Hopping-type aircraft interactive toy

A hopping-type aircraft interactive toy, comprising an aircraft body, wherein

• the aircraft body is equipped with a hopping assembly and a detection assembly, wherein the hopping assembly is elastically deformable to store and release elastic potential energy, and the detection assembly is configured to detect a flight state of the aircraft body, as well as an elastic energy storage state and a potential energy release state of the hopping assembly;
• and
• the hopping assembly comprises a bouncing rod and an elastic member, and the bouncing rod has a first end and a second end, wherein the first end of the bouncing rod penetrates out of the aircraft body and is configured to receive an external force, and drives a relative movement between the bouncing rod and the aircraft body;
• and
• at least one end of the elastic member is connected to the bouncing rod, and the elastic member is configured such that when the bouncing rod is subjected to an external force and moves, the elastic member undergoes elastic deformation and stores elastic potential energy;
• and
• wherein the hopping assembly further comprises a limiting member assembled on the aircraft body, the second end of the bouncing rod extends towards the limiting member and is equipped with a spring retainer, and the spring retainer is movably connected to the limiting member.

A hopping-type aircraft interactive toy, comprising an aircraft body, wherein

• the aircraft body is equipped with a hopping assembly and a detection assembly, wherein the hopping assembly is elastically deformable to store and release elastic potential energy, and the detection assembly is configured to detect a flight state of the aircraft body, as well as an elastic energy storage state and a potential energy release state of the hopping assembly;
• and the hopping assembly comprises a bouncing rod and an elastic member, and the bouncing rod has a first end and a second end, wherein the first end of the bouncing rod penetrates out of the aircraft body and is configured to receive an external force, and drives a relative movement between the bouncing rod and the aircraft body;
• at least one end of the elastic member is connected to the bouncing rod, and the elastic member is configured such that when the bouncing rod is subjected to an external force and moves, the elastic member undergoes elastic deformation and stores elastic potential energy;
• wherein the aircraft body comprises a housing, a spindle, an electric motor, a first rotor component and a second rotor component, wherein the first rotor component and the second rotor component are respectively installed on the spindle, the center of the first rotor component has an accommodating cavity, the electric motor is installed in the accommodating cavity, and the electric motor is fixedly installed with a cavity wall of the accommodating cavity;
• wherein a power supply and a control board are arranged in the accommodating cavity, and the power supply and the control board are respectively electrically connected to the electric motor;
• and wherein the second rotor component is located below the first rotor component, the spindle is arranged through the second rotor component, and an upper end of the spindle is rotatably installed with the housing;
• and
• wherein the hopping assembly further comprises a limiting member assembled on the aircraft body, wherein a lower end of the spindle is embedded in the limiting member, and the limiting member is movably connected to the bouncing rod.