CN205049049U - Howitzer transmitter - Google Patents
Howitzer transmitter Download PDFInfo
- Publication number
- CN205049049U CN205049049U CN201520565839.XU CN201520565839U CN205049049U CN 205049049 U CN205049049 U CN 205049049U CN 201520565839 U CN201520565839 U CN 201520565839U CN 205049049 U CN205049049 U CN 205049049U
- Authority
- CN
- China
- Prior art keywords
- groove
- rotating shaft
- closing cap
- power component
- box 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.)
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A9/00—Feeding or loading of ammunition; Magazines; Guiding means for the extracting of cartridges
- F41A9/38—Loading arrangements, i.e. for bringing the ammunition into the firing position
- F41A9/46—Loading arrangements, i.e. for bringing the ammunition into the firing position the cartridge chamber being formed by two complementary elements, movable one relative to the other for loading
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A9/00—Feeding or loading of ammunition; Magazines; Guiding means for the extracting of cartridges
- F41A9/01—Feeding of unbelted ammunition
- F41A9/02—Feeding of unbelted ammunition using wheel conveyors, e.g. star-wheel-shaped conveyors
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A9/00—Feeding or loading of ammunition; Magazines; Guiding means for the extracting of cartridges
- F41A9/50—External power or control systems
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
Abstract
The utility model discloses a howitzer transmitter, the utility model aims at providing a non - afterbody pushes away the howitzer transmitter that thorax and the multiple bullet kind of projectile are gone into to the bullet, it includes quick -witted casket, sheave box body, tail box body, combination formula cartridge chamber subassembly, plays groove closing cap power component, the rotatory groove power component of bullet, transmission power component, launching tube, combination formula cartridge chamber subassembly play the groove and play the groove closing cap including rotatory, the rotatory groove power component of bullet set up in quick -witted casket, the rotatory groove power component of bullet drives rotation axis no. 1 and is intermittent movement, bullet groove closing cap set up in quick -witted casket through playing groove closing cap power component, and be reciprocating motion in quick -witted casket, the launching tube setting on quick -witted casket, and be located rotatory the place ahead that plays the groove, transmission power component's trigger mechanism set up in the tail box body, the lamp post hole site examination tooling has the characteristics of being simple structure and reasonable in design, being convenient to use, etc.
Description
Technical field
The utility model relate to a kind of weapon, especially a kind of grenade launcher.
Background technology
Grenade launcher is mainly divided into single-shot grenade launcher, automatic grenade launcher and semi-automatic grenade launcher, single-shot grenade launcher has lower hanging and hand-held two kinds, the form of general employing single loading single shot, hangingly refers to the transmitter can hung with on other gun down.Hand-held on the basis of lower extension, adds the mechanism such as handle and gun stock, the transmitter that can be used alone.Automatic grenade launcher, refers to the grenade launcher that can carry out burst-firing, and the general powder gases energy that adopts completes auto-action, mainly contains gas operated and gunlock barrel extension and recoil type, and automatic grenade launcher is bullet drum or Ammunition Belt Links Feed mainly.Semi-automatic howitzer weapon delivery is between an above-mentioned class transmitter between the two, can only single shot, but comparatively single-shot grenade launcher firing rate is high, and firepower continuation is good, and weight can meet hand-held use again, adopts runner principle ammunition feed more.But above-mentioned multiple grenade launcher all adopts integral type cartridge chamber, be all adopt to push away from transmitter afterbody to spring into thorax, enter bullet mode single.
Utility model content
The purpose of this utility model is to overcome the deficiencies in the prior art, provides a kind of non-afterbody to push away and springs into thorax and the grenade launcher can launching multiple bullet kind.
