CN105571395A - Multifunctional rocket launcher - Google Patents

Multifunctional rocket launcher Download PDF

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Publication number
CN105571395A
CN105571395A CN201510986701.1A CN201510986701A CN105571395A CN 105571395 A CN105571395 A CN 105571395A CN 201510986701 A CN201510986701 A CN 201510986701A CN 105571395 A CN105571395 A CN 105571395A
Authority
CN
China
Prior art keywords
rocket launcher
rocket
axle sleeve
cable wire
stud
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
Application number
CN201510986701.1A
Other languages
Chinese (zh)
Inventor
银世德
Original Assignee
银世德
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by 银世德 filed Critical 银世德
Priority to CN201510986701.1A priority Critical patent/CN105571395A/en
Publication of CN105571395A publication Critical patent/CN105571395A/en
Pending legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41FAPPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00Rocket or torpedo launchers
    • F41F3/04Rocket or torpedo launchers for rockets
    • F41F3/045Rocket or torpedo launchers for rockets adapted to be carried and used by a person, e.g. bazookas
    • F41F3/0455Bazookas

Abstract

The invention provides a multifunctional rocket launcher. The multifunctional rocket launcher is characterized in that gathering is completed through elastic potential performance of a spring by means of a mechanism, kinetic energy for firing a rocket projectile and throwing other objects is formed, the rocket launcher is aimed at a target by means of a sighting telescope, and the rocket projectile be accurately fired and ejected forwards; the rocket projectile can be launched, the initial speed of the rocket projectile can be improved, the firing range of the firing range can be increased, and the accuracy of target blowing can be improved; missiles, napalm bombs, smoke projectiles, grenades, hand grenades and fire extinguishing bullets can be launched, and life-saving equipment such as ropes, long-handled hooks and life-saving rings can be thrown to the ideal positions; and an infrared night vision sighting device is used, and the night fighting capacity can be enhanced under the starlight condition or other poor light conditions.

