CN110030875A - A kind of launcher - Google Patents
A kind of launcher Download PDFInfo
- Publication number
- CN110030875A CN110030875A CN201910312222.XA CN201910312222A CN110030875A CN 110030875 A CN110030875 A CN 110030875A CN 201910312222 A CN201910312222 A CN 201910312222A CN 110030875 A CN110030875 A CN 110030875A
- Authority
- CN
- China
- Prior art keywords
- angle control
- frame
- rod
- plate
- bedframe
- 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
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F3/00—Rocket or torpedo launchers
- F41F3/04—Rocket or torpedo launchers for rockets
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
Abstract
The invention discloses a kind of launchers, including bedframe, explosion tape frame, position plate, frame, left plate, right side plate, block, orientation seat, orientation lever, slot stick, end socket, first axle, support, branch seat stand, angle control-rod, the second axis, angle control flume, oblique square tube, adjusting pad, square steel tube and casing, the inner cavity of the bedframe is provided with explosion tape frame, front-end and back-end on the left of the bedframe, which are respectively provided with, is connected to angle control-rod, branch seat stand is provided at the top of the angle control-rod, the screw top of the branch seat stand is connected with support.The present invention solves the problems, such as that rocket towing explosive device launcher safety is unstable by bedframe, explosion tape frame, position plate, frame, left plate, right side plate, block, the cooperation for orienting seat, orientation lever, slot stick, end socket, first axle, support, branch seat stand, angle control-rod, the second axis, angle control flume, oblique square tube, adjusting pad, square steel tube and casing.
Description
Technical field
The present invention relates to ammunition fuze technical field, specially a kind of launcher.
Background technique
The aircraft that rocket is pushed ahead by the reaction force that rocket engine injection working medium generates, own carry all
Propellant does not depend on extraneous working medium and generates thrust, can also fly outside dense atmosphere in dense atmosphere, fire
Arrow is the delivery vehicle for realizing space travel, and there are many kinds of rockets, and original rocket is attached on bow and arrow head with fire-lighter, then
It is mapped to enemy and causes a kind of arrow burned arrow with it, be originally only intended to celebrate a festival and put pyrotechnics use, modern rocket is with heat
Air-flow high speed spray backward, the jet-propulsion plant to be travelled forward using the reaction force of generation, own carry incendiary agent with
Oxidant does not depend on the oxygen and aiding combustion in air, can in an atmosphere, but also can not only can be used as fastly in outer-space flight, modern rocket
Fast long distance transportation tool can be used to emit satellite and deliver weapon warhead, and rocket bomb transmitting frame is for hanging and sending out
A kind of device of rocket projectile is penetrated, rocket towing explosive device is vehicle-mounted rocket towing explosive device, and it is unstable that there are the safeties of rocket towing explosive device launcher
Fixed problem.
Summary of the invention
The purpose of the present invention is to provide a kind of launchers, have the advantages of safety and stability, solve rocket towing explosive device hair
Penetrate the unstable problem of frame safety.
To achieve the above object, the invention provides the following technical scheme: a kind of launcher, including bedframe, explosion band
Frame, position plate, frame, left plate, right side plate, block, orientation seat, orientation lever, slot stick, end socket, first axle, support, support
Platform, angle control-rod, the second axis, angle control flume, oblique square tube, adjusting pad, square steel tube and casing, the inner cavity of the bedframe
It is provided with explosion tape frame, the front-end and back-end on the left of the bedframe, which are respectively provided with, is connected to angle control-rod, the angle control
Branch seat stand is provided at the top of bar processed, the screw top of the branch seat stand is connected with support, and the top of the support passes through first
Axis is flexibly connected with position plate, and the bottom of the position plate is fixedly connected with framed, the rear end and front end point of the position plate bottom
It is not provided with left plate and right side plate, the bottom of the frame is provided with orientation lever, and the bottom of the position plate is provided with orientation seat,
One end of the orientation lever is provided with end socket, is provided with block and bedframe at the top of the position plate.
Preferably, the surface of the angle control-rod is connect with frame by angle control flume, the angle control flume and frame
Between by the second axis be flexibly connected.