In order to achieve the above object, a kind of grenade launcher designed by the utility model, it comprises casing, sheave box body, tail box body, combined type cartridge chamber assembly, plays groove closing cap Power Component, rotating missile groove Power Component, launch power assembly, transmitting tube, power source; Described sheave box body is connected with casing, and is positioned at the rear side of casing, and described tail box body box body is connected with sheave box body, and is positioned at the rear side of sheave box body; Described combined type cartridge chamber assembly comprises rotating missile groove and plays groove closing cap; Described rotating missile groove rotates around the longitudinal center line of rotating missile groove, the radial direction of rotating missile groove is provided with the main cartridge chamber of the consistent outward opening of multiple shape size uniformly, and opening shaft is to running through rotating missile groove, be provided with rotating shaft one in the center of rotating missile groove, the center line of rotating shaft one overlaps with the longitudinal center line of rotating missile groove; Described rotating missile groove Power Component is arranged in casing, and rotating missile groove Power Component driven rotary axle one does intermittent movement; Described bullet groove closing cap is arranged in casing by playing groove closing cap Power Component, and moves reciprocatingly in casing, and the lower surface playing groove closing cap is provided with the secondary cartridge chamber of an outward opening, secondary cartridge chamber coordinates formation one complete cartridge chamber with main cartridge chamber; Described transmitting tube is arranged on casing, and is positioned at the front of rotating missile groove, the center line of transmitting tube all the time with the center line of complete cartridge chamber on the same line; The trigger mechanism of described launch power assembly is arranged in tail box body, is pulled the trigger the ammunition in cartridge chamber by trigger mechanism; Described power source is connected with bullet groove closing cap Power Component, rotating missile groove Power Component, launch power assembly.
For the ease of playing the fastening of the primary and secondary cartridge chamber on groove closing cap and rotating missile groove, the lower surface of described bullet groove closing cap is provided with one cartridge chamber, bullet groove closing cap is provided with guide hole in secondary cartridge chamber surrounding, guide pillar is provided with in guide hole, on guide pillar, cover has back-moving spring, guide pillar is connected with casing, plays groove closing cap and moves up and down along guide pillar direction under the effect playing groove closing cap Power Component; Described bullet groove closing cap also can be divided into left bullet groove and the right side time to play groove, and left bullet groove is played groove with the right side time and be connected with casing by traversing assembly or rotary components; Described bullet groove closing cap also can move reciprocatingly along the guide-track groove on casing.
In order to make the transmission of rotating missile groove more stable, described rotating missile groove Power Component comprises rotating shaft two, rotating shaft two driven rotary axle one does intermittent movement, rotating shaft two is provided with pivoted arm wheel, one end of rotating shaft one is provided with sheave, pivoted arm wheel drives sheave to rotate, and sheave driven rotary axle one rotates, and is respectively equipped with driven pulley one and driven pulley two at the two ends of rotating shaft two; Described rotating missile groove Power Component also can comprise rotating shaft two, sprocket wheel one, chain, sprocket wheel two, rotating shaft two driven rotary axle one does intermittent movement, rotating shaft two is provided with sprocket wheel one, the left end of rotating shaft one is provided with sprocket wheel two, sprocket wheel one is by chain-driving sprocket wheel two, and sprocket wheel two driven rotary axle one rotates.
Pump on guide pillar direction for the ease of playing groove closing cap, described bullet groove closing cap Power Component comprises rotating shaft three, cam, driven pulley three, rotating shaft three is arranged in casing, and be positioned at the top playing groove closing cap, cam is fixed on rotating shaft three, driven pulley three is arranged on one end of rotating shaft three, and driven pulley three coordinates with driven pulley two.
For the ease of arranging bullet groove, described rotating missile groove is provided with the main cartridge chamber of four outward openings.
For the ease of the work of the transmitting of howitzer, described power source selects motor.
As usual use when there is no Power supply to make grenade launcher, described tail box body is provided with manual percussion lock, this manual percussion lock comprises pedestal, rocking handle, rocking handle bar, spring, pedestal is fixed on the outer surface of tail box body, spring is arranged in pedestal, rocking handle is L-shaped, rocking handle bar is connected with one end of rotating shaft two through the spring in pedestal, the other end of rocking handle bar is connected with one end of rocking handle, when without the need to using manual, rocking handle is drawn in, rocking handle bar is outwards moved be separated with rotating shaft two, the rocking handle release when needs are manual, rocking handle bar moves inward and is connected with rotating shaft two.
In order to better complete percussion function, the base of described percussion cam is circular, a plane of base is provided with a spiral step, the central axis of spiral step and the central axes of base, the lowest part of spiral step and the plane of base tangent.
For the ease of the percussion of ammunition, described launch power assembly comprises percussion cam, hammer, trigger shaft, firing pin, firing pin cover, torsion spring, percussion cam is arranged on rotating shaft two, hammer is arranged in tail box body by hammer pin, trigger shaft is provided with in the below of hammer, trigger shaft and percussion cam engagement, firing pin cover is fixed in sheave box body, and the axis of the axis of firing pin cover and transmitting tube on the same line, firing pin is arranged in firing pin cover, torsion spring is arranged on hammer pin, and one end of torsion spring is connected with hammer, and the other end is connected with tail box body.
