WO2020244218A1 - 一种开放式机载或车载瞄具 - Google Patents

一种开放式机载或车载瞄具 Download PDF

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Publication number
WO2020244218A1
WO2020244218A1 PCT/CN2019/130413 CN2019130413W WO2020244218A1 WO 2020244218 A1 WO2020244218 A1 WO 2020244218A1 CN 2019130413 W CN2019130413 W CN 2019130413W WO 2020244218 A1 WO2020244218 A1 WO 2020244218A1
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WO
WIPO (PCT)
Prior art keywords
cam
carrier
limit
handwheel
red dot
Prior art date
Application number
PCT/CN2019/130413
Other languages
English (en)
French (fr)
Inventor
孙建华
程学文
Original Assignee
西安华科光电有限公司
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 西安华科光电有限公司 filed Critical 西安华科光电有限公司
Priority to JP2021570228A priority Critical patent/JP7265651B2/ja
Priority to EP19932062.3A priority patent/EP3982078A4/en
Priority to US17/613,032 priority patent/US11841210B2/en
Priority to KR1020217039010A priority patent/KR20220014872A/ko
Publication of WO2020244218A1 publication Critical patent/WO2020244218A1/zh

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G1/00—Sighting devices
    • F41G1/30—Reflecting-sights specially adapted for smallarms or ordnance
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G1/00—Sighting devices
    • F41G1/06—Rearsights
    • F41G1/065—Protection means therefor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G1/00—Sighting devices
    • F41G1/06—Rearsights
    • F41G1/16—Adjusting mechanisms therefor; Mountings therefor
    • F41G1/28—Adjusting mechanisms therefor; Mountings therefor wedge; cam; eccentric
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G1/00—Sighting devices
    • F41G1/32—Night sights, e.g. luminescent
    • F41G1/34—Night sights, e.g. luminescent combined with light source, e.g. spot light
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G1/00—Sighting devices
    • F41G1/32—Night sights, e.g. luminescent
    • F41G1/34—Night sights, e.g. luminescent combined with light source, e.g. spot light
    • F41G1/345—Night sights, e.g. luminescent combined with light source, e.g. spot light for illuminating the sights
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G1/00—Sighting devices
    • F41G1/06—Rearsights
    • F41G1/16—Adjusting mechanisms therefor; Mountings therefor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G1/00—Sighting devices
    • F41G1/46—Sighting devices for particular applications

