be reduced by choosing wisely materials and dimensions of the constituent elements.
- the propeller must not be dangerous. For that, it is flexible, which contributes to solidity. It has a hub 101, which plugs in and sticks on the axis 111 of the motor 11, and two blades 102.
- a blade is made from film flexible plastic, about 50 ⁇ m thick, folded in half and is slightly arched.
- Each blade root 103 of the hub is plugged into the fold of each fold 102 constituting a blade.
- the sides facing each other of each fold are glued incorporating the foot of corresponding blade.
- the propeller cone 106 protects the propeller and the engine. It is preferably made of plastic expanded to absorb shocks.
- FIG 4 is a detailed view of the model plane showing rudder 12 and its actuator 200.
- This actuator must be very light because the aircraft model yaw inertia must be very low in order to have maneuverability when cornering sufficient. Its weight is preferably around 0.3 g. It is advantageously of the type used for mobile equipment of needle multimeters.
- he includes a permanent magnet 201, Sm-Co or Fe-Nd, linked to an axis 202 (for example in piano string) integral with the rudder 12 and constituting the axis of rotation of this rudder.
- axis 202 for example in piano string
- the induction coil 203 is fixed to the fuselage 14 (see Figure 3) by a piece of tape adhesive.
- a plastic strand 16 in two parts, is fixed on the one hand to the fuselage 14 by gluing and on the other shares the rudder 12. It constitutes a spring element which tends to hold the rudder in neutral position.
- Figure 4 also allows you to realize of the rudder constitution, the rudder being also constituted on the same principle.
- a flexible plastic strand 204 with a diameter of 0.6 mm is closed on itself and heat-sealed so as to constitute the periphery of the rudder.
- Plastic strand 16 is glued to strand 204 on level and behind the actuator 200 which it surrounds.
- Plastic film 205 8 ⁇ m thick is stretched over the strand 204 and the edge of the film is folded around the strand 204 to be glued or heat sealed on itself.
- this part consists of an envelope made of plastic film 10 ⁇ m thick and shaped like the fuselage 14 and leading edges 15.
- the connection between the fuselage and leading edges (by gluing or heat sealing) must be rigid enough to avoid the wings do not collapse.
- a connecting flange at this level may possibly be necessary to increase the stiffness of the connection.
- Leading edges 15 are preferably slightly conical in shape, their diameter decreases as one moves away from the fuselage.
- Each leading edge and attached to the fuselage so as to give the corresponding wing a dihedral a few degrees and an incidence of 5 °.
- the envelope can also include 10 legs instead of usual wheels to support the aircraft model when he's on the ground. Alternatively, these legs can be of a different structure and related to the model plane.
- the envelope is inflated to a pressure about 5 mbar higher than atmospheric pressure.
- the envelope can be sealed or a re-inflation valve.
- the electric motor 11 is glued to the front face of the fuselage 14 with, optionally, interposition of a reinforcement pad.
- each wing consists of a flexible strand of plastic 17 of about 1 mm in diameter play the role of trailing edge, and of a plastic film 18 of 8 ⁇ m thick.
- Strand 17 is attached by one from its ends to the distal end of the edge attack 15 and by its other end to the fuselage 14.
- the film 18 is stretched between the leading edge 15, the trailing edge 17 and the fuselage. It is fixed by bonding or heat sealing at the leading edge and at fuselage. It is fixed by gluing or heat sealing on itself after covering the strand 17.
- Figure 6 shows, so structural, another model of aircraft.
- the fuselage and the leading edges of the wings consist of plastic tubes with very thin walls thin.
- a good example of usable tubes is made up of straws used for drinking. These straws have a diameter ranging from 5 to 7 mm and have a 150 ⁇ m thick wall.
- the landing gear can advantageously also be made up of such tubes.
- a central tube 50 constitutes the main axis of the structure. On its end advent will be fitted and stuck on the powertrain. On its end rear will be fixed the rudders and direction.
- the front part of the tube 50 supports also the landing gear consisting of two sections of tube 51 and 52.
- the tube sections 51 and 52 support tubes 53 and 54, respectively, serving leading edges.
- a small connecting tube 55 fixed between sections 51 and 52, ensures the rigidity of the landing gear.
- a small tube 56 is reported perpendicularly on the tube 50.
- junction pieces allow the tubes to be assembled together. These parts have shapes adapted to the tubes to be connected. They are advantageously made of plastic. The distance between the junction pieces 57 and 60 is equal to the wing chord. The other elements components of the aircraft model are glued to the tubes.
- the structure obtained can be dressed with a colored plastic film 6 or 8 ⁇ m thick.
- the bending stiffnesses and in torsion of the wings can be increased in the guy lines.
- Guy lines placed under the wings are particularly effective because they limit the bending due to lift.
- the plane simplified has a fixed rudder and the steering is more controllable in flight. Since there is no longer any actuator the electrical connection cable does not includes more than two wires and the controller no longer has a steering control.
- the user of the toy adjusts the turning radius of the front airplane the flight. The adjustment consists in shortening the shroud from the inner wing to the bend so as to bend it more.
- a 40 guy line is visible on the aircraft model 1 shown in Figure 1. It is located between a tab 10 showing a wheel and the trailing edge of the wing corresponding.
- Guy lines 61 and 62 are also visible in Figure 6.
- the stay 61 is arranged between the tube 51 and the trailing edge of the corresponding wing.
- the shroud 62 is disposed between the tube 52 and the edge of the corresponding wing.
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Abstract
Description
La présente invention concerne un avion jouet pouvant voler par téléguidage dans un espace clos ou protégé du vent, notamment dans une pièce. La pièce dans laquelle l'avion peut voler peut être une pièce de dimensions relativement restreintes comme une pièce d'un appartement ou d'une maison (salon, chambre, salle de jeux etc.).The present invention relates to a toy plane able to fly by remote control in an enclosed space or protected from the wind, especially in a room. The room in which the plane can fly can be a room relatively small dimensions like a room an apartment or a house (living room, bedroom, bathroom etc.).