Grenade launcher of the present utility model, rotating missile groove is arranged in casing by rotating missile groove Power Component, playing groove closing cap is arranged in casing by playing groove closing cap Power Component, rotating missile groove and bullet groove closing cap coordinate, after shooting, the main cartridge chamber shot rotates to transmitting site by rotating missile groove, bullet groove closing cap moves down and forms complete cartridge chamber with rotating missile slot fit, by launch power assembly, ammunition is pulled the trigger after having shot, after ammunition has been launched, bullet groove closing cap and rotating missile groove depart from, the main cartridge chamber that the next one has shot by rotating missile groove rotates to transmitting site, play groove closing cap again to move down and rotating missile slot fit, by this bullet feeding mode, make ammunition directly can add cartridge chamber, shorten the entire length of Weapons and Knives, reduce the weight of Weapons and Knives, be easy to carry installation, simultaneously because ammunition directly adds cartridge chamber, as long as make the ammunition meeting cartridge chamber size be suitable for, make the scope of application more extensive, therefore, it has the features such as structure is simple, reasonable in design and easy to use.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model;
Fig. 2 is internal structure explosive view of the present utility model;
Fig. 3 is the inner drive mechanism schematic diagram of magazine of the present utility model;
Fig. 4 is manual percussion lock connection diagram of the present utility model;
Fig. 5 is cam fire design schematic diagram of the present utility model;
Fig. 6 is rotating missile groove transmission schematic diagram.
Detailed description of the invention
Below in conjunction with accompanying drawing, the utility model will be further described.
As shown in Figure 1, Figure 2, shown in Fig. 3, Fig. 4, Fig. 5, Fig. 6, a kind of grenade launcher that the present embodiment describes, it comprises casing 1, sheave box body 27, tail box body 28, combined type cartridge chamber assembly, plays groove closing cap Power Component, rotating missile groove Power Component, launch power assembly, transmitting tube 7, manual percussion lock, motor 9, described sheave box body 27 is connected with casing 1, and is positioned at the rear side of casing 1, and described tail box body box body 28 is connected with sheave box body 27, and is positioned at the rear side of sheave box body 27, described combined type cartridge chamber assembly comprises rotating missile groove 2 and plays groove closing cap 3, and rotating missile groove 2 is arranged in casing 1, described rotating missile groove 2 is in cylindric, longitudinal center line around rotating missile groove 2 is provided with the main cartridge chamber of the consistent outward opening of four shape sizes diametrically uniformly, and main cartridge chamber axially runs through rotating missile groove, be provided with rotating shaft 1 in the center of rotating missile groove, the center line of rotating shaft 1 overlaps with the longitudinal center line of rotating missile groove 2, the radial direction of the lower surface of described bullet groove closing cap 3 is provided with the secondary cartridge chamber of outward opening, and secondary cartridge chamber axially runs through bullet groove closing cap 3, secondary cartridge chamber coordinates with main cartridge chamber and forms complete cartridge chamber, guide hole is provided with in the secondary cartridge chamber surrounding playing groove closing cap 3, casing 1 is provided with guide pillar 5, guide hole coordinates with guide pillar 5, and guide pillar spring 6 is provided with between guide hole and guide pillar 5, bullet groove closing cap 3 is moved reciprocatingly along guide pillar 5, transmitting tube 7 is arranged on casing 1, the center line of transmitting tube 7 all the time with the center line of a main cartridge chamber on the same line, sheave 8 is provided with in one end of rotating shaft 1, described rotating missile groove Power Component comprises rotating shaft 2 10, pivoted arm wheel 11, motor 9 is arranged on the outer surface of tail box body 28, rotating shaft 2 10 runs through casing 1 and tail box body 28, driven pulley 1 and driven pulley 2 25 is respectively equipped with at the two ends of rotating shaft 2 10, motor 9 drives driven pulley 1 by transition gear 29, driven pulley 1 driven rotary axle 2 10 rotates, pivoted arm wheel 11 to be arranged on rotating shaft 2 10 and to be positioned at sheave box body 24, and pivoted arm wheel 11 drives sheaves 8 to do intermittent movement, described bullet groove closing cap Power Component comprises rotating shaft 3 12, cam 13, driven pulley 3 14, rotating shaft 3 12 is arranged in casing 1, and be positioned at the top playing groove closing cap 2, cam 13 to be fixed on rotating shaft 3 12 and to contact with the upper surface playing groove closing cap 3 all the time, driven pulley 14 is arranged on one end of rotating shaft 3 12, is connected between driven pulley 3 14 with driven pulley 2 25 by transition gear 26, described launch power