CN112278303B - A kind of UAV fill light device - Google Patents

A kind of UAV fill light device Download PDF

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Publication number
CN112278303B
CN112278303B CN202011113741.2A CN202011113741A CN112278303B CN 112278303 B CN112278303 B CN 112278303B CN 202011113741 A CN202011113741 A CN 202011113741A CN 112278303 B CN112278303 B CN 112278303B
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guide support
groups
group
guide
support rods
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CN112278303A (en
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池翔
何国旋
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Liu Haonan
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00—Equipment not otherwise provided for
    • B64D47/08—Arrangements of cameras
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00—Equipment not otherwise provided for
    • B64D47/02—Arrangements or adaptations of signal or lighting devices
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00—UAVs specially adapted for particular uses or applications
    • B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Forklifts And Lifting Vehicles (AREA)

Abstract

本发明公开了一种新型无人机补光装置，包括云台、拍摄箱、机壳、第一导向支杆和第二导向支杆，所述云台固定在无人机主体的底端，所述拍摄箱安装在云台的底端面中心处，拍摄箱的内部设置有摄像头，拍摄箱的底端通过固定板、连接板和第一电机固定连接放置机壳的导向支架，所述导向支架的内部对称安装有两组第二电机，其中两组第二电机的机轴均在机壳内同轴固定连接有传动轴，所述第一导向支杆与第二导向支杆均设置有两组，其中在每组传动轴位于机壳外的一端上均套有一组第一导向支杆和一组第二导向支杆。该新型无人机补光装置，调节了两组补光灯之间的相对位置，进而可以根据需要调节补光的强度大小。

The present invention discloses a novel unmanned aerial vehicle fill-in light device, comprising a gimbal, a shooting box, a casing, a first guide support rod and a second guide support rod, wherein the gimbal is fixed to the bottom end of the unmanned aerial vehicle body, the shooting box is installed at the center of the bottom end surface of the gimbal, a camera is arranged inside the shooting box, the bottom end of the shooting box is fixedly connected to a guide support on which the casing is placed through a fixing plate, a connecting plate and a first motor, two groups of second motors are symmetrically arranged inside the guide support, wherein the shafts of the two groups of second motors are coaxially fixedly connected to a transmission shaft in the casing, and two groups of the first guide support rod and the second guide support rod are arranged, wherein a group of first guide support rods and a group of second guide support rods are sleeved on one end of each group of transmission shafts located outside the casing. The novel unmanned aerial vehicle fill-in light device adjusts the relative position between the two groups of fill-in lights, and thus the intensity of the fill-in light can be adjusted as needed.