Definitions

  • the invention relates to an open airborne or vehicle-mounted sight.
  • the purpose of the present invention is to overcome the above-mentioned problems of the existing large-scale open sights.
  • an open type airborne or vehicle-mounted sight including a carrier and an inner red dot module carrier installed on the carrier;
  • the inner red dot module carrier is installed on the top surface of the carrier through a pitch angle adjustment mechanism; the inner red dot module includes an LED light source that can project a graphic logo;
  • the LED light source includes a point light source, a peripheral light source surrounding the point light source, and the peripheral light source is a discontinuous line light source.
  • the pitch angle adjustment mechanism includes a front support assembly, a fulcrum piece and a rear angle adjustment assembly;
  • the front support assembly at least includes a return spring to cooperate with the rear angle adjustment assembly to use the fulcrum member as a rotation fulcrum to realize the angle adjustment of the inner red dot module bearing member;
  • the fulcrum member is a rotating shaft that crosses the shaft hole on the inner red dot module carrier, and two ends of the rotating shaft respectively penetrate the left and right side walls of the carrier;
  • the rear angle adjustment assembly at least includes an angle adjustment cam and an adjustment lever
  • the angle adjustment cam is installed in the cam installation cavity at the rear end of the top surface of the carrier;
  • the cam mounting end of the adjustment operating lever is inserted into the cam mounting cavity from a longitudinal side wall of the cam mounting cavity inward, it is inserted into the mounting shaft hole of the angle adjustment cam; a positioning pin is inserted and opened in The cam limit hole on the circumferential wall of the angle adjustment cam extends to the limit hole opened on the circumferential wall of the cam mounting end to realize the fixation of the angle adjustment cam.
  • the end of the adjustment operating rod placed outside the cam mounting cavity is the operating end, and the end of the operating end has at least a pair of opposite planes; and the circumferential side wall of the operating end is provided with a pair of innermost ends of the opposite planes.
  • a positioning ring with an inner hole adapted to the end is sleeved on the end and the inner side of the positioning ring abuts on the shoulder;
  • a handwheel retaining ring is threadedly connected to the outer end of the positioning ring to achieve a fixed limit on the positioning ring;
  • An empty tubular adjusting handwheel is sleeved on the end, the positioning ring and the handwheel retaining ring, and the inner cavity of the hollow tubular adjusting handwheel has the same cross-section as the positioning ring so as to be engaged with the Relative plane
  • a plurality of positioning posts arranged in the circumferential direction are arranged on the end surface of the inner end of the hollow tubular adjusting handwheel to limit the positions of the plurality of circumferentially arranged positioning posts opened on the outer wall of the cam mounting cavity Hole coordination to realize the circumferential limit of the hollow tubular adjustment handwheel;
  • the outer side of the cavity of the hollow tubular adjusting hand wheel is circular, and a hand wheel spiral spring is placed in the circular cavity and sleeved on the end;
  • the hollow cylindrical part of a handwheel limit sleeve is inserted into the inner hole of the handwheel coil spring, and the ring rib of the handwheel limit sleeve touches the outer diameter of the handwheel coil spring, and the ring stopper
  • the diameter of the side is greater than the inner diameter of the outer side of the cavity of the hollow tubular adjusting handwheel;
  • a handwheel connecting screw passes through the hollow cylinder and is threadedly connected with the screw hole on the end surface of the end portion.
  • a limit pin extending along the axial direction of the angle adjusting cam is arranged between the angle adjusting cam and the cam mounting end to prevent the rotation angle range of the angle adjusting cam.
  • the rear angle adjustment assembly further includes a limiting assembly, which is composed of a threaded pipe section and an extended arc part arranged on the outer side wall of the end of the threaded pipe section, and the positioning column limiting hole is opened in The extended arc part.
  • a limit pin is arranged on the outer ring of the limit assembly part for inserting into the circumferential limit groove on the bottom surface of the positioning ring to limit the rotation angle of the positioning ring.
  • the front support assembly further includes a mounting hole opened at the front end of the top surface of the carrier and a front cover detachably connected to the mounting hole;
  • the bottom surface of the inner red dot module carrier is sequentially provided with front support assembly mounting blind holes, battery compartment matching arc surfaces, and cam arc cavities that are matched with the front support assembly, battery compartment, and cam mounting cavity, respectively, from front to back;
  • the front support assembly further includes a mounting hole opened at the front end of the top surface of the carrier and a front cover plate detachably connected to the mounting hole;
  • the upper end of a dust cover is connected with the front support assembly blind hole screw, the lower end of the dust cover is connected with the front fixing ring, and the front fixing ring is detachably connected with the front cover plate;
  • the return spring and the guide and limit cylinder are both sleeved in the dust cover, and the return spring abuts on the top wall of the blind hole of the front support assembly.
  • the inner red dot module is installed at the end of the inner red dot module carrier, and the front end of the inner red dot module carrier is equipped with a lens through a lens mounting frame;
  • the top surface of the inner red dot module carrier is provided with a solar power generation panel assembly, and at the front and rear positions of the solar power panel assembly, a plurality of transverse corrugated strips are engraved on the top surface of the inner red dot module carrier, To eliminate the adverse effects of environmental stray light;
  • the rear end of the top surface of the carrier is provided with an inner red dot module mounting cavity placed on the rear side of the cam mounting cavity.
  • the end of the cam mounting end is a constricted neck, which is used to engage in the limiting groove on the corresponding side of the cam mounting cavity, and is fixed in the limiting position by screwing an arc-shaped positioning sleeve with ear holes on both sides In the groove; a magnification mirror is provided on the rear end side of the carrier.
  • the shooting meter can be adjusted accurately and conveniently, the adjustment of the trajectory can be completed, the operation is simple, and the rapid shooting is not affected.
  • Figure 1 is a top view of an open airborne or vehicle-mounted sight.
  • Figure 2 is a rear view of an open airborne or vehicle-mounted sight.
  • Figure 3 is a rear-oblique bird's-eye view of an open airborne or vehicle-mounted sight.
  • Figure 4 is an axial cross-sectional view of an open airborne or vehicle-mounted sight.
  • Figure 5 is an axial sectional view of the carrier.
  • Fig. 6 is a schematic diagram of the disassembly of the rear angle adjustment assembly.
  • Figure 7 is an overall view of the rear angle adjustment assembly.
  • Figure 8 is a schematic diagram of an open airborne or vehicle-mounted sighting device side limit hole setting.
  • Figure 9 is a schematic diagram of the partial construction and disassembly of the carrier.
  • Figure 10 is an axial cross-sectional view of the inner red dot module carrier.
  • Figure 11 is a structural disassembly diagram of the inner red dot module carrier.
  • Figure 12 is a structural diagram of the top block.
  • Fig. 13 is a split view when the rear angle adjustment assembly is placed vertically.
  • Figure 14 is a schematic diagram of the coordination between the positioning ring and the limit pin.
  • this embodiment provides an open type airborne or vehicle-mounted sight shown in FIGS. 1 to 3, which includes a carrier 1 (or referred to as To install the main body) and the inner red dot module carrier 2 installed on the carrier 1, the inner red dot module carrier 2 is installed on the top surface of the carrier 1 through the pitch angle adjustment mechanism, so that it can pass Adjust the angle of the inner red dot module carrier 2 to adjust the exit direction of the inner red dot sight, and complete the adjustment of the shooting table, that is, the adjustment of the trajectory.
  • a carrier 1 or referred to as To install the main body
  • the inner red dot module carrier 2 installed on the carrier 1 through the pitch angle adjustment mechanism, so that it can pass Adjust the angle of the inner red dot module carrier 2 to adjust the exit direction of the inner red dot sight, and complete the adjustment of the shooting table, that is, the adjustment of the trajectory.
  • the inner red dot module includes an LED light source capable of projecting graphic marks; the LED light source includes a point light source, a peripheral light source surrounding the point light source, and the peripheral light source is a discontinuous line light source. Therefore, specific reticle patterns can be projected, and the method of adding an aperture in front of the surface light source in the prior art can be overcome to obtain the defects of projected differentiation icons, complex structure and high power consumption.