Description

Multifunctional fire quiver
Technical field
The invention provides a kind of rocket launcher, specifically a kind of Multifunctional fire quiver, belong to weapon field.
Background technology
At present, army, in march, investigation and operation, often can run into the complicated landform such as steep cliff cliff and valley, river, stops army to move ahead sometimes.In fight, grenade is still less than on the position of enemy sometimes, and some rocket launchers are disposable, and soldier carries limited amount, and a miss target, will cause and suffer a defeat.Another shortcoming of rocket launcher is function singleness, is difficult to launch firebomb, smoke projectile and howitzer and grenade.Army is when high building fire extinguishing and floods rescue, if do not have desirable equipment of jettisoninging, being difficult to jettisonings fire extinguisher bomb and lifesaving appliance puts in place.
Summary of the invention
For above-mentioned deficiency, need to develop a kind of new rocket launcher, solve above problem.In view of this, the invention provides a kind of Multifunctional fire quiver, this rocket launcher efficiently solves the deficiencies in the prior art, it not only possesses rocket launcher and saving casting device two functions, and structure is simple, easy to carry, can increase the range of rocket projectile, the accurate performance thing of jettisoninging strengthened target is hit is jettisoninged more remote exactly.Technical scheme of the present invention is, the bullet gesture performance of spring is completed gathering by means of mechanism, forms the kinetic energy of percussion rocket projectile and other objects of jettisoninging, and by means of gun sight run-home, rocket projectile percussion also ejected forward exactly, thing of maybe jettisoninging is jettisoninged and is put in place.Described rocket launcher can be launched a guided missile, firebomb, smoke projectile, howitzer, grenade, fire extinguisher bomb, the lifesaving appliances such as rope, long-handled hook, lifebuoy of can also jettisoninging.
Technical scheme of the present invention is achieved in that described Multifunctional fire quiver is made up of launching tube, gun sight, energy storage device, percussion lock and rocket projectile 5 part.Launching tube is made up of stack shell, heat-barrier material, feed port cover, front and rear covers, carrying handle, bracing frame and braces hanging nose, and stack shell adopts alloy steel material to make, and makes stack shell lightweight, is easy to carry about with one; Gun sight is made up of mirror pipe, connection microscope base, protective cover and lighting tool, and enlargement ratio is 2.5,9 degree, visual field; Energy storage device forms by launching spring, piston, cable wire, macro-axis, axle sleeve, rocking arm and convex type ring; Percussion lock is made up of trigger, insurance, guard ring, striker.
Described Multifunctional fire quiver, can also use lll sight and infrared night vision gunsight, to use under starlight or under other poor light conditions, enhances its night fighting ability.
Accompanying drawing explanation
Below in conjunction with accompanying drawing, the present invention is further detailed explanation.
Fig. 1 is the structural representation of Multifunctional fire quiver.
Fig. 2 is the structural representation of clutch.
Fig. 3 is the schematic diagram of piston.
Reference numeral: striker (1), piston (2), cable wire (3), braces hanging nose (4), rocket launcher shell (5), heat-barrier material (6), feed port cover (7), gun sight (8), macro-axis (9), rocking arm (10), convex ring (11), axle sleeve (12), spring base (13), little spring (14), bonnet (15), handwheel (16), thread (17), rear carrying handle (18), guard ring (19), insurance (20), trigger (21), prerequisite is (22), launch spring (23), bracing frame (24), protecgulum (25), cable wire bearing (26), screw hole (27), skeleton (28).
Detailed description of the invention
Known according to Fig. 1, one section of stud is welded in one end of cable wire (3), stud is screwed in the screw hole (27) of piston (2), stud is made to expose 10-30 millimeter, namely exposed portion is striker (1), then rocket launcher shell (5) is together put into, macro-axis (9) is passed from axle sleeve (12), and be arranged on rocket launcher shell (5) rear end, the circle cross section of axle sleeve (12) right-hand member manufactures concavity, by the other end of cable wire (3), fix through with cable wire bearing (26) from transmitting spring (23), convex ring (11) and rocking arm (10) are installed in macro-axis (9) right side, little spring (14) is installed in left side, spindle nose manufactures thread (17), handwheel (16) is spun on thread (17), gun sight (8), feed port cover (7) and braces hanging nose (4) are set on rocket launcher shell (5) top, rear carrying handle (18), guard ring (19), insurance (20), trigger (21), prerequisite are installed (22) in bottom, install protecgulum (25) and bonnet (15) in the rear and front end of rocket launcher, heat-barrier material (6) is respectively installed in upper and lower.
With reference to the accompanying drawings shown in 2, by positive and negative rotation handwheel (16), the protuberance of convex ring (11) is made to combine with axle sleeve (12) recess and be separated.
With reference to the accompanying drawings shown in 3, blade-like will be made in the front portion of skeleton (26), to reduce the recoil of rocket launcher.
After all parts install, if need to launch a rocket shell, first, screw off front and rear covers, open bracing frame, according to rotating forward handwheel, arrangement of clutch is combined, then rocking arm is shaken, macro-axis is rotated together with axle sleeve, because one end of cable wire is fixed on axle sleeve, so cable wire is wound around by axle sleeve, cable wire drives piston to move down, when piston arrives trigger position, piston pins by trigger automatically, at this moment stop operating rocking arm, close insurance, rocket projectile is put into from emission port, rocket projectile is made to be in arm-to-arm, when transmission is required, chief of breech drops to the ground forward, rocket launcher is shouldered on right shoulder, rear carrying handle is against on front side of shoulder, left hand holds prerequisite handle, insurance is opened with the right hand, cocking after run-home, make that transmitting spring is out of hand to be expanded instantaneously, rocket projectile is pulled the trigger, rocket projectile flies out forward under the promotion of flame and under the launching of spring, flame sprays from rocket launcher afterbody, jettisoning grenade time, put in place by transmitting spring-compressed, after grenade is backed out bonnet, put into from filler, draw ring hangs on feed port cover axle, gets final product cocking.When needing closely, transmitting spring not exclusively can compress and put in place, and any joint spring can pin by trigger.

