Air-cooled laser

Abstract

The present application provides an air-cooled laser. The air-cooled laser comprises a main body structure, an air supply assembly, and heating devices mounted on the main body structure. The main body structure comprises at least two sub-structures arranged along the axial direction of the main body structure; two adjacent sub-structures are detachably connected; each sub-structure comprises an inner-layer heat dissipation portion and an outer-layer heat dissipation portion arranged around the inner-layer heat dissipation portion; a heat dissipation channel is formed between the inner-layer heat dissipation portion and the outer-layer heat dissipation portion, and heat dissipation channels of adjacent sub-structures are communicated with each other; the air supply assembly enables an airflow to be formed in the heat dissipation channels; and heat dissipation members connected to the inner-layer heat dissipation portions and / or the outer-layer heat dissipation portions are provided in the heat dissipation channels. By providing, in the heat dissipation channels, the heat dissipation members connected to the inner-layer heat dissipation portions and / or the outer-layer heat dissipation portions, heat generated by the heating devices is conducted to the heat dissipation members by means of the inner-layer heat dissipation portions and / or the outer-layer heat dissipation portions, and the air supply assembly forms the airflow to take away the heat from the heat dissipation members, thereby improving heat dissipation efficiency of the heating devices.

Description

air-cooled laser Technical Field

[0001] This application relates to the field of fiber laser technology, specifically to an air-cooled laser. Background Technology

[0002] In related technologies, lasers contain heat-generating devices that generate a large amount of heat while performing laser functions, thus requiring effective heat dissipation. However, the heat dissipation methods in related technologies have low efficiency and are not suitable for lasers with high power or small size.

[0003] Therefore, air-cooled lasers in related technologies suffer from the technical problem of low heat dissipation efficiency. Summary of the Invention

[0004] The embodiments of this application provide an air-cooled laser that can improve the technical problem of low heat dissipation efficiency in existing air-cooled lasers.

[0005] Embodiments of this application provide a wind-cooled laser, comprising:

[0006] The main structure includes at least two substructures arranged axially along the main structure, each of which

[0007] The substructure includes an inner heat dissipation section and an outer heat dissipation section surrounding the inner heat dissipation section, with a heat dissipation channel formed between the inner and outer heat dissipation sections.

[0008] An air supply assembly, connected to the main structure, is used to drive gas, causing the diffuser...

[0009] Airflow is formed within the hot channel;

[0010] And heating devices installed on the main structure;

[0011] The two adjacent substructures are detachably connected, and the heat dissipation channels of the two adjacent substructures are interconnected. The heat dissipation channels are provided with heat dissipation components that are connected to the inner heat dissipation part and / or the outer heat dissipation part.

[0012] In one embodiment, the main structure includes a first substructure and a second substructure. The first substructure includes a plurality of first mounting planes distributed sequentially along the circumference. The second substructure is a cylindrical structure. The heat-generating device includes a pump source and an optical fiber. The pump source is disposed on the inner wall of the inner heat dissipation part of the first substructure and / or the first mounting plane of the outer heat dissipation part. The optical fiber is wound around the outer wall of the outer heat dissipation part of the second substructure.

[0013] In one embodiment, the heat sink is a fin, the fin in the first substructure is connected between the outer heat sink and / or the inner heat sink, and the fin in the second substructure is connected to the inner wall of the outer heat sink. The arrangement density of the fins in the first substructure is greater than the arrangement density of the fins in the second substructure.

[0014] In one embodiment, the substructure further includes a third substructure disposed on the side of the second substructure away from the first substructure along the axial direction. The third substructure includes a plurality of second mounting planes distributed sequentially along the circumference. The second mounting plane includes a first region and a second region. The heat generation of the heating device in the first region is greater than the heat generation of the heating device in the second region. The fins in the third substructure include a first fin and a second fin. The length of the first fin is greater than the length of the second fin. The first fin is disposed corresponding to the first region, and the second fin is disposed corresponding to the second region.

[0015] In one embodiment, the substructure further includes a third substructure disposed on the side of the second substructure away from the first substructure along the axial direction. The third substructure includes a plurality of second mounting planes distributed sequentially along the circumference. The heating device further includes a power board disposed on the second mounting plane. The power board includes a chip and other components. The power board is disposed on the inner wall of the inner heat dissipation portion of the third substructure. The fins are disposed on the outer wall of the inner heat dissipation portion and are disposed opposite to the chip. And / or the power board is disposed on the second mounting plane of the third substructure. The fins are disposed on the inner wall of the outer heat dissipation portion and are disposed opposite to the chip.

[0016] In one embodiment, the third substructure includes a plurality of second mounting planes arranged sequentially along the circumference. The substructure also includes a third substructure. At least one of the second mounting planes of the third substructure is further provided with a plurality of fins of the same length. The second mounting plane includes a central region and an edge region surrounding the central region. The heat generation of the heating device in the central region is greater than the heat generation of the heating device in the edge region, and the arrangement density of the heat sink in the central region is greater than the arrangement density of the heat sink in the edge region.

[0017] In one embodiment, the inner heat dissipation portion and the outer heat dissipation portion of the first substructure and the third substructure are both multi-faceted prism structures, the inner heat dissipation portion of the second substructure is a multi-faceted prism structure, and the outer heat dissipation portion of the second substructure is a cylindrical structure.

[0018] In one embodiment, the first mounting plane includes a first sub-surface and a second sub-surface arranged at intervals. A heating device is disposed on the first sub-surface, and the second sub-surface is offset from the heating device. The surface area of ​​the first sub-surface is greater than or equal to the surface area of ​​the second sub-surface, and the heat sink is disposed on the back side of the first sub-surface.

[0019] In one embodiment, the air supply assembly is provided at one end of the third substructure. The air supply assembly includes blades and a motor. The motor is located inside the inner heat dissipation part of the third substructure. The motor is used to drive the blades to rotate. A steering mechanism is also connected between the motor and the blades. The steering mechanism is used to adjust the rotation direction of the blades to achieve the steering of the air-cooled laser.

[0020] In one embodiment, the blade includes a first part and a second part connected to each other. The first part is aligned with the heat dissipation channel and is used to drive gas to form an airflow in the heat dissipation channel. The second part is located outside the first part and is used to realize the lifting and lowering of the air-cooled laser. The angle between the second part and the plane perpendicular to the axial direction is less than or equal to the angle between the first part and the plane perpendicular to the axial direction.

[0021] The beneficial effects of the embodiments of this application are as follows:

[0022] In the embodiments of this application, the air-cooled laser is divided into at least two axially arranged substructures, with adjacent substructures being detachably connected. Each substructure includes an inner heat dissipation section, an outer heat dissipation section, and a heat dissipation channel located between the inner and outer heat dissipation sections. Adjacent heat dissipation channels are connected. A heat dissipation component is disposed within the heat dissipation channel and connected to the inner and / or outer heat dissipation sections, so that both the inner and / or outer heat dissipation sections can be thermally connected to the heat dissipation component. The air supply component forms an airflow within the heat dissipation channel to remove heat from the heat dissipation component, thereby improving the heat dissipation efficiency of the heat-generating device. Attached Figure Description

[0023] To more clearly illustrate the technical solutions in the embodiments of this application, the accompanying drawings used in the description of the embodiments will be briefly introduced below. Obviously, the accompanying drawings described below are only some embodiments of this application. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0024] Figure 1 is a first perspective view of a wind-cooled laser provided in an embodiment of this application;

[0025] Figure 2 is a three-dimensional schematic diagram of the inner side of the air-cooled laser housing in Figure 1 from a first viewing angle, provided in an embodiment of this application.

[0026] Figure 3 is an exploded schematic diagram of an air-cooled laser provided in an embodiment of this application;

[0027] Figure 4 is a second perspective view of the air-cooled laser provided in the embodiments of this application;

[0028] Figure 5 is a perspective view of the inner side of the air-cooled laser housing in Figure 4 from a second perspective, provided in an embodiment of this application.

[0029] Figure 6 is a three-dimensional schematic diagram of the inner side of the air-cooled laser housing provided in an embodiment of this application, viewed from a third perspective.

[0030] Figure 7 is a cross-sectional schematic diagram along the axis of the air-cooled laser provided in the embodiment of this application;

[0031] Figure 8 is a schematic diagram of the air-cooled laser provided in the embodiment of this application, viewed from the bottom.

[0032] Figure 9 is a cross-sectional schematic diagram of the first substructure of the air-cooled laser provided in an embodiment of this application;

[0033] Figure 10 is a cross-sectional schematic diagram of the second substructure of the air-cooled laser provided in an embodiment of this application;

[0034] Figure 11 is a cross-sectional schematic diagram of the third substructure of the air-cooled laser provided in an embodiment of this application. Detailed Implementation

[0035] 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 a part of the embodiments of this application, and not all of the 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. In addition, it should be understood that the specific embodiments described herein are only for illustration and explanation of this application and are not intended to limit this application. In this application, unless otherwise stated, directional terms such as "upper" and "lower" generally refer to the upper and lower positions of the device in actual use or operation, specifically the drawing directions in the accompanying drawings; while "inner" and "outer" refer to the outline of the device.

[0036] Furthermore, the terms "first," "second," and similar words do not indicate any order, quantity, or importance, but are merely used to distinguish different technical features. The terms "multiple" and similar words indicate two or more unless otherwise expressly specified.

[0037] The air-cooled laser provided in the embodiments of this application includes a main structure 1, an air supply assembly 2, a heat-generating device 3, and a heat sink 4. The main structure 1 includes at least a first substructure 11, a second substructure 12, and a third substructure 13 arranged sequentially along the axial direction of the main structure 1. The first substructure includes a plurality of first mounting planes arranged sequentially along the circumference. The third substructure includes a plurality of second mounting planes arranged sequentially along the circumference. The second substructure 12 is a cylindrical structure. The first substructure 11, the second substructure 12, and the third substructure 13 each include an inner heat sink 14 and an outer heat sink 15 disposed around the inner heat sink 14. A heat dissipation channel 5 is formed between the inner heat sink 14 and the outer heat sink 15. The first substructure 11, the second substructure 12, and the third substructure 13... The heat dissipation channels 5 within substructure 13 are interconnected; the air supply assembly 2 is located at at least one end of the main structure 1, and is used to drive gas to form airflow within the heat dissipation channels 5. The air supply assembly 2 includes blades 21 and a motor 22. The motor 22 is located inside the inner heat dissipation section 14 of the third substructure 13, and the blades 21 are located at the end of the third substructure 13 away from the second substructure 12; the heat-generating device 3 includes a pump source 31, a power supply board 33, and an optical fiber 32. The pump source 31 is located on the inner wall of the inner heat dissipation section 14 of the first substructure 11 and / or the first mounting plane of the outer heat dissipation section 15. The optical fiber 32 is located on the outer wall of the outer heat dissipation section 15 of the second substructure 12. The power supply board 33 is located on the inner wall of the inner heat dissipation section 14 of the third substructure 13 and / or the first mounting plane of the outer heat dissipation section 15. / or the second mounting plane of the outer heat dissipation part 15; the heat dissipation component 4 is connected to the outer wall of the inner heat dissipation part 14 and / or the inner wall of the outer heat dissipation part 15, the arrangement density of the heat dissipation component 4 in the first substructure 11 is greater than the arrangement density of the heat dissipation component 4 in the second substructure 12, the third substructure 13 includes a first region corresponding to the chip and a second region corresponding to the other components, the heat generation of the heat-generating device 3 in the first region is greater than the heat generation of the heat-generating device 3 in the second region, the heat dissipation component 4 in the third substructure 13 includes a first fin 41 and a second fin 42, the length of the first fin 41 is greater than the length of the second fin 42, the first fin 41 is disposed in the first region, and the second fin 42 is disposed in the second region; at least one of the first of the third substructures The second mounting plane is also provided with a plurality of fins of the same length. The second mounting plane includes a central region and an edge region surrounding the central region. The heat generation of the heating device 3 in the central region is greater than that of the heating device 3 in the edge region. The arrangement density of the heat sink 4 in the central region is greater than that of the heat sink 4 in the edge region. The blade 21 includes a first part 201 and a second part 202 connected to each other. The first part 201 is aligned with the heat dissipation channel 5. The second part 202 is located outside the first part 201. The angle between the second part 202 and the plane perpendicular to the axial direction is less than or equal to the angle between the first part 201 and the plane perpendicular to the axial direction.

[0038] Please refer to Figures 1 to 11. Another air-cooled laser provided by the embodiments of this application includes a main structure 1, an air supply assembly 2, and a heat-generating device 3 mounted on the main structure 1. The main structure 1 includes at least two substructures arranged along the axial direction of the main structure 1. Each substructure includes an inner heat dissipation part 14 and an outer heat dissipation part 15 disposed around the inner heat dissipation part 14. A heat dissipation channel 5 is formed between the inner heat dissipation part 14 and the outer heat dissipation part 15. The air supply assembly 2 is connected to the main structure 1 and is used to drive gas to form an airflow in the heat dissipation channel 5. Two adjacent substructures are detachably connected, and the heat dissipation channels 5 of adjacent substructures are interconnected. A heat dissipation element 4 connected to the inner heat dissipation part 14 and / or the outer heat dissipation part 15 is provided in the heat dissipation channel 5.

[0039] Among them, at least two substructures are spliced ​​together along the axial direction of the main structure 1.

[0040] In this embodiment, the air-cooled laser is divided into at least two axially arranged substructures, each substructure including an inner heat dissipation section 14, an outer heat dissipation section 15, and a heat dissipation channel 5 located between the inner heat dissipation section 14 and the outer heat dissipation section 15. Adjacent heat dissipation channels 5 are connected. A heat dissipation component 4 is provided in the heat dissipation channel 5 and connected to the inner heat dissipation section 14 and / or the outer heat dissipation section 15. The air supply component 2 causes airflow to form in the heat dissipation channel 5 and carries away the heat of the heat dissipation component 4, thereby improving the heat dissipation efficiency of the heat-generating device 3.

[0041] The technical solution of this application will now be described in conjunction with specific embodiments.

[0042] In one embodiment, please refer to Figures 1, 3, and 4. The air-cooled laser also includes a housing 6, in which a receiving cavity is formed, and the main structure 1 is housed within the receiving cavity.

[0043] In one embodiment, referring to Figures 2, 3, 5, and 6, the main structure 1 includes a first substructure 11 and a second substructure 12. The first substructure 11 includes a plurality of first mounting planes distributed sequentially along the circumference. The second substructure 12 is a cylindrical structure. The heating device 3 includes a pump source 31 and an optical fiber 32. The pump source 31 is disposed on the inner wall of the inner heat dissipation part 14 of the first substructure 11 and / or the first mounting plane of the outer heat dissipation part 15. The optical fiber 32 is wound around the outer wall of the outer heat dissipation part 15 of the second substructure 12.

[0044] The heating device 3 can also be at least one of the following: fiber optic coupler 32, main control board, and power supply board 33.

[0045] An adhesive layer is provided between the heating element 3 and the main structure 1, and the heating element 3 and the main structure 1 can be bonded together by the adhesive layer, which can be double-sided adhesive.

[0046] The heating element 3 can also be fixed to the main structure 1 by snapping it into the main structure 1, or by connecting the heating element 3 to the main structure 1 with bolts and screw holes.

[0047] The main structure 1 includes multiple first mounting planes and cylindrical structures as substructures to facilitate assembly with different heating devices 3.

[0048] It is understood that the first substructure 11 includes multiple first mounting planes distributed sequentially along the circumference. The first mounting planes are relatively flat and facilitate the installation of any one of the fiber optic coupler 32, main control board, power supply board 33, and pump source 31. The second substructure 12 is a cylindrical structure with an arc surface on the outer wall. The arc surface is conducive to the winding and setting of the fiber optic 32. The fiber optic 32 is wound on the arc surface to reduce the overall volume of the air-cooled laser.

[0049] It should be noted that the inner heat dissipation part 14 and the outer heat dissipation part 15 of the first substructure 11 are both multi-faceted prism structures, the inner heat dissipation part 14 of the second substructure 12 is a multi-faceted prism structure, and the outer heat dissipation part 15 of the second substructure 12 is a cylindrical structure. The multi-faceted prism structure can be used to set up the fiber optic coupler 32, the main control board, the power board 33, and the pump source 31, while the cylindrical structure can be used to set up the fiber optic 32.

[0050] It is worth noting that the outer wall of the outer heat dissipation part 15 of the second substructure 12 may be provided with a fiber routing groove surrounding the outer heat dissipation part 15. The fiber routing groove surrounds the second substructure 12, and the optical fiber 32 is located in the fiber routing groove. By placing the optical fiber 32 in the fiber routing groove, on the one hand, the bonding strength between the optical fiber 32 and the outer heat dissipation part 15 of the second substructure 12 can be enhanced. On the other hand, since only a part of the optical fiber 32 is located in the fiber routing groove, by hiding the optical fiber 32 in the fiber routing groove, the overall volume of the air-cooled laser is further reduced.

[0051] In this embodiment, the main structure 1 includes at least a multi-faceted prism structure and a cylindrical structure arranged along the axial direction. The multi-faceted prism structure and the cylindrical structure provide different surfaces for setting the heating device 3, so as to facilitate the assembly with different heating devices 3 and reduce the overall volume of the air-cooled laser.

[0052] In one embodiment, referring to Figures 9 and 10, the heat sink 4 is a fin. The fins in the first substructure 11 are connected between the outer heat sink 15 and / or the inner heat sink 14. The fins in the second substructure 12 are connected to the inner wall of the outer heat sink 15. The fin density in the first substructure 11 is greater than the fin density in the second substructure 12.

[0053] The first substructure 11 may have a heating device 3 provided only on the first mounting plane of the outer heat dissipation part 15, and the fins in the first substructure 11 may be connected only to the inner wall of the outer heat dissipation part 15.

[0054] The first substructure 11 may have a heating device 3 provided only on the inner wall of the inner heat dissipation part 14, and the fins in the first substructure 11 may be connected only to the outer wall of the inner heat dissipation part 14.

[0055] In this substructure, the first mounting plane of the outer heat dissipation part 15 and the inner wall of the inner heat dissipation part 14 can both be provided with heat-generating devices 3, and the fins in the first substructure 11 are connected between the inner wall of the outer heat dissipation part 15 and the outer wall of the inner heat dissipation part 14.

[0056] The main structure 1 includes two opposite ports, which are connected to the heat dissipation channel 5.

[0057] It is understandable that since the heat-generating device 3 set in the first substructure 11 is a pump source 31, its heat generation is greater than that of the optical fiber 32 set on the outer wall of the outer heat dissipation part 15 of the second substructure 12. This results in the fin density corresponding to the pump source 31 being greater than the fin density corresponding to the optical fiber 32. By increasing the fin density corresponding to the pump source 31, the heat dissipation efficiency of the pump source 31 is improved, so that the pump source 31, which generates more heat, can be better dissipated compared to the optical fiber 32, which generates less heat.

[0058] Understandably, the heat dissipation principle of the fins is as follows: the fins are arranged opposite to the heating device 3, and the fins are located on the back side of the surface on which the heating device 3 is located. The heat from the heating device 3 is conducted to the fins through the outer heat dissipation part 15 and / or the inner heat dissipation part 14. The air supply component 2 forms an airflow in the heat dissipation channel 5. The airflow enters the heat dissipation channel 5 from the port on the side where the air supply component 2 is located, and is transmitted along the heat dissipation channel 5 to the port on the other side and discharged to the outside. The airflow carries away the heat from the fins to achieve heat dissipation of the heating device 3.

[0059] It should be noted that since the main structure 1 includes an inner heat dissipation part 14 and an outer heat dissipation part 15, both the inner heat dissipation part 14 and the outer heat dissipation part 15 can be equipped with heat-generating devices 3. On the one hand, the heat-generating devices 3 can be hidden inside the inner heat dissipation part 14, which can reduce the overall volume of the air-cooled laser. On the other hand, the light-emitting device can be thermally connected to the fins through both the inner heat dissipation part 14 and the outer heat dissipation part 15, thereby improving the heat dissipation efficiency of the heat-generating devices 3.

[0060] In this embodiment, the heat dissipation efficiency of the pump source 31 inside the first substructure 11 is enhanced by making the fin density inside the first substructure 11 greater than that inside the second substructure 12.

[0061] In one embodiment, the air supply assembly 2 may also be disposed between adjacent substructures.

[0062] In one embodiment, referring to Figures 3 and 11, the substructure further includes a third substructure 13. The third substructure 13 is disposed on the side of the second substructure 12 away from the first substructure 11 along the axial direction. The third substructure 13 includes a plurality of second mounting planes distributed sequentially along the circumference. The third substructure 13 includes a first region and a second region. The heat generation of the heating device 3 in the first region is greater than the heat generation of the heating device 3 in the second region. The fins in the third substructure 13 include a first fin 41 and a second fin 42. The length of the first fin 41 is greater than the length of the second fin 42. The first fin 41 is disposed in the first region, and the second fin 42 is disposed in the second region.

[0063] The heat dissipation area of ​​the first fin 41 is larger than that of the second fin 42, which makes the heat dissipation efficiency of the first fin 41 greater than that of the second fin 42.

[0064] It is understandable that a first fin 41 can be provided in a first region that generates more heat than the second region. The first fin 41 is longer than the second fin 42 and has a larger heat dissipation area, thereby improving the heat dissipation efficiency of the corresponding position of the chip.

[0065] In one embodiment, referring to Figures 3, 6, and 7, the substructure further includes a third substructure 13. The third substructure 13 is disposed on the side of the second substructure 12 away from the first substructure 11 along the axial direction. The third substructure 13 includes a plurality of second mounting planes distributed sequentially along the circumference. The heat-generating device 3 also includes a power board 33. The power board 33 includes a chip and other components. The power board 33 is disposed on the inner wall of the inner heat dissipation part 14 of the third substructure 13, and the fins are disposed on the outer wall of the inner heat dissipation part 14 and are disposed opposite to the chip; and / or; the power board 33 is disposed on the second mounting plane of the outer heat dissipation part 15 of the third substructure 13, and the fins are disposed on the inner wall of the outer heat dissipation part 15 and are disposed opposite to the chip.

[0066] The fins can be offset from other components.

[0067] It is understandable that since the heat generated by the power board 33 mainly comes from the chip, while the heat generated by other components is low or non-existent, by not setting fins in the relative positions of other parts, the number of fins can be reduced, leaving more space in the heat dissipation channel 5. In some embodiments, some heat-generating devices 3 can also be set in the side wall of the heat dissipation channel 5. Since some heat-generating devices 3 are hidden in the heat dissipation channel 5, they do not occupy the overall volume of the air-cooled laser, thus reducing the overall volume of the air-cooled laser.

[0068] In one embodiment, referring to FIG6, the inner heat dissipation part 14 and the outer heat dissipation part 15 of the first substructure 11 and the third substructure 13 are both multi-faceted prism structures, the inner heat dissipation part 14 of the second substructure 12 is a multi-faceted prism structure, and the outer heat dissipation part 15 of the second substructure 12 is a cylindrical structure.

[0069] The top surface of the aforementioned polyhedral prism structure can be any one of a regular hexagon, a regular octagon, or a regular dodecagon.

[0070] In one embodiment, referring to FIG5, the first mounting plane includes a first sub-surface and a second sub-surface arranged at intervals. The first sub-surface is provided with a heating device 3, and the second sub-surface is staggered from the heating device 3. The surface area of ​​the first sub-surface is greater than or equal to the surface area of ​​the second sub-surface, and the heat sink 4 is provided on the back side of the first sub-surface.

