CN105571411A - Remote injection device - Google Patents
Remote injection device Download PDFInfo
- Publication number
- CN105571411A CN105571411A CN201610090894.7A CN201610090894A CN105571411A CN 105571411 A CN105571411 A CN 105571411A CN 201610090894 A CN201610090894 A CN 201610090894A CN 105571411 A CN105571411 A CN 105571411A
- Authority
- CN
- China
- Prior art keywords
- long
- injection device
- range
- injection
- coasting body
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B6/00—Projectiles or missiles specially adapted for projection without use of explosive or combustible propellant charge, e.g. for blow guns, bows or crossbows, hand-held spring or air guns
- F42B6/02—Arrows; Crossbow bolts; Harpoons for hand-held spring or air guns
- F42B6/08—Arrow heads; Harpoon heads
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
- F42B12/362—Arrows or darts
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Infusion, Injection, And Reservoir Apparatuses (AREA)
- Medicines Containing Antibodies Or Antigens For Use As Internal Diagnostic Agents (AREA)
Abstract
The invention discloses a remote injection device which comprises an arrow body, a coasting body and an injection mechanism. The arrow body is of a hollow structure. The coasting body is located in the hollow structure and can slide in the hollow structure. The injection mechanism is located at the front end of the arrow body, and a substance to be injected is contained in the injection mechanism. When the remote injection device collides with a target object, the coasting body slides forwards to collide with the injection mechanism to complete injection.
Description
Technical field
The present invention relates to injection device field, particularly a kind of long-range 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 depend primarily on the pressure (size that oral cavity puffs away suddenly) and blowpipe that produce instantaneously and arrow vow between gap, the less air-tightness in gap is better, and the gun pressure of generation is higher.Completely footpath is too little because of arrow to blow arrow, and stability is too poor, and by wind direction after injection, weather effect, precision extreme difference, so can not as destructive weapon.And compare and have its coverage of the weapon of rifling short too, this thing meaning does not under battle conditions have substantially.
For dangerous animal or personnel at risk, near subduing, can not can not injure its life again, to these animal or human persons, the medicine such as injecting narcotic is particularly important safely.Therefore, can safely, the device of long-range injection is effectively particularly important.
Summary of the invention
The object of this invention is to provide a kind of long-range injection device, safely, effectively can realize long-range injection.
Therefore, in first aspect, the invention provides a kind of long-range injection device, comprise 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 slides 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 such as, built with thing to be injected, anesthetic.
In one embodiment, the second buffer gear is equipped with at described injection mechanism rear portion.
In one embodiment, described coasting body is spherical, taper, cylindrical or dumbbell shape.
In one embodiment, 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.
In one embodiment, described rocket body hollow tube 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 comprise long-range injection device of the present invention.
Accompanying drawing explanation
Fig. 1 shows the long-range injection device according to one embodiment of the invention
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 invention can safely, long-range injection effectively, after long-range injection device is launched, arrow is hit target and is hampered power speed when die-offing or become inactive state from high-speed motion state, due to inertial force, namely coasting body departs from rocket body, continue the injection mechanism that " preshoot " clashes into rocket body front portion, the thing to be launched in described injection mechanism is launched by described injection mechanism.
In the present invention, coasting body refer to utilize contact target and complete injection there is inertia-responsive mechanical component.Described coasting body can be spherical, taper, cylindrical, dumbbell shape or other rules or irregularly shaped.Preferably, described coasting body is selected weight reduction and is increased the shape of kinetic energy and movement velocity.
In the present invention, coasting body preferred material density is greater 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 the container mechanism distance in rocket body also can set.
The effect of the first buffer gear is the shock strength slowed down between needle tubing mechanism and object.The effect of the second buffer gear is the strength that the described coasting body of buffering clashes into described injection mechanism, injection process is more balanced evenly.
Below in conjunction with drawings and Examples, the present invention will be further described:
In an embodiment of the present invention, emitting substance is for anesthetic fluid.