  • a magnifying mirror 46 is provided on the rear end side of the carrier 1, that is, the upper right end shown in FIG. 1 or the right rear end shown in FIG.
  • the front end of the supporting member 1, that is, the left end shown in FIG. 1 is provided with a supporting frame 48.
  • the left and right outer side walls of the supporting frame 48 are each equipped with a Pilcatini guide rail 47 for installing sights or other auxiliary tools to realize the function Extension.
  • the pitch angle adjustment mechanism includes a front support assembly 3, a fulcrum piece, and a rear angle adjustment assembly 5, thereby forming a fulcrum piece Leverage effect, wherein the front support assembly 3 includes at least a return spring 25 to cooperate with the rear angle adjustment assembly 5 with a fulcrum piece (the fulcrum piece is a rotating shaft that passes through the shaft hole 4 on the inner red dot module carrier 2 transversely, the The two ends of the rotating shaft respectively penetrate the left and right side walls of the bearing member 1, that is, the rotating shaft passes through the bearing member 1 and the inner red dot module bearing member 2 laterally, or by installing ball sleeves on the left and right side walls of the bearing member 1.
  • the front end of the inner red dot module carrier 2 is mounted with a lens 39 through the lens mounting frame 38 as shown in FIG. 11, and is used in conjunction with the inner red dot module 37.
  • the top surface of the inner red dot module carrier 2 provided in this embodiment is provided with a solar power generation panel assembly 40, and at the front and rear of the solar power panel assembly 40, the inner red dot module carrier 2 A number of transverse corrugated strips 41 are engraved on the top surface to eliminate the adverse effects of ambient stray light; and from Figure 9 it can be seen that the end of the top surface of the carrier 1 is provided with an inner red dot on the rear side of the cam mounting cavity 8 Module installation cavity 42.
  • the fulcrum member 4 provided in this embodiment is composed of arc-shaped ribs provided on the carrier 1, so as to be similar to the inner red dot module carrier 2 shown in FIG.
  • the fulcrum on the bottom surface matches the curved surface 32 for use.
  • the angle adjustment assembly 5 as shown in FIG. 6 includes at least an angle adjustment cam 6 and an adjustment operation lever 7; the angle adjustment cam 6 is installed in the cam mounting cavity 8 at the end of the top surface of the carrier 1; the adjustment operation lever 7 After the cam mounting end 9 is inserted into the cam mounting cavity 8 from a longitudinal side wall of the cam mounting cavity 8 inward, it is inserted into the mounting shaft hole 10 of the angle adjusting cam 6; a positioning pin 11 is inserted into the angle adjusting cam 6 The cam limit hole 12 on the circumferential wall of the cam is extended to the limit hole 13 opened on the circumferential wall of the cam mounting end 8 to realize the fixation of the angle adjustment cam 6.
  • a handwheel coil spring 20 is placed in the circular cavity and sleeved on the end of the operating end 14; the hollow cylindrical part of the handwheel limit sleeve 21 is inserted into the inner hole of the handwheel coil spring 20 , And the ring rib of the handwheel limit sleeve 21 touches the outer diameter of the handwheel coil spring 20, and the diameter of the ring rib is larger than the inner diameter of the cavity outside of the hollow tubular adjusting handwheel 18; a handwheel After passing through the hollow cylinder, the connecting screw 22 is threadedly connected with the threaded hole on the end surface of the end. The outer end surface of the hollow tubular adjusting handwheel 18 is threadedly connected to the handwheel blocking cover 23, which has a protective effect.
  • a limit pin 24 extending axially along the angle adjustment cam 6 is arranged between the angle adjustment cam 6 and the cam mounting end 9 in this embodiment to limit the rotation angle range of the angle adjustment cam 6 , That is, prevent the angle adjusting cam 6 from continuing to rotate beyond the angle at which the limit pin 24 is located.
  • this embodiment further includes a limit assembly 30 shown in FIGS. 7 and 8 on the basis of the foregoing embodiment, the limit assembly 30 30 is composed of a threaded pipe section and an extended arc portion arranged on the outer side wall of the end of the threaded pipe section, and the positioning pillar limiting hole 29 mentioned in the foregoing embodiment is opened on the extended arc portion.
  • the hollow tube adjustment handwheel 18 is pushed by the handwheel coil spring 20 to keep the positioning column 19 always inserted into the positioning column limit hole 29, so as to effectively prevent the hollow tube adjustment handwheel 18 from rotating when touched by external forces.
  • the rotation of the hollow tubular adjusting handwheel 18 can be realized to realize the angle adjustment cam.
  • the pitch angle of the red dot module carrier 2 is adjusted to complete the adjustment of the exit angle of the inner red dot module, thereby changing the shooting trajectory.
  • the hollow tube adjustment handwheel 18 is engraved on the outer surface Shooting table (dial) for easy and precise operation.
  • the present embodiment is provided with a limit pin 53 shown in FIGS. 8 and 13 on the outer ring of the limit assembly 30 for inserting into the position shown in FIG. 14
  • the shown positioning ring 16 is located in the circumferential limit groove 54 on the bottom surface of the positioning ring 16 to limit the rotation angle of the positioning ring 16 so as to effectively limit the rotation angle range of the hollow tube adjustment handwheel 18.
  • the end of the cam mounting end 9 is a constricted portion 43, which is used to engage in the limiting groove 44 on the corresponding side of the cam mounting cavity 8 (specifically, the end away from the hollow tubular adjusting handwheel 18) , And an arc-shaped positioning sleeve 45 with ear holes on both sides is fixed in the limiting groove 44 by screws, which more stably realizes the fixation of the cam mounting end 9 and ensures the balance and stability of operation.
  • the bottom surface of the inner red dot module carrier 2 can be seen from Fig. 10, from the front to the back are provided with front support assembly mounting blind holes 31 and battery compartment matching respectively with the front support assembly 3, the battery compartment 52, and the cam mounting cavity 8.
  • the arc-shaped surface 32 and the cam arc-shaped cavity 33 can realize the matching installation of the inner red dot module carrier 2 and the carrier 1 in this way.
  • the front support assembly 3 can be seen from FIG. 9 and further includes a mounting hole 26 opened at the front end of the top surface of the carrier 1 and a front cover 27 detachably connected to the mounting hole 26; and the aforementioned return spring 25 is two , The lower ends of the two return springs 25 are inserted side by side into the two guiding and limiting cylinders 28 arranged on the top surface of the front cover 27 and higher than the top surface of the carrier 1.
  • a dust cover 34 matched with the front support assembly 3 is shown in FIG. 11, the upper end of which is screwed to the front support assembly mounting blind hole 31, the lower end of the dust cover 34 is connected to the front fixing ring 35, the front fixing ring 35 and The front cover 27 is detachably connected, specifically by screw connection.
  • the return spring 25 and the guide limit cylinder 28 are all sleeved in the dust cover 34, and the return spring 25 abuts on the top wall of the blind hole 31 of the front support assembly.
  • the pitch angle of the inner red dot module carrier 2 can be adjusted under the action of the angle adjustment cam 6, that is, when the highest point of the angle adjustment cam 6 is rising, the rear of the inner red dot module carrier 2
  • the highest point of the angle adjustment cam 6 drops, the front end of the inner red dot module carrier 2 is lifted under the action of the return spring 25 to complete the pitch angle of the inner red dot module carrier 2 Adjustment.
  • the back side of the cam arc cavity 33 is provided with a top block 36 as shown in FIG. 12 to resist against the circumferential surface of the adjusting cam 6 when the adjusting cam 6 rotates, which is lower than the cam , It can stabilize the rotation of the cam, and at the same time reduce the friction caused by shaking and prolong the service life.
  • the top block 36 mainly includes an arc-shaped end at the front end, and the front and bottom surfaces of the arc-shaped end are mutually perpendicular planes, namely a vertical surface and a horizontal plane, and the arc-shaped surface is Connecting the vertical plane and the horizontal plane, the horizontal part of the top block 36 is placed at the rear end of the arc-shaped end, and is mainly used to fix the top block 36 on the back side of the cam arc-shaped cavity 33 by screws.
  • this embodiment specifically passes through the bearing member 1 through the two symmetrically installed spring pins 51 shown in FIG. 2 and FIG.
  • the side walls of the inner red dot module bear against the left and right outer walls of the inner red dot module carrier 2 to ensure the stability during the pitch angle adjustment of the inner red dot module carrier 2.

