CN215413408U - Flying target based on underwater launching - Google Patents
Flying target based on underwater launching Download PDFInfo
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- CN215413408U CN215413408U CN202121572487.2U CN202121572487U CN215413408U CN 215413408 U CN215413408 U CN 215413408U CN 202121572487 U CN202121572487 U CN 202121572487U CN 215413408 U CN215413408 U CN 215413408U
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- firing
- pole
- block
- balancing weight
- flying target
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Abstract
The utility model is suitable for the technical field of shooting training, and provides a flying target based on underwater launching, which comprises: the material casing, launch subassembly and firing subassembly, launch subassembly fixed connection in the plastic casing, the firing subassembly is located launch subassembly below, the subassembly that launches includes: the ejection plate is fixedly connected with the plastic shell through the spring, and the flying target is placed on the ejection plate; the firing assembly comprises: block pole, rigidity rope, firing bar and balancing weight, it is articulated to block the pole plastics casing, the firing bar is articulated plastics casing, but the firing bar joint block the pole, the balancing weight fag end the firing bar, the balancing weight is located plastics casing's below. Therefore, the utility model can be used in water, automatically launches, has simple structure, high repeated utilization rate and low use cost.
Description
Technical Field
The utility model relates to the technical field of shooting training, in particular to a flying target based on underwater launching.
Background
The target shooting is widely popular as a competitive entertainment item. The existing machine for throwing flying saucer mainly has two types of automatic and semi-automatic, and most of them are imported or imitated, and can only be used for special shooting training and competition. These machines are complex, expensive and inconvenient to use and operate. Meanwhile, the device can only be applied to land and is often limited when being launched on the water surface.
In view of the above, the prior art is obviously inconvenient and disadvantageous in practical use, and needs to be improved.
SUMMERY OF THE UTILITY MODEL
Aiming at the defects, the utility model aims to provide a flying target based on underwater launching, which can be used in water, can be launched automatically, and has the advantages of simple structure, high recycling rate and low use cost.
In order to achieve the above object, the present invention provides a flying target based on underwater launching, comprising: the ejection assembly is fixedly connected in the plastic shell, the firing assembly is located below the ejection assembly, and the ejection assembly comprises: the ejection plate is fixedly connected with the plastic shell through the spring, and the flying target is placed on the ejection plate;
the firing assembly comprises: block pole, rigidity rope, firing bar and balancing weight, it is articulated to block the pole plastic casing, the one end fixed connection of rigidity rope the ejection plate, the other end of rigidity rope can cup joint block the pole, the firing bar is articulated plastic casing, but the joint of firing bar blocks the pole, the balancing weight fag end the firing bar, the balancing weight is located plastic casing's below.
According to the flying target based on underwater launching, the firing rod is elastically connected with the plastic shell.
According to the flying target based on underwater launching, the outer side of the balancing weight is provided with the bearing film, and the balancing weight is tightly attached to the plastic shell through the bearing film.
According to the flying target based on underwater launching, the bearing film is connected with the plastic shell in a clamping mode.
According to the flying target based on underwater launching, the load-bearing film is made of a material easy to hydrolyze.
According to the flying target based on underwater launching, the easily hydrolyzed material is starch.
The utility model can be launched in water, increases the application range of the flying target, controls the launching time of the flying target by utilizing the sinking time of the balancing weight, automatically launches the flying target by utilizing the balancing weight and adds the hydrolysable bearing film, so that the flying target based on underwater launching is more convenient to store and transport, the sight line automatically delays to launch, and meanwhile, the flying target based on underwater launching can be repeatedly used and has low cost.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic view of the working state structure of the present invention;
in the figure, 1-plastic shell, 2-ejection component, 21-ejection plate, 22-spring, 3-firing component, 31-blocking rod, 32-rigid rope, 33-firing rod, 34-balancing weight, 35-bearing film and 4-flying target.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention is described in further 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 utility model and are not intended to limit the utility model.
Referring to fig. 1, the present invention provides a flying target based on underwater launch. The flight target based on underwater launching comprises: plastic casing 1, launch subassembly 2 and firing subassembly 3, launch the equal fixed connection of subassembly 2 and firing subassembly 3 in plastic casing 1, firing subassembly 3 is located the below of launching subassembly 2, launches subassembly 2 and includes: the ejection plate 21 is fixedly connected with the plastic shell 1 through the spring 22, the flying target 4 is placed on the ejection plate 21, and the ejection plate 21 ejects the flying target 4 through the elastic force provided by the spring 22. The firing assembly 3 includes: block pole 31, rigidity rope 32, firing bar 33 and balancing weight 34, block the articulated plastic casing 1 of pole 31, the one end fixed connection ejection plate 21 of rigidity rope 32, the other end of rigidity rope 32 can cup joint on blocking pole 31, rigidity rope 32 fixed connection blocks during pole 31 and ejection plate 21, spring 22 is in compression state, the articulated plastic casing 1 of firing bar 33, pole 31 is blocked to the joint of firing bar 33, it is spacing to blocking pole 31, balancing weight 34 rope connects firing bar 33, balancing weight 34 is located the outside below of plastic casing 1. Referring to fig. 2, when the plastic housing 1 is placed on the water surface, the weight block 34 begins to sink, when the weight block 34 sinks to a certain distance, the firing rod 33 is pulled, the firing rod 33 releases the blocking rod 31, the rigid rope 32 sleeved on the blocking rod 31 slides out, the ejection plate 21 ejects the flying target 4 under the action of the spring 22, and the ejection is completed.