Preferably, square steel tube is fixedly connected between the angle control-rod.
Preferably, the left side at the top of the position plate is provided with casing.
Compared with prior art, beneficial effects of the present invention are as follows:
The present invention is by being arranged bedframe, explosion tape frame, position plate, frame, left plate, right side plate, block, orientation seat, determining
To bar, slot stick, end socket, first axle, support, branch seat stand, angle control-rod, the second axis, angle control flume, oblique square tube, adjustment
Pad, square steel tube and casing cooperation, play will explosion band draw it is into a straight condition, finally fuse effect under explosion with quick-fried
Fried effect, improves safety, solves the problems, such as that rocket towing explosive device launcher safety is unstable.
Detailed description of the invention
Fig. 1 is schematic structural view of the invention；
Fig. 2 is side structure schematic view of the present invention；
Fig. 3 is left plate structural schematic diagram of the present invention；
Fig. 4 is stop block structure schematic diagram of the present invention；
Fig. 5 is square steel tube structural schematic diagram of the present invention.
In figure: 1 bedframe, 2 explosion tape frames, 3 position plates, 4 frames, 5 left plates, 6 right side plates, 7 blocks, 8 orientation seats,
9 orientation levers, 10 slot sticks, 11 end sockets, 12 first axles, 13 supports, 14 seat stands, 15 angle control-rods, 16 second axis, 17 angles
Control flume, 18 oblique square tubes, 19 adjusting pads, 20 square steel tubes, 21 casings.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
Please refer to Fig. 1-5, a kind of launcher, including bedframe 1, explosion tape frame 2, position plate 3, frame 4, left plate 5,
Right side plate 6, block 7, orientation seat 8, orientation lever 9, slot stick 10, end socket 11, first axle 12, support 13, branch seat stand 14, angle control
Bar 15, the second axis 16, angle control flume 17, oblique square tube 18, adjusting pad 19, square steel tube 20 and casing 21 processed, bedframe 1 it is interior
Chamber is provided with explosion tape frame 2, and the front-end and back-end in 1 left side of bedframe, which are respectively provided with, is connected to angle control-rod 15, angle control
The surface of bar 15 is connect with frame 4 by angle control flume 17, between angle control flume 17 and frame 4 even by 16 activity of the second axis
It connects, square steel tube 20 is fixedly connected between angle control-rod 15, the top of angle control-rod 15 is provided with branch seat stand 14, branch seat stand
14 screw top is connected with support 13, and the top of support 13 is flexibly connected by first axle 12 with position plate 3, and position plate 3 pushes up
Casing 21 is provided on the left of portion, the bottom of position plate 3 is fixedly connected with framed 4, and the rear end and front end of 3 bottom of position plate are set respectively
It is equipped with left plate 5 and right side plate 6, the bottom of frame 4 is provided with orientation lever 9, and the bottom of position plate 3 is provided with orientation seat 8, orientation lever
9 one end is provided with end socket 11, and the top of position plate 3 is provided with block 7 and bedframe 1, passes through setting bedframe 1, quick-fried
Fried tape frame 2, position plate 3, frame 4, left plate 5, right side plate 6, block 7, orientation seat 8, orientation lever 9, slot stick 10, end socket 11,
First axle 12, support 13, branch seat stand 14, angle control-rod 15, the second axis 16, angle control flume 17, oblique square tube 18, adjusting pad
19, the cooperation of square steel tube 20 and casing 21, play will explosion band draw it is into a straight condition, finally fuse effect under explode
Effect with explosion, improves safety, solves the problems, such as that rocket towing explosive device launcher safety is unstable.
In use, being first that warhead is ordered in explosion tape frame 2, then rocket projectile is packed by fixed by explosion band
In the launcher formed to parts such as seat 8, orientation lever 9, left plate 5, right side plate 6, block 7, slot sticks 10, then pass through angle control
Bar 15 and angle control flume 17 processed adjust launch angle, and by ignition device, rocket engine is in orientation seat 8, orientation lever
9, smoothly fly out under fixed angle and direction launcher under the guidance of slot stick 10, is then pulled and is exploded by bullet tail structure
Band flight forward, explosion band drawing is into a straight condition, and the finally explosion band explosion under fuse effect solves rocket explosion
The unstable problem of device launcher safety.
