Jumping type aircraft interactive toy

Abstract

The utility model relates to the technical field of aircraft interaction toys, and discloses a jumping type aircraft interaction toy which comprises an aircraft body, a jumping assembly and a detection assembly, and the detection assembly is used for detecting the flight state of the aircraft body; the jumping assembly comprises a bouncing rod and an elastic part, the bouncing rod penetrates through the bottom of the aircraft body, the bouncing rod is movably arranged, the elastic part and the bouncing rod are assembled, and the bouncing rod bears external force to enable the elastic part to be in an energy storage state. When the bouncing rod is subjected to external force, the bouncing assembly is in a compressed energy storage state, power generated by resetting and energy releasing is superposed on power of the aircraft, so that the energy loss of the aircraft is reduced, the cruising ability is improved, instantaneous large power is obtained, the aircraft has enough power to make different motion postures, and the ornamental value and playability of the aircraft are improved; the jumping assembly is in a compressed energy storage state through contact between a body part and the jumping assembly, and the aircraft body is in different flight motion postures by matching with the detection assembly, so that the interactivity of the aircraft toy is improved.

Description

Technical Field

[0001] This utility model patent relates to the technical field of interactive aircraft toys, and more specifically, to interactive jumping aircraft toys. Background Technology

[0002] With the development of science and technology and the continuous improvement of people's living standards, electronic toys are becoming more and more diverse and powerful; various related technologies of aerodynamic aircraft have been widely applied in the toy field, creating various types of aircraft.

[0003] For example, the prior patent with authorization announcement number CN214714349U discloses an aircraft toy, including a cage-like support frame, in which propellers and a motor driving the propellers to rotate are installed. The axis of rotation of the propellers is vertical. The cage-like support frame is a spherical cage-like support frame, which includes multiple warp frame strips extending along the meridian direction and multiple weft frame strips extending along the parallel direction; the warp frame strips and the weft frame strips are collectively referred to as frame strips; and each annular strip decorative element and frame strip is provided with a fastening structure.

[0004] In the existing technology, the flight movements of flying toys are monotonous and lack fun. At the same time, flying toys lack interaction with users, resulting in insufficient interactivity and playability, which affects the user experience. Utility Model Content

[0005] The purpose of this invention is to provide an interactive jumping aircraft toy, which aims to solve the problem of insufficient interactivity in existing aircraft toys.

[0006] This invention is implemented as follows: a jumping interactive toy includes a flying vehicle body, a jumping assembly, and a detection assembly. The jumping assembly and the detection assembly are respectively assembled with the flying vehicle body. The detection assembly is used to detect the flight status of the flying vehicle body and the energy storage status of the jumping assembly. The jumping assembly includes a bouncing rod and an elastic element. The bouncing rod passes through the bottom of the flying vehicle body and is movably arranged. The elastic element is assembled with the bouncing rod. When the bouncing rod is subjected to external force, the elastic element is in an elastic energy storage state.

[0007] Furthermore, the jumping assembly includes a locking component, which is assembled with the aircraft body. The upper part of the jumping rod is movably fitted with the locking component. One end of the elastic component is connected to the locking component, and the other end of the elastic component is sleeved on the jumping rod. The lower part of the jumping rod extends downward through the aircraft body, and the lower part of the jumping rod forms a rod seat for receiving external force.

[0008] Furthermore, the bouncing rod has a buckle, and the other end of the elastic element is arranged in a mating arrangement with the buckle; the aircraft body includes a shell, the shell has a lower shell opening, and the buckle is located inside the shell.

[0009] Furthermore, the jumping assembly includes a locking component, which is assembled with the aircraft body. The elastic component is located inside the locking component. The upper part of the jumping rod is movably embedded with the locking component, and the upper part of the jumping rod is connected to the elastic component. The lower part of the jumping rod extends downward through the aircraft body, and the lower part of the jumping rod forms a rod seat for receiving external force.

