Interactive Jump-Type Aircraft Toy

Abstract

To provide an interactive jump-type aircraft toy. 【Solution means】The interactive jump-type aircraft toy includes an aircraft body 100, and the aircraft body is equipped with a jump assembly 200 and a detection assembly. The jump assembly can generate elastic deformation, store elastic energy, and release potential energy. The detection assembly is used for detecting the flight state of the aircraft body and the detection of the elastic energy storage state and potential energy release state of the jump assembly. The jump assembly includes a bouncing rod 201 and an elastic member 202, and the bouncing rod has a first end and a second end.

Description

Technical Field

[0001] The present invention relates to the technical field of flying toys, and more specifically, to an interactive jump-type aircraft toy.

Background Art

[0002] With the development of science and technology and the continuous improvement of people's living standards, the types of electronic toys are becoming increasingly rich, and their functions are also becoming increasingly powerful. Various related technologies of aircraft have been widely used in the field of toys to manufacture various types of aircraft.

[0003] For example, the Chinese utility model with the authorization announcement number CN214714349U discloses an aircraft toy including a cage-shaped bracket. Inside the cage-shaped bracket, a blade and a motor for driving the blade to rotate are mounted. The rotation axis of the blade is vertical. The cage-shaped bracket is a spherical cage-shaped bracket, which includes a plurality of meridian frame strips extending along the meridian direction and a plurality of latitude frame strips extending along the latitude direction. The meridian frame strips and the latitude frame strips are collectively called frame strips. A fastening structure is provided between each annular belt-shaped decorative element and the frame strip.

[0004] The aircraft toy described in the above utility model has several drawbacks. For example, the flight motion posture of the aircraft toy is single and lacks interest. In addition, the aircraft toy lacks interaction with the user. As a result, the interactivity and playability of the aircraft toy are insufficient, which affects the user experience of the aircraft toy. Furthermore, the aircraft toy consumes a lot of energy and has a short flight duration. Moreover, especially when the aircraft takes various motion postures, a large amount of instantaneous power is required, but the conventional power of the aircraft itself cannot perform the operations of these postures.

[0005] Therefore, it is necessary to propose a new aircraft toy that has various flight states, high interactivity and playability, and can also reduce energy consumption and improve endurance.

Summary of the Invention

Problems to be Solved by the Invention

[0006] In order to solve the problems described in the above background art, the present invention provides an interactive jump-type aircraft toy.

Means for Solving the Problems

[0007] In order to achieve the object of the above invention, the present invention adopts the following technical solutions.

[0008] The present invention is an interactive jump-type aircraft toy including an aircraft body, wherein the aircraft body is equipped with a jump assembly and a detection assembly. The jump assembly can generate elastic deformation, store elastic energy, and release potential energy. The detection assembly is used for detecting the flight state of the aircraft body and the detection of the elastic energy storage state and potential energy release state of the jump assembly. The jump assembly includes a bouncing rod and an elastic member. The bouncing rod has a first end and a second end. The first end of the bouncing rod penetrates the aircraft body and, when receiving an external force, drives the bouncing rod and the aircraft body to move relatively. One end of the elastic member is directly or indirectly connected to the bouncing rod, and the other end is directly or indirectly connected to the aircraft body. The elastic member is configured to generate elastic deformation and store elastic potential energy when the bouncing rod moves under the action of an external force, providing an interactive jump-type aircraft toy.

[0009] Preferably, the jump assembly further includes a stopper attached to the aircraft body, and the second end of the bouncing rod is fitted into the stopper and slidably connected to the stopper.

[0010] Preferably, the other end of the elastic member is connected to the stopper, the first end of the bouncing rod is configured as a rod receiver, and the rod receiver is used to receive an external force.

[0011] Preferably, the bouncing rod has a rod buckle, the elastic member is fixed to the rod buckle, the aircraft body includes a housing, an opening is provided in the housing, the bouncing rod passes through the opening, and the rod buckle has a diameter larger than that of the opening and is located inside the housing.

[0012] Preferably, the elastic member is located inside the stopper, one end of the elastic member is connected to the second end of the bouncing rod, the other end is connected to the inside of the stopper, the first end of the bouncing rod is configured as a rod receiver, and the rod receiver is used to receive an external force.

[0013] Preferably, the jump assembly further includes a stopper attached to the aircraft body, the second end of the bouncing rod extends toward the stopper and a fixed base is attached, the fixed base is movably connected to the stopper, one end of the elastic member is connected to the fixed base, the other end is connected to the aircraft body, and when the bouncing rod receives an external force and moves axially, the bouncing rod drives the fixed base to move axially and extends the elastic member.