Description

Unmanned aerial vehicle light filling device
Technical Field
The invention belongs to the technical field of unmanned aerial vehicles, and particularly relates to an unmanned aerial vehicle light supplementing device.
Background
The existing unmanned aerial vehicle is usually carried with a visible light camera as a shooting device, when the unmanned aerial vehicle needs to work at night, the imaging effect of the visible light camera is poor and the definition is insufficient due to insufficient ambient light at night, and the influence of ambient light conditions is large. Therefore, how to improve the situation that the unmanned aerial vehicle can still normally shoot under the condition of insufficient illumination at night becomes a problem to be solved in the field.
When being applied to Jie Juemo man-machine at night the problem of shooting, most use supplementary shooting equipment of light filling lamp to shoot in the light filling, improve the definition, but current light filling device who uses the light filling lamp, it is when using, the light filling lamp position is fixed, and the angle of light filling lamp is inconvenient for adjusting, lead to the light filling in using, can not be according to the demand of using, adjust the intensity of light filling, and the position of light filling, realize the light filling under the different circumstances, lead to the scope of adaptation little, can't satisfy the use at present.
Disclosure of Invention
The invention aims to provide an unmanned aerial vehicle light supplementing device, which aims to solve the problems in the background technology.
In order to achieve the purpose, the unmanned aerial vehicle light supplementing device comprises a cradle head, a shooting box, a shell, first guide struts and second guide struts, wherein the cradle head is fixed at the bottom end of a unmanned aerial vehicle main body, the shooting box is installed at the center of the bottom end surface of the cradle head, a camera is arranged in the shooting box, the bottom end of the shooting box is fixedly connected with a guide bracket for placing the shell through a fixing plate, a connecting plate and the first motor, two groups of second motors are symmetrically installed in the guide bracket, shafts of the two groups of second motors are coaxially and fixedly connected with transmission shafts in the shell, the first guide struts and the second guide struts are respectively provided with two groups, one end of each group of transmission shafts, which is located outside the shell, is respectively sleeved with one group of first guide struts and one group of second guide struts, and the two groups of first guide struts and the two groups of second guide struts are respectively provided with light supplementing lamps.
Preferably, positioning holes are tapped at four corners of the top end surface of the cradle head, and are fixedly connected with the bottom end of the unmanned aerial vehicle body through positioning bolts.
Preferably, the fixed plate is fixed on the bottom end surface of the shooting box in an adhering way, and connection screw holes are tapped at four corners of the upper end surface of the fixed plate, which is positioned on the outer side of the shooting box, one end of the connecting plate is of a semicircular structure, the other end of the connecting plate is of a rectangular structure, and the four corners of the rectangular structure are also tapped with the connection screw holes, and the connecting screw holes penetrate through the fixed plate through fixing bolts and are detachably connected with the fixed plate.
Preferably, the top end of the fixed end of the first motor is embedded and fixed on the bottom end surface of the semicircular structure of the connecting plate, and the output shaft of the first motor is fixedly connected with the top end of the guide bracket.
Preferably, the guide bracket is of a U-shaped rod structure, a semicircular protruding block protrudes towards one side from the middle of the horizontal top end of the guide bracket, a bottom hole for placing an output shaft of the first motor is formed in the center of the top end face of the protruding block, insertion holes are formed in the bottom ends of one side face of two groups of end legs of the guide bracket, one group of insertion holes are hinged to the outer side face of the shell through pin shafts, an output shaft of a third motor fixedly connected with the outer side face of the shell is inserted into the other group of insertion holes, and the third motor is fixed on the side face of the guide bracket.
Preferably, the bottom of casing has the bottom through screw fixation seal, and two sets of second motors are embedded to be fixed at the inner wall of casing, just first direction branch is L type structure with second direction branch, and wherein the both ends of the L type structure of first direction branch and second direction branch all are arc structure, and open there is curved through-hole, the light filling lamp is embedded to be fixed in two sets of horizontally through-holes.
Preferably, one of the two groups of the first guiding support rods and the two groups of the second guiding support rods is fixedly sleeved on one group of transmission shafts, the other group of the first guiding support rods and the two groups of the second guiding support rods are slidably sleeved on the other group of transmission shafts, and the first guiding support rods and the second guiding support rods are not adjacently arranged with one group of transmission shafts.
The light supplementing device for the unmanned aerial vehicle has the technical effects and advantages that two groups of first guide support rods and two groups of second guide support rods are arranged, light supplementing lamps are arranged on the two groups of first guide support rods and the two groups of second guide support rods, the two groups of first guide support rods and the two groups of second guide support rods are respectively sleeved on transmission shafts extending out of two sides of a machine shell, the two groups of first guide support rods and the two groups of second guide support rods rotate on the machine shell, the relative positions between the two groups of light supplementing lamps are adjusted, and the intensity of light supplementing can be adjusted according to requirements, meanwhile, the two groups of light supplementing lamps on the first guide support rods and the two groups of second guide support rods can be further finely adjusted in the overall horizontal angle and the vertical angle of the light supplementing lamps through a first motor connected with the bottom end of a shooting box and a second motor fixed on the guide support rods, and shooting requirements under different angles are met.
Drawings
FIG. 1 is a front view of the present invention;
FIG. 2 is a schematic view of the structure of a first guide strut and a second guide strut according to the present invention;
FIG. 3 is a cross-sectional view of the housing of the present invention;
FIG. 4 is an enlarged schematic view of the structure of FIG. 1A according to the present invention;
fig. 5 is a schematic view of the guide bracket structure of the present invention.
In the figure, 1, a cradle head, 2, a positioning hole, 3, a shooting box, 4, a camera, 5, a first guide supporting rod, 6, a second guide supporting rod, 7, a light supplementing lamp, 8, a shell, 9, a rotating shaft, 10, a connecting plate, 11, a first motor, 12, a guide bracket, 13, a bottom cover, 14, a second motor, 15, a transmission shaft, 16, a fixing plate, 17, a fixing bolt, 18, a third motor, 19, an inserting hole, 20 and a bump.
Detailed Description
The following description of the embodiments of the present invention will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present invention, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the invention without making any inventive effort, are intended to be within the scope of the invention.
The invention provides an unmanned aerial vehicle light supplementing device as shown in fig. 1-5, which comprises a tripod head 1, a shooting box 3, a shell 8, a first guide strut 5 and a second guide strut 6, wherein the tripod head 1 is fixed at the bottom end of an unmanned aerial vehicle main body, the shooting box 3 is arranged at the center of the bottom end surface of the tripod head 1, a camera 4 is arranged in the shooting box 3, the bottom end of the shooting box 3 is fixedly connected with a guide bracket 12 for placing the shell 8 through a fixing plate 16, a connecting plate 10 and a first motor 11, two groups of second motors 14 are symmetrically arranged in the guide bracket 12, shafts of the two groups of second motors 14 are coaxially and fixedly connected with transmission shafts 15 in the shell 8, the first guide strut 5 and the second guide strut 6 are respectively provided with two groups, one end of each group of transmission shafts 15, which is positioned outside the shell 8, is respectively sleeved with a group of first guide strut 5 and a group of second guide strut 6, and the two groups of first guide struts 5 and the two groups of second guide struts 6 are respectively provided with light supplementing lamps 7.
Specifically, locating holes 2 are all attacked in top face four corners department of cloud platform 1 to through the bottom fixed connection of locating bolt and unmanned aerial vehicle main part, make things convenient for the installation in the initial time.
Specifically, the fixing plate 16 is fixedly adhered to the bottom end surface of the shooting box 3, and connection screw holes are tapped at four corners of the upper end surface of the fixing plate 16 located at the outer side of the shooting box 3, one end of the connecting plate 10 is of a semicircular structure, the other end of the connecting plate is of a rectangular structure, and connection screw holes are tapped at four corners of a part of the rectangular structure, and the connecting screw holes penetrate through the fixing plate 16 through fixing bolts 17 and are detachably connected with the fixing plate 16.
Specifically, the top end of the fixed end of the first motor 11 is embedded and fixed on the bottom end surface of the semicircular structure of the connecting plate 10, and the output shaft of the first motor 11 is fixedly connected with the top end of the guide bracket 12, so that the first motor 11 is rotated to drive the guide bracket 12 and the shell 8 to finely adjust the horizontal angle.
Specifically, the guide bracket 12 is in a U-shaped rod structure, a semicircular protruding block 20 protrudes to one side from the middle of the horizontal top end of the guide bracket 12, a bottom hole for placing the output shaft of the first motor 11 is formed in the center of the top end face of the protruding block 20, insertion holes 19 are formed in the bottom ends of one side face of two groups of end legs of the guide bracket 12, one group of insertion holes 19 are hinged to the outer side face of the machine shell 8 through pin shafts, the output shaft of a third motor 18 fixedly connected with the outer side face of the machine shell 8 is inserted into the other group of insertion holes 19, the third motor 18 is fixed to the side face of the guide bracket 12, when the third motor 18 rotates, fine adjustment of the vertical angle of the machine shell 8 is achieved, and meanwhile, the first motor 11, the second motor 14 and the third motor 18 are all servo motors, so that forward and reverse rotation motions can be achieved.
Specifically, the bottom of casing 8 has bottom 13 through screw fixation seal, can carry out subsequent dismantlement, and two sets of second motors 14 are built-in to be fixed at the inner wall of casing 8, just first direction branch 5 is L type structure with second direction branch 6, and wherein the both ends of the L type structure of first direction branch 5 and second direction branch 6 all are the arc structure, and open and have curved through-hole, built-in the fixing of light filling lamp 7 is in two sets of horizontally through-holes, makes things convenient for the installation and the fixing of light filling lamp 7.
Specifically, one of the two groups of the first guiding support rods 5 and the two groups of the second guiding support rods 6 is fixedly sleeved on one group of transmission shafts 15, the other group of the first guiding support rods and the two groups of the second guiding support rods are slidably sleeved on the other group of transmission shafts 15, and the first guiding support rods 5 and the second guiding support rods 6 are not adjacent to the group of the transmission shafts 15, so that when the first guiding support rods 5 and the other group of the second guiding support rods 6 rotate, the other group of the second guiding support rods can be driven to rotate.
The theory of operation, this unmanned aerial vehicle light filling device, when using, operating personnel finishes each part fixed connection of novel unmanned aerial vehicle light filling device earlier according to corresponding needs, then fix cloud platform 1 in the bottom position department of unmanned aerial vehicle main part, when navigating at night, two sets of light filling lamps 7 are in the in-process of shooing, shoot the shooting of camera 4 in shooting case 3 and carry out the light filling, simultaneously when need to the distance between two sets of light filling lamps 7 adjust (i.e. when the distance between with camera 4), start two sets of second motors 14 work in the quick-witted incasement, here two sets of second motors 14 can start respectively, second motor 14 rotates, drive transmission shaft 15's rotation, thereby drive transmission shaft 15 on with transmission shaft 15 fixed connection's first direction branch 5 or second direction branch 6 rotate, first direction branch 5 and second direction branch 6 rotate on another set of transmission shaft 15, and then drive light filling lamp 7's rotation, realize doing arc motion to light filling lamp 7, still can start first motor 11 and third motor 18 drive transmission shaft 8 and drive light filling lamp 7 and change the demand by two sets of light filling lamp 8, drive horizontal adjustment support 8 and drive light filling lamp 7, the casing 8 and the rotation angle is adjusted to two sets of light filling lamp 7, the casing 8 is reached at the time, the rotation of two sets of light filling lamp 7 is adjusted.
It should be noted that the foregoing description is only a preferred embodiment of the present invention, and although the present invention has been described in detail with reference to the foregoing embodiments, it should be understood that modifications, equivalents, improvements and modifications to the technical solution described in the foregoing embodiments may occur to those skilled in the art, and all modifications, equivalents, and improvements are intended to be included within the spirit and principle of the present invention.