Further, trigger bar 33 elastic connection plastic housing 1 guarantees that trigger bar 33 normality joint down is on blockking rod 31 for the performance is more stable, places plastic housing 1 in the rope body on the balancing weight 34, through the length of the restriction rope body, controls the emission time.
Referring to fig. 2, further, balancing weight 34 outside is equipped with bearing membrane 35, and bearing membrane 35 pastes tight plastic casing 1 with balancing weight 34, and bearing membrane 35 joint is on plastic casing 1, can tear bearing membrane 35 down when using, convenient transportation.
Furthermore, the bearing film 35 is made of a material easy to hydrolyze, starch is preferred, the bearing film 35 starts to dissolve after contacting water, when the weight of the balancing weight 34 cannot be borne, the balancing weight 34 sinks, then the triggering rod 33 rotates to release the blocking rod 31, and the ejection plate 21 ejects the flying target 4. The load-bearing membrane 35 facilitates storage and transport of the underwater launch-based flight target and utilizes the hydrolysis time of the hydrolyzed material to extend the excitation time and provide safe evacuation time for the personnel.
When the underwater launching-based flying target is used, the plastic shell 1 is placed on the water surface, the bearing film 35 starts to dissolve, when the bearing film 35 cannot bear the weight of the balancing weight 34, the balancing weight 34 sinks, when the bearing film sinks to a certain distance, the firing rod 33 rotates to release the blocking rod 31, the rigid rope 32 on the blocking rod 31 slides out of the blocking rod 31 under the action of the spring 22, the ejection plate 21 breaks away from the limit of the blocking rod 31 and is ejected outwards under the elastic force of the spring 22 to eject the flying target 4; after the underwater launching flying target is used, the underwater launching flying target is recovered, a new bearing film 35 is replaced, the ejection plate 21 is reset, the rigid rope 32 is sleeved on the blocking rod 31, and the triggering rod 33 is used for clamping the blocking rod 31 for the next use.
In conclusion, the underwater launching flying target can be launched in water, the using range of the flying target is enlarged, the launching time of the flying target is controlled by utilizing the sinking time of the balancing weight, the flying target is automatically launched by utilizing the balancing weight, and the hydrolysable bearing film is added, so that the underwater launching flying target is more convenient to store and transport, the sight line is automatically delayed to launch, and meanwhile, the underwater launching flying target can be reused and is low in cost.
In the description of the present invention, it is to be understood that the terms "upper", "lower", and the like, indicate orientations or positional relationships based on those shown in the drawings, are merely for convenience in describing the present invention and simplifying the description, and do not indicate or imply that the referred device or element must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention.
The present invention may be embodied in other specific forms without departing from the spirit or essential attributes thereof, and it should be understood that various changes and modifications can be effected therein by one skilled in the art without departing from the spirit and scope of the utility model as defined in the appended claims.
Claims (6)
1. A flying target based on underwater launch, comprising: the ejection device comprises a plastic shell, an ejection assembly and a firing assembly, wherein the ejection assembly is fixedly connected in the plastic shell, and the firing assembly is positioned below the ejection assembly; the ejection assembly includes: the ejection plate is fixedly connected with the plastic shell through the spring, and the flying target is placed on the ejection plate;
the firing assembly comprises: block pole, rigidity rope, firing bar and balancing weight, it is articulated to block the pole plastics housing, it is located to block the pole the below of spring, the one end fixed connection of rigidity rope the ejection plate, the other end of rigidity rope cup joints block the pole, the firing bar is articulated plastics housing, but the firing bar joint block the pole, the balancing weight rope connects the firing bar, the balancing weight is located plastics housing's below.
2. The underwater launch based flight target of claim 1, wherein the firing bar is resiliently coupled to the plastic housing.
3. The underwater launching-based flying target of claim 1, wherein a bearing film is arranged on the outer side of the counterweight block, and the bearing film enables the counterweight block to be tightly attached to the plastic shell.
4. The underwater launch based flight target of claim 3, wherein the load bearing membrane is snap-fit connected to the plastic housing.
5. The underwater launch based flight target of claim 4, wherein the load bearing membrane is made of a material that is easily hydrolyzed.
6. The underwater launch based flight target of claim 5, wherein the easily hydrolyzable material is starch.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202121572487.2U CN215413408U (en) | 2021-07-12 | 2021-07-12 | Flying target based on underwater launching |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202121572487.2U CN215413408U (en) | 2021-07-12 | 2021-07-12 | Flying target based on underwater launching |
Publications (1)
Publication Number | Publication Date |
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CN215413408U true CN215413408U (en) | 2022-01-04 |
Family
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN202121572487.2U Active CN215413408U (en) | 2021-07-12 | 2021-07-12 | Flying target based on underwater launching |
Country Status (1)
Country | Link |
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CN (1) | CN215413408U (en) |
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2021
- 2021-07-12 CN CN202121572487.2U patent/CN215413408U/en active Active
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Legal Events
Date | Code | Title | Description |
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GR01 | Patent grant | ||
GR01 | Patent grant | ||
PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: Flight target based on underwater launch Effective date of registration: 20230427 Granted publication date: 20220104 Pledgee: China Construction Bank Co.,Ltd. Weihai Zhangcun Sub branch Pledgor: Shandong Lanjian Intelligent Equipment Technology Co.,Ltd. Registration number: Y2023980039488 |
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PE01 | Entry into force of the registration of the contract for pledge of patent right |