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  • Physics & Mathematics (AREA)
  • Optics & Photonics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Fittings On The Vehicle Exterior For Carrying Loads, And Devices For Holding Or Mounting Articles (AREA)
  • Pivots And Pivotal Connections (AREA)
  • Non-Portable Lighting Devices Or Systems Thereof (AREA)
  • Mutual Connection Of Rods And Tubes (AREA)
  • Lighting Device Outwards From Vehicle And Optical Signal (AREA)

Abstract

一种开放式机载或车载瞄具，包括承载件（1）和安装在该承载件（1）上的内红点模组承载件（2）；内红点模组承载件（2）通过俯仰角调整机构安装在所述承载件（1）顶面。内红点模组，包括可投射图形标识的LED光源；LED光源包括点光源，环绕在该点光源周围的周边光源，且该周边光源为非连续线光源。该开放式机载或车载瞄具可以精准、方便的调整射表，完成弹道的调整，操作简便，不影响快速射击，且功耗低。

Description

一种开放式机载或车载瞄具 技术领域
本发明涉及一种开放式机载或车载瞄具。
背景技术
现有的车载或机载瞄具具有体积大，瞄射角度宽的要求，同时对于不同的射击距离及相应的弹道有对应的要求，需要调整内红点瞄点的出射角度，现有大型开放式瞄具红点模组承载件部分外露在支架以上，没有必要的保护，在受到碰撞后，结构或多或少会受到损坏，从而影响瞄准精度。同时，光源部分传统瞄镜采用在面光源前增加光栏的方式，得到投射分化图标，此方式带来很大的功耗消耗。
发明内容
本发明的目的是克服现有的大型开放式瞄具存在的上述问题。
为达上述目的，一种开放式机载或车载瞄具，包括承载件和安装在该承载件上的内红点模组承载件；
所述内红点模组承载件通过俯仰角调整机构安装在所述承载件顶面；内红点模组，包括可投射图形标识的LED光源；
所述LED光源包括点光源，环绕在该点光源周围的周边光源，且该周边光源为非连续线光源。
俯仰角调整机构包括前支撑组件、支点件和后角度调整组件；
所述前支撑组件至少包括一复位弹簧，以配合所述后角度调整组件以所述支点件为转动支点、实现对所述内红点模组承载件的角度调整；
所述支点件为横向穿过所述内红点模组承载件上的轴孔的转轴，该转轴的两端分别穿透所述承载件的左右侧壁；
所述后角度调整组件至少包括一角度调节凸轮、一调节操作杆；
所述角度调节凸轮安装在所述承载件的顶面尾端的凸轮安装腔内；
所述调节操作杆的凸轮安装端自所述凸轮安装腔的一纵向侧壁外向内插入至该凸轮安装腔内后，插入所述角度调节凸轮的安装轴孔内；一定位顶销插入开设在所述角度调节凸轮的周向壁上的凸轮限位孔后延伸至开设在所述凸轮安装端的周向壁上的限位孔内实现对角度调节凸轮的固定。
调节操作杆置于所述凸轮安装腔外的一端为操作端，该操作端的端部具有至少一对相对平面；且该操作端的周向侧壁上于所述相对平面的最内端设置一对台肩；
一具有与所述端部相适配的内孔的定位圈套设在所述端部且定位圈的内侧抵触在所述台肩上；
一手轮挡圈螺纹连接在所述定位圈外侧的端部上，实现对所述定位圈的固定限位；
一空管状调节手轮套设在所述端部、定位圈和手轮挡圈上，且所述空管状调节手轮的空腔内侧为与所述定位圈相同的截面，从而卡合在所述相对平面上；
所述空管状调节手轮的内端端部的端面上设置有多个沿周向排列的定位柱，用以与开设在所述凸轮安装腔外壁上的多个呈圆周排列的定位柱限位孔配合，实现对空管状调节手轮的周向限位；
所述空管状调节手轮的空腔外侧为圆形，一手轮螺旋弹簧置于该圆形腔内、并套设在所述端部上；
一手轮限位套的空心圆柱部插入所述手轮螺旋弹簧的内孔、且该手轮限位套的圆环挡边触压在所述手轮螺旋弹簧外径上，且该圆环挡边的直径大于所述空管状调节手轮的空腔外侧的内径；
一手轮连接螺钉穿过所述空心圆柱后与所述端部的端面上的螺孔螺纹联接。
角度调节凸轮与凸轮安装端之间设置有沿角度调节凸轮轴向延伸的限位销，以阻止角度调节凸轮的转动角度范围。
所述后角度调整组件还包括一限位装配件，该限位装配件由螺纹管段和设置在该螺纹管段端部的外侧壁上的外延弧形部构成，所述定位柱限位孔开设在该外延弧形部上。
所述限位装配件的外圈上设置一限位柱销，用以插入所述定位圈的底面上周向限位槽内，以实现对所述定位圈的转动角度的限制。
前支撑组件还包括开设在所述承载件顶面前端的安装孔和与该安装孔可拆卸连接的前盖板；
所述复位弹簧是两个，该两个复位弹簧的下端并排插入设置在所述前盖板的顶面上且高出所述承载件顶面的两个导向限位筒内。
内红点模组承载件的底面自前向后依次设置有分别与前支撑组件、电池仓、凸轮安装腔配合的前支撑组件安装盲孔、电池仓匹配弧形面、凸轮弧形腔；
所述前支撑组件还包括开设在所述承载件顶面前端的安装孔和与该安装孔可拆卸连接的前盖板；
所述复位弹簧是两个，该两个复位弹簧的下端并排插入设置在所述前盖板的顶面上且高出所述承载件顶面的两个导向限位筒内；
一防尘套的上端与所述前支撑组件安装盲孔螺钉连接，该防尘套下端与前固定圈连接，该前固定圈与所述前盖板可拆卸连接；
所述复位弹簧、导向限位筒均套设在所述防尘套内，且所述复位弹簧抵触在所述前支撑组件安装盲孔的顶壁上。
所述内红点模组承载件的尾端安装内红点模组，内红点模组承载件的前端通过 透镜安装框架安装透镜；
所述内红点模组承载件的顶面设置有太阳能发电板组件，且于该太阳能发电板组件的前后部位，所述内红点模组承载件的顶面刻设多条横向楞条，用以消除环境杂光的不利影响；
所述承载件的顶面尾端开设有置于所述凸轮安装腔后侧的内红点模组安装腔。
所述凸轮安装端的末端为一缩颈部，用以卡合在所述凸轮安装腔的相应侧的限位凹槽内，并通过螺钉连接一两侧具有耳孔的弧形定位套固定在限位凹槽内；所述承载件的尾端一侧设置有倍率镜。
本发明的优点是：可以精准、方便的调整射表，完成弹道的调整，操作简便，不影响快速射击。
下面结合附图和实施例对本发明做详细说明。
附图说明
图1是一种开放式机载或车载瞄具俯视图。
图2是一种开放式机载或车载瞄具后视图。
图3是一种开放式机载或车载瞄具后斜鸟瞰图。
图4是一种开放式机载或车载瞄具轴向剖视图。
图5是承载件轴向剖视图。
图6是后角度调整组件拆分示意图。
图7是后角度调整组件整体图。
图8是一种开放式机载或车载瞄具侧限位孔设置示意图。
图9是承载件局部构建拆分示意图。
图10是内红点模组承载件轴向剖视图。
图11是内红点模组承载件的结构分拆图。
图12是顶块结构图。
图13是后角度调整组件竖直放置时拆分图。
图14是定位圈与限位柱销配合示意图。
附图标记说明：
1、承载件；2、内红点模组承载件；3、前支撑组件；4、支点件；5、后角度调整组件；6、角度调节凸轮；7、调节操作杆；8、凸轮安装腔；9、凸轮安装端；10、安装轴孔；11、定位顶销；12、凸轮限位孔；13、限位孔；14、操作端；15、相对平面；16、定位圈；17、手轮挡圈；18、空管状调节手轮；19、定位柱；20、手轮螺旋弹簧；21、手轮限位套；22、手轮连接螺钉；23、手轮堵盖；24、限位销；25、复位弹簧；26、安装孔；27、前盖板；28、导向限位筒；29、定位柱限位孔；30、限位装配件；31、安装盲孔；32、支点匹配弧形面；33、凸轮弧形腔；34、防尘套；35、前固定圈；36、顶块；37、内红点模组；38、透镜安装框架；39、透镜；40、太阳能发电板组件；41、横向楞条；42、内红点模组安装腔；43、缩颈部；44、限位凹槽；45、弧形定位套；46、倍率镜；47、皮尔卡汀尼导轨；48、支撑框架；49、档位槽；50、台肩；51、弹簧顶销；52、电池仓；53、限位柱销；54、周向限位槽；55、定位柱安装孔。
具体实施方式
为了方便和更精准的调整内红点瞄具的出射角度或方向，本实施例提供了一种图1至图3所示的开放式机载或车载瞄具，包括承载件1(或称之为安装主体)和安装在该承载件1上的内红点模组承载件2，内红点模组承载件2通过俯仰角调整机构安装在承载件1顶面，如此一来，便可通过对内红点模组承载件2的角度调整而实现对内红点瞄具的出射方向的调整，完成射表的调整即弹道的调整。内红点模组，包括可投射图形标识的LED光源；LED光源包括点光源，环绕在该点光源周围的周边光源，且该周边光源为非连续线光源。从而可以投射具体的分划图案，克服现有技术中的面光源前增加光栏的方式，得到投射分化图标，结构复杂且功耗高的缺陷。
由图1或图2清晰可见，承载件1的后端一侧即图1所示的右端上侧或图2所示的后端右侧设置有倍率镜46，用以辅助瞄准。而承载件1的前端即图1所示的左端设置有支撑框架48，该支撑框架48的左右外侧壁上各安装一皮尔卡汀尼导轨47， 用以安装瞄具或其他辅助用具，实现功能的扩展。
本实施例主要是关于俯仰角调整机构进行展开说明，具体参见图4至图11，该俯仰角调整机构包括前支撑组件3、支点件和后角度调整组件5，从而形成以支点件为支点的杠杆效用，其中，前支撑组件3至少包括一复位弹簧25，以配合后角度调整组件5以支点件(支点件为横向穿过内红点模组承载件2上的轴孔4的转轴，该转轴的两端分别穿透承载件1的左右侧壁，即转轴横向穿过承载件1和内红点模组承载件2，也可以是通过在承载件1的左右侧壁上安装球套，主要起到联接承载件1的侧壁与相应的内红点模组承载件2的侧壁，且具有轴承的效用，如此可以确保以该左右侧壁的球套为支点完成俯仰角转动调整；)为转动支点、实现对内红点模组承载件2的角度调整即俯仰角的调整，完成对安装在内红点模组承载件2的尾端的内红点模组37的出射光的角度调整，完成弹道辅助射击的调整。而内红点模组承载件2的前端如图11所示通过透镜安装框架38安装透镜39，与内红点模组37配合使用。
为了节约电池电能，本实施例提供的内红点模组承载件2的顶面设置有太阳能发电板组件40，且于该太阳能发电板组件40的前后部位，内红点模组承载件2的顶面刻设多条横向楞条41，用以消除环境杂光的不利影响；而借由图9可知，承载件1的顶面尾端开设有置于凸轮安装腔8后侧的内红点模组安装腔42。
借由图4和图5可知，本实施例中提供的支点件4由设置在承载件1上的弧形凸棱构成，从而与图10所示的开设在内红点模组承载件2的底面上的支点匹配弧形面32配合使用。
而后角度调整组件5如图6所示，至少包括一角度调节凸轮6、一调节操作杆7；角度调节凸轮6安装在承载件1的顶面尾端的凸轮安装腔8内；调节操作杆7的凸轮安装端9自凸轮安装腔8的一纵向侧壁外向内插入至该凸轮安装腔8内后，插入 角度调节凸轮6的安装轴孔10内；一定位顶销11插入开设在角度调节凸轮6的周向壁上的凸轮限位孔12后延伸至开设在凸轮安装端8的周向壁上的限位孔13内实现对角度调节凸轮6的固定。