In summary: the launcher passes through bedframe 1, explosion tape frame 2, position plate 3, frame 4, left plate 5, right side
Plate 6, block 7, orientation seat 8, orientation lever 9, slot stick 10, end socket 11, first axle 12, support 13, branch seat stand 14, angle control-rod
15, the cooperation of the second axis 16, angle control flume 17, oblique square tube 18, adjusting pad 19, square steel tube 20 and casing 21, solves rocket
The unstable problem of blaster launcher safety.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
A variety of variations, modification, replacement can be carried out to these embodiments without departing from the principles and spirit of the present invention by understanding
And modification, the scope of the present invention is defined by the appended.
Claims (4)
1. a kind of launcher, including bedframe (1), explosion tape frame (2), position plate (3), frame (4), left plate (5), right side
Plate (6), block (7), orientation seat (8), orientation lever (9), slot stick (10), end socket (11), first axle (12), support (13), branch
Seat stand (14), angle control-rod (15), the second axis (16), angle control flume (17), oblique square tube (18), adjusting pad (19), square steel
Manage (20) and casing (21), it is characterised in that: the inner cavity of the bedframe (1) is provided with explosion tape frame (2), the pedestal
Front-end and back-end on the left of frame (1), which are respectively provided with, to be connected to angle control-rod (15), the top setting of the angle control-rod (15)
Have branch seat stand (14), the screw top of the branch seat stand (14) is connected with support (13), and the top of the support (13) passes through the
One axis (12) is flexibly connected with position plate (3), and the bottom of the position plate (3) is fixedly connected framed (4), the position plate (3)
The rear end and front end of bottom are respectively arranged with left plate (5) and right side plate (6), and the bottom of the frame (4) is provided with orientation lever
(9), the bottom of the position plate (3) is provided with orientation seat (8), and one end of the orientation lever (9) is provided with end socket (11), described
Block (7) and bedframe (1) are provided at the top of position plate (3).
2. a kind of launcher according to claim 1, it is characterised in that: the surface of the angle control-rod (15) and frame
(4) it is connected by angle control flume (17), between the angle control flume (17) and frame (4) even by the second axis (16) activity
It connects.
3. a kind of launcher according to claim 1, it is characterised in that: be fixedly connected between the angle control-rod (15)
There are square steel tube (20).
4. a kind of launcher according to claim 1, it is characterised in that: the left side at the top of the position plate (3) is provided with
Casing (21).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910312222.XA CN110030875A (en) | 2019-04-18 | 2019-04-18 | A kind of launcher |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910312222.XA CN110030875A (en) | 2019-04-18 | 2019-04-18 | A kind of launcher |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110030875A true CN110030875A (en) | 2019-07-19 |
Family
ID=67238929
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910312222.XA Pending CN110030875A (en) | 2019-04-18 | 2019-04-18 | A kind of launcher |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110030875A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111547266A (en) * | 2020-05-13 | 2020-08-18 | 陕西中天火箭技术股份有限公司 | Multi-channel foldable box-type low-altitude sounding rocket launching device |
| CN113624070A (en) * | 2021-07-08 | 2021-11-09 | 陕西中天火箭技术股份有限公司 | Portable ground guidance rocket launcher with adjustable launch angle |
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|---|---|---|---|---|