Les jouets reproduisant des avions sont très appréciés des enfants surtout lorsqu'on peut les faire voler. Les plus élaborés sont des modèles réduits reproduisant les caractéristiques essentielles d'un véritable avion et qui sont télécommandés par voie hertzienne. Ils possèdent un moteur thermique ou électrique pour faire tourner l'hélice, un réservoir de carburant ou une batterie et un mécanisme de commande des gouvernes de direction et de profondeur. Le moteur et le mécanisme de commande des gouvernes sont commandés grâce à un émetteur logé dans un boítier de commande et à un récepteur installé dans l'avion. Ces modèles réduits sont destinés à des adolescents ou à des adultes et, dans la plupart des cas, on ne peut guère les qualifier de jouets.Airplane toys are very popular with children especially when you can make them steal. The most elaborate are scale models reproducing the essential characteristics of a real airplane and which are remotely controlled by track over the air. They have a heat engine or electric to turn the propeller, a tank fuel or battery and control mechanism rudders and elevators. Engine and the control mechanism for the control surfaces are controlled thanks to a transmitter housed in a control box and a receiver installed on the aircraft. These models discounts are for teenagers or adults and in most cases you can hardly qualify as toys.
Ces avions télécommandés par voie hertzienne sont relativement lourds et, par conséquent, ils volent à une vitesse relativement élevée. Ce sont obligatoirement des avions d'extérieur. Aucune modification structurelle ne permettrait de les transformer en joue d'intérieur pour un espace réduit Bel qu'une pièce d'appartement. La nécessité de trouver un terrain dégagé limite considérablement l'utilisation de ces avions.These radio controlled airplanes are relatively heavy and therefore fly at a relatively high speed. Those are must have outdoor planes. Any structural modification would only allow them transform into an interior cheek for a reduced space Nice than an apartment. The need to find open land considerably limits use of these planes.
Comme avions volants d'intérieur on ne connaít que certains avions à moteur caoutchouc, qui sont très légers et peuvent être utilisés sans danger dans des pièces d'habitation. Ce ne sont cependant pas des avions que l'on peut diriger et leur intérêt ludique s'en trouve d'autant réduit. De plus, leur temps de vol est réduit à quelques secondes, sauf pour des prototypes de concours réservés à des adultes.As indoor flying planes we do not know that some rubber powered airplanes, which are very lightweight and can be safely used in living rooms. However, it is not airplanes that are can direct and their playful interest is all the more reduced. In addition, their flight time is reduced to a few seconds, except for prototypes of contests reserved for adults.
On connaít cependant, par le document DE-A-1603271, un modèle d'aéroport jouet comportant un terrain d'atterrissage pourvu d'un mât central. Des modèles d'avions pourvus de moteurs électriques sont reliés au mât par l'intermédiaire de câbles électriques autorisant un vol circulaireWe know however, from document DE-A-1603271, a toy airport model with a landing field provided with a central mast. Aircraft models with engines cables are connected to the mast by cables electric allowing circular flight
Il n'existe donc pas d'avion jouet téléguidé et volant, destiné à être utilisé dans un espace restreint tel qu'une pièce ou un appartement. Il n'est pas non plus possible de modifier les avions téléguidés existant pour les utiliser en tant que jouet dans un tel espace.There is therefore no remote-controlled toy plane and steering wheel, intended for use in a tight space such as a room or apartment. It is also not possible to modify existing remote-controlled aircraft to use them as that toy in such a space.
La présente invention a été conçue pour apporter une solution à ce problème. Elle a permis de concevoir un engin volant facilement utilisable.The present invention has been designed to provide a solution to this problem. It made it possible to design a flying machine easily usable.
Elle a pour objet un avion jouet pouvant voler dans un espace clos et notamment dans une pièce, comprenant :
- un modèle d'avion pourvu d'un moteur électrique, entraínant une hélice de propulsion,
- un dispositif de commande à distance du vol du modèle d'avion, comportant une source d'énergie électrique et des moyens de commande électrique du vol du modèle d'avion,
- un câble souple assurant la liaison électrique
entre le dispositif de commande à distance et le modèle d'avion
pour alimenter le moteur électrique à partir de la source
d'énergie électrique,
caractérisé en ce que le modèle d'avion est pourvu de moyens d'action sur sa direction de vol, le câble souple reliant également lesdits moyens de commande électrique auxdits moyens d'action et étant attaché sous le modèle d'avion et à proximité de son centre de gravité, la charge alaire du modèle d'avion traínant le câble de liaison étant ≤ 1,5 g/dm2.
- an airplane model fitted with an electric motor, driving a propeller,
- a device for remote control of the flight of the aircraft model, comprising a source of electrical energy and means for electrical control of the flight of the aircraft model,
- a flexible cable providing the electrical connection between the remote control device and the aircraft model to supply the electric motor from the source of electrical energy,
characterized in that the aircraft model is provided with means of action on its flight direction, the flexible cable also connecting said electrical control means to said action means and being attached under the aircraft model and near its center of gravity, the wing loading of the aircraft model trailing the connecting cable being ≤ 1.5 g / dm 2.
Dans le cas où l'avion téléguidé et volant selon l'invention est destiné à un enfant, ce qui est le cas le plus vraisemblable pour ce type d'objet, il faut impérativement qu'il ne soit pas dangereux, non seulement quand il vole mais aussi quand l'enfant le manipule. Il faudra aussi que ce jouet soit robuste pour pouvoir résister aux chocs et aux manipulations tout en restant extrêmement léger.In the case where the remote-controlled and flying airplane according to the invention is intended for a child, which is the most likely case for this type of object, it is imperative that it is not dangerous, not only when he flies but also when the child manipulates it. This toy will also have to be robust to be able to resist impact and manipulation while remaining extremely light.