[0010] Furthermore, the jump assembly includes a locking component and a spring fastener. The locking component is assembled with the aircraft body, and the locking component is movably assembled with the spring fastener. The upper part of the elastic component is assembled with the spring fastener, and the lower part of the elastic component is docked with the aircraft body. The jump bar is fixedly assembled with the spring fastener. When the jump bar is subjected to force and moves axially, it causes the spring fastener to move axially, and the axial movement of the spring fastener causes the elastic component to be in a stretched state.

[0011] Furthermore, the aircraft body includes a control board, and the detection assembly includes an acceleration sensor. The acceleration sensor is electrically connected to the control board. The acceleration sensor is used to detect the acceleration change of the aircraft body and feed back the data to the control board. The acceleration sensor is also used to detect the real-time status of the energy storage and reset energy release of the jump assembly.

[0012] Furthermore, the detection assembly includes a gyroscope, which is used to detect the flight attitude of the aircraft body and feed the data back to the control board.

[0013] Furthermore, the aircraft body includes an outer shell, a spindle, a motor assembly, an upper rotating blade assembly, and a lower rotating blade assembly. The upper and lower rotating blade assemblies are respectively mounted on the spindle. The upper rotating blade assembly has a cavity at its center. The motor assembly is mounted in the cavity and is fixedly installed to the cavity wall. A power supply and a control board are disposed inside the cavity. The power supply and the control board are electrically connected to the motor assembly. The lower rotating blade assembly is located below the upper rotating blade assembly. The spindle passes through the lower rotating blade assembly, and its upper end is rotatably mounted to the outer shell. The lower end of the spindle is embedded in the locking member, and the locking member is movably connected to the bouncing rod. The motor assembly drives the lower rotating blade assembly to rotate through a reduction gear. The upper and lower rotating blade assemblies are linked together.

[0014] Furthermore, the aircraft body includes an outer shell and a light strip component. The outer shell has a frame arranged in a ring shape, and the light strip component is installed on the frame and is used to emit light outward. The detection assembly includes multiple infrared sensors, each of which is arranged at intervals along the frame and is used to detect the distance between the outer shell and an object.

[0015] Furthermore, the bouncing rod includes a rod body and a rod seat. Along the axial direction, the rod body and the rod seat are arranged in a mating arrangement, and the elastic element is assembled with the rod body. The cross-sectional area of ​​the rod seat is larger than the cross-sectional area of ​​the rod body.

[0016] Compared with existing technologies, the jumping aircraft interactive toy provided by this utility model has the following characteristics: When the aircraft flies autonomously, the jumping bar is subjected to external force, causing the elastic component to be in a compressed or stretched state, and the jumping assembly to be in a compressed energy storage state. Then, when the jumping bar returns to its original position and releases the force, it simultaneously increases the lift by superimposing the aircraft's own power, reducing energy loss during flight and providing instantaneous high-power support for the aircraft, enabling it to make different movement postures. This increases the aircraft's visual appeal and playability, as well as the battery's endurance. Furthermore, when the user comes into contact with the jumping assembly through body parts, the jumping assembly is compressed and stored in energy. Then, through the cooperation of the jumping bar and the detection assembly, the aircraft body makes different flight postures, greatly increasing the interactivity of the aircraft toy. Attached Figure Description

[0017] Figure 1 This is a cross-sectional schematic diagram of one embodiment of the interactive jumping flight toy provided by this utility model;

[0018] Figure 2 This is a three-dimensional layout schematic diagram of the jumping assembly of Embodiment 1 of the interactive jumping toy provided by this utility model.

[0019] Figure 3 This is a three-dimensional schematic diagram of one embodiment of the interactive jumping flight toy provided by this utility model;

[0020] Figure 4 This is a cross-sectional schematic diagram of Embodiment 2 of the interactive jumping flight toy provided by this utility model;

[0021] Figure 5 This is an exploded view of the jumping assembly of Embodiment 2 of the interactive jumping toy provided by this utility model;

[0022] Figure 6 This is a three-dimensional schematic diagram of a second embodiment of the interactive jumping flight toy provided by this utility model;

[0023] Figure 7 This is a three-dimensional schematic diagram of the layout of the battery components of the interactive jumping toy provided by this utility model.

[0024] Figure 8 This is an exploded view of Embodiment 3 of the interactive jumping toy provided by this utility model.