[0014] Preferably, the aircraft body includes a housing, a spindle, a motor, a first rotor assembly, and a second rotor assembly. The first rotor assembly and the second rotor assembly are respectively mounted on the spindle. There is a receiving chamber at the center of the first rotor assembly. The motor is mounted in the receiving chamber and is fixedly mounted on the chamber wall of the receiving chamber.

[0015] Preferably, a power supply and a control board are provided in the receiving chamber. The power supply and the control board are respectively electrically connected to the motor. The second rotor assembly is located below the first rotor assembly. The spindle is disposed through the second rotor assembly, and the upper end of the spindle is rotatably mounted on the housing. The jump assembly further includes a stopper attached to the aircraft body. The lower end of the spindle is fitted into the stopper, and the stopper is movably connected to the bouncing rod. The motor rotationally drives the second rotor assembly via a reduction gear, and the first rotor assembly and the second rotor assembly are connected in an interlocking manner.

[0016] Preferably, the aircraft body includes a housing and a lamp. The housing has a frame, and the frame is arranged in a ring shape. The lamp is mounted on the frame and is for emitting light outward. The detection assembly includes a plurality of infrared sensors. The plurality of infrared sensors are correspondingly arranged at intervals along the frame and are used to detect the distance between the housing and an object.

[0017] Preferably, the bouncing rod includes a rod body and a rod receiver. The rod receiver is configured as the first end. The elastic member is connected to the rod body, and the cross-sectional area of the rod receiver is larger than that of the rod body.

Advantages of the Invention

[0018] Compared with the prior art, the beneficial effects of the present invention are as follows.

[0019] In the interactive jump-type aircraft toy according to the present invention, when the aircraft body is flying autonomously, the bouncing rod receives an external force, the elastic member is in a compressed state or an extended state, and the jump assembly is in a compressed energy storage state. Then, when the bouncing rod recovers and rebounds to release the acting force, the power of the aircraft itself is added, the lift is improved, the energy loss during flight is reduced, and an instantaneous large power for supporting the aircraft is obtained, enabling the aircraft to take various motion postures, improving the appreciation and playability of the aircraft, and also enhancing the battery life. Furthermore, when the user's body part contacts the jump assembly, the jump assembly is put into the compressed energy storage state, and then, through the cooperation of the bouncing rod and the detection assembly, the aircraft body takes various flight motion postures, thereby greatly improving the interactivity of the aircraft toy.

Brief Description of the Drawings

[0020] The drawings in the specification constituting a part of this application are used to provide a further understanding of the present invention. The schematic embodiments and their descriptions of the present invention are used to explain the present invention and do not unduly limit the present invention.

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Mode for Carrying Out the Invention

[0021] Hereinafter, with reference to the drawings in the embodiments of the present invention, the technical solution means in the embodiments of the present invention will be clearly and completely described. Obviously, the described embodiments are part of the embodiments of the present invention, not all of them. The description of at least one exemplary embodiment below is actually illustrative and is not intended to impose any limitation on the invention and its application or use. Based on the embodiments of the present invention, all other embodiments obtained by those skilled in the art without creative labor belong to the protection scope of the present invention.

[0022] It should be noted that the terms used here are for explaining specific embodiments and are not intended to limit the exemplary embodiments according to the present application. As used in this specification, the singular form is intended to include the plural form as well, unless the context clearly indicates otherwise. Furthermore, when the terms "comprising" and / or "including" are used in this specification, it should also be understood that features, steps, operations, devices, components, and / or combinations thereof are present.

[0023] The relative arrangements, mathematical formulas, and numerical values of the components and steps described in these embodiments do not limit the scope of the present invention unless otherwise specified. It should be understood that the dimensions of each part shown in the drawings are not drawn based on the actual proportional relationship for the convenience of explanation. Although the techniques, methods, and devices known to those skilled in the art may not be examined in detail, when appropriate, the said techniques, methods, and devices should be regarded as part of the authorized specification. In all examples shown and discussed here, any specific value should be construed as illustrative and not limiting. Therefore, in other examples of the exemplary embodiments, different values may be used. It should be noted that the same reference numerals and characters indicate the same items in the following drawings. Therefore, if an item is defined in one drawing, there is no need to further examine it in subsequent drawings.