Claims (1)

1. a Multifunctional fire quiver, one section of stud is welded in one end of cable wire (3), stud is screwed in the screw hole (27) of piston (2), stud is made to expose 10-30 millimeter, namely exposed portion is striker (1), together put into rocket launcher shell (5), macro-axis (9) passes from axle sleeve (12), and be arranged on rocket launcher shell (5) rear end, the circle cross section of axle sleeve (12) right-hand member manufactures concavity, cable wire (3) passes and links with cable wire bearing (26) from transmitting spring (23), convex ring (11) and rocking arm (10) are installed in macro-axis (9) right side, little spring (14) is installed in left side, spindle nose manufactures thread (17), handwheel (16) is spun on thread (17), on rocket launcher shell (5) top, gun sight (8) is set, feed port cover (7) and braces hanging nose (4), rear carrying handle (18) is installed in bottom, guard ring (19), insurance (20), trigger (21), prerequisite is (22), in the rear and front end of rocket launcher, protecgulum (25) and bonnet (15) are installed, heat-barrier material (6) is respectively installed in upper and lower, the protuberance of convex ring (11) can be made with the combination of axle sleeve (12) recess by rotation hand wheel (16) and be separated, blade-like will be made in the front portion of skeleton (26), to reduce the recoil of rocket launcher.
CN201510986701.1A 2015-12-26 2015-12-26 Multifunctional rocket launcher Pending CN105571395A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510986701.1A CN105571395A (en) 2015-12-26 2015-12-26 Multifunctional rocket launcher

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201510986701.1A CN105571395A (en) 2015-12-26 2015-12-26 Multifunctional rocket launcher

Publications (1)

Publication Number Publication Date
CN105571395A true CN105571395A (en) 2016-05-11

Family

ID=55881804

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201510986701.1A Pending CN105571395A (en) 2015-12-26 2015-12-26 Multifunctional rocket launcher

Country Status (1)

Country Link
CN (1) CN105571395A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107179018A (en) * 2017-06-05 2017-09-19 沈阳东朗科技开发有限公司 A kind of cartridge type ejection emitter for launching simulation dummy round

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2110204U (en) * 1991-11-30 1992-07-15 顾本科 Toy cannon
JPH10225877A (en) * 1997-02-15 1998-08-25 Takahiro Agata Hand-operated car window glass crushing tool using spring
CN2840429Y (en) * 2005-08-12 2006-11-22 王维 Strong crossbow Rope shooter
CN101315262A (en) * 2008-06-03 2008-12-03 北京航空航天大学 Movement objective generating device
US20100170486A1 (en) * 2009-01-07 2010-07-08 Precision Shooting Equipment, Inc. Crossbow Accessory for Lower Receiver of Rifle and Related Method
CN104197780A (en) * 2014-09-01 2014-12-10 银世德 Multifunctional spring thrower
CN104848744A (en) * 2015-05-18 2015-08-19 浏阳市浏河机械有限公司 Fire extinguishing bomb launching ejector with remote marks

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2110204U (en) * 1991-11-30 1992-07-15 顾本科 Toy cannon
JPH10225877A (en) * 1997-02-15 1998-08-25 Takahiro Agata Hand-operated car window glass crushing tool using spring
CN2840429Y (en) * 2005-08-12 2006-11-22 王维 Strong crossbow Rope shooter
CN101315262A (en) * 2008-06-03 2008-12-03 北京航空航天大学 Movement objective generating device
US20100170486A1 (en) * 2009-01-07 2010-07-08 Precision Shooting Equipment, Inc. Crossbow Accessory for Lower Receiver of Rifle and Related Method
CN104197780A (en) * 2014-09-01 2014-12-10 银世德 Multifunctional spring thrower
CN104848744A (en) * 2015-05-18 2015-08-19 浏阳市浏河机械有限公司 Fire extinguishing bomb launching ejector with remote marks

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107179018A (en) * 2017-06-05 2017-09-19 沈阳东朗科技开发有限公司 A kind of cartridge type ejection emitter for launching simulation dummy round

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RJ01 Rejection of invention patent application after publication

Application publication date: 20160511

RJ01 Rejection of invention patent application after publication