[0025] Figure 9 This is a schematic diagram of the data graphs showing the coordination between the accelerometer and the flight control system of the interactive jumping toy provided by this utility model. Detailed Implementation

[0026] To make the objectives, technical solutions, and advantages of this utility model clearer, the present utility model will be further described in detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the present utility model and are not intended to limit the present utility model.

[0027] The implementation of this utility model will be described in detail below with reference to specific embodiments.

[0028] In the accompanying drawings of this embodiment, the same or similar reference numerals correspond to the same or similar components. In the description of this utility model, it should be understood that if terms such as "upper," "lower," "left," and "right" indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings, they are only for the convenience of describing this utility model and simplifying the description, and do not indicate or imply that the device or component referred to must have a specific orientation, or be constructed and operated in a specific orientation. Therefore, the terms used to describe positional relationships in the accompanying drawings are only for illustrative purposes and should not be construed as limiting this patent. For those skilled in the art, the specific meaning of the above terms can be understood according to the specific circumstances.

[0029] Reference Figure 1-9 The image shown is a preferred embodiment of the present invention.

[0030] A jumping aircraft interactive toy includes an aircraft body 2, a jumping assembly 1, and a detection assembly. The jumping assembly 1 and the detection assembly are respectively assembled with the aircraft body 2. The detection assembly is used to detect the flight status of the aircraft body 2 and the energy storage status of the jumping assembly 1. The jumping assembly 1 includes a bouncing rod 11 and an elastic element 12. The bouncing rod 11 passes through the bottom of the aircraft body 2 and is movably arranged. The elastic element is assembled with the bouncing rod. When the bouncing rod is subjected to external force, the elastic element is in an elastic energy storage state.

[0031] In the aforementioned interactive jumping toy, when the aircraft body 2 flies autonomously, the spring element 12 is compressed or stretched under external force on the jumping bar 11, causing the jumping assembly 1 to be in a compressed energy storage state. Then, when the jumping bar 11 returns to its original position and releases the force, it simultaneously increases lift by superimposing the aircraft's own power, reducing energy loss during flight and providing instantaneous high-power support for the aircraft. This allows the aircraft to perform different motion postures, increasing the toy's visual appeal and playability, as well as battery life. Furthermore, when the user contacts the jumping assembly 1 with their body parts, the jumping assembly 1 is compressed and stored in energy. Through the coordination of the jumping bar 11 and the detection assembly, the aircraft body 2 can perform different flight motion postures, greatly increasing the toy's interactivity.

[0032] The elastic energy storage state can be achieved by compressing or stretching the elastic element 12 to achieve the elastic energy storage state.

[0033] When the external force is removed or fails, the elastic component resets to a released state. In this released state, the potential energy stored in the elastic component is converted into kinetic energy, causing the bouncing rod to quickly pop out and push against obstacles, thus converting the force into the power of the aircraft. This reduces the energy loss of the aircraft toy during flight and provides instantaneous high-power support for the aircraft, enabling it to make different movement postures. This increases the visual appeal and playability of the aircraft toy, as well as the battery's endurance.

[0034] The vertical line of the aircraft body 2 coincides with the vertical line of the bouncing bar 11; this makes the flight attitude of the aircraft body 2 more stable.

[0035] The aircraft body 2 includes a control board 5, and the detection assembly includes an acceleration sensor. The acceleration sensor is electrically connected to the control board 5. The acceleration sensor is used to detect the acceleration change of the aircraft body 2 and feed back the data to the control board 5. The acceleration sensor is also used to detect the energy storage state of the jump assembly 1.

[0036] In this way, through the preset program on the control panel 5, the aircraft body 2 can make different flight motion attitudes based on the state switching of the jump assembly 1.

[0037] For example, the control board 5, based on data from various sensors, makes the aircraft body 2 jump, such as by simulating shuttlecock, to provide entertainment and fitness for the aircraft body 2.

[0038] Furthermore, under the control of the control board 5, and in conjunction with data from various sensors, the aircraft body 2 can be made to roll, jump forward, backward, left, and right; this increases the visual appeal and playability of the aircraft toy, as well as its interactivity.