L'invention sera mieux comprise et d'autres avantages et particularités apparaítront à la lecture de la description qui va suivre, donnée à titre d'exemple non limitatif, accompagnée des dessins annexés parmi lesquels :
- la figure 1 est une vue d'ensemble de l'avion jouet selon l'invention, le modèle d'avion étant représenté en vol,
- la figure 2 représente un câble de liaison électrique utilisable dans l'avion jouet selon l'invention,
- la figure 3 est une vue éclatée d'une première variante de modèle d'avion selon l'invention,
- la figure 4 est une vue de détail montrant le gouvernail de direction du modèle d'avion selon l'invention ainsi que sa motorisation,
- la figure 5 est une vue de dessous du fuselage et des ailes de la première variante du modèle d'avion selon l'invention,
- la figure 6 est une vue structurelle d'une seconde variante de modèle d'avion selon l'invention.
- FIG. 1 is an overall view of the toy airplane according to the invention, the airplane model being represented in flight,
- FIG. 2 represents an electrical connection cable usable in the toy airplane according to the invention,
- FIG. 3 is an exploded view of a first variant of an airplane model according to the invention,
- FIG. 4 is a detailed view showing the rudder of the aircraft model according to the invention as well as its motorization,
- FIG. 5 is a bottom view of the fuselage and the wings of the first variant of the aircraft model according to the invention,
- Figure 6 is a structural view of a second variant of aircraft model according to the invention.
Afin que le modèle d'avion puisse voler sans problème dans un espace aussi restreint qu'un appartement, la vitesse maximale à laquelle le modèle d'avion doit voler a été évaluée à 2 m/s. A cette faible vitesse, un enfant peut arriver facilement à contrôler le vol du modèle d'avion. Le câble de liaison n'est pas destiné à être tendu. Le domaine du vol n'est donc pas limité à la surface d'une sphère comme dans le cas du vol circulaire. Le modèle d'avion peut évoluer librement dans toutes les directions. So that the plane model can fly without problem in a space as small as a apartment, the maximum speed at which the model plane must fly has been rated at 2 m / s. To this weak speed, a child can easily control the flight of the airplane model. The connecting cable is not not intended to be stretched. The flight domain is therefore not not limited to the surface of a sphere as in the case of circular flight. The airplane model can evolve freely in all directions.
Pour voler à si faible vitesse, le modèle d'avion doit être très léger. On estime que la charge alaire du modèle d'avion traínant le câble de liaison doit être ≤ 1,5 g/dm2. On a pu obtenir cette faible valeur de charge alaire parce que, l'avion jouet selon l'invention étant à câble de liaison, il n'y a pas de source d'énergie ni de récepteur de radio-commande emportés à bord du modèle d'avion.To fly at such a low speed, the plane model must be very light. It is estimated that the wing loading of the aircraft model trailing the connecting cable should be ≤ 1.5 g / dm 2 . We were able to obtain this low wing loading value because, the toy aircraft according to the invention being with connecting cable, there is no power source or radio control receiver carried on board the model. plane.
Les exemples de réalisation qui vont maintenant être décrits offrent des modèles d'avion très légers et en même temps robustes, et pas dangereux, ce qui est très important pour un jouet.The examples of realization which will now be described offer airplane models very light and at the same time robust, and not dangerous, which is very important for a toy.
La figure 1 montre les trois éléments essentiels de l'avion jouet selon l'invention : le modèle d'avion 1, le dispositif de commande 2 et le câble 3 assurant la liaison électrique entre le modèle d'avion et le dispositif de commande.Figure 1 shows the three elements essentials of the toy aircraft according to the invention: the airplane model 1, the control device 2 and the cable 3 ensuring the electrical connection between the model aircraft and the control device.
Le dispositif de commande 2 comprend une
batterie 21 servant ce source d'énergie électrique
pouvant être mise en circuit par le commutateur 22.
Pour rendra le dispositif de commande plus attrayant,
on peut lui donner la forme d'un volant d'avion moderne
c'est-à-dire le pourvoir de deux poignées 23 et 24
se rattachent à la partie centrale 25 qui comporte
les éléments électriques et électroniques de commande.
Sur la poignée gauche 23, se trouve l'organe de commande
26 du moteur 11 du modèle d'avion entraínant l'hélice
19. Sur le poignée droite 24, se trouve l'organe de
commande 27 du gouvernail de direction.The control device 2 comprises a
On a choisi, par souci de légèreté, de laisser
fixe le gouvernail de profondeur 13, la montée et le
descente de l'avion en vol se faisant par modification
du régime moteur.We chose, for the sake of lightness, to leave
fixes the
Les organes de commande 26 et 27 actionnent
des résistances variables ou des variateurs
électroniques de puissance que l'on peut trouver
facilement dans le commerce. La tension aux bornes
du moteur doit être ajustable de 0 à la tension maximum.
La tension aux bornes de l'actionneur du gouvernail
(qui sera décrit plus loin) doit être ajustable entre
une valeur négative de tension maximum et une valeur
positive de tension maximum, cette tension maximum
pouvant être différente de celle alimentant le moteur.