assembly comprises percussion cam 15, hammer 16, trigger shaft 17, firing pin 18, firing pin cover 19, torsion spring 20, percussion cam 15 is arranged on rotating shaft 2 10, the base of this percussion cam 15 is circular, a plane of base is provided with a spiral step, the central axis of spiral step and the central axes of base, the lowest part of spiral step and the plane of base tangent, hammer 16 is arranged in tail box body 28 by hammer pin, trigger shaft 17 is provided with in the below of hammer 16, trigger shaft 17 coordinates with the spiral step on percussion cam 15, firing pin cover 19 is fixed in sheave box body 27, and the axis of the axis of firing pin cover 19 and transmitting tube 7 on the same line, firing pin 18 is arranged in firing pin cover 19, torsion spring 20 is arranged on hammer pin, one end of torsion spring 20 is connected with hammer 16, the other end is connected with tail box body 28, described manual percussion lock comprises pedestal 21, rocking handle 22, rocking handle bar 23, spring, pedestal 21 is fixed on the outer surface of tail box body 28, spring is arranged in pedestal 21, rocking handle 22 is L-shaped, one end of rocking handle bar 23 is connected with one end of rotating shaft 2 10 through the spring in pedestal 21, other end of rocking handle bar 23 is connected with one end of rocking handle 22, when without the need to using manual, drawn in by rocking handle 22, rocking handle bar 23 is outwards moved and is separated with rotating shaft 2 10, rocking handle 22 discharges when needs are manual, and rocking handle bar 23 moves inward and is connected with rotating shaft 2 10.
Claims (10)
1. a grenade launcher, is characterized in that: it comprises casing, sheave box body, tail box body, combined type cartridge chamber assembly, plays groove closing cap Power Component, rotating missile groove Power Component, launch power assembly, transmitting tube, power source; Described sheave box body is connected with casing, and is positioned at the rear side of casing, and described tail box body is connected with sheave box body, and is positioned at the rear side of sheave box body; Described combined type cartridge chamber assembly comprises rotating missile groove and plays groove closing cap; Described rotating missile groove rotates around the longitudinal center line of rotating missile groove, the radial direction of rotating missile groove is provided with the main cartridge chamber of the consistent outward opening of multiple shape size uniformly, and opening shaft is to running through rotating missile groove, be provided with rotating shaft one in the center of rotating missile groove, the center line of rotating shaft one overlaps with the longitudinal center line of rotating missile groove; Described rotating missile groove Power Component is arranged in casing, and rotating missile groove Power Component driven rotary axle one does intermittent movement; Described bullet groove closing cap is arranged in casing by playing groove closing cap Power Component, and moves reciprocatingly in casing, and the lower surface playing groove closing cap is provided with the secondary cartridge chamber of an outward opening, secondary cartridge chamber coordinates formation one complete cartridge chamber with main cartridge chamber; Described transmitting tube is arranged on casing, and is positioned at the front of rotating missile groove, the center line of transmitting tube all the time with the center line of complete cartridge chamber on the same line; The trigger mechanism of described launch power assembly is arranged in tail box body, is pulled the trigger the ammunition in cartridge chamber by trigger mechanism; Described power source is connected with bullet groove closing cap Power Component, rotating missile groove Power Component, launch power assembly.
2. a kind of grenade launcher according to claim 1, it is characterized in that: the lower surface of described bullet groove closing cap is provided with one cartridge chamber, bullet groove closing cap is provided with guide hole in secondary cartridge chamber surrounding, guide pillar is provided with in guide hole, on guide pillar, cover has back-moving spring, guide pillar is connected with casing, plays groove closing cap and moves up and down along guide pillar direction under the effect playing groove closing cap Power Component.
3. a kind of grenade launcher according to claim 1, is characterized in that: described bullet groove closing cap also can be divided into left bullet groove and the right side time to play groove, and left bullet groove is played groove with the right side time and be connected with casing by traversing assembly or rotary components.
4. a kind of grenade launcher according to claim 1, it is characterized in that: described rotating missile groove Power Component comprises rotating shaft two, rotating shaft two driven rotary axle one does intermittent movement, rotating shaft two is provided with pivoted arm wheel, one end of rotating shaft one is provided with sheave, pivoted arm wheel drives sheave to rotate, and sheave driven rotary axle one rotates, and is respectively equipped with driven pulley one and driven pulley two at the two ends of rotating shaft two.