[0039] The detection assembly includes a gyroscope, which is used to detect the flight attitude of the aircraft body 2 and feed the data back to the control board 5; the gyroscope realizes the monitoring of the flight attitude of the aircraft body 2, such as detecting the angular velocity of the aircraft body 2.

[0040] The detection assembly includes an accelerometer and a barometer. The accelerometer is used to detect the speed changes of the aircraft body 2 and the energy storage state changes of the jump assembly 1. The compression and release states of the jump assembly are detected by the accelerometer and transmitted to the main control board, so that the elastic force generated by the jump assembly can be matched with the aircraft's own power in real time to achieve different flight attitude control. The barometer is used to detect the altitude changes of the aircraft body 2. The descent speed of the aircraft can be set according to the altitude of the aircraft to set the corresponding rebound force generated by the jump assembly.

[0041] The detection assembly includes an infrared sensor 3, which is mounted on the pole base 111. The infrared sensor 3 is used to determine the distance between the pole base 111 and the object. In this way, when the aircraft body 2 jumps on its own, the infrared sensor 3 can determine the distance between it and the ground. When the user interacts with the aircraft body 2, the infrared sensor 3 can determine the distance between the user and the pole base 111.

[0042] The aircraft body 2 includes an outer shell, a spindle, a motor component 23, an upper rotating blade assembly 21, and a lower rotating blade assembly 22. The upper rotating blade assembly 21 and the lower rotating blade assembly 22 are respectively mounted on the spindle. The upper rotating blade assembly 21 has a cavity at its center. The motor component 23 is mounted in the cavity and is fixedly installed to the cavity wall. A power supply and a control board are provided inside the cavity and are electrically connected to the motor component 23. The lower rotating blade assembly 22 is located below the upper rotating blade assembly 21. The spindle passes through the lower rotating blade assembly 22 and is rotatably mounted to the outer shell. The lower end of the spindle is embedded in the locking member, and the locking member is movably connected to the bouncing rod. The motor component drives the lower rotating blade assembly to rotate through a reduction gear. The upper rotating blade assembly and the lower rotating blade assembly are linked together.

[0043] When the motor component 23 is energized, the rotating shaft of the motor component 23 drives the lower rotating blade assembly 22 to rotate through the reduction gear 24. The reverse torque of the rotation of the motor component 23 drives the upper rotating blade assembly 21 to rotate. The upper rotating blade assembly 21 and the lower rotating blade assembly 22 rotate in opposite directions and generate downward wind force to generate lift for the aircraft. The high-speed rotation of the upper rotating blade assembly 21 generates a gyro effect, which keeps the flight angle of the aircraft constant and achieves self-stabilized flight.

[0044] Furthermore, under the action of the spindle, the upper rotating blade group 21 and the lower rotating blade group 22 are arranged differentially.

[0045] The aircraft body 2 includes an outer shell and a light strip 4. The outer shell has a frame arranged in a ring. The light strip 4 is installed on the frame and is used to emit light outward. In this way, the light strip 4 enhances the atmosphere and visual appeal of the aircraft toy.

[0046] The detection assembly includes multiple infrared sensors 3, which are arranged at intervals along the shell frame. Each infrared sensor 3 is used to detect the distance between the shell and the object. In this way, with the cooperation of each infrared sensor 3, the flight attitude of the aircraft body 2 can be detected, and the force on the aircraft body 2 can be quickly fed back.

[0047] Specifically, the user can interact with the aircraft body 2 by using their hands, feet, or body parts to contact the stick 111, thus achieving a bouncing interaction.

[0048] The aircraft body 2 has two working states. One is passive compression and energy storage. When the aircraft is flying in the air or starting from a standstill, it is hit or kicked by a person at the bottom of the bouncing bar 11, which causes the bouncing bar 11 to push the elastic element 12, making the elastic element 12 compress and store energy. At this time, the sensors of the aircraft body 2 can detect the force and angle of the hit or kick. The control board 5 can control the aircraft body 2 to make different flight movements based on the data from the sensors, which increases the interactivity of the toy.

[0049] Another method involves controlling the aircraft to descend rapidly. When the bottom of the bouncing bar 11 touches the ground, the bouncing bar 11 pushes the elastic element 12, causing the elastic element 12 to compress and store energy. The rebound release of the bouncing bar 11 is detected by an internal sensor. At the same time, the lift of the aircraft is rapidly increased by the propeller blades. The power generated by the aircraft toy and the elastic force released by the rebound of the bouncing bar 11 are superimposed, reducing the energy loss of the aircraft toy and giving the aircraft toy instantaneous high power. The aircraft toy is more energy-efficient and powerful, supports the aircraft to make different movement postures, and increases the aircraft's visual appeal.

[0050] like Figure 9 As shown, the control process waveform diagrams corresponding to the control throttle and aircraft altitude are generated based on the acceleration count value of the detection assembly 1. The rising edge of the accelerometer waveform represents the compression and energy storage process of the jump assembly 1 under the action of external force, and the falling edge of the waveform represents the rebound and release process. During the release process, the aircraft toy's own power throttle value increases, and the rebound force generated by the jump assembly 1 is superimposed, giving the aircraft toy a momentary large power lift, and the altitude changes. The corresponding motion process from 0 to -300 after the falling edge of the accelerometer curve is the rapid bouncing of the aircraft. When the aircraft toy reaches the target altitude, it begins to descend or hover, entering the next cycle. Example

[0051] The jump assembly 1 includes a locking component 13, which is assembled with the aircraft body 2. The upper part of the jump bar 11 is movably fitted with the locking component 13. One end of the elastic component 12 is connected to the locking component 13, and the other end of the elastic component 12 is fitted with the jump bar 11. The lower part of the jump bar 11 extends downward through the aircraft body 2, and the lower part of the jump bar 11 forms a pole seat 111, which is used to receive external force.

[0052] In this way, when the rod base 111 is subjected to external force, it pushes the jumping rod 11 to drive the rod buckle 112 to compress the elastic element 12 and store potential energy, realizing the switching between the extended energy release state and the compressed energy storage state of the jumping assembly 1. The flight state and the energy storage and release state of the jumping assembly are detected by various sensors inside the aircraft, and then combined with the aircraft's own power in real time, so that the aircraft can obtain a large instantaneous power, making the aircraft toy more energy-efficient and powerful, supporting the aircraft to make different movement postures, and increasing the interactivity and ornamental value of the aircraft.

[0053] Meanwhile, under the action of the locking component 13, the axial movement of the jumping rod 11 and the elastic change of the elastic component 12 play a role in positioning and limiting the offset, which facilitates the state switching of the jumping assembly 1.

[0054] The bouncing rod 11 has a rod buckle 112, which is arranged protrudingly along the circumference. The other end of the elastic member 12 is arranged in a mating arrangement with the rod buckle 112. The aircraft body 2 includes an outer shell with a lower shell opening. The rod buckle 112 is located inside the outer shell, and the cross-sectional area of ​​the rod buckle 112 is larger than that of the lower shell opening.

[0055] Under the action of the lever buckle 112, the movement stroke of the jumping lever 11 and the elastic change stroke of the elastic component 12 are positioned and limited, ensuring the movable assembly between the jumping assembly 1 and the aircraft body 2.

[0056] The elastic element 12 is arranged externally, and the elastic element 12 has a larger axial setting range to meet the setting of elastic elements 12 of different specifications, and to meet the setting of elastic elements 12 with greater elastic force.

[0057] The bouncing stick 11 includes a stick body and a stick base 111. Along the axial direction, the stick body and the stick base 111 are arranged in a mating arrangement, and the elastic element 12 is assembled with the stick body. The cross-sectional area of ​​the stick base 111 is larger than that of the stick body. In this way, the stick base 111 has a larger contact area, which makes it easier for the user to pat or kick the stick base 111 of the bouncing stick 11, and facilitates the interaction between the user and the aircraft body 2. Example

[0058] The jump assembly 1 includes a locking component 13, which is assembled with the aircraft body 2. The elastic component 12 is located inside the locking component 13. The upper part of the jump bar 11 is movably fitted with the locking component 13, and the upper part of the jump bar 11 is connected to the elastic component 12. The lower part of the jump bar 11 extends downward through the aircraft body 2. The lower part of the jump bar 11 forms a support 111, which is used to receive external force.

[0059] In this way, the elastic component 12 is arranged internally, which facilitates the elastic deformation of the elastic component 12 and at the same time protects the elastic component 12 and improves its service life. When the rod base 111 is subjected to external force, it pushes the jumping rod 11 to compress the elastic component 12 to store potential energy, realizing the switching between the extended energy release state and the compressed energy storage state of the jumping assembly 1. Various sensors inside the aircraft detect its flight status and the energy storage and release state of the jumping assembly, and then combine it with the aircraft's own power in real time to enable the aircraft to obtain instantaneous large power, making the aircraft toy more energy-efficient and powerful, supporting the aircraft to make different movement postures, and increasing the interactivity and ornamental value of the aircraft.

[0060] Meanwhile, under the action of the locking component 13, the axial movement of the jumping rod 11 and the elastic change of the elastic component 12 play a role in positioning and limiting the offset, which facilitates the state switching of the jumping assembly 1.

[0061] The bouncing stick 11 includes a stick body and a stick base 111. Along the axial direction, the stick body and the stick base 111 are arranged in a mating arrangement, and the elastic element 12 is assembled with the stick body. The cross-sectional area of ​​the stick base 111 is larger than that of the stick body. In this way, the stick base 111 has a larger contact area, which makes it easier for the user to pat or kick the stick base 111 of the bouncing stick 11, and facilitates the interaction between the user and the aircraft body 2.

[0062] The bouncing stick 11 has a buckle 112, which is arranged protrudingly along the circumference. The aircraft body 2 includes an outer shell with a lower shell opening. The buckle 112 is located inside the outer shell, and the cross-sectional area of ​​the buckle 112 is larger than that of the lower shell opening. Under the action of the buckle 112, the movement stroke of the bouncing stick 11 is positioned and limited, ensuring the movable assembly between the jumping assembly 1 and the aircraft body 2. Example

[0063] The jump assembly 1 includes a locking component 13 and a spring fastener 14. The locking component 13 is assembled with the aircraft body 2, and the locking component 13 and the spring fastener 14 are movably assembled. The upper part of the elastic component 12 is assembled with the spring fastener 14, and the lower part of the elastic component 12 is docked with the aircraft body 2. The jump bar 11 and the spring fastener 14 are fixedly assembled. When the jump bar 11 is subjected to force and moves axially, it causes the spring fastener 14 to move axially. The axial movement of the spring fastener 14 causes the elastic component 12 to be in a stretched state.

[0064] Thus, when the bouncing rod 11 is subjected to an external force, the elastic element 12 is stretched and in an elastic energy storage state. After the external force is removed, the elastic element 12 returns to its original position and pushes the bouncing rod 11 to move and release. That is, the potential energy stored in the elastic element 12 is converted into kinetic energy, which causes the bouncing rod 11 to quickly pop out and push the obstacle into the power of the aircraft.

[0065] Two or more elastic components 12 can be set.

[0066] Furthermore, the side of the locking component forms a locking groove, and the spring fastener 14 is movably embedded in the locking groove. Under the action of the locking groove, the axial movement of the spring fastener 14 is positioned and limited, which facilitates the axial movement of the spring fastener 14.

[0067] The above description is only a preferred embodiment of the present utility model and is not intended to limit the present utility model. Any modifications, equivalent substitutions and improvements made within the spirit and principles of the present utility model should be included within the protection scope of the present utility model.

Claims

1. A jump-vehicle interactive toy characterized in that, The application relates to a flying device, which comprises a flying device body, a jumping assembly and a detection assembly, the jumping assembly and the detection assembly are arranged on the flying device body, the detection assembly is used for detecting the flying state of the flying device body and detecting the energy storage state of the jumping assembly; the jumping assembly comprises a jumping rod and an elastic piece, the jumping rod penetrates the bottom of the flying device body, the jumping rod is arranged in a movable mode, and the elastic piece is arranged on the jumping rod in a combined mode; the jumping rod is driven by external force to make the elastic piece in an elastic energy storage state.

