Rocket with landing cabin

Abstract

The present disclosure discloses a rocket with a landing cabin, which belongs to the technical field of toy rockets, comprising a rocket body, a cabin shell which comprising two concave shell bodies, the edges of the two shell bodies cling to each other to enclose an accommodating cavity; the upper ends of the two shell bodies are hinged respectively with the lower end of the rocket body, and the two shell bodies are relatively rotatable to open or close the accommodating cavity; a parachute cloth, received within the accommodating cavity in a compressed mode and provided with a connector for connection with the shell bodies or the rocket body. The present disclosure is convenient for taking in a parachute.

I claim: 
     
         1 . A rocket with a landing cabin, wherein it comprises:
 a rocket body;   a cabin shell, comprising two concave shell bodies, and the edges of the two shell bodies cling to each other to enclose an accommodating cavity; the upper ends of the two shell bodies are hinged respectively with the lower end of the rocket body, and the two shell bodies are relatively rotatable to open or close the accommodating cavity;   a parachute cloth, received within the accommodating cavity in a compressed mode and provided with a connector for connection with the shell bodies or the rocket body.   
     
     
         2 . The rocket with a landing cabin of  claim 1 , wherein the shell body extends downward to form a pressing portion, and the pressing portions of the two shell bodies are opposite to each other. 
     
     
         3 . The rocket with a landing cabin of  claim 2 , wherein the edges of the two opposite pressing portions are in concave-convex match. 
     
     
         4 . The rocket with a landing cabin of  claim 1 , wherein the connector is a connecting strip, and the connecting strip is connected with the inner side of one of the pressing portions. 
     
     
         5 . The rocket with a landing cabin of  claim 1 , wherein the rocket body comprises a rocket main body and a rocket head sheathing the upper end of the rocket main body, the shell bodies are hinged at the lower end of the rocket main body, and the end of the rocket head is presented in the form of a spherical surface. 
     
     
         6 . The rocket with a landing cabin of  claim 5 , wherein the rocket head is made of a soft material. 
     
     
         7 . The rocket with a landing cabin of  claim 5 , wherein the rocket main body extends downward to form two spaced hinging portions, the shell body upward extends to form a connecting portion, and the connecting portions are upward embedded between the two hinging portions and hinged with the rocket main body. 
     
     
         8 . The rocket with a landing cabin of  claim 5 , wherein the rocket main body outward extends to form a clamping hook and a plurality of rocket wings that are arranged circumferentially. 
     
     
         9 . The rocket with a landing cabin of  claim 5 , wherein the rocket main body is internally provided with a light-emitting component. 
     
     
         10 . The rocket with a landing cabin of  claim 5 , wherein the light-emitting component comprises a mounting base embedded into the lower end of the rocket head; the mounting base extends downward to form a positioning ring, a supporting column and a positioning column; the rocket main body is embedded between the rocket head and the positioning ring; a control board is embedded in the inner side of the positioning ring; the positioning column penetrates through the control board; the support column props downward against the control board and is fixedly connected with the control board; a battery and a vibration sensor are arranged at the upper side of the control board; the control board is provided with a light source; and the battery, the vibration sensor and the light source are electrically connected with the control board respectively. 
     
     
         11 . The rocket with a landing cabin of  claim 1 , wherein the size of one end of the shell body, the end of which close to the rocket body, is smaller than the middle of the shell body or the end, away from the rocket body, of the shell body. 
     
     
         12 . The rocket with a landing cabin of  claim 1 , wherein the shell body is a half shell body. 
     
     
         13 . The rocket with a landing cabin of  claim 11 , wherein the cross section of the two shell bodies after the shell bodies cling to each other is of a rhombus shape. 
     
     
         14 . The rocket with a landing cabin of  claim 11 , wherein the structure after the two shell bodies cling to each other presents an oval shape.