Launching control device
By using a servo motor to drive gears and gear components, the cantilever can be automatically controlled to extend and retract, solving the problem of unrealistic rocket launches caused by manual operation in existing technologies, and realizing automated and efficient demonstrations of rocket launches.
Patent Information
- Application Number
- CN202423148167.0
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-12-19
- Publication Date
- 2025-12-26
- Estimated Expiration
- 2034-12-19
AI Technical Summary
Existing rocket launch control devices rely on manual operation, resulting in unrealistic cantilever deployment and retraction, which affects the effectiveness of rocket launch demonstrations.
It uses a servo motor to drive a combination of gears and teeth to automatically control the cantilever's deployment and retraction, and uses a projectile to automatically eject the rocket. The display screen shows the countdown and launch command.
It has enabled automated control of rocket launches, improving the realism and effectiveness of launch demonstrations.
Smart Images

Figure CN223726956U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model relates to the field of space technology, especially launch control device. BACKGROUND
[0002] With the continuous progress of science and technology, the construction and construction technology of rockets in the field of space technology in China are also developing and progressing, so that more students have a strong interest in the launch of rockets, at present, the rocket launch control device mostly is that the cantilever of tower frame is expanded manually first, then the ejection of rocket is controlled, the expansion and folding of the cantilever of tower frame is completely relied on manual operation, which is far from the real rocket launch, so that the rocket launch demonstration effect is poor. SUMMARY
[0003] Therefore, the utility model aims at overcoming the defects in prior art, and provides a launch control device.
[0004] The utility model provides a launch control device, including base 1 and bottom box 2, the bottom of base 1 is provided with control module 6, the servo motor 7 of electric connection with control module 6, the output shaft of servo motor 7 is keyed with drive gear 8, the bottom of base 1 is transversely slidably equipped with the gear 9 of drive gear 8 drive, the upper end of base 1 is vertically provided with tower frame 3, the cantilever 4 of drive expansion, folding of gear 9 drive is rotatably arranged on tower frame 3, the elastic column 5 of gear 9 drive is ejected and is elastically arranged on base 1.
[0005] Further, the gear 9 is composed of the upper double-sided rack and the lower single-sided rack, the single-sided rack is engaged with the drive gear 8, and the bottom of the double-sided rack is provided with a push block.
[0006] Further, the cantilever 4 is keyed with a long shaft rotating on the tower frame 3 and the base 1, and the lower end of the long shaft is keyed with a driven gear 10 engaged with the double-sided rack.
[0007] Further, the lower end of the elastic column 5 is provided with an annular protrusion, the elastic column 5 is connected with the bottom box 2 through an elastic member, and a limiting rod 11 is twisted on the base 1 for limiting the annular protrusion and being pushed by the push block.
[0008] Further, the upper end of the limiting rod 11 is provided with an inclined surface 11.1.
[0009] Further, the outer wall of the base 1 is provided with a display screen 12 electrically connected with the control module 6.
[0010] The advantages of this invention are: it can automatically extend and retract the cantilever, and after the cantilever extends, it drives the projectile to launch the rocket, improving the rocket demonstration effect; the drive gear controlled by the servo motor drives the gear component to move to the right, and the racks on both sides of the gear component drive the driven gears on both sides to rotate. The driven gears drive the cantilever to extend through the long shaft. After the projectile is launched and pressed back by the rocket, the drive gear drives the cantilever to retract and reset through the racks; when the push block of the gear component moves to the right, the push block pushes the limit rod and makes it rotate, and the limit rod releases the ring of the projectile. The rocket is launched by a protrusion and a spring-loaded protrusion. The bottom of the base has a stepped hole, which stops the ejected protrusion. After the protrusion is pushed back by the rocket, the push block of the gear moves to the left and resets. The limiting rod that is disengaged from the push block resets to limit the protrusion, keeping it in a state of elasticity ready for launch. After the protrusion is launched, the pushed-back protrusion can be pushed open by the inclined surface. Then, the limiting rod resets under the action of the torsion spring and limits the annular protrusion. The display screen controlled by the control module can display the countdown and launch command. Attached Figure Description
[0011] Figure 1 This is a perspective view of the present utility model;
[0012] Figure 2 This is the front view of the present invention;
[0013] Figure 3 This is a partial structural schematic diagram of the present invention;
[0014] Figure 4 This is the right view of the present invention;
[0015] Figure 5 for Figure 3 Enlarged view of part A. Detailed Implementation
[0016] The present invention will now be described in detail with reference to the accompanying drawings.
[0017] 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 only used to explain this utility model and are not intended to limit this utility model.
[0018] See Figures 1 to 5The utility model provides a kind of launch control device, it includes base 1 and bottom box 2, the bottom of base 1 is provided with control module 6, servo motor 7 electrically connected with control module 6, servo motor is controlled by the system of control module, the output shaft of servo motor 7 is keyed with driving gear 8, the bottom of base 1 is transversely slidably equipped with the gear piece 9 driven by driving gear 8, gear piece 9 is composed of the single side rack of the double side rack of upside, single side rack is engaged with driving gear 8, the bottom of double side rack is provided with push block, the upper end of base 1 is vertically provided with tower 3, tower 3 is rotatably provided with cantilever 4 unfolded by gear piece 9, drive and contract, elastic column 5 is elastically provided on base 1 by gear piece 9.
[0019] Cantilever 4 is keyed with long shaft rotating in tower 3, base 1, the lower end of long shaft is keyed with driven gear 10 engaged with double side rack. Driving gear drives gear piece right, the double side rack of gear piece drives two sides driven gear to rotate, driven gear drives cantilever to unfold by long shaft, after elastic column is ejected and is pressed back by rocket, driving gear drives cantilever to contract reset by rack.
[0020] Refer to Figure 3 、 Figure 5 The lower end of elastic column 5 is provided with annular protrusion, and elastic member is connected between elastic column 5 and bottom box 2. Limiting rod 11 is twisted on base 1 for limiting annular protrusion and being pushed by push block. When push block of gear piece moves right, push block pushes limiting rod and makes it rotate, limiting rod releases annular protrusion of elastic column, elastic column is ejected by rocket under the action of elastic member, the bottom of base is provided with stepped hole, the ejected elastic column is blocked by stepped hole, after elastic column is pressed back by rocket, push block of gear piece moves left to reset, limiting rod of push block resets to limit elastic column, so that elastic column maintains elastic force state for launching.
[0021] The upper end of limiting rod 11 is provided with inclined plane 11.1. After elastic column is ejected, the elastic column that is pressed back can be supported by inclined plane to open limiting rod, then limiting rod resets and limits annular protrusion under the action of torsional spring, so that elastic column maintains elastic force state for launching.
[0022] The outer wall of base 1 is provided with display screen 12 electrically connected with control module 6. Display screen controlled by control module can display countdown and launch instruction.
[0023] The above merely is the preferred implementation manner of the present application, and it should be noted that, for the ordinary skilled in the art, without departing from the technical principles of the present application, a number of improvements and refinements can be made, and these improvements and refinements should also be considered as the protection scope of the present application.
Claims
1. A transmission control device, characterized by: The utility model provides a bottom box and a base, the bottom of base is provided with control module, servo motor is electrically connected with control module, the output shaft of servo motor is keyed with drive gear, the bottom of base is transversely slidably fitted with gear piece driven by drive gear, the upper end of base is vertically provided with tower, the cantilever driven to spread, contract by gear piece is rotatably arranged on tower, the elastic column driven to pop out by gear piece is elastically arranged on base.
2. A transmission control device as claimed in claim 1, characterized in that: The gear piece is composed of the upper double-sided rack and the lower single-sided rack, the single-sided rack is engaged with the drive gear, and the bottom of the double-sided rack is provided with a push block.
3. A transmission control device as claimed in claim 2, characterised in that: The long shaft of the cantilever is keyed to the tower and the base, the lower end of the long shaft is keyed with a driven gear engaged with the double-sided rack.
4. A transmission control apparatus as claimed in claim 2, characterized in that: The lower end of the elastic column is provided with an annular protrusion, an elastic member is connected between the elastic column and the bottom box, and a limiting rod for limiting the annular protrusion and pushed by the push block is twisted on the base.
5. A transmission control apparatus as claimed in claim 4, characterised in that: The upper end of the limiting rod is provided with an inclined surface.
6. A transmit control apparatus as claimed in claim 1, characterized in that: The outer wall of the base is provided with a display screen electrically connected with the control module.