2. The jump-in aircraft interactive toy of claim 1, wherein, The jumping assembly comprises a clamping piece, the clamping piece is arranged on the flying device body in a combined mode, the upper part of the jumping rod is movably arranged in the clamping piece, one end of the elastic piece is arranged in butt joint with the clamping piece, and the other end of the elastic piece is sleeved on the jumping rod; the lower part of the jumping rod penetrates the flying device body and extends downward, the lower part of the jumping rod forms a rod seat, and the rod seat is used for receiving external force.

3. The jump-in aircraft interactive toy of claim 2, wherein, The jumping rod has a rod buckle, and the other end of the elastic piece is arranged in butt joint with the rod buckle; the flying device body comprises a shell, the shell has a lower shell opening, and the rod buckle is arranged in the shell.

4. The jump-in aircraft interactive toy of claim 1, wherein, The jumping assembly comprises a clamping piece, the clamping piece is arranged on the flying device body in a combined mode, the elastic piece is arranged in the clamping piece, the upper part of the jumping rod is movably arranged in the clamping piece, and the upper part of the jumping rod is arranged in butt joint with the elastic piece; the lower part of the jumping rod penetrates the flying device body and extends downward, the lower part of the jumping rod forms a rod seat, and the rod seat is used for receiving external force.

5. The jump-in aircraft interactive toy of claim 1, wherein, The jumping assembly comprises a clamping piece and a spring fixing piece, the clamping piece is arranged on the flying device body in a combined mode, the clamping piece is movably arranged on the spring fixing piece, the upper part of the elastic piece is arranged on the spring fixing piece in a combined mode, and the lower part of the elastic piece is arranged in butt joint with the flying device body; the jumping rod is fixedly arranged on the spring fixing piece, the jumping rod is axially moved to drive the spring fixing piece to be axially moved, and the spring fixing piece is axially moved to make the elastic piece in a tensile state.

6. The jump-in aircraft interactive toy according to any one of claims 1 to 5, wherein The flying device body comprises a control panel, the detection assembly comprises an acceleration sensor, the acceleration sensor is arranged in electric connection with the control panel, the acceleration sensor is used for detecting the acceleration change of the flying device body and feeding back data to the control panel, and the acceleration sensor is used for detecting the real-time state of energy storage and reset energy release of the jumping assembly.

7. The jump-in aircraft interactive toy of claim 6, wherein, The detection assembly comprises a gyroscope, the gyroscope is used for detecting the flying posture of the flying device body and feeding back data to the control panel.

8. The jump-in aircraft interactive toy of any one of claims 2-5, wherein, The aircraft body comprises a shell, a mandrel, a motor, an upper rotating blade group and a lower rotating blade group, the upper rotating blade group and the lower rotating blade group are arranged on the mandrel respectively, the center of the upper rotating blade group has a cavity, the motor is arranged in the cavity, and the motor is fixedly installed with the cavity wall, the cavity is provided with a power supply and a control panel, the power supply and the control panel are electrically connected with the motor respectively, the lower rotating blade group is below the upper rotating blade group, the mandrel penetrates through the lower rotating blade group and is arranged, the upper end of the mandrel is rotatably arranged with the shell, the lower end of the mandrel is embedded into the clamping part, and the clamping part is movably connected with the elastic rod; the motor drives the lower rotating blade group to rotate through the reduction gear, and the upper rotating blade group is connected with the lower rotating blade group.

9. The jump-in interactive toy of any one of claims 2-4, wherein, The aircraft body comprises a shell and a lamp strip, the shell has a shell frame, the shell frame is arranged in a ring shape, the lamp strip is arranged in the shell frame, and the lamp strip is used for emitting light outward; the detection assembly comprises a plurality of infrared sensors, each infrared sensor is arranged in correspondence with the shell frame at intervals, and each infrared sensor is used for detecting the distance between the shell and an object.

10. The jump-in interactive toy of any one of claims 2-4, wherein, The elastic rod comprises a rod body and a rod seat, and the rod body and the rod seat are arranged in butt joint along the axial direction, and the elastic member is assembled with the rod body; the cross-sectional area of the rod seat is greater than that of the rod body.

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