由图9清晰可见，其中，调节操作杆7置于凸轮安装腔8外的一端为操作端14(结合图6所示)，该操作端14的端部具有至少一对相对平面15；且该操作端14的周向侧壁上于相对平面15的最内端设置一对台肩50；一具有与操作端14的端部相适配的内孔的定位圈16套设在操作端14的端部且定位圈16的内侧抵触在台肩50上；一手轮挡圈17螺纹连接在定位圈16外侧的端部上，实现对定位圈16的固定限位；一空管状调节手轮18套设在端部、定位圈16和手轮挡圈17上，且空管状调节手轮18的空腔内侧为与定位圈16相同的截面，从而卡合在相对平面15上；空管状调节手轮18的内端端部的端面上设置有多个沿周向排列的定位柱19(具体是通过图13所示的空管状调节手轮18底面的定位柱安装孔55，一般是螺孔，螺纹联接)，用以与开设在凸轮安装腔8外壁上的多个呈圆周排列的定位柱限位孔29配合，实现对空管状调节手轮18的周向限位；空管状调节手轮18的空腔外侧为圆形，一手轮螺旋弹簧20置于该圆形腔内、并套设在操作端14的端部上；一手轮限位套21的空心圆柱部插入手轮螺旋弹簧20的内孔、且该手轮限位套21的圆环挡边触压在手轮螺旋弹簧20外径上，且该圆环挡边的直径大于空管状调节手轮18的空腔外侧的内径；一手轮连接螺钉22穿过空心圆柱后与端部的端面上的螺孔螺纹联接，空管状调节手轮18的外端端面上螺纹联接手轮堵盖23，具有防护作用。
通过上述的零部件的组合，实现了通过转动空管状调节手轮18即可实现对角度调节凸轮6的转动。
为了确保角度调节凸轮6可靠转动，本实施例在角度调节凸轮6与凸轮安装端9 之间设置有沿角度调节凸轮6轴向延伸的限位销24，以限制角度调节凸轮6的转动角度范围，即阻止角度调节凸轮6越过该限位销24所在的角度继续转动。
同时，为了避免意外碰触空管状调节手轮18而导致转动，本实施例在前述实施方式的基础上，还包括一图7和图8所示的限位装配件30，该限位装配件30由螺纹管段和设置在该螺纹管段端部的外侧壁上的外延弧形部构成，而前述实施例中提及的定位柱限位孔29则开设在该外延弧形部上。如此以来，空管状调节手轮18在手轮螺旋弹簧20的推挤下，保持定位柱19始终插入定位柱限位孔29内，从而有效防止空管状调节手轮18受外力触碰发生转动，而只有当外力沿轴向向外拉拔空管状调节手轮18直至将定位柱19从定位柱限位孔29内拉出后才能实现空管状调节手轮18的转动，进而实现对角度调节凸轮6的转动，当角度调节凸轮6的最高点顶触内红点模组承载件2的后端底面，使得内红点模组承载件2后端抬升，从而绕支点件4转动，实现对内红点模组承载件2的俯仰角的调整，进而完成对内红点模组的出射角度的调整，从而改变射击弹道，与之对应的是，空管状调节手轮18的外表面上刻设射表(刻度盘)，便于精准操作。
而为了防止空管状调节手轮18超过360度的转动角，本实施在限位装配件30的外圈上设置一图8及图13所示的限位柱销53，用以插入图14所示的定位圈16的底面上周向限位槽54内，以实现对定位圈16的转动角度的限制，从而有效限制空管状调节手轮18的转动角度范围。
由图9可见，凸轮安装端9的末端为一缩颈部43，用以卡合在凸轮安装腔8的相应侧的限位凹槽44内(具体是远离空管状调节手轮18的一端)，并通过螺钉连接一两侧具有耳孔的弧形定位套45固定在限位凹槽44内，更稳固的实现对凸轮安装端9的固定，确保操作的平衡性和稳定性。
而内红点模组承载件2的底面由图10可知，自前向后依次设置有分别与前支撑组件3、电池仓52、凸轮安装腔8配合的前支撑组件安装盲孔31、电池仓匹配弧形面32、凸轮弧形腔33，如此便可实现内红点模组承载件2与承载件1的匹配安装。
其中，前支撑组件3借由图9可知，还包括开设在所述承载件1顶面前端的安装孔26和与该安装孔26可拆卸连接的前盖板27；而前述复位弹簧25是两个，该两个复位弹簧25的下端并排插入设置在前盖板27的顶面上且高出承载件1顶面的两个导向限位筒28内。
与前支撑组件3配合的一防尘套34如图11所示，其上端与前支撑组件安装盲孔31螺钉连接，该防尘套34下端与前固定圈35连接，该前固定圈35与前盖板27可拆卸连接，具体是采用螺钉连接。
而复位弹簧25、导向限位筒28均套设在防尘套34内，且复位弹簧25抵触在前支撑组件安装盲孔31的顶壁上。这样，便可在角度调节凸轮6的作用下实现对内红点模组承载件2的俯仰角的调整，即当角度调节凸轮6的最高点在上升时，内红点模组承载件2后端被顶起，而当角度调节凸轮6的最高点下降时，内红点模组承载件2的前端在复位弹簧25的作用下抬起，从而完成内红点模组承载件2的俯仰角的调整。
由图10可知，凸轮弧形腔33的后侧设置有一图12所示的顶块36，用以在调节凸轮6转动时抵触在调节凸轮6的周向面上，该周向面比凸轮低，可以很好的稳定凸轮的转动，同时能减少晃动产生的摩擦，延长使用寿命。
由图12清晰可见，顶块36主要包括前端的弧形端部，且该弧形端部的前侧面和底面为相互垂直的平面，即一个竖直面和一个水平面，而其弧形面则连接竖直面和水平面，顶块36的水平部则置于弧形端部的后端，主要用于通过螺钉实现将该顶 块36固定在凸轮弧形腔33的后侧。
为了方便档位调节，结合图7和图9可知，本实施例在台肩50左侧的操作端14的端部外壁上开设有多个周向对应限位孔29的档位槽49，提升管状调节手轮18的操作的平稳性。
而为了确保内红点模组承载件2在俯仰角的调整过程中的平稳性，本实施例特通过图2和图3所示的两个对称安装的弹簧顶销51，穿过承载件1的侧壁后抵触在内红点模组承载件2的左右外壁上，从而确保内红点模组承载件2的俯仰角调整过程中的稳定性。

Claims (10)

  1. 一种开放式机载或车载瞄具，其特征在于：包括承载件(1)和安装在该承载件(1)上的内红点模组承载件(2)；
    所述内红点模组承载件(2)通过俯仰角调整机构安装在所述承载件(1)顶面；
    内红点模组，包括可投射图形标识的LED光源；
    所述LED光源包括点光源，环绕在该点光源周围的周边光源，且该周边光源为非连续线光源。
  2. 如权利要求1所述的开放式机载或车载瞄具，其特征在于：所述俯仰角调整机构包括前支撑组件(3)、支点件和后角度调整组件(5)；
    所述前支撑组件(3)至少包括一复位弹簧(25)，以配合所述后角度调整组件(5)以所述支点件为转动支点、实现对所述内红点模组承载件(2)的角度调整；
    所述支点件为横向穿过所述内红点模组承载件(2)上的轴孔(4)的转轴，该转轴的两端分别穿透所述承载件(1)的左右侧壁；
    所述后角度调整组件(5)至少包括一角度调节凸轮(6)、一调节操作杆(7)；
    所述角度调节凸轮(6)安装在所述承载件(1)的顶面尾端的凸轮安装腔(8)内；
    所述调节操作杆(7)的凸轮安装端(9)自所述凸轮安装腔(8)的一纵向侧壁外向内插入至该凸轮安装腔(8)内后，插入所述角度调节凸轮(6)的安装轴孔(10)内；一定位顶销(11)插入开设在所述角度调节凸轮(6)的周向壁上的凸轮限位孔(12)后延伸至开设在所述凸轮安装端(8)的周向壁上的限位孔(13)内实现对角度调节凸轮(6)的固定。
  3. 如权利要求2所述的开放式机载或车载瞄具，其特征在于：所述调节操作杆(7)置于所述凸轮安装腔(8)外的一端为操作端(14)，该操作端(14)的端部具 有至少一对相对平面(15)；且该操作端(14)的周向侧壁上于所述相对平面(15)的最内端设置一对台肩；
    一具有与所述端部相适配的内孔的定位圈(16)套设在所述端部且定位圈(16)的内侧抵触在所述台肩上；
    一手轮挡圈(17)螺纹连接在所述定位圈(16)外侧的端部上，实现对所述定位圈(16)的固定限位；
    一空管状调节手轮(18)套设在所述端部、定位圈(16)和手轮挡圈(17)上，且所述空管状调节手轮(18)的空腔内侧为与所述定位圈(16)相同的截面，从而卡合在所述相对平面(15)上；
    所述空管状调节手轮(18)的内端端部的端面上设置有多个沿周向排列的定位柱(19)，用以与开设在所述凸轮安装腔(8)外壁上的多个呈圆周排列的定位柱限位孔(29)配合，实现对空管状调节手轮(18)的周向限位；
    所述空管状调节手轮(18)的空腔外侧为圆形，一手轮螺旋弹簧(20)置于该圆形腔内、并套设在所述端部上；
    一手轮限位套(21)的空心圆柱部插入所述手轮螺旋弹簧(20)的内孔、且该手轮限位套(21)的圆环挡边触压在所述手轮螺旋弹簧(20)外径上，且该圆环挡边的直径大于所述空管状调节手轮(18)的空腔外侧的内径；
    一手轮连接螺钉(22)穿过所述空心圆柱后与所述端部的端面上的螺孔螺纹联接。
  4. 如权利要求3所述的开放式机载或车载瞄具，其特征在于：所述角度调节凸轮(6)与凸轮安装端(9)之间设置有沿角度调节凸轮(6)轴向延伸的限位销(24)，以阻止角度调节凸轮(6)转动角度范围。
  5. 如权利要求3所述的开放式机载或车载瞄具，其特征在于：所述后角度调整组件还包括一限位装配件(30)，该限位装配件(30)由螺纹管段和设置在该螺纹管段端部的外侧壁上的外延弧形部构成，所述定位柱限位孔(29)开设在该外延弧形部上。
  6. 如权利要求5所述的开放式机载或车载瞄具，其特征在于：所述限位装配件(30)的外圈上设置一限位柱销(53)，用以插入所述定位圈(16)的底面上周向限位槽(54)内，以实现对所述定位圈(16)的转动角度的限制。
  7. 如权利要求1或2或3或4或5或6所述的开放式机载或车载瞄具，其特征在于：所述前支撑组件(3)还包括开设在所述承载件(1)顶面前端的安装孔(26)和与该安装孔(26)可拆卸连接的前盖板(27)；
    所述复位弹簧(25)是两个，该两个复位弹簧(25)的下端并排插入设置在所述前盖板(27)的顶面上且高出所述承载件(1)顶面的两个导向限位筒(28)内。
  8. 如权利要求2所述的开放式机载或车载瞄具，其特征在于：所述内红点模组承载件(2)的底面自前向后依次设置有分别与前支撑组件(3)、电池仓(52)、凸轮安装腔(8)配合的前支撑组件安装盲孔(31)、电池仓匹配弧形面(32)、凸轮弧形腔(33)；
    所述前支撑组件(3)还包括开设在所述承载件(1)顶面前端的安装孔(26)和与该安装孔(26)可拆卸连接的前盖板(27)；
    所述复位弹簧(25)是两个，该两个复位弹簧(25)的下端并排插入设置在所述前盖板(27)的顶面上且高出所述承载件(1)顶面的两个导向限位筒(28)内；
    一防尘套(34)的上端与所述前支撑组件安装盲孔(31)螺钉连接，该防尘套(34)下端与前固定圈(35)连接，该前固定圈(35)与所述前盖板(27)可拆卸 连接；
    所述复位弹簧(25)、导向限位筒(28)均套设在所述防尘套(34)内，且所述复位弹簧(25)抵触在所述前支撑组件安装盲孔(31)的顶壁上。
  9. 如权利要求2所述的开放式机载或车载瞄具，其特征在于：所述内红点模组承载件(2)的尾端安装内红点模组(37)，内红点模组承载件(2)的前端通过透镜安装框架(38)安装透镜(39)；
    所述内红点模组承载件(2)的顶面设置有太阳能发电板组件(40)，且于该太阳能发电板组件(40)的前后部位，所述内红点模组承载件(2)的顶面刻设多条横向楞条(41)，用以消除环境杂光的不利影响；
    所述承载件(1)的顶面尾端开设有置于所述凸轮安装腔(8)后侧的内红点模组安装腔(42)。
  10. 如权利要求2所述的开放式机载或车载瞄具，其特征在于：所述凸轮安装端(9)的末端为一缩颈部(43)，用以卡合在所述凸轮安装腔(8)的相应侧的限位凹槽(44)内，并通过螺钉连接一两侧具有耳孔的弧形定位套(45)固定在限位凹槽(44)内；
    所述承载件(1)的尾端一侧设置有倍率镜(46)。
PCT/CN2019/130413 2019-06-04 2019-12-31 一种开放式机载或车载瞄具 WO2020244218A1 (zh)