Les deux organes de commande 26 et 27 sont pourvus
de ressorts qui les ramènent à une position neutre
correspondent à 0 V dans les deux cas.The
Le câble de liaison électrique doit être
le plus léger possible et pour cela las fils électriques
qui le composent doivent être les plus légers possible,
donc les plus fins possible. L'intensité au courent
qui les parcourt doit donc être limitée à une faible
valeur. Il est donc nécessaire, pour disposer d'une
puissance suffisante, de prévoir une tension
relativement importante. A titre d'exemple, le tension
maximale d'alimentation du moteur électrique 11 peut
être de 9 V tandis que la tension de commande de
l'actionneur peut varier entre + 9 V et - 9 V.The electrical connection cable must be
as light as possible and for that the electric wires
that make it up should be as light as possible,
therefore the finest possible. Intensity
who runs through them must therefore be limited to a low
value. It is therefore necessary, to have a
sufficient power, to provide a voltage
relatively large. For example, the tension
maximum power of the
La câble électrique de liaison 3 doit être
souple et très léger pour ne pas gêner les évolutions
du modèle d'avion 1. Une longueur d'environ 1,75 m
semble bien appropriée pour un fonctionnement dans
une pièce d'habitation de taille moyenne. On propose,
pour l'avion jouet selon l'invention, un câble
électrique de cette longueur et ne pesant, sens les
prises de connexion, que 0,6 g sait environ 0,35 g/m.
Ce câble est représenté seul à la figure 2. Il est
composé de quatre fils conducteurs 31, 32, 33 et 34
de 0,1 mm de diamètre, deux fils étant destines à
alimenter la moteur électrique et deux fils étant
réservés pour l'actionneur du gouvernail de direction.
Ces fils sont en cuivre et sont isolés électriquement
par un vernis. On peut ainsi les regrouper dans la
pliure d'un pli 35 réalisé à partir d'un ruban de
plastique plié en deux. Après insertion des fils, les
deux côtés du pli sont collés. Le ruban de plastique
utilisé peut avoir 4 mm de large pour 10 ou 12 µm
d'épaisseur ce qui est une épaisseur courante pour
les fabricants de films plastiques. Il est avantageux
d'utiliser un plastique peu déchirable parce que
s'allongeant beaucoup avant rupture, par exemple le
polyéthylène ou le polypropylène.The electrical connection cable 3 must be
flexible and very light so as not to hinder developments
of the airplane model 1. A length of about 1.75 m
seems well suited for operation in
a medium-sized living room. We propose,
for the toy plane according to the invention, a cable
electric of this length and not weighing, feel them
connection sockets, which 0.6 g knows about 0.35 g / m.
This cable is shown alone in Figure 2. It is
composed of four conducting
Le câble est terminé, côté dispositif de commande, par un connecteur à quatre contacts. Un autre connecteur à quatre contacts relie la câble au modèle d'avion. Ce dernier connecteur peut avoir un poids égal ou inférieur à 0,1 g si on le choisit parmi certains connecteurs minaturisés utilisés en informatique ou dans le matériel téléphonique portable.The cable is finished, device side control, by a connector with four contacts. Another four-way connector connects the cable to the model plane. This last connector can have a weight equal to or less than 0.1 g if chosen from certain minaturized connectors used in computer or mobile phone equipment.
Ces connecteurs sont de préférence dimensionnés afin de pouvoir se déconnecter facilement au moindre effort anormal. Ceci permet de protéger la câble électrique et la modèle d'avion de contraintes mécaniques trop importantes.These connectors are preferably sized to allow easy disconnection at the slightest abnormal effort. This protects the electric cable and the constraints aircraft model mechanical too important.
Le figure 3 représente un modèle d'avion 1 en vue éclatée mais avec des ailes incomplètes. A titre d'exemple, son envergure peut être de 45 cm, sa longueur de 40 cm, la surface des ailes de 4,5 dm2 et son poids de 6 g. La câble de liaison électrique est attaché eu modèle d'avion par son connecteur, au-dessous du modèle et près de son centre de gravité.FIG. 3 represents an airplane model 1 in exploded view but with incomplete wings. For example, its wingspan can be 45 cm, its length by 40 cm, the surface area of the wings by 4.5 dm 2 and its weight by 6 g. The electrical connection cable is attached to the airplane model by its connector, below the model and near its center of gravity.
Le modèle d'avion peut être divisé en les sous-ensembles suivants :
- la groupe moto-
propulseur 100, - l'actionneur du gouvernail de
direction 200, le fuselage 14 et les bords d'attaque desailes 15,- le reste des ailes,
- les gouvernails de profondeur 13 et de
direction 12.
- 100 powertrain,
- the
rudder actuator 200, - the
fuselage 14 and the leading edges of thewings 15, - the rest of the wings,
- the
depth rudders 13 and therudders 12.
Selon l'invention, le poids correspondant à chaque sous-ensemble peut être avantageusement distribué de la manière suivante :
- groupe moto-propulseur 2,5 g,
- actionneur 0,3 g,
- fuselage et bords d'attaque 1,5 g,
- le reste des ailes 1 g,
- les gouvernails 0,3 g,
- la moitié de la longueur de câble avec
son connecteur au modèle d'avion 0,4 g.
Le total fait donc 6 g.
- 2.5 g powertrain,
- actuator 0.3 g,
- fuselage and leading edges 1.5 g,
- the rest of the wings 1 g,
- 0.3 g rudders,
- half the cable length with its connector to the airplane model 0.4 g.
The total therefore makes 6 g.
Le groupe moto-propulseur 100 est constitué
du moteur électrique 11, d'une hélice et d'un cône
d'hélice 106.The
Le moteur 11 doit avoir un excellent rapport
puissance sur poids. Il peut s'agir d'un moteur à
courant continu avec balais et à aimants très puissants
(aimants aux terres rares). La consommation de ce moteur
est de l'ordre de 200 mA sous une tension
d'alimentation de 7 V. Le groupe moto-propulseur doit
être capable de soulever, à l'arrêt, les deux tiers
du poids de l'avion, soit dans ce cas 4 g, c'est-à-dire
un peu moins de deux fois le poids du groupe
moto-propulseur. Le moteur peut être du type utilisé
en micro-mécanisme et équipé d'aimants au
samarium-cobalt. Des moteurs de ce type sont
disponibles pour un poids d'environ 3,2 g. Ce poids
petit être réduit en choisissant judicieusement les
matériaux et les dimensions des éléments constitutifs.