| FR1270211A (en) * | 1959-10-30 | 1961-08-25 | Bofors Ab | Improvements to demining lines |
| FR1272799A (en) * | 1960-11-03 | 1961-09-29 | Comet Appbau G M B H | Device for detonating, by means of explosive charges, mines located on minefields |
| US4273048A (en) * | 1979-03-26 | 1981-06-16 | The United States Of America As Represented By The Secretary Of The Navy | Surface-launched fuel-air explosive minefield clearance round |
| JP2003269893A (en) * | 2002-03-15 | 2003-09-25 | Ihi Aerospace Co Ltd | Cable projecting device |
| US6766745B1 (en) * | 2002-10-08 | 2004-07-27 | The United States Of America As Represented By The Secretary Of The Navy | Low cost rapid mine clearance system |
| CN202101606U (en) * | 2011-06-03 | 2012-01-04 | 江西钢丝厂 | Vehicular power-driven launcher with bomb storage |
| US8893604B1 (en) * | 2012-02-03 | 2014-11-25 | The United States Of America As Represented By The Secretary Of The Army | Modular munitions deployment platform |
| CN204649077U (en) * | 2015-05-12 | 2015-09-16 | 武汉华益欣电子有限公司 | The rocket projector that a kind of emission angle is adjustable |
| EP2937662A1 (en) * | 2014-04-18 | 2015-10-28 | Wojskowy Instytut Techniki Inzynieryjnej im. profesora Jozefa Kosackiego | Mine-clearing system |
| US20150345900A1 (en) * | 2014-05-28 | 2015-12-03 | Chief Of Naval Research, Office Of Counsel | Missile Launcher System |
| CN205192334U (en) * | 2015-12-16 | 2016-04-27 | 齐齐哈尔北方机器有限责任公司 | Towed rocket projectile launcher |
| CN209910506U (en) * | 2019-04-18 | 2020-01-07 | 永卓防务科技有限公司 | Launching cradle |
-
2019
- 2019-04-18 CN CN201910312222.XA patent/CN110030875A/en active Pending
Patent Citations (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1270211A (en) * | 1959-10-30 | 1961-08-25 | Bofors Ab | Improvements to demining lines |
| FR1272799A (en) * | 1960-11-03 | 1961-09-29 | Comet Appbau G M B H | Device for detonating, by means of explosive charges, mines located on minefields |
| US4273048A (en) * | 1979-03-26 | 1981-06-16 | The United States Of America As Represented By The Secretary Of The Navy | Surface-launched fuel-air explosive minefield clearance round |
| JP2003269893A (en) * | 2002-03-15 | 2003-09-25 | Ihi Aerospace Co Ltd | Cable projecting device |
| US6766745B1 (en) * | 2002-10-08 | 2004-07-27 | The United States Of America As Represented By The Secretary Of The Navy | Low cost rapid mine clearance system |
| CN202101606U (en) * | 2011-06-03 | 2012-01-04 | 江西钢丝厂 | Vehicular power-driven launcher with bomb storage |
| US8893604B1 (en) * | 2012-02-03 | 2014-11-25 | The United States Of America As Represented By The Secretary Of The Army | Modular munitions deployment platform |
| EP2937662A1 (en) * | 2014-04-18 | 2015-10-28 | Wojskowy Instytut Techniki Inzynieryjnej im. profesora Jozefa Kosackiego | Mine-clearing system |
| US20150345900A1 (en) * | 2014-05-28 | 2015-12-03 | Chief Of Naval Research, Office Of Counsel | Missile Launcher System |
| CN204649077U (en) * | 2015-05-12 | 2015-09-16 | 武汉华益欣电子有限公司 | The rocket projector that a kind of emission angle is adjustable |
| CN205192334U (en) * | 2015-12-16 | 2016-04-27 | 齐齐哈尔北方机器有限责任公司 | Towed rocket projectile launcher |
| CN209910506U (en) * | 2019-04-18 | 2020-01-07 | 永卓防务科技有限公司 | Launching cradle |
Non-Patent Citations (2)
| Title |
|---|
| 刁海龙;: "两栖登陆作战中反水雷的利剑――爆炸排雷", 现代舰船, no. 11, pages 25 - 27 * |
| 邸雪颖;尚尔雨;徐春海;: "利用火箭布设林火阻隔索状炸药", 林业科技, no. 03, pages 40 - 41 * |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111547266A (en) * | 2020-05-13 | 2020-08-18 | 陕西中天火箭技术股份有限公司 | Multi-channel foldable box-type low-altitude sounding rocket launching device |
| CN113624070A (en) * | 2021-07-08 | 2021-11-09 | 陕西中天火箭技术股份有限公司 | Portable ground guidance rocket launcher with adjustable launch angle |
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