[0024] Referring to FIGS. 1 to 12, the present invention provides an interactive jump-type aircraft toy including an aircraft body. The aircraft body 100 is equipped with a jump assembly 200 and a detection assembly. The jump assembly 200 can generate elastic deformation, store elastic energy, and release potential energy. The detection assembly is used for detecting the flight state of the aircraft body 100 and the elastic energy storage state and potential energy release state of the jump assembly 200. The jump assembly 200 includes a bouncing rod 201 and an elastic member 202. The bouncing rod 201 has a first end and a second end. The first end of the bouncing rod 201 penetrates the aircraft body 100 and, when subjected to an external force, drives the bouncing rod 201 and the aircraft body 100 to move relative to each other. The elastic member 202 has at least one end connected to the bouncing rod 201. The elastic member 202 is configured to generate elastic deformation and store elastic potential energy when the bouncing rod 201 moves under the action of an external force.

[0025] As described above, the aircraft body 100 of the present invention further includes a rotor mechanism 700, and the aircraft body 100 autonomously flies by the rotor mechanism 700. When the aircraft body 100 is autonomously flying, the bouncing rod 201 receives an external force, the elastic member 202 is in a compressed state or an extended state, the jump assembly 200 is in a compressed state, and elastic positional energy is stored. Then, when the bouncing rod 201 recovers and rebounds to release the acting force, the power of the aircraft itself is added, the lift is improved, the energy loss during flight is reduced, and an instantaneous large power for supporting the aircraft is obtained, so that the aircraft can take various motion postures, the appreciation and playability of the aircraft toy are improved, and the battery life is increased. Further, when a part of the user's body contacts the jump assembly 200, the jump assembly 200 is in a compressed state to store elastic positional energy. Then, through the cooperation of the bouncing rod 201 and the detection assembly, the aircraft body 100 takes various flight motion postures, thereby greatly improving the interactivity of the aircraft toy.

[0026] Here, the elastic energy storage state may be achieved by deforming the elastic member 202 through compression or extension to achieve the elastic energy storage state. When the external force is removed or becomes ineffective, the elastic member 202 recovers to a released state. The released state means converting the positional energy stored by the elastic member 202 into kinetic energy, and the bouncing rod 201 quickly pops out to push an obstacle, thereby converting the kinetic energy into the power of the aircraft. Thereby, the energy loss of the aircraft toy during flight is reduced, and an instantaneous large power for supporting the aircraft is obtained, so that the aircraft can take various motion postures, the appreciation and playability of the aircraft toy are improved, and the battery life is further increased.

[0027] Furthermore, in the present invention, the vertical bisector of the aircraft body 100 and the vertical bisector of the bouncing rod 201 overlap, so that the change in the flight motion posture of the aircraft body 100 becomes more stable.

[0028] In the present invention, the aircraft main body 100 includes a control board 400. As shown in FIGS. 3 and 5, the detection assembly includes an acceleration sensor. The acceleration sensor is configured to be electrically connected to the control board 400, and is used to detect changes in the acceleration of the aircraft main body 100 and feedback data to the control board 400. It is also used to detect the energy storage state of the jump assembly 200.

[0029] In this way, based on the state switching of the jump assembly 200 by a program preset by the control board 400, the aircraft main body 100 can take various flight motion postures.

[0030] For example, when kicking or hitting the rod receiver 2011 of the bouncing rod 201, the control board 400 makes the aircraft main body 100 jump based on the data of each sensor, and realizes entertainment and fitness by the aircraft main body 100, such as simulating lenses.

[0031] Furthermore, under the control of the control board 400, by combining with the data from each sensor, the aircraft main body 100 can roll or jump in each direction of forward, backward, left, and right, thereby improving the appreciation and playability of the aircraft toy, and also improving the interactivity of the aircraft toy.

[0032] In the present invention, the detection assembly includes a gyroscope. The gyroscope is used to detect the flight posture of the aircraft main body 100 and feedback data to the control board 400, and monitors the flight posture of the aircraft main body 100, such as detecting the angular velocity of the aircraft main body 100.

[0033] The detection assembly further includes an accelerometer and a barometer. The accelerometer is used to detect changes in the speed of the aircraft body 100 and changes in the energy storage state of the jump assembly 200. The compression and release states of the jump assembly 200 are detected by the accelerometer and transmitted to the control board 400. Thereby, the biasing force generated by the jump assembly 200 is coordinated with the power of the aircraft itself in real time to achieve the control of various flight postures. The barometer is used to detect changes in the height of the aircraft body 100. Thereby, the descent speed of the aircraft can be designed according to the height of the aircraft, and the magnitude of the repulsive force generated by the jump assembly 200 can be further set.

[0034] The detection assembly further includes an infrared sensor 500. The infrared sensor 500 is mounted on the rod receiver 2011. As shown in FIGS. 3 and 5, the infrared sensor 500 is used to determine the distance between the rod receiver 2011 and an object. In this way, when the aircraft body 100 jumps spontaneously, the infrared sensor 500 can determine the distance from the ground. When the user interacts with the aircraft body 100, the infrared sensor 500 can determine the distance between the user and the rod receiver 2011.

[0035] In other embodiments (not shown), the detection assembly also includes an electronic switch, which may be an ordinary mechanical switch, a magnetic control switch, an infrared switch, etc. Among them, the electronic switch is configured to generate a switching operation when the jump assembly 200 is compressed or released, thereby supplying a switching signal to the control board 400. In this embodiment, the use of the electronic switch for detection can reduce the processing and manufacturing costs.

[0036] In an embodiment of the rotor mechanism 700, as shown in FIGS. 11 and 12, the rotor mechanism 700 includes a housing 101, a spindle 107, a motor 104, a first rotor assembly 105, and a second rotor assembly 106. The first rotor assembly 105 and the second rotor assembly 106 are respectively mounted on the spindle 107. There is a housing chamber 102 at the center of the first rotor assembly 105. The motor 104 is mounted within the housing chamber 102 and is fixedly mounted on the chamber wall of the housing chamber 102. A power supply 300 and a control board 400 are provided within the housing chamber 102. The power supply 300 and the control board 400 are respectively electrically connected to the motor 104. The second rotor assembly 106 is located below the first rotor assembly 105. The spindle 107 is provided through the second rotor assembly 106. The upper end of the spindle 107 is rotatably mounted on the housing 101. The lower end of the spindle 107 is fitted into a stopper 203, and the stopper 203 is movably connected to a bouncing rod 201. The motor 104 rotationally drives the second rotor assembly 106 via a reduction gear 108. The first rotor assembly 105 and the second rotor assembly 106 are connected in an interlocking manner.

[0037] When the motor 104 is energized, the rotating shaft of the motor 104 rotationally drives the second rotor assembly 106 by means of the reduction gear 108. Due to the reverse torque generated by the rotation of the motor 104, the first rotor assembly 105 is rotationally driven. The first rotor assembly 105 and the second rotor assembly 106 differentially rotate in opposite directions, and both simultaneously generate a downward wind force to generate a lift force on the aircraft. Further, the first rotor assembly 105 rotates at a high speed to generate a gyroscopic effect, preventing the flight angle of the aircraft from changing, thereby realizing self-stabilized flight.

[0038] Furthermore, due to the action of the spindle 107, the first rotor assembly 105 and the second rotor assembly 106 are differentially arranged respectively.

[0039] In another embodiment of the rotor mechanism 700, as shown in FIGS. 1 to 6, the rotor mechanism 700 directly rotationally drives the rotor by the motor 104, and a plurality of sets of the rotor mechanism 700 are provided. The plurality of sets of the rotor mechanism 700 are evenly distributed within the housing 101. Thereby, the plurality of sets of the rotor mechanism 700 realize the flight of the aircraft body 100.

[0040] In one embodiment, the aircraft body 100 further includes a housing 101 and a lamp 600. The housing 101 has a frame 1011, the frame 1011 is arranged in a ring shape, the lamp 600 is mounted on the frame 1011, and the lamp 600 is for emitting light outward. In this way, due to the action of the lamp 600, the atmosphere and appreciation value of the aircraft toy are improved.

[0041] In one embodiment, the detection assembly includes a plurality of infrared sensors 500. Each infrared sensor 500 is correspondingly provided at intervals along the frame 1011, and each infrared sensor 500 is used to detect the distance between the housing 101 and an object. In this way, each infrared sensor 500 cooperates to assist in detecting the flight attitude of the aircraft body 100 and facilitates quickly feedback of the force received by the aircraft body 100.

[0042] Specifically, regarding the interaction and contact between the user and the aircraft body 100, interaction by jumping can be realized by the hands, feet, and body parts contacting the rod receiver 2011.

[0043] The aircraft body 100 has the following two operating states. One is passive compression energy storage. When the aircraft is flying in the air or starting from a stationary state, the bottom of the bouncing rod 201 is tapped or kicked by a person, causing the bouncing rod 201 to press against the elastic member 202, and the elastic member 202 is compressed to store energy. At this time, the sensor of the aircraft body 100 can detect the tapping force and angle, or the kicking force and angle, and the control board 400 can control the aircraft body 100 through the sensor data to take various flight motion postures, so as to enhance the interactivity of the toy.

[0044] The other is to control the aircraft to descend rapidly. When the rod receiver 2011 of the bouncing rod 201 contacts the ground, the bouncing rod 201 presses against the elastic member 202, and the elastic member 202 is compressed to store energy. Next, the internal sensor detects the rebound of the bouncing rod 201 and releases it. In addition, in combination with the blades of the aircraft, the lift of the aircraft is rapidly increased, and the power generated by the aircraft toy and the biasing force released by the rebound of the bouncing rod 201 are superimposed, so that the energy loss of the aircraft toy is reduced, and an instantaneous large power is provided to the aircraft toy. In this way, the aircraft toy is more energy-efficient, has sufficient power, supports taking various motion postures, thereby improving the appreciation value of the aircraft.

[0045] As shown in FIG. 13, a waveform diagram of a control process corresponding to controlling the throttle and the height of the aircraft is generated according to the value of the accelerometer of the detection assembly. The rising edge of the acceleration waveform is a process in which the jump assembly 200 is compressed by the action of an external force to store energy, and the falling edge of the waveform is a rebound release process. In the release process, when the power throttle value of the aircraft toy itself increases and the rebound force generated by the jump assembly 200 is superimposed, the aircraft toy obtains a large instantaneous upward power, and its height increases and changes. The corresponding operation process from the falling edge of the acceleration curve to the change in value is the rapid bounce of the aircraft. When the aircraft toy reaches the target height, it starts to descend or stop and enters the next cycle.

[0046] In one embodiment of the jump assembly 200, as shown in FIGS. 1 to 3, the jump assembly 200 further includes a stopper 203 assembled to the aircraft body 100. The second end of the bouncing rod 201 is fitted into the stopper 203 and slidably connected to the stopper 203. The other end of the elastic member 202 is connected to the stopper 203. The first end of the bouncing rod 201 is configured as a rod receiver 2011, and the rod receiver 2011 is used to receive an external force. The bouncing rod 201 has a rod buckle 2012, and the elastic member 202 is fixed to the rod buckle 2012. The aircraft body 100 includes a housing 101. An opening 103 is formed in the housing 101. The bouncing rod 201 passes through the opening 103. The diameter of the rod buckle 2012 is larger than that of the opening 103, and it is located inside the housing 101.

[0047] In this embodiment, the stopper 203 is a single casing, and the bouncing rod 201 is inserted into the stopper 203 and can slide within the stopper 203. Thereby, when the rod receiver 2011 receives an external force, the bouncing rod 201 is pushed to drive the rod buckle 2012 to compress the elastic member 202 and store potential energy. Thereby, the jump assembly 200 switches between an extended energy release state and a compressed energy storage state. Various sensors inside the aircraft detect the flight state of the aircraft and the energy storage state and energy release state of the jump assembly 200. By superimposing the power of the aircraft itself in real time, an instantaneous large power is provided to the aircraft toy. In this way, the aircraft toy is more energy-efficient, has sufficient power, supports taking various motion postures, thereby improving the interactivity and appreciation of the aircraft.

[0048] Also, due to the action of the stopper 203, a role of positioning and displacement limitation is played with respect to the axial movement of the bouncing rod 201 and the elastic deformation of the elastic member 202, making it easier to switch the state of the jump assembly 200. Due to the action of the rod buckle 2012, positioning and position regulation are performed with respect to the movement stroke of the bouncing rod 201 and the elastic change stroke of the elastic member 202, ensuring that the jump assembly 200 and the aircraft body 100 are assembled movably. Furthermore, by externally attaching the elastic member 202, the arrangement space of the elastic member 202 in the axial direction becomes larger, making it possible to arrange elastic members 202 of various specifications, and also making it possible to arrange an elastic member 202 with a greater biasing force. By making the cross-sectional area of the rod receiver 2011 larger than the cross-sectional area of the rod body, the contact area of the rod receiver 2011 becomes larger, facilitating the user to tap or kick the rod receiver 2011 of the bouncing rod 201 and facilitating the interaction between the user and the aircraft body 100.

[0049] In this embodiment, the rod buckle 2012 is annular and fixed to the bouncing rod 201. In other embodiments of the rod buckle 2012 (not shown), the rod buckle 2012 may be a structure such as a bolt or a pin inserted into the bouncing rod 201, or may be other removable or non-removable structures protruding from the bouncing rod 201.

[0050] In a modification of this embodiment (not shown), the bouncing rod 201 may be a hollow rod. In this case, the stopper 203 is inserted into the bouncing rod 201, whereby the bouncing rod 201 may reciprocate and slide along the stopper 203. On the other hand, the elastic member 202 is fitted outside the stopper 203, and both ends thereof are connected to the bouncing rod 201 and the stopper 203, respectively.

[0051] In another modification of this embodiment (not shown), in the jump assembly 200, instead of the stopper 203, a slide groove for accommodating and sliding the bouncing rod 201 up and down may be formed in the aircraft body 100. The elastic member 202 is fitted outside the bouncing rod 201, and both ends thereof are connected to the aircraft body 100 and the bouncing rod 201, respectively. Thereby, when the bouncing rod 201 moves, the bouncing rod 201 also slides up and down, and the elastic member 202 also generates elastic deformation and stores energy elastically.

[0052] In another embodiment of the jump assembly 200, as shown in FIGS. 4 and 5, the jump assembly 200 further includes a stopper 203 assembled to the aircraft body 100. The second end of the bouncing rod 201 is fitted into the stopper 203 and slidably connected to the stopper 203. The elastic member 202 is located inside the stopper 203, one end of which is connected to the second end of the stopper 203 and the other end is fixed inside the stopper 203. The bouncing rod 201 has a rod buckle 2012, and the elastic member 202 is fixed to the rod buckle 2012. The aircraft body 100 includes a housing 101, an opening 103 is formed in the housing 101, the bouncing rod 201 passes through the opening 103, and the rod buckle 2012 has a diameter larger than that of the opening 103 and is located inside the housing 101.

[0053] In this embodiment, the elastic member 202 is built-in and provided, which facilitates the elastic deformation of the elastic member 202, protects the elastic member 202, and prolongs the service life of the elastic member 202. When the rod receiver 2011 receives an external force, the bouncing rod 201 is pushed, the elastic member 202 is compressed to store potential energy, whereby the jump assembly 200 switches between the extended energy release state and the compressed energy storage state. Various sensors inside the aircraft detect the flight state of the aircraft and the energy storage and energy release states of the jump assembly 200. By superimposing the power of the aircraft itself in real time, an instantaneous large power is provided to the aircraft. In this way, the aircraft toy is more energy-saving, has sufficient power, supports various motion postures, thereby improving the interactivity and appreciation of the aircraft.

[0054] Also, due to the action of the stopper 203, a role of positioning and displacement limitation is played with respect to the axial movement of the bouncing rod 201 and the elastic deformation of the elastic member 202, making it easier to switch the state of the jump assembly 200. By making the cross-sectional area of the rod receiver 2011 larger than the cross-sectional area of the rod body, the contact area of the rod receiver 2011 becomes larger, facilitating the user to tap or kick the rod receiver 2011 of the bouncing rod 201 and facilitating the interaction between the user and the aircraft body 100. Due to the action of the rod buckle 2012, positioning and position regulation are performed with respect to the movement stroke of the bouncing rod 201, ensuring that the jump assembly 200 and the aircraft body 100 are assembled movably.

[0055] In a modification (not shown) of this embodiment, the bouncing rod 201 may be a hollow rod. In this case, the stopper 203 is inserted into the bouncing rod 201, whereby the bouncing rod 201 may reciprocate and slide along the stopper 203. On the other hand, the elastic member 202 is located inside the bouncing rod 201, and both ends thereof are connected to the bouncing rod 201 and the stopper 203, respectively.

[0056] In another modification (not shown) of this embodiment, in the jump assembly 200, instead of the stopper 203, a slide groove for accommodating the bouncing rod 201 and sliding it up and down may be formed in the aircraft body 100. The elastic member 202 is mounted in the slide groove, and both ends thereof are connected to the aircraft body 100 and the bouncing rod 201, respectively. Thereby, when the bouncing rod 201 moves, the bouncing rod 201 also slides up and down, and the elastic member 202 also generates elastic deformation and stores energy elastically.

[0057] In the third embodiment of the jump assembly 200, as shown in FIGS. 6 to 7, the jump assembly 200 further includes a stopper 203 assembled to the aircraft body 100. The second end of the bouncing rod 201 extends toward the stopper 203. A fixed base 204 is provided, and the fixed base 204 is movably connected to the stopper 203. One end of the elastic member 202 is connected to the fixed base 204, and the other end is connected to the aircraft body 100 by a connecting member 205. When the bouncing rod 201 receives an external force and moves axially, the bouncing rod 201 drives the fixed base 204 to move axially, putting the elastic member 202 in an extended state.