L'hélice ne doit pas être dangereuse. Pour
cela, elle est souple, ce qui contribue à la solidité.
Elle comporte un moyeu 101, qui s'enfiche et se colle
sur l'axe 111 du moteur 11, et deux pales 102.The propeller must not be dangerous. For
that, it is flexible, which contributes to solidity.
It has a
Une pale est faite à partir d'un film
plastique souple, d'environ 50 µm d'épaisseur, plié
en deux et est légèrement arquée. Chaque pied de pale
103 du moyeu s'enfiche dans la pliure de chaque pli
102 constituant une pale. Les côtés se faisant face
de chaque pli sont collés en incorporant le pied de
pale correspondant.A blade is made from film
flexible plastic, about 50 µm thick, folded
in half and is slightly arched. Each
Le cône d'hélice 106 protège l'hélice et le
moteur. Il est de préférence en matière plastique
expansé pour amortir les chocs.The
Dans le détail, le groupe moto-propulseur est constitué d'éléments ayant les caractéristiques suivantes :
- moteur 2,25 g,
- hélice plus cône 0,25 g dont 0,02 g pour le cône d'hélice,
- diamètre de l'hélice 8 cm,
- calage de l'hélice 15°,
- vitesse de rotation maximale du moteur 6000 t/min.
- 2.25 g engine,
- propeller plus cone 0.25 g including 0.02 g for the propeller cone,
- diameter of the propeller 8 cm,
- propeller setting 15 °,
- maximum engine speed 6000 rpm.
La figure 4 est une vue de détail du modèle
d'avion montrant le gouvernail de direction 12 et son
actionneur 200. Cet actionneur doit être très léger
car l'inertie en lacet du modèle d'avion doit être
très faible afin d'avoir une maniabilité en virage
suffisante. Son poids est de préférence de l'ordre
de 0,3 g. Il est avantageusement du type utilisé pour
les équipages mobiles des multimètres à aiguille. Il
comprend un aimant permanent 201, au Sm-Co ou au Fe-Nd,
lié à un axe 202 (par exemple en corde de piano)
solidaire du gouvernail de direction 12 et constituant
l'axe de rotation de ce gouvernail. L'aiment 201 est
disposé à l'intérieur d'une bobine d'induction plate
203 dont les deux extrémités sont réliées électriquement
à deux fils du câble de liaison électrique. Suivant
l'intensité et le sens du courant qui traverse la bobine
203, l'aimant 201 est soumis à un champ magnétique
d'amplitude et de direction variable. Il en résulte
un couple de forces qui fait tourner l'aimant 201,
donc le gouvernail 12 qui lui est solidaire.Figure 4 is a detailed view of the model
La bobine d'induction 203 est fixée au
fuselage 14 (voir la figure 3) par un morceau de ruban
adhésif. Un brin plastique 16, en deux parties, est
fixé d'une part au fuselage 14 par collage et d'autre
part au gouvernail de direction 12. Il constitue un
élément ressort qui tend à maintenir le gouvernail
en position neutre.The
Afin de diminuer le couple de commande du
gouvernail de direction, celui-ci est compensé (son
axe de rotation 202 divise sa surface en deux parties
presque égales) et est équilibré (l'axe de rotation
202 passe par le centre de gravité de l'équipage
mobile).In order to reduce the control torque of the
rudder, this is compensated (its
axis of
La figure 4 permet aussi de se rendre compte
de la constitution du gouvernail de direction, le
gouvernail de profondeur étant d'ailleurs constitué
selon le même principe. Un brin plastique souple 204
de diamètre 0,6 mm est refermé sur lui-même et
thermosoudé de façon à constituer le pourtour du
gouvernail de profondeur. Le brin plastique 16 est
collé au brin 204 eu niveau et en arrière de
l'actionneur 200 qu'il entoure. Un film plastique 205
de 8 µm d'épaisseur est tendu sur le brin 204 et le
bord du film est rabattu autour du brin 204 pour être
collé ou thermosoudé sur lui-même. Figure 4 also allows you to realize
of the rudder constitution, the
rudder being also constituted
on the same principle. A flexible
On va maintenant décrire, en relation avec
les figures 3 et 5, la formation du fuselage et du
bord d'attaque des ailes. Afin d'être suffisamment
léger et raide devant les forces en vol, cette partie
est constituée d'une enveloppe faite d'un film plastique
de 10 µm d'épaisseur et qui a la forme du fuselage
14 et des bords d'attaque 15. La liaison entre le
fuselage et les bords d'attaque (par collage ou
thermosoudage) doit être suffisamment rigide pour éviter
que les ailes ne s'affaissent. Une collerette de liaison
à ce niveau peut éventuellement être nécessaire pour
augmenter la raideur de la liaison. Les bords d'attaque
15 sont de préférence de forme légèrement conique,
leur diamètre diminuant à mesure qu'on s'éloigne du
fuselage. Chaque bord d'attaque et fixé au fuselage
de façon à donner à l'aile correspondante un dièdre
de quelques degrés et une incidence de 5°. L'enveloppe
peut aussi comprendre des pattes 10 à la place des
roues habituelles pour supporter le modèle d'avion
quand il est au sol. En variante, ces pattes peuvent
être d'une structure différente et rapportées au modèle
d'avion.We will now describe, in relation to
Figures 3 and 5, the formation of the fuselage and
leading edge of the wings. In order to be sufficiently
light and stiff in front of the forces in flight, this part
consists of an envelope made of
L'enveloppe est gonflée à une pression supérieure d'environ 5 mbar à la pression atmosphérique. L'enveloppe peut être scellée ou on peut prévoir une valve de regonflage.The envelope is inflated to a pressure about 5 mbar higher than atmospheric pressure. The envelope can be sealed or a re-inflation valve.