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JP2021570228A JP7265651B2 (ja) 2019-06-04 2019-12-31 オープン式航空機又は車両用サイト
EP19932062.3A EP3982078A4 (en) 2019-06-04 2019-12-31 OPEN AIRBOARD OR VEHICLE MOUNTED SIGHTING DEVICE
US17/613,032 US11841210B2 (en) 2019-06-04 2019-12-31 Open airborne or vehicle-mounted sight
KR1020217039010A KR20220014872A (ko) 2019-06-04 2019-12-31 오픈식 항공기 또는 차량용 사이트

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20210231407A1 (en) * 2020-01-24 2021-07-29 Axts Inc Optic guard for firearm

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP4232770A1 (en) * 2020-10-20 2023-08-30 Sheltered Wings, Inc. D/b/a/ Vortex Optics Viewing optic with a solar panel

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN200989749Y (zh) * 2006-12-22 2007-12-12 潍坊学院 狙击步枪遥控瞄准装置
WO2008140830A2 (en) * 2007-01-08 2008-11-20 Irwin Jere F Shotgun sight and adjustable gun sight
US7647720B1 (en) * 2008-12-08 2010-01-19 The United States Of America As Represented By The Secretary Of The Navy Bore-sight alignment device
CN102472604A (zh) * 2009-08-20 2012-05-23 Yt产品有限责任公司 双模式的反射式和望远镜式瞄准器组合
US20150198421A1 (en) * 2014-01-13 2015-07-16 Leupold & Stevens, Inc. Removable aiming sight and sight mounting shoe with pitch and yaw adjustment for pistols and other weapons
CN207456288U (zh) * 2017-11-30 2018-06-05 深圳市大疆创新科技有限公司 一种激光瞄准调节装置
CN109186346A (zh) * 2018-11-08 2019-01-11 南通神目机械有限公司 一种霰弹枪专用瞄准镜

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6516551B2 (en) * 2000-12-27 2003-02-11 American Technologies Network Corporation Optical sight with switchable reticle
KR100906159B1 (ko) 2007-07-06 2009-07-03 정인 대구경 도트 사이트 장치
KR101059035B1 (ko) 2008-09-11 2011-08-24 정인 탄도 보정 장치
US8215050B2 (en) 2008-10-02 2012-07-10 Trijicon, Inc. Optical sight
US20130008072A1 (en) * 2011-07-08 2013-01-10 Sung Giu Chung Dot sight device
US9593907B2 (en) 2013-12-18 2017-03-14 Leupold & Stevens, Inc. Micro-pixelated LED reticle display for optical aiming devices
US9982965B2 (en) 2014-03-01 2018-05-29 Huanic Corporation Inner red-dot gun sighting device powered by solar cell and provided with micro-current LED light source
CN107782199B (zh) * 2016-08-30 2023-09-22 西安华科光电有限公司 一种可消除杂光的内红点瞄具
US11555669B2 (en) * 2020-06-23 2023-01-17 Sellmark Corporation Firearm sight with modular interchangeable hoods

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN200989749Y (zh) * 2006-12-22 2007-12-12 潍坊学院 狙击步枪遥控瞄准装置
WO2008140830A2 (en) * 2007-01-08 2008-11-20 Irwin Jere F Shotgun sight and adjustable gun sight
US7647720B1 (en) * 2008-12-08 2010-01-19 The United States Of America As Represented By The Secretary Of The Navy Bore-sight alignment device
CN102472604A (zh) * 2009-08-20 2012-05-23 Yt产品有限责任公司 双模式的反射式和望远镜式瞄准器组合
US20150198421A1 (en) * 2014-01-13 2015-07-16 Leupold & Stevens, Inc. Removable aiming sight and sight mounting shoe with pitch and yaw adjustment for pistols and other weapons
CN207456288U (zh) * 2017-11-30 2018-06-05 深圳市大疆创新科技有限公司 一种激光瞄准调节装置
CN109186346A (zh) * 2018-11-08 2019-01-11 南通神目机械有限公司 一种霰弹枪专用瞄准镜

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of EP3982078A4 *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20210231407A1 (en) * 2020-01-24 2021-07-29 Axts Inc Optic guard for firearm

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JP2022535348A (ja) 2022-08-08
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US20220244015A1 (en) 2022-08-04
CN211696074U (zh) 2020-10-16
EP3982078A4 (en) 2022-07-27
EP3982078A1 (en) 2022-04-13

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