[0058] In this embodiment, when the bouncing rod 201 receives an external force, the elastic member 202 is in an extended state, indicating an elastic energy storage state at this time. When the external force is removed, the elastic member 202 recovers and moves the bouncing rod 201 in the reverse direction, indicating a released state. That is, the potential energy stored in the elastic member 202 is converted into kinetic energy, and the bouncing rod 201 quickly pops out to push an obstacle, thereby converting the kinetic energy into the power of the aircraft.

[0059] In this embodiment, two elastic members 202 are provided, but a plurality of elastic members may be provided. Further, a guide groove 2031 is formed on the side of the stopper 203, and the fixed base 204 is movably fitted in the guide groove 2031. Due to the action of the guide groove 2031, positioning and position regulation effects are achieved for the axial movement of the fixed base 204, facilitating the axial movement of the fixed base 204.

[0060] In the fourth embodiment of the jump assembly 200, as shown in FIGS. 9 and 10, the stopper 203 is connected to the housing 101 of the aircraft body 100. The bouncing rod 201 penetrates the stopper 203 and is slidable within the stopper 203. The elastic member 202 is fitted outside the bouncing rod 201 and is located inside the stopper 203, with both ends thereof connected to the stopper 203 and the bouncing rod 201 respectively.

[0061] In this embodiment, when the bouncing rod 201 moves axially under an external force, the bouncing rod 201 moves the fixed base 204 axially, compresses or extends the elastic member 202, thereby elastically storing energy. When the external force is removed, the elastic member 202 recovers and moves the bouncing rod 201 in the reverse direction to show a released state, that is, the potential energy stored by the elastic member 202 is converted into kinetic energy, and the bouncing rod 201 quickly pops out to push an obstacle, thereby converting the kinetic energy into the power of the aircraft.

[0062] As described above, as can be seen from the above description, the present invention realizes the following technical effects.

[0063] In the interactive jump-type aircraft toy according to the present invention, when the aircraft body 100 is flying autonomously, the bouncing rod 201 receives an external force, the elastic member 202 is in a compressed state or an extended state, and the jump assembly 200 is in a state of storing compression energy. Then, when the bouncing rod 201 recovers and rebounds to release the acting force, the power of the aircraft itself is added, the lift is improved, the energy loss during flight is reduced, and an instantaneous large power for supporting the aircraft is obtained, so that the aircraft can take various motion postures, the appreciation and playability of the aircraft are improved, and the battery endurance is increased. Furthermore, when the user's body part contacts the jump assembly 200, the jump assembly 200 is put into a state of storing compression energy, and then, through the cooperation of the bouncing rod 201 and the detection assembly, the aircraft body 100 is made to take various flight motion postures, thereby greatly improving the interactivity of the aircraft toy.

[0064] In the description of the present invention, the directions or positional relationships indicated by orientation terms such as "front, rear, top, bottom, left, right", "lateral direction, longitudinal direction, vertical, horizontal", and "top, bottom" are usually based on the directions or positional relationships shown in the drawings, and are only for facilitating the description of the present invention and simplifying the description. Conversely, unless otherwise stated, these orientation terms do not indicate or imply that the device or element being referred to must have a specific orientation or be configured and operate in a specific orientation, and thus cannot be understood as limiting the protection scope of the present invention. The orientation terms "inside, outside" mean inside and outside with respect to the contour of each member itself.

[0065] For the sake of easy explanation, here, in order to describe the spatial positional relationship between one device or feature and another device or feature as shown in the figure, spatial relative terms such as "above", "above of", "upper surface of", "higher than" may be used. It should be understood that the spatial relative terms are intended to include other orientations in the use or operation other than the orientation of the device described in the drawing. For example, when the device in the drawing is reversed, a device described as "above another device or configuration" or "above another device or configuration" is positioned as "below another device or configuration" or "below another device or configuration". Therefore, the exemplary term "above" can include two orientations, "above" and "below". This device can also be positioned in other different ways (rotated 90 degrees or other orientations) and can be interpreted according to the spatially relative description used here.

[0066] Note that the use of terms such as "first", "second" to limit members is for the purpose of easily distinguishing the corresponding members. Without further explanation, the above terms do not have a special meaning, and thus cannot be understood as limiting the protection scope of the present invention.

[0067] The above description is only a preferred embodiment of the present invention and does not limit the present invention. For those skilled in the art, various modifications and changes are possible to the present invention. Any modifications, equivalent substitutions, improvements, etc. made without departing from the spirit and principle of the present invention should be included in the protection scope of the present invention.

Description of Reference Numerals

[0068] Aircraft body (100), housing (101), frame (1011), accommodation chamber (102), opening (103), motor (104), first rotor assembly (105), second rotor assembly (106), spindle (107), reduction gear (108), jump assembly (200), bouncing rod (201), rod receiver (2011), rod buckle (2012), elastic member (202), stopper (203), guide groove (2031), fixed base (204), connecting member (205), power supply (300), control board (400), infrared sensor (500), lamp (600), rotor mechanism (700)

Claims

1. An interactive jump type aircraft toy including an aircraft body, The aircraft body is equipped with a jump assembly and a detection assembly, the jump assembly can generate elastic deformation, store elastic energy, and release potential energy, and the detection assembly is used to detect the flight state of the aircraft body and detect the elastic energy storage state and potential energy release state of the jump assembly; The jump assembly includes a bouncing rod and an elastic member, the bouncing rod having a first end and a second end, the first end of the bouncing rod penetrating the aircraft body and receiving an external force to drive the bouncing rod and the aircraft body to move relative to each other; The elastic member has one end connected directly or indirectly to the bouncing rod and the other end connected directly or indirectly to the aircraft body; The interactive jump type aircraft toy, wherein the elastic member is configured to generate elastic deformation and store elastic potential energy when the bouncing rod receives an external force and moves.

2. The interactive jump type aircraft toy of claim 1, characterized in that the jump assembly further includes a stopper attached to the aircraft body, and a second end of the bouncing rod is fitted into the stopper and slidably connected to the stopper.

3. The interactive jump type aircraft toy according to claim 2, characterized in that the other end of the elastic member is connected to the stopper, and the first end of the bouncing rod is configured as a rod receiver, and the rod receiver is used to receive an external force.

4. The interactive jump type aircraft toy according to claim 3, characterized in that the bouncing rod has a rod buckle, the elastic member is fixed to the rod buckle, the aircraft body includes a housing having an opening, the bouncing rod passes through the opening, and the rod buckle has a diameter larger than the opening and is located inside the housing.

5. The interactive jump type aircraft toy according to claim 2, characterized in that the elastic member is located inside the stopper, one end of the elastic member is connected to the second end of the bouncing rod and the other end is connected to the inside of the stopper, the first end of the bouncing rod is configured as a rod receiver, and the rod receiver is used to receive an external force.

6. The interactive jump type aircraft toy according to claim 1, characterized in that the jump assembly further includes a stopper attached to the aircraft body, the second end of the bouncing rod extends toward the stopper and has a fixed base attached thereto, the fixed base is movably connected to the stopper, the elastic member has one end connected to the fixed base and the other end connected to the aircraft body, and when the bouncing rod moves axially due to an external force, the bouncing rod drives the fixed base to move axially and puts the elastic member into an extended state.

7. The interactive jump type aircraft toy of claim 1, characterized in that the aircraft body includes a housing, a spindle, a motor, a first rotor assembly, and a second rotor assembly, the first rotor assembly and the second rotor assembly are each attached to the spindle, a storage chamber is located at the center of the first rotor assembly, the motor is attached within the storage chamber, and the motor is fixedly attached to a wall of the storage chamber.

8. The interactive jump type aircraft toy according to claim 7, characterized in that a power supply and a control board are provided in the accommodation chamber, the power supply and the control board are each electrically connected to the motor, the second rotor assembly is located below the first rotor assembly, the spindle is disposed through the second rotor assembly, and an upper end of the spindle is rotatably attached to the housing, the jump assembly further includes a stopper attached to the aircraft body, a lower end of the spindle is fitted into the stopper, and the stopper is movably connected to the bouncing rod, the motor rotates and drives the second rotor assembly via a reduction gear, and the first rotor assembly and the second rotor assembly are connected to be interlocked.

9. The interactive jump type aircraft toy of claim 1, characterized in that the aircraft body includes a housing and a lamp, the housing has a frame, the frame is arranged in a ring shape, the lamp is attached to the frame, and the lamp is for emitting light to the outside, the detection assembly includes a plurality of infrared sensors, the plurality of infrared sensors are correspondingly arranged at intervals along the frame, and the plurality of infrared sensors are used to detect the distance between the housing and an object.

10. The interactive jump type aircraft toy of claim 1, characterized in that the bouncing rod includes a rod body and a rod receiver, the rod receiver is configured as the first end, the elastic member is connected to the rod body, and a cross-sectional area of ​​the rod receiver is larger than a cross-sectional area of ​​the rod body.

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