Le moteur électrique 11 est collé sur la
face avant du fuselage 14 avec, éventuellement,
interposition d'une pastille de renforcement.The
Ainsi qu'on peut le voir sur le figure 5,
le reste de chaque aile est constitué d'un brin souple
de plastique 17 d'environ 1 mm de diamètre jouent le
rôle de bord de fuite, et d'un film plastique 18 de
8 µm d'épaisseur. Le brin 17 est attaché par l'une
de ses extrémités à l'extrémité distale du bord
d'attaque 15 et par son autre extrémité au fuselage
14. Le film 18 est tendu entre le bord d'attaque 15,
le bord de fuite 17 et le fuselage. Il y est fixé par
collage ou thermosoudage au bord d'attaque et au
fuselage. Il est fixé par collage ou thermosoudage
sur lui-même après recouvrement du brin 17.As can be seen in Figure 5,
the rest of each wing consists of a flexible strand
of
La figure 6 représente, de manière structurelle, un autre modèle d'avion. Dans cette variante, le fuselage et les bords d'attaque des ailes sont constitués de tubes en plastique à parois très minces. Un bon exemple de tubes utilisables est constitué par les pailles utilisées pour boire. Ces pailles ont un diamètre allant de 5 à 7 mm et ont une paroi de 150 µm d'épaisseur. Le train d'atterrissage peut, avantageusement, être aussi constitué de tels tubes.Figure 6 shows, so structural, another model of aircraft. In this variant, the fuselage and the leading edges of the wings consist of plastic tubes with very thin walls thin. A good example of usable tubes is made up of straws used for drinking. These straws have a diameter ranging from 5 to 7 mm and have a 150 µm thick wall. The landing gear can advantageously also be made up of such tubes.
Un tube central 50 constitue l'axe principal
de la structure. Sur son extrémité avent sera emmanché
et collé le groupe moto-propulseur. Sur son extrémité
arrière seront fixés les gouvernails de profondeur
et de direction. Le partie avant du tube 50 supporte
aussi le train d'atterrissage constitué de deux tronçons
de tube 51 et 52. Les tronçons de tube 51 et 52
supportent des tubes 53 et 54, respectivement, servant
de bords d'attaque. Un petit tube de liaison 55, fixé
entre les tronçons 51 et 52, assure le rigidité du
train d'atterrissage. Un petit tube 56 est rapporté
perpendiculairement sur la tube 50.A
Des pièces de jonction, référencées 57 à
60, permettent d'assembler les tubes entre eux. Ces
pièces ont des formes adaptées aux tubes à relier.
Elles sont avantageusement réalisées en plastique.
La distance entre les pièces de jonction 57 et 60 est
égale à le corde de l'aile. Les autres éléments
constitutifs du modèle d'avion sont collés aux tubes.Junction pieces, referenced 57 to
60, allow the tubes to be assembled together. These
parts have shapes adapted to the tubes to be connected.
They are advantageously made of plastic.
The distance between the
La structure obtenue peut être habillée avec un film plastique coloré de 6 ou 8 um d'épaisseur. The structure obtained can be dressed with a colored plastic film 6 or 8 μm thick.
Pour les deux modèles d'avion décrits ci-dessus à titre d'exemple, les raideurs en flexion et en torsion des ailes peuvent être augmentées en les haubanant. Des haubans placés en-dessous des ailes sont particulièrement efficaces car ils limitent la flexion due à la portance.For the two aircraft models described above as an example, the bending stiffnesses and in torsion of the wings can be increased in the guy lines. Guy lines placed under the wings are particularly effective because they limit the bending due to lift.
Une bonne façon de haubaner consiste à relier par un fil le bord de fuite de l'aile, vers son extrémité externe, au bas du train d'atterissage et ceci pour chaque aile. En outre, en rendant réglable la longueur de chacun des haubans par un moyen approprié aux points de fixation au train d'atterrissage, on obtient les deux possibilités suivantes :
- en tirant pareillement les haubans droit et gauche, donc en cintrant également les deux ailes, on modifie l'incidence des ailes et on règle ainsi la stabilité longitudinale de l'avion ;
- en tirant différemment les deux haubans, on crée ou on corrige le vrillage des ailes et on règle ainsi la stabilité en lacet et en roulis de l'avion.
- by similarly pulling the right and left shrouds, therefore also bending the two wings, the incidence of the wings is modified and the longitudinal stability of the aircraft is thus adjusted;
- by pulling the two shrouds differently, the twisting of the wings is created or corrected, thereby adjusting the yaw and roll stability of the aircraft.
Grâce à ces haubans, il est possible de fabriquer une version simplifiée de ce jouet. L'avion simplifié a un gouvernail fixe et la direction n'est plus pilotable en vol. Puisqu'il n'y a plus d'actionneur correspondant, le câble de liaison électrique ne comprend plus que deux fils et le dispositif de commande ne possède plus de commande de direction. L'utilisateur du jouet règle le rayon de giration de l'avion avant le vol. Le réglage consiste à raccourcir le hauban de l'aile intérieure au virage de façon à le cintrer davantage.Thanks to these shrouds, it is possible to make a simplified version of this toy. The plane simplified has a fixed rudder and the steering is more controllable in flight. Since there is no longer any actuator the electrical connection cable does not includes more than two wires and the controller no longer has a steering control. The user of the toy adjusts the turning radius of the front airplane the flight. The adjustment consists in shortening the shroud from the inner wing to the bend so as to bend it more.