5. a kind of grenade launcher according to claim 1, it is characterized in that: described rotating missile groove Power Component also can comprise rotating shaft two, sprocket wheel one, chain, sprocket wheel two, rotating shaft two driven rotary axle one does intermittent movement, rotating shaft two is provided with sprocket wheel one, the left end of rotating shaft one is provided with sprocket wheel two, sprocket wheel one is by chain-driving sprocket wheel two, and sprocket wheel two driven rotary axle one rotates.
6. a kind of grenade launcher according to claim 1, it is characterized in that: described bullet groove closing cap Power Component comprises rotating shaft three, cam, driven pulley three, rotating shaft three is arranged in casing, and be positioned at the top playing groove closing cap, cam is fixed on rotating shaft three, driven pulley three is arranged on one end of rotating shaft three, and driven pulley three coordinates with driven pulley two.
7. a kind of grenade launcher according to claim 1, is characterized in that: described rotating missile groove is provided with the main cartridge chamber of four outward openings.
8. a kind of grenade launcher according to claim 1, it is characterized in that: described tail box body is provided with manual percussion lock, this manual percussion lock comprises pedestal, rocking handle, rocking handle bar, spring, pedestal is fixed on the outer surface of tail box body, spring is arranged in pedestal, rocking handle is L-shaped, rocking handle bar is connected with one end of rotating shaft two through the spring in pedestal, the other end of rocking handle bar is connected with one end of rocking handle, when without the need to using manual, rocking handle is drawn in, rocking handle bar is outwards moved be separated with rotating shaft two, the rocking handle release when needs are manual, rocking handle bar moves inward and is connected with rotating shaft two.
9. a kind of grenade launcher according to claim 1, it is characterized in that: the base of described percussion cam is circular, a plane of base is provided with a spiral step, the central axis of spiral step and the central axes of base, the lowest part of spiral step and the plane of base tangent.
10. a kind of grenade launcher according to claim 1, it is characterized in that: described launch power assembly comprises percussion cam, hammer, trigger shaft, firing pin, firing pin cover, torsion spring, percussion cam is arranged on rotating shaft two, hammer is arranged in tail box body by hammer pin, trigger shaft is provided with in the below of hammer, trigger shaft and percussion cam engagement, firing pin cover is fixed in sheave box body, and the axis of the axis of firing pin cover and transmitting tube on the same line, firing pin is arranged in firing pin cover, torsion spring is arranged on hammer pin, one end of torsion spring is connected with hammer, the other end is connected with tail box body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520565839.XU CN205049049U (en) | 2015-07-28 | 2015-07-28 | Howitzer transmitter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520565839.XU CN205049049U (en) | 2015-07-28 | 2015-07-28 | Howitzer transmitter |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205049049U true CN205049049U (en) | 2016-02-24 |
Family
ID=55342621
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520565839.XU Active CN205049049U (en) | 2015-07-28 | 2015-07-28 | Howitzer transmitter |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205049049U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105258556A (en) * | 2015-07-28 | 2016-01-20 | 浙江先锋机械有限公司 | Grenade launcher |
| CN106359363A (en) * | 2016-08-31 | 2017-02-01 | 樊钥宽 | Titanium laser cannon anti-bird device |
| CN108955377A (en) * | 2018-07-16 | 2018-12-07 | 哈尔滨工业大学 | A kind of small-diameter circular cylindricality target Consecutive launcher |
| CN111947514A (en) * | 2020-07-24 | 2020-11-17 | 北斗安泽防务科技有限公司 | Grenade launcher |
-
2015
- 2015-07-28 CN CN201520565839.XU patent/CN205049049U/en active Active
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105258556A (en) * | 2015-07-28 | 2016-01-20 | 浙江先锋机械有限公司 | Grenade launcher |
| CN106359363A (en) * | 2016-08-31 | 2017-02-01 | 樊钥宽 | Titanium laser cannon anti-bird device |
| CN106359363B (en) * | 2016-08-31 | 2019-05-07 | 樊钥宽 | A kind of titanium radium bomb scarer |
| CN108955377A (en) * | 2018-07-16 | 2018-12-07 | 哈尔滨工业大学 | A kind of small-diameter circular cylindricality target Consecutive launcher |
| CN111947514A (en) * | 2020-07-24 | 2020-11-17 | 北斗安泽防务科技有限公司 | Grenade launcher |
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| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |