A gimbal for a drone

Abstract

The utility model discloses a kind of unmanned aerial vehicle tripod, including rotating component and three light components, the rotating component and three light components connection;The rotating component includes relay power board, yaw support front cover, yaw support back cover, upper shield cover, hollow encoder, lower shield cover, roll support front cover, roll support left cover and roll support right cover.The utility model passes through conductive sealing strip and relay power board and blocks through hole, each part junction is treated by conductive sealing, improve the good conduction and sealing between assembly parts, in addition, hollow encoder control motor rotation is sealed using upper and lower shield cover at motor rotating joint, relay adapter plate is arranged at rotating joint, the problem that electromagnetic leakage caused by joint movement gap of unavoidable activity is solved, and the electromagnetic shielding performance of equipment is improved.

Description

Technical Field

[0001] This application relates to the field of drones and their applications, and in particular to a drone gimbal. Background Technology

[0002] With the widespread application of drones in fields such as aerial photography, agricultural monitoring, industrial inspection, and emergency rescue, the performance requirements for gimbals are increasing.

[0003] Existing industrial drone gimbals are generally three-light gimbals, which contain thermal imaging, laser, and visible light core modules. During the operation of these three modules, a lot of heat is generated. Due to the small size, light weight, and compact structure of drone gimbals, the heat is often difficult to dissipate. High heat accumulation can cause a decrease in core performance or even loss of function. Although some gimbals can be equipped with fans to cool the system, the rotation of the fans will increase the vibration of the gimbal, affecting the stability of the gimbal's image or increasing the difficulty and cost of the equipment's algorithm design.

[0004] In certain special situations, such as strong electromagnetic fields with high voltage, high-precision aerial photography, military and petrochemical areas, gimbals need to have electromagnetic interference protection capabilities. Most existing gimbals have relatively poor electromagnetic shielding capabilities, and there is an urgent need for a gimbal with strong electromagnetic shielding. Utility Model Content

[0005] The purpose of this utility model is to provide a drone gimbal. The gimbal design solves the problems of insufficient heat dissipation and poor electromagnetic shielding performance of existing gimbals through innovative features such as conductive sealing treatment, hollow encoder shielding cover, nano carbon heat dissipation coating and boss heat conduction structure.

[0006] To achieve the above objectives, this utility model provides the following technical solution:

[0007] A drone gimbal includes a rotating assembly and a three-light assembly. The rotating assembly includes: an upper cover, a yaw stator, a yaw motor, a relay power board, a yaw bracket, an inner cavity, a yaw inner sealing groove, a front cavity, a rear cavity, a yaw rear sealing groove, a yaw bracket front cover, a yaw bracket rear cover, an upper shield, a hollow encoder, a lower shield, a roll bracket front cover, a roll bracket left cover, a roll bracket right cover, a roll bracket right cover, a roll bracket, a second rear cavity, a second front cavity, a roll front sealing groove, a right first cavity, a roll right sealing groove, a right second cavity, a left cavity, a bearing, an auxiliary shaft, a pitch transition plate, a roll motor, and a pitch motor.

[0008] Preferably, the surface of the yaw bracket is treated with conductive oxidation, and its upper end is connected to the rotor of the yaw motor. The stator of the yaw motor is fixedly connected to the yaw stator to form a yaw rotation joint. The relay power board is installed on the upper side of the yaw bracket, and its installation position is opposite to the mounting surface of the yaw motor rotor. The mounting surface of the relay power board is completely conductively attached to the yaw bracket and seals the axial through hole of the yaw motor.

[0009] Preferably, a hollow encoder is installed inside the yaw stator, and a top cover is installed on the upper surface. The upper and lower surfaces of the hollow encoder are sealed with an upper shield and a lower shield, respectively, to prevent electromagnetic leakage of the hollow encoder. The surfaces of the upper shield and the lower shield are treated with conductive material.

[0010] Preferably, the inner cavity of the yaw bracket has an annular yaw inner sealing groove at its edge. The yaw inner sealing groove is used to install a conductive sealing strip. The front cover of the yaw bracket is installed inside the yaw bracket and presses down on the conductive sealing strip.

[0011] Preferably, the lower end of the yaw bracket is divided into two cavities, front and rear. The stator of the roll motor is fixed in the front cavity, and a hollow encoder is installed in the rear cavity. The upper and lower surfaces of the hollow encoder are sealed with an upper shield and a lower shield, respectively. The rear cavity has a yaw rear sealing groove on its rear end face for installing a conductive sealing strip. The rear cover of the yaw bracket is installed on this end face and presses down on the conductive sealing strip.

[0012] Preferably, the roll motor rotor is installed in the second rear cavity of the roll bracket, forming a roll joint.

[0013] Preferably, a relay power board is installed inside the second front cavity of the roll bracket. The mounting surface of the relay power board is in complete conductive contact with the roll bracket and seals the axial through hole of the roll motor.

[0014] Preferably, the surface of the roll support is treated with conductive oxidation, and the right cavity and the second front cavity are provided with a right roll sealing groove and a front roll sealing groove for installing conductive sealing strips. The right cover and the front cover of the roll support are respectively installed on the right side and the front side of the roll support and press down on the conductive sealing strips.

[0015] Preferably, a hollow encoder is installed in the right cavity of the roll bracket, and the upper and lower surfaces of the hollow encoder are sealed with upper and lower shielding covers respectively to prevent electromagnetic leakage of the hollow encoder; the stator of the pitch motor is fixedly installed in the second right cavity of the roll bracket, and the rotor of the pitch motor is fixedly connected to the pitch transition plate to form a pitch-rotation joint. A relay power board is installed on the other side of the pitch transition plate, and the mounting surface of the relay power board is completely conductively attached to the roll bracket and seals the axial through hole of the roll motor.

[0016] Preferably, a left cover of the roll bracket is installed at the outer end of the left cavity of the roll bracket, and a bearing is installed at the end. An auxiliary shaft is installed on the inner ring of the bearing, and the threaded end of the auxiliary shaft is connected to the three-light assembly.

[0017] Preferably, the three-light assembly includes a laser module, a thermal imaging module, a visible light module, an upper shell, an upper shell boss, a right shell, a front cover, a lower shell, a lower shell boss, a left shell, a rear cover, a center shell front sealing groove, a center shell rear sealing groove, a center shell right sealing groove, an expansion board, a motherboard, a middle shell, a center shell assembly, a center frame, and a vision module.

[0018] Preferably, the upper shell, right shell, lower shell, and left shell constitute a middle shell. The middle shell includes a front sealing groove and a rear sealing groove for installing a conductive sealing strip. The front cover and rear cover are respectively installed at the front and rear ends of the middle shell and press down on the conductive sealing strip to form a middle shell assembly.

[0019] Preferably, the inner surface of the central shell assembly is treated with conductive oxidation, and the outer surface is coated with a nano-carbon heat dissipation coating.

[0020] Preferably, the vision module is installed inside the central shell assembly, and the central frame serves as the basic load-bearing frame of the vision module, used to install the thermal imaging module, visible light module, expansion board and motherboard. The visible light module and motherboard are the main heat sources and are respectively arranged at the upper and lower ends of the visible light module.

[0021] Preferably, the inner surfaces of the upper and lower shells are provided with dense upper shell protrusions and lower shell protrusions, which contact and conduct heat with the heat-generating chips on the motherboard and expansion board, respectively.

[0022] Preferably, the outer side of the right shell is provided with a central shell right sealing groove for installing a conductive sealing strip. The right shell is fixedly connected to the pitch transition plate of the rotating assembly, and the connection surfaces are electrically conductive to each other. The transition plate presses down on the conductive sealing strip in the central shell right sealing groove.

[0023] Compared with the prior art, the beneficial effects of this utility model are:

[0024] This invention effectively transfers the heat from the main heat source to the outer casing. In addition, the outer surface of the casing is coated with a nano-carbon heat dissipation coating, which can better dissipate heat, ensure that the system operates at a lower temperature, and improve the operating performance of the equipment under high load conditions. Through the combination of heat conduction of the outer casing and the coating, the impact of fan vibration on the stability of the gimbal is avoided, which has structural differences.

[0025] This invention improves the conductivity and sealing between assembled parts by applying conductive sealing treatment to the joints of each component. In addition, the motor rotation joint is controlled by a hollow encoder with upper and lower shielded covers. A relay adapter plate is arranged at the rotation joint to solve the problem of electromagnetic leakage caused by the unavoidable gaps in the movement of the moving joint, thereby improving the electromagnetic shielding performance of the equipment.

[0026] This invention significantly improves electromagnetic shielding performance by sealing the through holes with conductive sealing strips and relay power boards. Attached Figure Description

[0027] Figure 1 This is an isometric view of the present invention;

[0028] Figure 2 This is a cross-sectional view of the rotating component of this utility model;

[0029] Figure 3 This is an exploded view of the rotating component of this utility model;

[0030] Figure 4 This is an isometric view of the yaw support of this utility model;

[0031] Figure 5 This is an isometric view of the roll support of this utility model;

[0032] Figure 6 This is a schematic diagram of the installation of the hollow encoder of this utility model;

[0033] Figure 7 This is a schematic diagram of the installation of the central shell assembly and vision module of this utility model;

[0034] Figure 8 This is an exploded view of the central shell assembly of this utility model;

[0035] Figure 9 This is an isometric drawing of the middle shell of this utility model;

[0036] Figure 10 This is an axonometric view of the central skeleton of this utility model;

[0037] Figure 11 This is a schematic diagram of the installation of the vision module of this utility model;

[0038] Figure 12 This is a schematic diagram of the front sealing groove of the central shell of this utility model;

[0039] Figure 13 This is a schematic diagram of the rear sealing groove and the right sealing groove of the central shell of this utility model;

[0040] Figure 14 This is a schematic diagram of the upper shell boss of this utility model;

[0041] Figure 15 This is a schematic diagram of the lower shell boss of this utility model.

[0042] In the picture:

[0043] 1000 Rotating assembly, 1001 Upper cover, 1002 Yaw stator; 1003 Yaw motor, 1004 Relay power board, 1005 Yaw bracket, 1005-1 Inner cavity, 1005-2 Yaw inner sealing groove, 1005-3 Front cavity, 1005-4 Rear cavity, 1005-5 Yaw rear sealing groove, 1006 Yaw bracket front cover, 1007 Yaw bracket rear cover, 1008 Upper shield, 1009 Hollow encoder, 1010 Lower shield, 101 1. Roll bracket front cover, 1012. Roll bracket left cover, 1013. Roll bracket right cover, 1014. Roll bracket, 1014-1. Second rear cavity, 1014-2. Second front cavity, 1014-3. Roll front sealing groove, 1014-4. Right first cavity, 1014-5. Roll right sealing groove, 1014-6. Right second cavity, 1014-7. Left side cavity, 1015. Bearing, 1016. Auxiliary shaft, 1017. Pitch transition plate, 1018. Roll motor, 1019. Pitch motor.

[0044] 2000 Three-Light Components: 2001 Laser Module, 2002 Thermal Imaging Module, 2003 Visible Light Module, 2004 Upper Shell, 2004-1 Upper Shell Boss, 2005 Right Shell, 2006 Front Cover, 2007 Lower Shell, 2007-1 Lower Shell Boss, 2008 Left Shell, 2009 Rear Cover, 2010 Front Sealing Groove of Center Shell, 2011 Rear Sealing Groove of Center Shell, 2012 Right Sealing Groove of Center Shell, 2013 Expansion Board, 2014 Main Board, 2015 Middle Shell, 2016 Center Shell Assembly, 2017 Center Frame, 2018 Vision Module. Detailed Implementation

[0045] The technical solutions of the embodiments of this application will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of this application, not all embodiments. Based on the embodiments of this application, all other embodiments obtained by those skilled in the art without creative effort are within the scope of protection of this application.

[0046] It should be understood that, when used in this specification and the appended claims, the terms "comprising" and "including" indicate the presence of the described features, integrals, steps, operations, elements and / or components, but do not exclude the presence or addition of one or more other features, integrals, steps, operations, elements, components and / or collections thereof.

[0047] It should also be understood that the terminology used in this application specification is for the purpose of describing particular embodiments only and is not intended to limit the application. As used in this application specification and the appended claims, the singular forms “a,” “an,” and “the” are intended to include the plural forms unless the context clearly indicates otherwise.

[0048] It should also be further understood that the term “and / or” as used in this application specification and the appended claims means any combination of one or more of the associated listed items and all possible combinations, and includes such combinations.

[0049] This embodiment provides a UAV gimbal, including a rotating assembly 1000 and a three-light assembly 2000. The rotating assembly 1000 includes: an upper cover 1001, a yaw stator 1002, a yaw motor 1003, a relay power board 1004, a yaw bracket 1005, an inner cavity 1005-1, a yaw inner sealing groove 1005-2, a front cavity 1005-3, a rear cavity 1005-4, a yaw rear sealing groove 1005-5, a yaw bracket front cover 1006, a yaw bracket rear cover 1007, an upper shield 1008, a hollow encoder 1009, a lower shield 1010, and a horizontal... Roller support front cover 1011, roll support left cover 1012, roll support right cover 1013, roll support 1014, second rear cavity 1014-1, second front cavity 1014-2, roll front sealing groove 1014-3, right first cavity 1014-4, roll right sealing groove 1014-5, right second cavity 1014-6, left cavity 1014-7, bearing 1015, auxiliary shaft 1016, pitch transition plate 1017, roll motor 1018, pitch motor 1019.

[0050] The surface of the yaw bracket 1005 is treated with conductive oxidation. The upper end is connected to the rotor of the yaw motor 1003. The stator of the yaw motor 1003 is fixedly connected to the yaw stator 1002 to form a yaw rotation joint. The relay power board 1004 is installed on the upper side of the yaw bracket 1005. The installation position is opposite to the mounting surface of the rotor of the yaw motor 1003. The mounting surface of the relay power board 1004 is completely conductively attached to the yaw bracket 1005 and seals the axial through hole of the yaw motor 1003, thereby relaying and isolating the circuits above the yaw joint.

[0051] A hollow encoder 1009 is installed inside the yaw stator 1002, and a cover 1001 is installed on the upper surface. The upper and lower surfaces of the hollow encoder 1009 are sealed with an upper shield 1008 and a lower shield 1010 respectively to prevent electromagnetic leakage of the hollow encoder 1009. The surfaces of the upper shield 1008 and the lower shield 1010 are treated with conductive material.

[0052] The inner cavity 1005-1 of the yaw bracket 1005 has an annular yaw inner sealing groove 1005-2 on its edge. The yaw inner sealing groove 1005-2 is used to install a conductive sealing strip. The front cover 1006 of the yaw bracket is installed inside the yaw bracket 1005 and presses down the conductive sealing strip.

[0053] The lower end of the yaw bracket 1005 is divided into two cavities, front and rear. The stator of the roll motor 1018 is fixed in the front cavity 1005-3, and the hollow encoder 1009 is installed in the rear cavity 1005-4. The upper and lower surfaces of the hollow encoder 1009 are sealed by the upper shield 1008 and the lower shield 1010, respectively. The rear end face of the rear cavity 1005-4 is provided with a yaw rear sealing groove 1005-5 for installing a conductive sealing strip. The rear cover 1007 of the yaw bracket is installed on this end face and presses down on the conductive sealing strip.

[0054] The rotor of the roll motor 1018 is installed in the second rear cavity 1014-1 of the roll bracket 1014, forming a roll joint.

[0055] A relay power board 1004 is installed in the second front cavity 1014-2 of the roll bracket 1014. The mounting surface of the relay power board 1004 is completely conductively attached to the roll bracket 1014 and seals the axial through hole of the roll motor 1018, thereby relaying and isolating the circuits of the roll joint and above.

[0056] The surface of the roll support 1014 is treated with conductive oxidation. The right cavity 1014-4 and the second front cavity 1014-2 are provided with a right roll sealing groove 1014-5 and a front roll sealing groove 1014-3 for installing conductive sealing strips. The right cover 1013 and the front cover 1011 of the roll support are respectively installed on the right side and the front side of the roll support 1014 and press down the conductive sealing strips.

[0057] A hollow encoder 1009 is installed in the right cavity 1014-4 of the roll bracket 1014. The upper and lower surfaces of the hollow encoder 1009 are sealed with an upper shield 1008 and a lower shield 1010, respectively, to prevent electromagnetic leakage of the hollow encoder 1009. The stator of the pitch motor 1019 is fixedly installed in the right cavity 1014-6 of the roll bracket 1014. The rotor of the pitch motor 1019 is fixedly connected to the pitch transition plate 1017 to form a pitch-rotation joint. A relay power board 1004 is installed on the other side of the pitch transition plate 1017. The mounting surface of the relay power board 1004 is completely conductively bonded to the roll bracket 1014 and seals the axial through hole of the roll motor 1019, thus relaying and isolating the circuit of the pitch joint and above.

[0058] The left cover 1012 of the roll bracket is installed at the outer end of the left cavity 1014-7 of the roll bracket 1014, and the bearing 1015 is installed at the end. The inner ring of the bearing 1015 is equipped with an auxiliary shaft 1016, and the threaded end of the auxiliary shaft 1016 is connected to the three-light assembly.

[0059] The three-light module 2000 includes a laser module 2001, a thermal imaging module 2002, a visible light module 2003, an upper shell 2004, an upper shell boss 2004-1, a right shell 2005, a front cover 2006, a lower shell 2007, a lower shell boss 2007-1, a left shell 2008, a rear cover 2009, a center shell front sealing groove 2010, a center shell rear sealing groove 2011, a center shell right sealing groove 2012, an expansion board 2013, a main board 2014, a middle shell 2015, a center shell assembly 2016, a center frame 2017, and a vision module 2018.

[0060] The upper shell 2004, right shell 2005, lower shell 2007, and left shell 2008 constitute the middle shell 2015. The middle shell 2015 contains a front sealing groove 2010 and a rear sealing groove 2011 for installing a conductive sealing strip. The front cover 2006 and rear cover 2009 are respectively installed at the front and rear ends of the middle shell 2015 and press down on the conductive sealing strip, forming the middle shell assembly 2016. The middle shell assembly 2016 has a sealed cavity with good conductivity and sealing performance. The inner surface is treated with conductive oxidation, and the outer surface is sprayed with a nano-carbon heat dissipation coating.

[0061] The vision module 2018 is installed inside the central shell assembly 2016. The central frame 2017 serves as the basic load-bearing frame for the vision module 2018 and is used to install the thermal imaging module 2002, the visible light module 2003, the expansion board 2013, and the main board 2014. The visible light module 2003 and the main board 2014 are the main heat sources and are respectively arranged at the upper and lower ends of the visible light module 2003. The separate arrangement of the main heat sources avoids the concentration of heat.

[0062] The inner surfaces of the upper shell 2004 and the lower shell 2007 are provided with dense upper shell bosses 2004-1 and lower shell bosses 2007-1. The upper shell bosses 2004-1 and lower shell bosses 2007-1 contact and conduct heat with the heat-generating chips on the motherboard 2014 and the expansion board 2013, respectively.

[0063] The outer side of the right shell 2005 is provided with a center shell right sealing groove 2012 for installing a conductive sealing strip. The right shell 2005 is fixedly connected to the pitch transition plate 1017 of the rotating assembly 1000, and the connection surfaces are electrically conductive to each other. The transition plate 1017 presses down on the conductive sealing strip in the center shell right sealing groove 2012.

[0064] The gimbal of this utility model works in concert with a rotating component (for attitude control) and a three-light component (integrated sensor). The rotating component is used to achieve yaw / roll / pitch control. The yaw motor drives the yaw bracket to rotate, thereby adjusting the gimbal in the horizontal direction. The roll motor controls the roll bracket to achieve lateral angle adjustment. The pitch motor adjusts the vertical angle of the three-light component through a pitch transition plate.

[0065] The hollow encoder seals electromagnetic leakage through upper and lower shields (conductive treatment); the relay power board seals the axial through hole of the motor and is conductively bonded to the bracket to form a continuous shielding layer.

[0066] The three-light module is used for sensor integration: thermal imaging, visible light, and laser modules are integrated into the central frame, and data acquisition and transmission are controlled by the motherboard; it also includes a heat dissipation mechanism, thermal design, and heat conduction through direct contact between the heat-generating chips of the motherboard and expansion board via the upper / lower shell bosses to conduct heat to the outer shell; nano-coating: the outer shell is sprayed with nano-carbon material to enhance radiative heat dissipation efficiency; sealing and shielding: the central shell assembly achieves full-enclosure shielding through conductive sealing strips (front / rear / right sealing grooves of the central shell); conductive oxidation treatment on the outer surface further blocks electromagnetic interference; overall workflow: attitude adjustment: during UAV flight, the rotating component adjusts the gimbal angle through motor drive to ensure that the three-light module is aligned with the target; data acquisition: the three-light module simultaneously acquires thermal imaging, visible light, and laser data, which are processed by the motherboard and transmitted to the ground terminal; thermal management: heat from the heat source is conducted to the outer shell through the bosses, combined with rapid heat dissipation through the nano-coating; electromagnetic protection: conductive seals and shielding covers suppress electromagnetic leakage throughout the process, adapting to complex environments such as high-voltage electric fields.

[0067] Although embodiments of the present invention have been shown and described above, it is understood that the above embodiments are exemplary and should not be construed as limiting the present invention. Those skilled in the art can make changes, modifications, substitutions and variations to the above embodiments within the scope of the present invention.

Claims

1. A drone gimbal, characterized in that: It includes a rotating assembly (1000) and a three-light assembly (2000), which are connected to each other; The rotating assembly (1000) includes a relay power board (1004), a yaw bracket front cover (1006), a yaw bracket rear cover (1007), an upper shield (1008), a hollow encoder (1009), a lower shield (1010), a roll bracket front cover (1011), a roll bracket left cover (1012), and a roll bracket right cover (1013).

2. The UAV gimbal according to claim 1, characterized in that: The rotating assembly (1000) also includes a top cover (1001), a yaw stator (1002), a yaw motor (1003), a yaw bracket (1005), a roll bracket (1014), a bearing (1015), an auxiliary rotating shaft (1016), a pitch transition plate (1017), a roll motor (1018), and a pitch motor (1019); the upper end of the yaw bracket (1005) is connected to the rotor of the yaw motor (1003), and the stator of the yaw motor (1003) is fixedly connected to the yaw stator (1002) to form a yaw rotation joint; The relay power board (1004) is installed on the upper side of the yaw bracket (1005), and the installation position is opposite to the rotor mounting surface of the yaw motor (1003). The mounting surface of the relay power board (1004) is completely conductively attached to the yaw bracket (1005) and seals the axial through hole of the yaw motor (1003).

3. The UAV gimbal according to claim 2, characterized in that: The yaw stator (1002) is equipped with a hollow encoder (1009), and the upper cover (1001) is installed on the upper surface of the yaw stator (1002). The upper and lower surfaces of the hollow encoder (1009) are sealed with an upper shield (1008) and a lower shield (1010) respectively to prevent electromagnetic leakage of the hollow encoder (1009). The surfaces of the upper shield (1008) and the lower shield (1010) are treated with conductive material.

4. A drone gimbal according to claim 3, characterized in that: The inner cavity (1005-1) of the yaw bracket (1005) has an annular yaw inner sealing groove (1005-2) at its edge. The yaw inner sealing groove (1005-2) is used to install a conductive sealing strip. The front cover (1006) of the yaw bracket is installed inside the yaw bracket (1005) and presses down on the conductive sealing strip. The lower end of the yaw bracket (1005) includes a front cavity (1005-3) and a rear cavity (1005-4). The front cavity (1005-3) is used to fix the stator of the roll motor (1018), and the rear cavity (1005-4) is used to install the hollow encoder (1009). The rear end face of the rear cavity (1005-4) is provided with a yaw rear sealing groove (1005-5) for installing a conductive sealing strip. The rear cover (1007) of the yaw bracket is installed on the end face of the yaw rear sealing groove (1005-5) and presses down the conductive sealing strip.

5. A drone gimbal according to claim 4, characterized in that: The rotor of the roll motor (1018) is installed in the second rear cavity (1014-1) of the roll bracket (1014), forming a roll joint; a relay power board (1004) is installed in the second front cavity (1014-2) of the roll bracket (1014), the mounting surface of the relay power board (1004) is completely conductively bonded to the roll bracket (1014), and the axial through hole of the roll motor (1018) is sealed. The surface of the roll bracket (1014) is treated with conductive oxidation. 014) also includes a right cavity (1014-4), the right cavity (1014-4) and the second front cavity (1014-2) are provided with a right rolling sealing groove (1014-5) and a front rolling sealing groove (1014-3), the right rolling sealing groove (1014-5) and the front rolling sealing groove (1014-3) are used to install conductive sealing strips, the right cover (1013) of the rolling bracket and the front cover (1011) of the rolling bracket are respectively installed on the right side and the front side of the rolling bracket (1014) and press down the conductive sealing strips.

6. A drone gimbal according to claim 4, characterized in that: A hollow encoder (1009) is installed in the rightmost cavity (1014-4) of the roll support (1014); the stator of the pitch motor (1019) is fixedly installed in the second right cavity (1014-6) of the roll support (1014). The rotor of the pitch motor (1019) is fixedly connected to the pitch transition plate (1017) to form a pitch-rotation joint. A relay power board (1004) is installed on the other side of the pitch transition plate (1017). The mounting surface of the plate (1004) is fully conductively bonded to the roll bracket (1014) and seals the axial through hole of the pitch motor (1019); the outer end of the left cavity (1014-7) of the roll bracket (1014) is used to install the left cover (1012) of the roll bracket, and the end is used to install the bearing (1015); the inner ring of the bearing (1015) is connected to the auxiliary shaft (1016), and the threaded end of the auxiliary shaft (1016) is connected to the three-light assembly (2000).

7. A drone gimbal according to claim 1, characterized in that: The three-light assembly (2000) includes a laser module (2001), a thermal imaging module (2002), a visible light module (2003), an upper shell (2004), a right shell (2005), a front cover (2006), a lower shell (2007), a left shell (2008), a rear cover (2009), a front sealing groove (2010) of the center shell, a rear sealing groove (2011) of the center shell, a right sealing groove (2012) of the center shell, an expansion plate (2013), a main board (2014), a middle shell (2015), a center shell assembly (2016), a central frame (2017), and a vision system. Module (2018); The middle shell (2015) is composed of an upper shell (2004), a right shell (2005), a lower shell (2007) and a left shell (2008). The middle shell (2015) contains a front sealing groove (2010) and a rear sealing groove (2011) for installing a conductive sealing strip. The front cover (2006) and the rear cover (2009) are respectively installed at the front and rear ends of the middle shell (2015) and press down the conductive sealing strip to form the middle shell assembly (2016).

8. A drone gimbal according to claim 7, characterized in that: The central shell assembly (2016) houses a vision module (2018); the central frame (2017) serves as the basic load-bearing frame for the vision module (2018) and is used to install the thermal imaging module (2002), the visible light module (2003), the expansion board (2013), and the motherboard (2014); the visible light module (2003) and the motherboard (2014) are the main heat sources and are respectively arranged at the upper and lower ends of the visible light module (2003).

9. A drone gimbal according to claim 8, characterized in that: The inner surfaces of the upper shell (2004) and lower shell (2007) are provided with dense upper shell bosses (2004-1) and lower shell bosses (2007-1). The upper shell bosses (2004-1) and lower shell bosses (2007-1) contact and conduct heat with the heat-generating chips on the motherboard (2014) and expansion board (2013), respectively.

10. A drone gimbal according to claim 9, characterized in that: The outer side of the right shell (2005) is provided with a central shell right sealing groove (2012) for installing a conductive sealing strip; the right shell (2005) is fixedly connected to the pitch transition plate (1017) of the rotating assembly (1000), and the connecting surfaces are electrically conductive to each other; the transition plate (1017) presses down on the conductive sealing strip in the central shell right sealing groove (2012).

Images