Un hauban 40 est visible sur le modèle d'avion
1 représenté à le figure 1. Il est situé entre une
patte 10 figurant une roue et le bord de fuite de l'aile
correspondante. A 40 guy line is visible on the aircraft model
1 shown in Figure 1. It is located between a
Des haubans 61 et 62 sont également visibles
sur la figure 6. Le hauban 61 est disposé entre le
tube 51 et le bord de fuite de l'aile correspondante.
Le hauban 62 est disposé entre le tube 52 et le bord
de fuite de l'aile correspondante.Guy lines 61 and 62 are also visible
in Figure 6. The
L'absence de danger de ce jouet vient de son faible poids et de sa faible inertie, de sa faible puissance (inférieure à 3 W) et de la souplesse de ses constituants et notamment de l'hélice.The lack of danger of this toy comes from its low weight and its low inertia, its low power (less than 3 W) and flexibility of its constituents and in particular the propeller.
Claims (24)
- Toy aircraft capable of flying in a closed space and particularly in a room, comprising:a model aircraft (1) fitted with an electric motor (11) driving a propeller (19);a remote control device (2) controlling the flight of the model aircraft, comprising an electrical power source (21) and electrical means of controlling the flight of the model aircraft;a flexible cable (3) forming the electrical connection between the remote control device (2) and the model aircraft (1) to power the electric motor (11) from the electrical power source;
characterized in that the model aircraft (1) is equipped with means of acting on its flight direction, the flexible cable (3) also connecting said electrical control means to said actuation means and being attached under the model aircraft (1) close to its center of gravity, the airborne weight of the model aircraft (1) supporting the connecting cable (3) being ≤ 1.5 g/dm2. - Toy aircraft according to claim 1, characterized in that the model aircraft (1) is equipped with a fixed elevator (13), the flight direction being modified by making the model aircraft go up or down (1) by varying the motor speed, the means of controlling the aircraft going up or down then consisting of the electric motor (11), the corresponding electrical control means consisting of means of varying the electrical energy supplied to the motor by the electrical power source (21).
- Toy aircraft according to either of claims 1 or 2, characterized in that the means for making a turn comprise a permanent magnet (201) fixed to a hinge pin (202) itself fixed to the rudder (12) and an induction coil (203) fixed to the model aircraft (1) and capable of applying the action of a magnetic field generated by passing a DC electrical current in said induction coil (203) to said permanent magnet (201), the corresponding electrical control means consisting of means of varying the intensity of the DC electrical current passing through the induction coil (203).
- Toy aircraft according to claim 3, characterized in that said means of varying the intensity of the DC electrical current passing through the induction coil (203) comprise means of varying the DC voltage applied to the terminals of the induction coil (203) to generate said electrical current, and capable of varying this DC voltage making it negative or positive about the zero value corresponding to the neutral position of the rudder (12).
- Toy aircraft according to any one of claims 1 to 4, characterized in that the model aircraft (1) comprises a spring (16) tending to hold the rudder (12) in its neutral position.
- Toy aircraft according to claim 5, characterized in that said spring (16) comprises at least one plastic strand mechanically connecting the rudder (12) to the fuselage (14) of the model aircraft.
- Toy aircraft according to any one of claims 1 to 6, characterized in that the electric motor (11) is a DC motor with rare earth brushes and magnets.
- Toy aircraft according to any one of claims 1 to 7, characterized in that each blade (102) of the propeller (19) is composed of a folded flexible plastic film, the sides of which are fixed to each other.
- Toy aircraft according to claim 8, characterized in that each blade (102) is fixed to the hub of the propeller (19) by a blade shank (103) fixed to the hub, penetrating into the pleat of the fold forming the blade (102) so that it is fixed in it.
- Toy aircraft according to any one of claims 1 to 9, characterized in that the model aircraft (1) comprises a spinner (106) made of expanded plastic.
- Toy aircraft according to any one of claims 1 to 10, characterized in that the fuselage (14) and the leading edges (15) of the wings are composed of an envelope of inflated plastic film.
- Toy aircraft according to claim 11, characterized in that the plastic film envelope is inflated to a pressure exceeding atmospheric pressure by about 5 mbars.
- Toy aircraft according to any one of claims 11 or 12, characterized in that each wing comprises a flexible strand (17) attached at one of its ends to the distal end of the leading edge (15), and at its other end to the fuselage (14) to delimit the wing leading edge, a plastic film (18) being fixed between the leading edge (15), the strand (17) delimiting the leading edge and the fuselage (14) to complete the wing.
- Toy aircraft according to any one of claims 1 to 10, characterized in that the fuselage and the leading edges of the wings are made from tubes (50 to 56).
- Toy aircraft according to any one of claims 1 to 14, characterized in that the elevator (13) of the model aircraft is composed of a flexible strand delimiting its extent and supporting a plastic film.
- Toy aircraft according to any one of claims 1 to 15, characterized in that the model aircraft rudder (12) is composed of a flexible strand (204) delimiting its extent and supporting a plastic film (205).
- Toy aircraft according to any one of claims 1 to 16, characterized in that the model aircraft (1) comprises tabs (10) instead of wheels to support it when it is on the floor.
- Toy aircraft according to any one of claims 1 to 17, characterized in that the remote control device (2) is contained in a box in the form of a modern aircraft flight control wheel.
- Toy aircraft according to claim 18, characterized in that one (23) of the flight control wheel handles is fitted with a maneuverable device (26) used to make the model aircraft go up or down in flight while the other handle (24) of the flight control wheel comprises a maneuverable device (27) used to make the model aircraft turn (1).
- Toy aircraft according to any one of the previous claims, characterized in that the cable (3) comprises insulated wires (31 to 34), conducting electricity, housed in the pleat of a fold obtained by longitudinally folding a flexible ribbon, the facing sides of which are fixed to each other.
- Toy aircraft according to claim 20, characterized in that the flexible ribbon is a plastic film.
- Toy aircraft according to any one of the previous claims, characterized in that the cable (3) is electrically connected to the model aircraft by a disconnectable pin.
- Toy aircraft according to any one of the previous claims, characterized in that it comprises guys (40, 61, 62) to increase the bending and torsional stiffnesses of the wings.
- Toy aircraft according to claim 23, characterized in that the length of the guys is adjustable.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9509083 | 1995-07-26 | ||
FR9509083A FR2737130B1 (en) | 1995-07-26 | 1995-07-26 | TOY AIRPLANE THAT CAN FLY BY REMOTE CONTROL IN AN ENCLOSED SPACE, ESPECIALLY IN A ROOM |
PCT/FR1996/001177 WO1997004848A1 (en) | 1995-07-26 | 1996-07-25 | Remote-controlled toy aircraft for use in a confined space, particularly a room |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0840641A1 EP0840641A1 (en) | 1998-05-13 |
EP0840641B1 true EP0840641B1 (en) | 1999-03-24 |
Family
ID=9481399
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP96927084A Expired - Lifetime EP0840641B1 (en) | 1995-07-26 | 1996-07-25 | Remote-controlled toy aircraft for use in a confined space, particularly a room |
Country Status (10)
Country | Link |
---|---|
EP (1) | EP0840641B1 (en) |
JP (1) | JPH11509758A (en) |
CN (1) | CN1135130C (en) |
AT (1) | ATE177968T1 (en) |
AU (1) | AU714378B2 (en) |
CA (1) | CA2227736A1 (en) |
DE (1) | DE69601879T2 (en) |
ES (1) | ES2132945T3 (en) |
FR (1) | FR2737130B1 (en) |
WO (1) | WO1997004848A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10675551B2 (en) | 2014-09-24 | 2020-06-09 | SZ DJI Technology Co., Ltd. | Remote controller and handle structure thereof, and method for controlling a UAV |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2809026B1 (en) | 2000-05-18 | 2003-05-16 | Philippe Louvel | ELECTRIC FLYING SAUCER, PILOTED AND REMOTELY POWERED |
DE10209881A1 (en) | 2002-03-06 | 2003-09-18 | Aloys Wobben | aircraft |
US20050230036A1 (en) * | 2004-04-16 | 2005-10-20 | John Lampl | Lightweight airfoil and method of manufacturing same |
CN103407580B (en) * | 2013-08-19 | 2015-04-08 | 空气动力学国家重点实验室 | Manufacturing method of light aerofoil with super-high aspect ratio and high lift-drag ratio and aerofoil manufactured thereby |
CN106672260B (en) * | 2015-11-11 | 2018-11-02 | 成都飞机工业(集团)有限责任公司 | A kind of high aspect ratio wing type frame configuration designing method |
CN106781988A (en) * | 2017-03-15 | 2017-05-31 | 佛山市三水区希望火炬教育科技有限公司 | A kind of special global prompt-strike system model of teenager's defence education |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3292304A (en) * | 1964-04-17 | 1966-12-20 | Robert A Wolfe | Remotely controlled toy space ship |
DE1603271A1 (en) * | 1967-02-25 | 1971-01-07 | Juergen Ebinger | Model airport for play purposes |
BE875196A (en) * | 1979-03-29 | 1979-07-16 | Cie Generale Du Jouet Imp Atio | CIRCULAR FLIGHT AIRPLANE |
-
1995
- 1995-07-26 FR FR9509083A patent/FR2737130B1/en not_active Expired - Fee Related
-
1996
- 1996-07-25 AU AU67032/96A patent/AU714378B2/en not_active Ceased
- 1996-07-25 JP JP9507284A patent/JPH11509758A/en active Pending
- 1996-07-25 ES ES96927084T patent/ES2132945T3/en not_active Expired - Lifetime
- 1996-07-25 AT AT96927084T patent/ATE177968T1/en not_active IP Right Cessation
- 1996-07-25 DE DE69601879T patent/DE69601879T2/en not_active Expired - Fee Related
- 1996-07-25 EP EP96927084A patent/EP0840641B1/en not_active Expired - Lifetime
- 1996-07-25 WO PCT/FR1996/001177 patent/WO1997004848A1/en active IP Right Grant
- 1996-07-25 CA CA002227736A patent/CA2227736A1/en not_active Abandoned
- 1996-07-25 CN CNB961969873A patent/CN1135130C/en not_active Expired - Fee Related
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10675551B2 (en) | 2014-09-24 | 2020-06-09 | SZ DJI Technology Co., Ltd. | Remote controller and handle structure thereof, and method for controlling a UAV |
US11179650B2 (en) | 2014-09-24 | 2021-11-23 | SZ DJI Technology Co., Ltd. | Remote controller and handle structure thereof, and method for controlling a UAV |
Also Published As
Publication number | Publication date |
---|---|
EP0840641A1 (en) | 1998-05-13 |
DE69601879T2 (en) | 1999-09-30 |
FR2737130B1 (en) | 1997-10-10 |
CN1195998A (en) | 1998-10-14 |
WO1997004848A1 (en) | 1997-02-13 |
AU6703296A (en) | 1997-02-26 |
ATE177968T1 (en) | 1999-04-15 |
CA2227736A1 (en) | 1997-02-13 |
ES2132945T3 (en) | 1999-08-16 |
JPH11509758A (en) | 1999-08-31 |
FR2737130A1 (en) | 1997-01-31 |
CN1135130C (en) | 2004-01-21 |
DE69601879D1 (en) | 1999-04-29 |
AU714378B2 (en) | 1999-12-23 |
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