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 PDFInfo
- 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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- China
- Prior art keywords
- hoodle
- roller
- rifle
- protrusion
- sliding rail
- 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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Links
- 238000005183 dynamical system Methods 0.000 claims abstract description 22
- 230000035939 shock Effects 0.000 claims abstract description 6
- 230000000903 blocking effect Effects 0.000 claims description 9
- 230000005540 biological transmission Effects 0.000 claims description 3
- 238000000034 method Methods 0.000 abstract description 9
- 230000008602 contraction Effects 0.000 abstract 1
- 238000010586 diagram Methods 0.000 description 10
- 230000000694 effects Effects 0.000 description 2
- 238000004880 explosion Methods 0.000 description 2
- 238000005194 fractionation Methods 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 238000005096 rolling process Methods 0.000 description 2
- 239000000243 solution Substances 0.000 description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical group [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 1
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004134 energy conservation Methods 0.000 description 1
- 238000001746 injection moulding Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000004806 packaging method and process Methods 0.000 description 1
- 238000005381 potential energy Methods 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 229910002027 silica gel Inorganic materials 0.000 description 1
- 239000000741 silica gel Substances 0.000 description 1
- 229960001866 silicon dioxide Drugs 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 230000009469 supplementation Effects 0.000 description 1
Classifications
-
- 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
- F41A19/00—Firing or trigger mechanisms; Cocking mechanisms
- F41A19/58—Electric firing mechanisms
- F41A19/64—Electric firing mechanisms for automatic or burst-firing mode
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
Landscapes
- 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
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.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201810996118.2A CN109141106B (en) | 2018-08-29 | 2018-08-29 | Repeating gun and unmanned aerial vehicle |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN201810996118.2A CN109141106B (en) | 2018-08-29 | 2018-08-29 | Repeating gun and unmanned aerial vehicle |
Publications (2)
Publication Number | Publication Date |
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CN109141106A true CN109141106A (en) | 2019-01-04 |
CN109141106B CN109141106B (en) | 2020-08-14 |
Family
ID=64829093
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Application Number | Title | Priority Date | Filing Date |
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CN201810996118.2A Active CN109141106B (en) | 2018-08-29 | 2018-08-29 | Repeating gun and unmanned aerial vehicle |
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Cited By (1)
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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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 |
-
2018
- 2018-08-29 CN CN201810996118.2A patent/CN109141106B/en active Active
Patent Citations (5)
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)
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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CN109141106B (en) | 2020-08-14 |
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Denomination of invention: A continuous firing gun and a drone Effective date of registration: 20231225 Granted publication date: 20200814 Pledgee: Bank of Beijing Limited by Share Ltd. Shanghai branch Pledgor: Goertek Robotics Co.,Ltd. Registration number: Y2023980074084 |
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