Claims (3)

1.一种无人机补光装置，包括云台（1）、拍摄箱（3）、机壳（8）、第一导向支杆（5）和第二导向支杆（6），其特征在于：所述云台（1）固定在无人机主体的底端，所述拍摄箱（3）安装在云台（1）的底端面中心处，拍摄箱（3）的内部设置有摄像头（4），拍摄箱（3）的底端通过固定板（16）、连接板（10）和第一电机（11）固定连接放置机壳（8）的导向支架（12），所述导向支架（12）的内部对称安装有两组第二电机（14），其中两组第二电机（14）的机轴均在机壳（8）内同轴固定连接有传动轴（15），所述第一导向支杆（5）与第二导向支杆（6）均设置有两组，其中在每组传动轴（15）位于机壳（8）外的一端上均套有一组第一导向支杆（5）和一组第二导向支杆（6），且两组第一导向支杆（5）与两组第二导向支杆（6）上均安装有补光灯（7）；1. A fill light device for an unmanned aerial vehicle, comprising a pan head (1), a shooting box (3), a housing (8), a first guide support rod (5) and a second guide support rod (6), characterized in that: the pan head (1) is fixed to the bottom end of the unmanned aerial vehicle body, the shooting box (3) is installed at the center of the bottom end surface of the pan head (1), a camera (4) is arranged inside the shooting box (3), the bottom end of the shooting box (3) is fixedly connected to a guide bracket (12) on which the housing (8) is placed through a fixing plate (16), a connecting plate (10) and a first motor (11), and the Two groups of second motors (14) are symmetrically mounted inside the guide bracket (12), wherein the shafts of the two groups of second motors (14) are coaxially fixedly connected to the transmission shaft (15) inside the housing (8), and two groups of the first guide support rods (5) and the second guide support rods (6) are provided, wherein one group of first guide support rods (5) and one group of second guide support rods (6) are sleeved on one end of each group of transmission shafts (15) located outside the housing (8), and fill lights (7) are mounted on the two groups of first guide support rods (5) and the two groups of second guide support rods (6); 所述云台（1）的顶端面四角处均攻有定位孔（2），并通过定位螺栓与无人机主体的底端固定连接；The top surface of the gimbal (1) is provided with positioning holes (2) at the four corners thereof, and is fixedly connected to the bottom end of the drone body via positioning bolts; 所述固定板（16）粘接固定在拍摄箱（3）的底端面，且位于拍摄箱（3）外侧的固定板（16）上端面四角处攻有连接螺孔，所述连接板（10）一端呈半圆形结构，另一端呈矩形结构，且矩形结构的部分上的四角处也攻有连接螺孔，并通过固定螺栓（17）穿过固定板（16）的连接螺孔与固定板（16）可拆卸连接；The fixing plate (16) is adhesively fixed to the bottom end surface of the shooting box (3), and the fixing plate (16) located outside the shooting box (3) has connecting screw holes at four corners of its upper end surface. One end of the connecting plate (10) is in a semicircular structure, and the other end is in a rectangular structure. The four corners of the rectangular structure are also connected with connecting screw holes, and the fixing bolts (17) are passed through the connecting screw holes of the fixing plate (16) to be detachably connected to the fixing plate (16); 所述第一电机（11）的固定端顶端内嵌固定在连接板（10）的半圆形结构的底端面，且第一电机（11）的输出轴与导向支架（12）的顶端固定连接；The top end of the fixed end of the first motor (11) is embedded and fixed in the bottom end surface of the semicircular structure of the connecting plate (10), and the output shaft of the first motor (11) is fixedly connected to the top end of the guide bracket (12); 所述导向支架（12）呈U型杆结构，导向支架（12）的水平顶端中间处向一侧凸出有半圆形的凸块（20），且凸块（20）的顶端面中心处开有置放第一电机（11）输出轴的底孔，导向支架（12）的两组端腿一侧面底端均开有插孔（19），其中一组插孔（19）内通过销轴与机壳（8）的外侧面铰接相连，另一组插孔（19）内插入有与机壳（8）的外侧面固定连接的第三电机（18）的输出轴，且第三电机（18）固定在导向支架（12）的侧面上。The guide bracket (12) is in a U-shaped rod structure. A semicircular protrusion (20) protrudes toward one side from the middle of the horizontal top of the guide bracket (12). A bottom hole for placing the output shaft of the first motor (11) is formed at the center of the top surface of the protrusion (20). Plug holes (19) are formed at the bottom of one side surface of two groups of end legs of the guide bracket (12). One group of the plug holes (19) is hingedly connected to the outer side surface of the housing (8) via a pin shaft. The output shaft of a third motor (18) fixedly connected to the outer side surface of the housing (8) is inserted into the other group of the plug holes (19). The third motor (18) is fixed to the side surface of the guide bracket (12). 2.根据权利要求1所述的一种无人机补光装置，其特征在于：所述机壳（8）的底端通过螺丝固定密封有底盖（13），两组第二电机（14）内嵌固定在机壳（8）的内壁，且所述第一导向支杆（5）与第二导向支杆（6）均为L型结构，其中第一导向支杆（5）和第二导向支杆（6）的L型结构的两端均呈弧形结构，且开有弧形的通孔，所述补光灯（7）内嵌固定在两组水平的通孔内。2. A fill light device for an unmanned aerial vehicle according to claim 1, characterized in that: the bottom end of the housing (8) is sealed with a bottom cover (13) fixed by screws, two sets of second motors (14) are embedded and fixed on the inner wall of the housing (8), and the first guide support rod (5) and the second guide support rod (6) are both L-shaped structures, wherein both ends of the L-shaped structures of the first guide support rod (5) and the second guide support rod (6) are arc-shaped structures and have arc-shaped through holes, and the fill light (7) is embedded and fixed in the two sets of horizontal through holes. 3.根据权利要求2所述的一种无人机补光装置，其特征在于：两组所述第一导向支杆（5）与两组所述第二导向支杆（6）的其中一组固定套在一组传动轴（15）上，另一组滑动套在另一组传动轴（15）上，且第一导向支杆（5）和第二导向支杆（6）与传动轴（15）固定的一组不相邻设置。3. A fill light device for an unmanned aerial vehicle according to claim 2, characterized in that: one of the two groups of the first guide support rods (5) and the two groups of the second guide support rods (6) is fixedly sleeved on one group of transmission shafts (15), and the other group is slidably sleeved on the other group of transmission shafts (15), and the first guide support rod (5) and the second guide support rod (6) are not arranged adjacent to the group fixed to the transmission shaft (15).
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CN211001897U (en) * 2019-11-14 2020-07-14 绍兴市芷竹文化创意有限公司 Unmanned aerial vehicle movie & TV shoots cloud platform
CN213921531U (en) * 2020-10-17 2021-08-10 广东空航航空科技有限公司 Novel unmanned aerial vehicle light filling device

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