CN109141106A - Rifle and a kind of unmanned plane are matched in a kind of running fire - Google Patents

Rifle and a kind of unmanned plane are matched in a kind of running fire Download PDF

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Publication number
CN109141106A
CN109141106A CN201810996118.2A CN201810996118A CN109141106A CN 109141106 A CN109141106 A CN 109141106A CN 201810996118 A CN201810996118 A CN 201810996118A CN 109141106 A CN109141106 A CN 109141106A
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CN
China
Prior art keywords
hoodle
roller
rifle
protrusion
sliding rail
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Granted
Application number
CN201810996118.2A
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Chinese (zh)
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CN109141106B (en
Inventor
杨雪
姜广存
徐顺义
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Goertek Robotics Co Ltd
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Goertek Robotics Co Ltd
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Priority to CN201810996118.2A priority Critical patent/CN109141106B/en
Publication of CN109141106A publication Critical patent/CN109141106A/en
Application granted granted Critical
Publication of CN109141106B publication Critical patent/CN109141106B/en
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A19/00Firing or trigger mechanisms; Cocking mechanisms
    • F41A19/58Electric firing mechanisms
    • F41A19/64Electric firing mechanisms for automatic or burst-firing mode
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/02Aircraft not otherwise provided for characterised by special use

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)

Abstract

The invention discloses a kind of running fires to match rifle and unmanned plane.The running fire includes trigger mechanism and dynamical system with rifle;Trigger mechanism includes launcher shell, roller and at least two resilient push, roller is placed in launcher shell, resilient push is in axial direction arranged in the side of roller, and the first sliding rail is equipped in launcher shell, and resilient push is equipped with the first protrusion for protruding into the first sliding rail;When dynamical system drives roller rotation, first protrusion is slided backward along the first sliding rail, resilient push is set to store power to after-contraction, when the first protrusion of a resilient push slides to the reverse-running section of the first sliding rail, the resilient push stretches forward reset, hoodle shock is launched, then, first protrusion of another resilient push continues to slide to reverse-running section, hits and emits another hoodle.The application makes the contraction of resilient push circulation and stretching process, continuously to hit hoodle, realizes at least two hoodle running fires by the first protrusion and the first guide rail of roller and cooperation.

Description

Rifle and a kind of unmanned plane are matched in a kind of running fire
Technical field
The present invention relates to unmanned plane accessory technical field, in particular to rifle and a kind of unmanned plane are matched in a kind of running fire.
Background technique
With the development of unmanned air vehicle technique, it is applied to the every field such as takes photo by plane, detect, entertain and educate more and more In.During being educated using unmanned plane, in order to improve the enjoyment in educational unmanned plane teaching, it can pacify to unmanned plane Assembly parts, such as with rifle and manipulator etc..
And existing unmanned plane, although can be realized the transmitting of hoodle, mostly lacks running fire function in rifle, it cannot The running fire hoodle effect for being placed in unmanned plane is shown for user.
Summary of the invention
In view of the problem of running fire is with rifle is lacked in prior art unmanned plane accessory, a kind of running fire of the invention is proposed with rifle With a kind of unmanned plane, to overcome the above problem or at least to be partially solved the above problem.
To achieve the goals above, present invention employs following technical solutions:
According to one aspect of the present invention, a kind of running fire is provided with rifle, including trigger mechanism and dynamical system;Transmitter Structure includes that launcher shell, roller and at least two resilient push, roller are placed in launcher shell, and the side of roller is along axial direction Resilient push is arranged in direction, and the first sliding rail is equipped in launcher shell, and resilient push is equipped with the first protrusion for protruding into the first sliding rail; When dynamical system drives roller rotation, the first protrusion is slided backward along the first sliding rail, so that resilient push is stored power to after-contraction, to one When first protrusion of a resilient push slides to the reverse-running section of the first sliding rail, which stretches forward reset, and hoodle is hit Launch, then, the first protrusion of another resilient push continues to slide to reverse-running section, hits another hoodle of running fire.
Optionally, the first sliding rail includes a spiral section, and the head and the tail of spiral section are by being parallel to returning for resilient push telescopic direction The connection of journey section.
Optionally, the side of roller is equipped with sets respectively with the one-to-one push rod groove of resilient push, multiple resilient push In in push rod groove.
Optionally, resilient push includes hoodle push rod, spring and sleeve, and the first protrusion of setting, spring are set on hoodle push rod In hoodle push rod rear, sleeve is placed on hoodle push rod and spring outwards.
Optionally, the second sliding rail is additionally provided in launcher shell, sleeve is equipped with the second protrusion for protruding into the second sliding rail, works as rolling When cylinder rotation, the second protrusion is slided along the second sliding rail, slides back and forth sleeve cooperation hoodle push rod.
Optionally, sleeve is additionally provided with guide groove and limited block, and guide groove provides guiding for the first protrusion, and limited block prevents set Cylinder rotates in push rod groove.
Optionally, the front of roller is equipped with multiple transmitting cylinders, and transmitting cylinder and resilient push correspond.
Optionally, emit and be equipped with flexible blocking member between cylinder and roller, flexible blocking member stop hoodle before transmission from By skidding off.
Optionally, dynamical system includes: motor, driving wheel and driven wheel, and driven wheel is fixed on roller rear and and roller Coaxially, motor driven driving wheel rotates, and roller rotation is driven under gear drive.
According to one aspect of the present invention, a kind of unmanned plane is provided, which is provided with running fire any one of as above With rifle.
In conclusion the beneficial effects of the present invention are:
Resilient push of the setting at least two with the first protrusion on the outside of roller, it is sliding by the first of launcher shell Rail makes resilient push in roller rotation process shrink storage power, and replys and stretch in reverse-running section, and hoodle shock is launched, is led to Continuous shock hoodle is crossed, the running fire of at least two hoodles is realized.
Detailed description of the invention
Fig. 1 is the schematic perspective view that rifle is matched in running fire provided by one embodiment of the present invention;
Fig. 2 is the perspective view of the explosion that rifle is matched in running fire shown in Fig. 1;
Fig. 3 is the trigger mechanism schematic diagram of internal structure that rifle is matched in running fire shown in Fig. 1;
Fig. 4 is schematic diagram of the running fire shown in Fig. 1 with rifle as viewed from transmitting cylinder direction;
Fig. 5 is section B-B schematic diagram shown in Fig. 4;
Fig. 6 is launcher shell fractionation schematic diagram of the running fire shown in Fig. 1 with rifle;
Fig. 7 is that schematic diagram of the rifle as viewed from trigger mechanism rear is matched in running fire shown in Fig. 1;
Fig. 8 is C-C schematic cross-section shown in Fig. 7;
Fig. 9 is the use state sectional view that magazine is installed in running fire shown in Fig. 1 with the top of rifle;
In figure, 110, trigger mechanism;120, dynamical system;1, hoodle;2, flexible blocking member;3, emit cylinder fixed plate; 4, emit cylinder;5, roller;6, hoodle push rod;61, the first protrusion;7, transmitter lower casing;71, the first sliding rail lower part;72, second Sliding rail lower part;73, reverse-running section;8, transmitter upper casing;81, the first sliding rail top;82, the second sliding rail top;83, hoodle entrance; 9, sleeve;91, the second protrusion;92, guide groove;93, limited block;10, spring;11, driven wheel;12, dynamical system lower casing;13, Motor;14, dynamical system upper casing;15, driving wheel;16, pin;17, dynamical system fixed plate;18, screw;100, running fire is matched Rifle;200, magazine.
Specific embodiment
To make the object, technical solutions and advantages of the present invention clearer, below in conjunction with attached drawing to embodiment party of the present invention Formula is described in further detail.
In the description of the present application, it should be noted that term " center ", "upper", "lower", "left", "right", "vertical", The orientation or positional relationship of the instructions such as "horizontal", "inner", "outside" be based on the orientation or positional relationship shown in the drawings, merely to Convenient for describe the application and simplify description, rather than the device or element of indication or suggestion meaning must have a particular orientation, It is constructed and operated in a specific orientation, therefore should not be understood as the limitation to the application.In addition, term " first ", " second ", " third " is used for descriptive purposes only and cannot be understood as indicating or suggesting relative importance.
In the description of the present application, it should be noted that unless otherwise clearly defined and limited, term " installation ", " phase Even ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or be integrally connected;It can To be mechanical connection, it is also possible to be electrically connected;It can be directly connected, can also can be indirectly connected through an intermediary Connection inside two elements.For the ordinary skill in the art, above-mentioned term can be understood at this with concrete condition Concrete meaning in application.
Technical concept of the invention is: at least two resilient push with the first protrusion are set on the outside of roller, by First sliding rail of launcher shell makes resilient push in roller rotation process shrink storage power, and replys and stretch in reverse-running section, by bullet Pearl, which is hit, launches, and by continuously hitting hoodle, realizes the running fire of at least two hoodles.
Fig. 1-Fig. 9 discloses one embodiment that rifle is matched in the application running fire.Wherein, Fig. 1 mentions for one embodiment of the invention The schematic perspective view of rifle is matched in the running fire of confession, and Fig. 2 is the perspective view of the explosion that rifle is matched in running fire shown in Fig. 1, and Fig. 3 is to connect shown in Fig. 1 It is transported to the trigger mechanism schematic diagram of internal structure of rifle, Fig. 4 is signal of the running fire shown in Fig. 1 with rifle as viewed from transmitting cylinder direction Figure, Fig. 5 are section B-B schematic diagram shown in Fig. 4, and Fig. 6 is launcher shell fractionation schematic diagram of the running fire shown in Fig. 1 with rifle, and Fig. 7 is Schematic diagram of the rifle as viewed from trigger mechanism rear is matched in running fire shown in Fig. 1, and Fig. 8 is C-C schematic cross-section shown in Fig. 7, Fig. 9 Fig. 1 The use state sectional view of top installation magazine of the shown running fire with rifle.
With reference to as shown in figs. 1-9: rifle, including trigger mechanism 110 and dynamical system 120 are matched in a kind of running fire;Trigger mechanism 110 include launcher shell, roller 5 and at least two resilient push, and roller 5 is placed in launcher shell, the side edge of roller 5 Resilient push is arranged in axial direction, and the first sliding rail is equipped in launcher shell, and resilient push is equipped with and protrudes into the first of the first sliding rail Protrusion 61;When dynamical system drives roller 5 to rotate, the first protrusion 61 is slided backward along the first sliding rail, receives resilient push backward Contracting stores power, and when the first protrusion 61 of a resilient push slides to the reverse-running section of the first sliding rail, resilient push stretches forward reset, The shock of hoodle 1 is launched, then, the first protrusion 61 of another resilient push continues to slide to reverse-running section, and it is another to hit running fire One hoodle 1, to realize the running fire of at least two hoodles 1.
With in rifle embodiment, running fire is provided with continuous row with 5 side of roller of rifle altogether for the application Fig. 1-running fire shown in Fig. 9 Six resilient push of column, the structure of six resilient push is identical, all has the first protrusion 61 with the cooperation of the first sliding rail, can be with Realize six 1 running fires of hoodle.Certainly, on the basis of the running fire function of the application, the push rod of other different structures is additionally set, it is real The scheme of now 1 running fire of part hoodle is also within the scope of protection of this application.
Since roller 5 can constantly rotate under the driving of dynamical system 120, thus above-mentioned resilient push shrink store power and The continuous circulating repetition of process of hoodle is hit in stretching, extension, in the case where continuous supplementation hoodle 1, so that it may be realized hoodle running fire, be joined Sectional view shown in Fig. 9 is examined, the magazine 200 that the running fire of the present embodiment is installed with the cooperation of rifle 100 top uses, and magazine 200 is continuously Hoodle 1 is put into running fire in the trigger mechanism of rifle 100, realizes hoodle running fire.
As shown in the trigger mechanism schematic diagram of internal structure of Fig. 3, the side of roller 5 is equipped with one-to-one with resilient push Push rod groove, multiple resilient push are respectively placed in push rod groove.In the present embodiment, push rod groove is evenly arranged with 6, bullet Property push rod be also correspondingly arranged 6, the cross section of push rod groove is semicircle, smooth surface, has and limits and guiding resilient push Effect.
Resilient push includes hoodle push rod 6, spring 10 and sleeve 9.First protrusion 61, rear side are set on hoodle push rod 6 It is additionally provided with the positioning column protruded into inside spring 10.Spring 10 is placed in the rear of hoodle push rod 6, for squeezing hoodle push rod 6 forward, The impact force for hitting transmitting hoodle 1 is provided.Sleeve 9 is sheathed on 10 outside of hoodle push rod 6 and spring, for accommodating, limiting and protect Hoodle push rod 6 and spring 10 are protected, hoodle push rod 6 and spring 10 is avoided to scratch or shake in push rod groove.
With reference to the application Fig. 5-6, in the present embodiment, launcher shell is made of transmitter upper casing 8 and transmitter lower casing 7, First sliding rail is composed of the part sliding rail of transmitter upper casing 8 and transmitter lower casing 7, as shown in fig. 6, the first sliding rail includes position In the first sliding rail top 81 of transmitter upper casing 8, positioned at the first sliding rail lower part 71 of transmitter lower casing 7 and reverse-running section 73.
In addition, transmitter upper casing 8 is additionally provided with hoodle entrance 83, hoodle 1 enters launcher shell from the hoodle entrance 83, sets In the front of hoodle push rod 6.
In the present embodiment, as seen in figs. 5-6, the first sliding rail includes a spiral section, and the head and the tail of spiral section are by being parallel to bullet Property push rod telescopic direction reverse-running section 73 connect (see shown in Fig. 6 transmitter lower casing 7).
The hoodle emission principle for introducing the present embodiment in conjunction with Fig. 5-6 is as follows:
It (is buckled on the transmitter lower casing b on right side after the transmitter upper casing a overturning in left side) with reference to Fig. 6 transmitter upper and lower shell, First protrusion 61 is slided along hollow arrow direction, and the movement of the first protrusion 61 starts from the right end of reverse-running section 73.In turning for roller 5 Under movement is used, the first protrusion 61 is squeezed by the first sliding rail, is slided backward relatively along the first sliding rail, so that hoodle push rod 6 squeezes backward Pressing spring 10 stores power.When the first protrusion 61 slides to the first sliding rail top 81, hoodle 1 enters transmitter shell from hoodle entrance 83 It is interior, it is placed in 6 front of hoodle push rod.Then, the first protrusion 61 continues to slide, and slips back to the first sliding rail lower part 71 from below, finally The left end for sliding into linear reverse-running section 73, since the first protrusion 61 loses extruding at this time, spring 10 discharges potential energy stretching, extension, Emit to which hoodle push rod 6 hits hoodle 1.Hereafter, the first protrusion 61 is repeated the above process from the right end of reverse-running section 73, spring 10 It is in compressive state in the whole process.So circulation, multiple resilient push can successively emit hoodle, realize that hoodle is quick Running fire.
Wherein, the first sliding rail not necessarily uses stringent helicoidal structure, smoothly limits hoodle as long as can be realized Push rod 6 moves backward.
As shown in figure 3, the sleeve 9 of the present embodiment is additionally provided with guide groove 92 and limited block 93, limited block 93 prevents sleeve 9 from existing Rotation in push rod groove, it is final to guide hoodle push rod 6 along being parallel to so that guide groove 92 is that the first protrusion 61 provides guiding role The rectilinear direction of push rod groove is moved forward and backward.
In the present embodiment, the second sliding rail is additionally provided in launcher shell, as shown in Fig. 5-6, the second sliding rail is also by hair The part sliding rail of emitter upper casing 8 and transmitter lower casing 7 is composed, and the second sliding rail includes sliding positioned at the second of transmitter upper casing 8 Rail top 82 and the second sliding rail lower part 72 positioned at transmitter lower casing 7.Sleeve 9 is equipped with the second protrusion 91 for protruding into the second sliding rail. When roller 5 rotates, the second protrusion 91 is slided along the second sliding rail, makes sleeve 9 that hoodle push rod 6 be cooperated to slide back and forth.
Specifically, the position of the corresponding hoodle entrance 83 in the second sliding rail top 82 is recessed backward, so that sleeve 9 cooperates hoodle to push away Bar 6 avoids hoodle 1 and enters, and the position of the corresponding reverse-running section 73 in the second sliding rail lower part 72 is forwardly convex, so that sleeve 9 cooperates hoodle to push away Bar 6 hits hoodle 1 and emits.
In the way of 91 cooperation of second sliding rail and the second protrusion, sleeve 9 is enabled to slide back and forth with hoodle push rod 6, it can It prevents the first protrusion 61 from deviating from from guide groove 92, improves guiding stability.Meanwhile it can not also be taken off guaranteeing the first protrusion 61 Out in the case where guide groove 92, shorten the length of used sleeve 9 as much as possible, mitigates the material weight of sleeve 9.
In the present embodiment, shown in referring to figs. 2 and 5, the front of roller 5 is equipped with multiple transmitting cylinders 4, emits cylinder 4 It is corresponded with resilient push.As shown in figure 8, multiple transmitting cylinders 4 are fixed on roller 5 by transmitting cylinder fixed plate 3, with rolling Cylinder 5 rotates together.Transmitting cylinder fixed plate 3 is tightened on roller 5 by screw 18.
In the present embodiment, as shown in Figures 2 and 3, emit and be equipped with flexible blocking member 2 between cylinder 4 and roller 5, it is flexible Block piece 2 stops hoodle 1 freely to skid off before transmission.As shown in figure 3, flexible blocking member 2 is located at the front of hoodle 1, use is smaller Power stop hoodle 1 freely skid off, when hoodle push rod 6 shock hoodle 1 when, then can overcome the lesser blocking of flexible blocking member 2 Power launches hoodle 1, and flexible blocking member 2 is, for example, silicagel pad etc..
In the present embodiment, as shown in figs. 2,7 and 8, dynamical system includes: motor 13, driving wheel 15 and driven wheel 11, driven wheel 11 is fixed on 5 rear of roller and, motor 13 driving driving wheel 15 rotation coaxial with roller 5, the band under gear drive Dynamic roller 5 rotates.
C-C sectional view as shown in Figure 8, driven wheel 11 are coaxially fixed on 5 rear end of roller and use as bottom plate, 11 court of driven wheel It is additionally provided with the extension bar for protruding into push rod groove one by one to the side of roller 5, assembles spring 10 for playing the role of.Driving wheel 15 It is engaged with driven wheel 11, driving wheel 15 and motor 13 are coaxially connected, and specifically, driving wheel 15 and pin 16 pass through insert injection moulding Mode processes, and motor 13 connect, is attached on dynamical system upper casing 14, dynamical system with driving wheel 15 (including pin 16) close-fitting Lower casing 12 of uniting is connected by buckle and dynamical system upper casing 14, packaging protection driving wheel 15 and motor 13, and the structure after assembling is logical It crosses dynamical system fixed plate 17 to be connected on launcher shell, realizes the assembling of dynamical system 120 and trigger mechanism 110.
In the present embodiment, motor 13 is hollow-cup motor, to mitigate weight, raising driving stabilization of the application running fire with rifle Property and save the energy.Hollow-cup motor is also hollow cup rotor using iron-core-free rotor.This novel rotor structure Completely eliminate as iron core formed vortex and caused by electric energy loss, have energy conservation characteristic outstanding, sensitive convenient control Characteristic and stable operation characteristic, while its weight and rotary inertia are greatly reduced, to reduce the mechanical energy of rotor itself Loss.
Disclosed herein as well is a kind of unmanned plane, which is provided with running fire any one of as above with rifle, to provide nothing Man-machine running fire shows that for dynamical system 120 of the running fire with rifle by software control, unmanned plane is also equipped with remote controler with the running fire of rifle, leads to The switch by key control running fire function of remote controler is crossed, that is, control 13 turns of motor or is not turned.
The above description is merely a specific embodiment, under above-mentioned introduction of the invention, those skilled in the art Other improvement or deformation can be carried out on the basis of the above embodiments.It will be understood by those skilled in the art that above-mentioned tool Body description only preferably explains that the purpose of the present invention, protection scope of the present invention should be subject to the protection scope in claims.

Claims (10)

1. rifle is matched in a kind of running fire, which is characterized in that including trigger mechanism and dynamical system;The trigger mechanism includes outside transmitter Shell, roller and at least two resilient push, the roller are placed in the launcher shell, and the side of the roller is along axial side To the resilient push is arranged, the first sliding rail is equipped in the launcher shell, the resilient push is equipped with and protrudes into described first First protrusion of sliding rail;When the dynamical system drives roller rotation, first protrusion along first sliding rail backward Sliding, makes the resilient push store power to after-contraction, and the first protrusion to a resilient push slides to returning for first sliding rail When journey section, which stretches forward reset, hoodle shock is launched, then, the first of another resilient push is convex It rises and continues to slide to the reverse-running section, hit another hoodle of running fire.
2. rifle is matched in running fire according to claim 1, which is characterized in that first sliding rail includes a spiral section, the spiral shell The head and the tail for revolving section are connected by the reverse-running section for being parallel to the resilient push telescopic direction.
3. rifle is matched in running fire according to claim 1, which is characterized in that the side of the roller is equipped with and the resilient push One-to-one push rod groove, multiple resilient push are respectively placed in the push rod groove.
4. running fire according to claim 3 match rifle, which is characterized in that the resilient push include hoodle push rod, spring and First protrusion is arranged on the hoodle push rod for sleeve, and the spring is placed in hoodle push rod rear, and the sleeve is placed on The hoodle push rod and the spring outwards.
5. rifle is matched in running fire according to claim 4, which is characterized in that the second sliding rail is additionally provided in the launcher shell, The sleeve is equipped with the second protrusion for protruding into second sliding rail, and when roller rotation, second protrusion is along described the The sliding of two sliding rails, makes the sleeve that the hoodle push rod be cooperated to slide back and forth.
6. rifle is matched in running fire according to claim 4, which is characterized in that the sleeve is additionally provided with guide groove and limited block, institute It states guide groove and provides guiding for first protrusion, the limited block prevents the sleeve from rotating in the push rod groove.
7. rifle is matched in running fire according to claim 1, which is characterized in that the front of the roller is equipped with multiple transmitting cylinders, The transmitting cylinder and the resilient push correspond.
8. rifle is matched in running fire according to claim 7, which is characterized in that be equipped between the transmitting cylinder and the roller soft Property block piece, the flexible blocking member stops the hoodle freely to skid off before transmission.
9. rifle is matched in running fire according to claim 1-8, which is characterized in that the dynamical system includes: motor, master Driving wheel and driven wheel, the driven wheel are fixed on the roller rear and, the motor driven described in master coaxial with the roller Wheel rotation drives the roller to rotate under gear drive.
10. a kind of unmanned plane, which is characterized in that the unmanned plane is provided with -9 described in any item running fires according to claim 1 and matches Rifle.
CN201810996118.2A 2018-08-29 2018-08-29 Repeating gun and unmanned aerial vehicle Active CN109141106B (en)

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CN201810996118.2A CN109141106B (en) 2018-08-29 2018-08-29 Repeating gun and unmanned aerial vehicle

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Application Number Priority Date Filing Date Title
CN201810996118.2A CN109141106B (en) 2018-08-29 2018-08-29 Repeating gun and unmanned aerial vehicle

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CN109141106A true CN109141106A (en) 2019-01-04
CN109141106B CN109141106B (en) 2020-08-14

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11796271B1 (en) 2022-08-30 2023-10-24 Florian KOHLI Firing pin release system

Citations (5)

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Publication number Priority date Publication date Assignee Title
US4329907A (en) * 1980-02-04 1982-05-18 General Electric Company Gun bolt for high rate of fire revolving battery guns
CN1910424A (en) * 2003-11-26 2007-02-07 费尔南多·乔治·马尔多纳多·费雷拉·洛佩斯 Childproof and accident-proof rotating percussion handgun
CN1954970A (en) * 2005-10-28 2007-05-02 上海海行机械有限公司 Nailing tool of continuous nailing
CN205808237U (en) * 2016-07-15 2016-12-14 朱广科 A kind of novel running fire catapult
CN206609343U (en) * 2017-02-27 2017-11-03 广州灵动创想文化科技有限公司 A kind of continuous shooting toy gun

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4329907A (en) * 1980-02-04 1982-05-18 General Electric Company Gun bolt for high rate of fire revolving battery guns
CN1910424A (en) * 2003-11-26 2007-02-07 费尔南多·乔治·马尔多纳多·费雷拉·洛佩斯 Childproof and accident-proof rotating percussion handgun
CN1954970A (en) * 2005-10-28 2007-05-02 上海海行机械有限公司 Nailing tool of continuous nailing
CN205808237U (en) * 2016-07-15 2016-12-14 朱广科 A kind of novel running fire catapult
CN206609343U (en) * 2017-02-27 2017-11-03 广州灵动创想文化科技有限公司 A kind of continuous shooting toy gun

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11796271B1 (en) 2022-08-30 2023-10-24 Florian KOHLI Firing pin release system

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Denomination of invention: A continuous firing gun and a drone

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