Lift-off rocket firework capable of improving flight stability
By employing a triangular arc-shaped smoke tube and fuse design in the rocket fireworks, combined with a spiral-wound main fuse, the problem of unstable flight trajectory in traditional fireworks has been solved, achieving a stable straight-line ascent, enhancing the viewing experience and reducing safety risks.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-03-28
- Publication Date
- 2026-03-13
AI Technical Summary
Traditional rocket fireworks are difficult to predict in terms of flight trajectory due to the instability of wind direction, wind speed and gunpowder formula during launch, which affects the viewing experience and may cause safety hazards.
It adopts a triangular arc-shaped smoke tube design, with three secondary lead wires and a ring-shaped connecting lead wire. Combined with the spiral-wound main lead wire and support rod, stable flight is achieved through the coordinated ignition of multiple lead wires, and the semi-circular top shell is used to reduce wind resistance.
This achieved a stable, linear ascent of the rocket fireworks, enhancing the viewing experience and reducing safety risks.
Smart Images

Figure CN223992563U_ABST
Abstract
Description
Technical Field
[0001] This utility model relates to the field of fireworks technology, and in particular to a rocket firework that improves flight stability. Background Technology
[0002] Traditional rocket fireworks are often affected by various factors during launch, such as wind direction, wind speed, and the instability of gunpowder formula, making the rocket's flight trajectory unpredictable and causing the fireworks' trajectory to deviate. This not only affects the audience's viewing experience but may also pose a safety hazard to the surrounding environment. Therefore, a rocket fireworks design to improve flight stability is proposed. Utility Model Content
[0003] To address at least one of the aforementioned technical shortcomings, this utility model provides an aerial rocket firework that improves flight stability, comprising a smoke tube, three secondary fuses that ignite simultaneously below the smoke tube, and a ring-shaped connecting fuse at the bottom of each secondary fuse.
[0004] Furthermore, a spirally wound main lead is arranged in a circular array below the connecting lead, and a circular support rod is connected to the middle of the main lead.
[0005] Furthermore, a matching platform is provided at the bottom of the support rod, and a hollow support rod is provided at the top of the platform. The support rod is inserted into the hollow support rod.
[0006] Furthermore, the chimney is triangular in shape, with a gunpowder cartridge located at one corner of the triangle, and each cartridge containing the same type of gunpowder.
[0007] Beneficial effects: Inserting the support rod at the center of the bottom of the smoke tube into the hollow support rod of the platform ignites multiple spirally wound main fuses, causing three secondary fuses to be ignited simultaneously by the connecting fuses. This drives the triangular arc-shaped smoke tube to maintain a continuous upward direction within the support rod. At the same time, the semi-circular top shell reduces wind resistance until it ascends into the air. The high amount of gunpowder enables the rocket fireworks to maintain a stable, straight upward trajectory.
[0008] The purpose, features, and advantages of this utility model will be further explained in conjunction with the embodiments and with reference to the accompanying drawings. Attached Figure Description
[0009] Figure 1 This is a schematic diagram of the overall structure of this utility model.
[0010] Figure 2 This is a schematic diagram of the secondary lead structure of this utility model.
[0011] exist Figures 1 to 2The correspondence between the component names or lines and the attached drawing numbers is as follows: chimney 1, top shell 101, secondary lead wire 102, connecting lead wire 103, main lead wire 104, support rod 2, platform 3, and support rod 301. Detailed Implementation
[0012] Please refer to Figures 1 to 2 ;
[0013] This embodiment provides a rocket firework for improving flight stability, including a smoke tube 1, three secondary fuses 102 that ignite simultaneously are arranged below the smoke tube 1, and a ring-shaped connecting fuse 103 is connected to the bottom of the secondary fuses 102; Reference Figure 1 and Figure 2 Below the connecting lead 103, there is also a spirally wound main lead 104 arranged in a circular array. A circular support rod 2 is connected to the middle of the main lead 104. A matching platform 3 is also provided at the bottom of the support rod 2. A hollow carrier rod 301 is provided at the top of the platform 3. The support rod 2 and the hollow carrier rod 301 are inserted into each other. The chimney 1 is triangular arc-shaped. A gunpowder cartridge is provided at one corner of the triangle of the chimney 1. Each gunpowder cartridge is filled with the same gunpowder.
[0014] In a specific embodiment, the support rod 2 at the center of the bottom of the chimney 1 is inserted into the hollow carrier rod 301 of the platform 3. The multiple spirally wound main fuses 104 are ignited, and the three secondary fuses 102 are simultaneously ignited by the connecting fuses 103. This causes the gunpowder cartridges in each corner of the triangular arc-shaped chimney 1 to be ignited by the secondary fuses 102 and to maintain a continuous upward direction within the carrier rod 301. At the same time, the semi-circular top shell 101 reduces wind resistance until the rocket takes off. With a large amount of gunpowder, the rocket fireworks can maintain a stable, straight upward trajectory.
Claims
1. A sky rocket firework for improving flight stability, comprising a smoke cylinder (1), characterized in that: The chimney (1) is provided with three secondary ignition lines (102) below, which are simultaneously ignited.
2. The aerial rocket firework for improving flight stability according to claim 1, wherein: The lower part of the connecting ignition line (103) is further provided with a circular array of spiral winding main ignition lines (104), and the middle part of the main ignition line (104) is connected with a circular support rod (2).
3. The aerial rocket firework for improving flight stability according to claim 2, wherein: The bottom of the support rod (2) is further provided with a matched carrier (3), and the top of the carrier (3) is provided with a hollow carrier rod (301), and the support rod (2) and the hollow carrier rod (301) are insertedly arranged.
4. The aerial rocket firework for improving flight stability according to claim 1, wherein: The chimney (1) is triangular arc-shaped, and one of the three angles of the chimney (1) is provided with a firecracker, and the same firecracker is arranged in each firecracker.