Fig. 1 shows the long-range injection device according to one embodiment of the invention, and coasting body 03 can relative movement in the hollow structure of rocket body 01, and coasting body 03 is installed on arrow tail by Weak link device 07.During percussion, kinetic energy passes 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 with the relatively independent coasting body 03 of rocket body 01 structure because effect of inertia continues to move forward with certain speed, 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, the present invention also has other embodiments, and visible relevant equivalent replacement technology scheme all should drop on the protection domain of application claims.
Claims (9)
1. a long-range injection device, it is characterized in that, described long-range injection device comprises rocket body, coasting body and injection mechanism, described rocket body is hollow structure, described coasting body is arranged in described hollow structure and can slides 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, is characterized in that, described injection mechanism front portion is provided with the first buffer gear.
3. long-range injection device according to claim 1, is characterized in that, described injection mechanism is built with thing to be injected.
4. long-range injection device according to claim 3, is characterized in that, described thing to be injected is anesthetic.
5. long-range injection device according to claim 1, is characterized in that, the second buffer gear is equipped with at described injection mechanism rear portion.
6. long-range injection device according to claim 1, is characterized in that, described coasting body is spherical, taper, cylindrical or dumbbell shape.
7. according to the long-range injection device of 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, is characterized in that, described rocket body hollow tube 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, is characterized in that, described bow and arrow or crossbow bolt comprise the long-range injection device according to any one of claim 1-8.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610090894.7A CN105571411A (en) | 2016-02-05 | 2016-02-05 | Remote injection device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610090894.7A CN105571411A (en) | 2016-02-05 | 2016-02-05 | Remote injection device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105571411A true CN105571411A (en) | 2016-05-11 |
Family
ID=55881820
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610090894.7A Pending CN105571411A (en) | 2016-02-05 | 2016-02-05 | Remote injection device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105571411A (en) |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2477007A1 (en) * | 1980-02-29 | 1981-09-04 | Maret Jean Paul | Weapon for anaesthetising animal at close range - is shaped like hammer with head comprising hypodermic syringe |
| US5202533A (en) * | 1992-01-28 | 1993-04-13 | Vandersteen Douglas G A | Drug injection apparatus for an animal |
| CN202437392U (en) * | 2011-12-28 | 2012-09-19 | 东北林业大学 | Simple blowpipe injector |
| CN203089448U (en) * | 2013-03-13 | 2013-07-31 | 佟艳明 | Blowpipe injector for injection |
| CN203609540U (en) * | 2013-11-04 | 2014-05-28 | 广州动物园 | Automatic remote drug injection device for wild animals |
| CN204033536U (en) * | 2014-07-17 | 2014-12-24 | 李先强 | Launch special syringe |
| CN205403617U (en) * | 2016-02-05 | 2016-07-27 | 田悦丰 | Long -range injection device |
-
2016
- 2016-02-05 CN CN201610090894.7A patent/CN105571411A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2477007A1 (en) * | 1980-02-29 | 1981-09-04 | Maret Jean Paul | Weapon for anaesthetising animal at close range - is shaped like hammer with head comprising hypodermic syringe |
| US5202533A (en) * | 1992-01-28 | 1993-04-13 | Vandersteen Douglas G A | Drug injection apparatus for an animal |
| CN202437392U (en) * | 2011-12-28 | 2012-09-19 | 东北林业大学 | Simple blowpipe injector |
| CN203089448U (en) * | 2013-03-13 | 2013-07-31 | 佟艳明 | Blowpipe injector for injection |
| CN203609540U (en) * | 2013-11-04 | 2014-05-28 | 广州动物园 | Automatic remote drug injection device for wild animals |
| CN204033536U (en) * | 2014-07-17 | 2014-12-24 | 李先强 | Launch special syringe |
| CN205403617U (en) * | 2016-02-05 | 2016-07-27 | 田悦丰 | Long -range injection device |
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| C06 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination |