CN208291495U - A kind of unmanned plane cradle head mechanism of carry firearms - Google Patents
A kind of unmanned plane cradle head mechanism of carry firearms Download PDFInfo
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- CN208291495U CN208291495U CN201820719481.5U CN201820719481U CN208291495U CN 208291495 U CN208291495 U CN 208291495U CN 201820719481 U CN201820719481 U CN 201820719481U CN 208291495 U CN208291495 U CN 208291495U
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- firearms
- clamping piece
- slide mass
- unmanned plane
- cradle head
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Abstract
The utility model discloses a kind of unmanned plane cradle head mechanisms of carry firearms, including front clamping piece, rear clamping piece, slide mass, firing lock, luffing mechanism, upper plate, two guide rods, two buffer spring groups and two side support plates.Firing lock is connect with firearms, guide rod is symmetrically positioned at left and right sides of firearms, two guide rod Parallel Symmetrics are set at left and right sides of firearms, two equal one end of guide rod are connect with front clamping piece, the other end is connect with rear clamping piece, slide mass covers on two guide rods, it slides along, every guide rod is equipped with a buffer spring group, luffing mechanism one end and the top surface of slide mass are rotatablely connected, the other end and upper plate bottom are connected, and two side support plate Parallel Symmetrics are fixed on the bottom surface of upper plate, and are rotatablely connected with slide mass two sides.The utility model structure is simple, part is easy to process, total quality is small, and the ejection path of firearms is avoided in structure, there is buffer function, reduces influence of the setback-impact to unmanned plane.
Description
Technical field
The utility model belongs to unmanned plane field, and in particular to a kind of unmanned plane cradle head mechanism of carry firearms.
Background technique
Unmanned plane is since its is at low cost, the features such as performance is high, and mobility strong is adaptable using simplicity, hidden safe,
It is widely used in dual-use field.When fight against terrorism and violence and future city are fought at home, guarantee that public security is military
Alert and our soldier life security, it is critically important for reducing injures and deaths.It is a kind of have examine beat integrated function weapon may
It is a more safely and effectively selection.Therefore, it is proposed to a kind of mechanism of the unmanned machine head of carry firearms.
2017, Duke Robotics company was proposed its last word TIKAD tactical drone, supported carry a variety of
Tactical weapon, including M32 grenade launcher, M4 rifle etc..The problem of that there are volumes is larger for its flying platform, and structure is complicated.
The miniaturization of the unmanned machine head of carry firearms, lightness simultaneously reduce the direction that cost is its development.
Summary of the invention
The purpose of this utility model is to provide a kind of unmanned plane cradle head mechanism of carry firearms, solve flat in unmanned plane
Carry firearms on platform, the problem of mitigating recoil, adjusting pitching and aim at.
Realize the technical solution of the utility model aim are as follows: a kind of unmanned plane cradle head mechanism of carry firearms, including
Front clamping piece, rear clamping piece, slide mass, firing lock, luffing mechanism, upper plate, two guide rods, two buffer spring groups
With two side support plates, firing lock is connect with firearms, and two guide rod Parallel Symmetrics are set at left and right sides of firearms, two guide rods
Equal one end is connect with front clamping piece, and the other end is connect with rear clamping piece, and slide mass covers on two guide rods, along its cunning
Dynamic, every guide rod is equipped with a buffer spring group, and each buffer spring group includes two springs, and a spring is located at slide mass
Between the clamping piece of rear, another is located at spring between slide mass and front clamping piece, luffing mechanism one end and sliding
The top surface of body connects, and the other end and upper plate bottom are connected, and two side support plate Parallel Symmetrics are fixed on the bottom surface of upper plate, and
It is rotatablely connected with slide mass two sides.
Compared with prior art, remarkable advantage is the utility model: (1) structure is simple, part is easy to process, whole
Quality is small；(2) shell throwing-out window of firearms is avoided；(3) influence of the setback-impact to unmanned plane is reduced.
Detailed description of the invention
Fig. 1 is the overall structure diagram of the unmanned plane cradle head mechanism of the utility model carry firearms.
Fig. 2 is the slide mass structural schematic diagram of the unmanned plane cradle head mechanism of the utility model carry firearms.
Fig. 3 is the luffing mechanism structural schematic diagram of the unmanned plane cradle head mechanism of the utility model carry firearms.
Specific embodiment
The utility model is described in further detail with reference to the accompanying drawing.
In conjunction with Fig. 1, Fig. 2 and Fig. 3, a kind of unmanned plane cradle head mechanism of carry firearms described in the utility model, including it is preceding
Square clamping piece 1, rear clamping piece 8, slide mass 4, firing lock 9, luffing mechanism 5, the guide rod 3, two of upper plate 6, two buffering
Groups of springs 2 and two side support plates 7.
Firing lock 9 and firearms are connected by bolt, and two 3 Parallel Symmetrics of guide rod are set at left and right sides of firearms, and two
The equal front end of guide rod 3 is connect with front clamping piece 1, and rear end is connect with rear clamping piece 8,4 sets of slide mass on two guide rods 3,
It slides along, every guide rod 3 is equipped with a buffer spring group 2, and each buffer spring group 2 includes two springs, a spring
Between slide mass 4 and rear clamping piece 8, another is located at spring between slide mass 4 and front clamping piece 1, pitching
5 one end of mechanism and the top surface of slide mass 4 are rotatablely connected, and the other end and 6 bottom of upper plate are connected by bolt, two side support plates
7 Parallel Symmetrics are fixed on the bottom surface of upper plate 6, and are rotatablely connected with 4 two sides of slide mass.
The front clamping piece 1 two symmetrical "T"-shaped parts, are provided with semicircular opening in the top surface of "T"-shaped part, "T"-shaped
The lower part of part is provided with first circular hole, and two "T"-shaped parts are horizontal, and two top surfaces are connected by bolt, and semicircle is opened
Mouth cooperatively forms circular hole, and for clamping gun barrel, the first circular hole is protruded into 3 one end of guide rod, and is connected.
The rear clamping piece 8 is "T"-shaped plate, replaces gun stock position, with rifle rear pin connection.
The firing lock 9 is plate, replaces the handle of firearms, is bolted with the casing of firearms.
Luffing mechanism 5 includes pitching motor 5-5, electric machine support 5-4, shaft coupling 5-3, crank 5-2 and connecting rod 5-1.Pitching
Motor 5-5 uses band self-locking function motor, such as Worm reduction motor, and impacting when preventing small arms firing excessive can not consolidate
Determine pitch angle.Pitching motor 5-5 is connected by electric machine support 5-4 with the bottom surface of upper plate 6, and shaft coupling 5-3 is located at electric machine support
The side of 5-4, pitching motor 5-5 are connected by shaft coupling 5-3 with one end of crank 5-2, the other end and connecting rod 5- of crank 5-2
The rotation of 1 one end is hinged, and the other end and slide mass 4 of connecting rod 5-1 rotates hingedly.
The slide mass 4 includes four sliding block 4-2, two U-shaped sliding block connector 4-4, two top link 4-3 and two
A sliding tube 4-1, two top link 4-3 are arranged in parallel, and its top end is respectively symmetrically equipped with protrusion, for the company of connection
Bar 5-1, two U-shaped sliding block connector 4-4 are separately fixed at the front-end and back-end of two top link 4-3, each U-shaped sliding block
The open end lateral wall of connector 4-4 is connected a sliding block 4-2, the both ends sliding tube 4-1 are each passed through be located at positioned at the same side before
Two sliding block 4-2 at end and rear end, sliding tube 4-1 covers on guide rod 3, wherein a spring in the same buffer spring group 2
Between rear end sliding block 4-2 and rear clamping piece 8, another be located at spring be located at front end sliding block 4-2 and front clamping piece 1 it
Between.This structure avoids the lateral shell throwing-out window and bolt handle of firearms.
It can be installed additional on the sliding block 4-2 of 4 left and right sides of slide mass and take aim at tool bracket 10, can installed on taking aim at tool bracket 10
The sighting devices such as small-sized image pickup head or laser sight.
Upper plate 6 can directly be connect with unmanned plane, can also be increased and be circumferentially rotated device.
Principle of the pitch regulation based on four-bar mechanism.When the motor shaft rotation of pitching motor 5-5, firearms, front clamping
Part 1, rear clamping piece 8, guide rod 3, buffer spring 2 and slide mass 4 as a whole, the axis around two 7 lower sections of side support plates
The axis in hole rotates, to realize the function of adjusting pitching.
In shooting course, firing lock 9 pulls the trigger of firearms, fires firearms, the recoil that ballistic projections generate
Move firearms, front clamping piece 1, rear clamping piece 8 and guide rod 3 backward as a whole, two front clamping pieces 1 are with before
Spring between the sliding block 4-2 of end is compressed, and temporarily converts spring potential energy for recoil kinetic energy, is reduced after unmanned plane is subject to
The peak value for sitting impact, realizes the function of buffering.
Claims (7)
1. a kind of unmanned plane cradle head mechanism of carry firearms, it is characterised in that: including front clamping piece (1), rear clamping piece
(8), slide mass (4), firing lock (9), luffing mechanism (5), upper plate (6), two guide rods (3), two buffer spring groups (2)
With two side support plates (7), firing lock (9) is connect with firearms, and two guide rod (3) Parallel Symmetrics are set to firearms or so two
Side, two guide rod (3) one end are connect with front clamping piece (1), and the other end is connect with rear clamping piece (8), slide mass (4)
It covers on two guide rods (3), slides along, every guide rod (3) is equipped with a buffer spring group (2), each buffer spring group
It (2) include two springs, a spring is located between slide mass (4) and rear clamping piece (8), and another is located at spring and is located at cunning
Between kinetoplast (4) and front clamping piece (1), the top surface of luffing mechanism (5) one end and slide mass (4) is rotatablely connected, the other end with
Upper plate (6) bottom is connected, and two side support plate (7) Parallel Symmetrics are fixed on the bottom surface of upper plate (6), and with slide mass (4)
Two sides rotation connection.
2. the unmanned plane cradle head mechanism of carry firearms according to claim 1, it is characterised in that: further include taking aim at tool bracket
(10), the side wall taken aim at tool bracket (10) and be fixed on slide mass (4).
3. the unmanned plane cradle head mechanism of carry firearms according to claim 1, it is characterised in that: the front clamping piece
(1) two symmetrical "T"-shaped part, is provided with semicircular opening in the top surface of "T"-shaped part, the lower part of "T"-shaped part is provided with one first
Circular hole, two "T"-shaped parts are horizontal, and two top surfaces are connected, semicircular opening cooperatively forms circular hole, for clamping gun barrel,
The first circular hole is protruded into guide rod (3) one end, and is connected.
4. the unmanned plane cradle head mechanism of carry firearms according to claim 1, it is characterised in that: the rear clamping piece
(8) it is "T"-shaped plate, replaces gun stock position, with rifle rear pin connection.
5. the unmanned plane cradle head mechanism of carry firearms according to claim 1, it is characterised in that: the firing lock (9)
For plate, replace the handle of firearms, is connect with the casing of firearms.
6. the unmanned plane cradle head mechanism of carry firearms according to claim 1, it is characterised in that: the luffing mechanism (5)
Including pitching motor (5-5), electric machine support (5-4), shaft coupling (5-3), crank (5-2) and connecting rod (5-1), pitching motor (5-
5) it is connected by electric machine support (5-4) with the bottom surface of upper plate (6), shaft coupling (5-3) is located at the side of electric machine support (5-4),
Pitching motor (5-5) is connected by shaft coupling (5-3) with one end of crank (5-2), the other end and connecting rod (5- of crank (5-2)
1) one end is rotatablely connected, and the other end of connecting rod (5-1) is connect with slide mass (4).
7. the unmanned plane cradle head mechanism of carry firearms according to claim 6, it is characterised in that: slide mass (4) packet
Four sliding blocks (4-2), two U-shaped sliding block connectors (4-4), two top links (4-3) and two sliding tubes (4-1) are included,
Two top links (4-3) are arranged in parallel, and its top end is respectively symmetrically equipped with protrusion, for connecting connecting rod (5-1), two
A U-shaped sliding block connector (4-4) is separately fixed at the both ends of two top links (4-3), each U-shaped sliding block connector (4-
4) the connected sliding block (4-2) of open end lateral wall, the both ends sliding tube (4-1) are each passed through two sliding blocks positioned at the same side
(4-2), sliding tube (4-1) cover on guide rod (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820719481.5U CN208291495U (en) | 2018-05-15 | 2018-05-15 | A kind of unmanned plane cradle head mechanism of carry firearms |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820719481.5U CN208291495U (en) | 2018-05-15 | 2018-05-15 | A kind of unmanned plane cradle head mechanism of carry firearms |
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| Publication Number | Publication Date |
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| CN208291495U true CN208291495U (en) | 2018-12-28 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201820719481.5U Active CN208291495U (en) | 2018-05-15 | 2018-05-15 | A kind of unmanned plane cradle head mechanism of carry firearms |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108423188A (en) * | 2018-05-15 | 2018-08-21 | 南京理工大学 | A kind of unmanned plane cradle head mechanism of carry firearms |
| KR102383127B1 (en) * | 2021-11-12 | 2022-04-08 | 최종필 | Rifle recoil absorber for drones |
| WO2023096616A3 (en) * | 2021-11-25 | 2023-08-17 | Asis Elektronik Ve Bilisim Sistemleri Anonim Sirketi | Automatic shooting system with gimbal |
-
2018
- 2018-05-15 CN CN201820719481.5U patent/CN208291495U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108423188A (en) * | 2018-05-15 | 2018-08-21 | 南京理工大学 | A kind of unmanned plane cradle head mechanism of carry firearms |
| CN108423188B (en) * | 2018-05-15 | 2024-05-17 | 南京理工大学 | Unmanned aerial vehicle cloud deck mechanism for mounting firearms |
| KR102383127B1 (en) * | 2021-11-12 | 2022-04-08 | 최종필 | Rifle recoil absorber for drones |
| WO2023096616A3 (en) * | 2021-11-25 | 2023-08-17 | Asis Elektronik Ve Bilisim Sistemleri Anonim Sirketi | Automatic shooting system with gimbal |
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