CN205403617U - Long -range injection device - Google Patents
Long -range injection device Download PDFInfo
- Publication number
- CN205403617U CN205403617U CN201620123122.4U CN201620123122U CN205403617U CN 205403617 U CN205403617 U CN 205403617U CN 201620123122 U CN201620123122 U CN 201620123122U CN 205403617 U CN205403617 U CN 205403617U
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- long
- injection device
- range
- injection
- range injection
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- Expired - Fee Related
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- Infusion, Injection, And Reservoir Apparatuses (AREA)
Abstract
The utility model discloses a long -range injection device, long -range injection device includes rocket body, inertial body and injection mechanism, the rocket body is hollow structure, inertial body is located and can wherein slide among the hollow structure, the injection mechanism is located rocket body front end, injection mechanism install inside and remain to be injected the thing, work as when long -range injection device impactes the object, the inertial body striking that slides forward the injection is accomplished to the injection mechanism.
Description
Technical field
This utility model relates to injection device field, particularly a kind of remotely injection device.
Technical background
Blowing this kind of device of arrow is from rear portion moment to supercharging in blowpipe by oral cavity, pressure advances arrow to vow injection, so how far injection distance depends primarily on the size of gun pressure, and the size of gun pressure depends primarily on the gap between the pressure (size that oral cavity puffs away suddenly) of moment generation and blowpipe and arrow arrow, the more little air-tightness in gap is more good, and the gun pressure of generation is more high.Blowing arrow because arrow completely footpath is too little, stability is too poor, and by wind direction after injection, weather affects, and precision extreme difference, so cannot function as destructive weapon.And, to compare too short with its coverage of weapon having rifling, this thing meaning under battle conditions is substantially free of.
For dangerous animal or personnel at risk, it is impossible near subduing, its life can not be injured again, the medicines such as these animal or human persons injecting narcotic safely is particularly important.Therefore, it can the device of safely, effectively remotely injection particularly important.
Utility model content
The purpose of this utility model is to provide a kind of remotely injection device, it is possible to safely, effectively realize long-range injection.
Therefore, in first aspect, this utility model provides a kind of remotely injection device, including rocket body, coasting body and injection mechanism, described rocket body is hollow structure, and described coasting body is arranged in described hollow structure and can slide wherein, and described injection mechanism is positioned at described rocket body front end, when described long-range injection device strikes object, described coasting body forward slip clashes into described injection mechanism and completes injection.
In one embodiment, described injection mechanism front portion is provided with the first buffer gear.
In one embodiment, described injection mechanism is built with thing to be injected, for instance anesthetis.
In one embodiment, described injection mechanism rear portion is equipped with the second buffer gear.
In one embodiment, described coasting body is spherical, taper, cylinder or dumbbell shape.
In one embodiment, described coasting body Weak link is in described rocket body hollow structure rear end before transmission, when described secondary fire arrow device strike object time, described coasting body is along described rocket body hollow structure forward slip.
In one embodiment, described rocket body hollow pipe rear end is provided with elastic mechanism, and described coasting body Weak link is on described elastic mechanism before transmission.
In second aspect, described bow and arrow or crossbow bolt include long-range injection device of the present utility model.
Accompanying drawing explanation
Fig. 1 illustrates the long-range injection device according to an embodiment of the present utility model
Rocket body-01 syringe needle-02 coasting body-03 buffer unit-04 anesthetic fluid-05 syringe container-06 Weak link device-07
Detailed description of the invention
Long-range injection device of the present utility model can safely, effectively remotely be injected, after long-range injection device is launched, arrow hit target be hampered power speed die-off or from high-speed motion state become resting state time, due to inertial force, namely coasting body departs from rocket body, continuing " preshoot " and clash into the injection mechanism that rocket body is anterior, the thing to be launched in described injection mechanism is launched by described injection mechanism.
In this utility model, coasting body refers to that what utilize contact target and complete injection has inertia-responsive mechanical component.Described coasting body can be spherical, taper, cylinder, dumbbell shape or other are regular or irregularly shaped.Preferably, described coasting body is selected and is alleviated weight and increase the shape of kinetic energy and movement velocity.
In this utility model, coasting body preferred material density is more than the heavier mechanical component of rocket body, and for reaching different effects, the weight-adjustable joint of coasting body or setting, coasting body and container mechanism distance in rocket body also can set.
The effect of the first buffer gear is to slow down the shock strength between needle tubing mechanism and object.The effect of the second buffer gear is to cushion described coasting body to clash into the strength of described injection mechanism so that injection process more balances, evenly.
Below in conjunction with drawings and Examples, this utility model is described further:
In embodiment of the present utility model, emitting substance is for anesthetic fluid.
Fig. 1 illustrates the long-range injection device according to an embodiment of the present utility model, coasting body 03 in the hollow structure of rocket body 01 can relative movement, coasting body 03 is installed on arrow tail by Weak link device 07.During percussion, kinetic energy is passed to coasting body 03 by rocket body 01 and obtains kinetic energy simultaneously and move forward, when meeting obstructions, according to physics principle, the speed of rocket body 01 die-offs or stops suddenly, and the coasting body 03 relatively independent with rocket body 01 structure continues to move forward with certain speed due to effect of inertia, until secondary impact syringe container 06, anesthetic fluid 05 in syringe container 06 is outwards launched by syringe needle 02, syringe needle 02 is provided with buffer unit 04, to alleviate impulsive force when syringe needle 02 clashes into object.
Should be noted that, except above-described embodiment, this utility model also has other embodiments, it is seen that relevant equivalent replacement technology scheme all should drop on the protection domain that this utility model requires.
Claims (9)
1. a long-range injection device, it is characterized in that, described long-range injection device includes rocket body, coasting body and injection mechanism, described rocket body is hollow structure, described coasting body is arranged in described hollow structure and can slide wherein, described injection mechanism is positioned at described rocket body front end, and when described long-range injection device strikes object, described coasting body forward slip clashes into described injection mechanism and completes injection.
2. long-range injection device according to claim 1, it is characterised in that described injection mechanism front portion is provided with the first buffer gear.
3. long-range injection device according to claim 1, it is characterised in that described injection mechanism is built with thing to be injected.
4. long-range injection device according to claim 3, it is characterised in that described thing to be injected is anesthetis.
5. long-range injection device according to claim 1, it is characterised in that described injection mechanism rear portion is equipped with the second buffer gear.
6. long-range injection device according to claim 1, it is characterised in that described coasting body is spherical, taper, cylinder or dumbbell shape.
7. the long-range injection device according to any one of claim 1-6, it is characterized in that, described coasting body Weak link is in described rocket body hollow structure rear end before transmission, and when described long-range injection device strikes object, described coasting body is along described rocket body hollow structure forward slip.
8. long-range injection device according to claim 7, it is characterised in that described rocket body hollow pipe rear end is provided with elastic mechanism, and described coasting body Weak link is on described elastic mechanism before transmission.
9. a set of bow and arrow or crossbow bolt, it is characterised in that described bow and arrow or crossbow bolt include the long-range injection device according to any one of claim 1-8.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620123122.4U CN205403617U (en) | 2016-02-05 | 2016-02-05 | Long -range injection device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620123122.4U CN205403617U (en) | 2016-02-05 | 2016-02-05 | Long -range injection device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205403617U true CN205403617U (en) | 2016-07-27 |
Family
ID=56447445
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620123122.4U Expired - Fee Related CN205403617U (en) | 2016-02-05 | 2016-02-05 | Long -range injection device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205403617U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105571411A (en) * | 2016-02-05 | 2016-05-11 | 田悦丰 | Remote injection device |
| CN109990671A (en) * | 2019-05-17 | 2019-07-09 | 陈冬雪 | A kind of general penetration Extinguishing bomb shell |
-
2016
- 2016-02-05 CN CN201620123122.4U patent/CN205403617U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105571411A (en) * | 2016-02-05 | 2016-05-11 | 田悦丰 | Remote injection device |
| CN109990671A (en) * | 2019-05-17 | 2019-07-09 | 陈冬雪 | A kind of general penetration Extinguishing bomb shell |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160727 Termination date: 20190205 |