[0071] The second sub-surface may not have a heating element 3. The second sub-surface serves as a transition between adjacent first sub-surfaces and also helps to prevent the heating elements 3 on adjacent first sub-surfaces from interfering with or short-circuiting each other.

[0072] Both the first and second sub-faces can be rectangles.

[0073] It is understandable that, compared with air-cooled lasers in related technologies, this embodiment can effectively reduce the overall size of the laser by mounting the heating device close to the first sub-surface in the first mounting plane, making it easier to carry and thus improving the portability of the laser.

[0074] In one embodiment, referring to Figures 3 and 6, the heat-generating device 3 further includes an optical cable head 9, which is disposed on the first mounting plane of the outer heat dissipation portion 15 of the first substructure 11.

[0075] In one embodiment, please refer to Figures 3, 6, 7 and 8. One end of the third substructure 13 is provided with an air supply component 2. The air supply component 2 includes blades 21 and a motor 22. The motor 22 is located inside the inner heat dissipation part 14 of the third substructure 13. The motor 22 is used to drive the blades 21 to rotate. A steering mechanism 10 is also connected between the motor 22 and the blades 21. The steering mechanism 10 is used to adjust the rotation direction of the blades 21.

[0076] The motor 22 is connected to the blade 21 via a rotating shaft. The motor 22 drives the rotating shaft to rotate, thereby realizing the rotation of the blade 21.

[0077] Among them, blade 21 is located at the end of the third substructure 13 that is far away from the first substructure 11.

[0078] Multiple blades 21 rotate around the same center to form a fan, and the number of blades 21 can be any of 4, 6, 8, 10 or 12.

[0079] Among them, adjacent blades 21 are arranged at equal intervals.

[0080] Among them, multiple blades 21 can be arranged in a centrally symmetrical manner about the same center.

[0081] It is understandable that the steering mechanism 10 is connected between the electrode and the blade 21. The steering mechanism 10 can be used to adjust the offset direction of the rotating shaft, so that the rotation direction of the blade 21 connected to the rotating shaft is improved. When the wind-cooled laser is applied to the drone, the rotation of the blade 21 can also play the role of the drone's take-off, landing and steering.

[0082] It should be noted that the steering mechanism 10 may also include multiple sub-steering units, each of which can be individually connected to a blade 21. The multiple blades 21 are set independently of each other, so that the rotation direction of each blade 21 can be individually controlled through the sub-steering units, thereby better adjusting the movement of the UAV in different directions.

[0083] In this embodiment, the air supply assembly 2 also includes blades 21, a motor 22, and a steering mechanism 10. The steering mechanism 10 is used to adjust the rotation direction of the blades 21, so that the air-cooled laser can be applied to drones. The air supply assembly 2 of the air-cooled laser can realize the functions of drone lifting, turning and steering.

[0084] In one embodiment, referring to Figures 2, 5, and 6, the blade 21 includes a first part 201 and a second part 202 connected to each other. The first part 201 is aligned with the heat dissipation channel 5, and the second part 202 is located outside the first part 201. The angle between the second part 202 and the plane perpendicular to the axial direction is less than or equal to the angle between the first part 201 and the plane perpendicular to the axial direction.

[0085] The fan also includes an annular portion, with a first portion 201 connected to the inner wall of the annular portion and a second portion 202 connected to the outer wall of the annular portion. The first portion 201 and the second portion 202 rotate around the same center.

[0086] Understandably, the blade 21 can be fixed to the annular part. The first part 201 located inside the annular part is used to drive the gas to form an airflow in the heat dissipation channel 5. The second part 202 located outside the annular part is used to provide traction for the air-cooled laser or the drone containing the air-cooled laser, so that the air-cooled laser or the drone containing the air-cooled laser can rise, fall and turn under the drive of the air supply assembly 2.

[0087] It should be noted that since the second part 202 is fixed to the outer wall of the same annular part, when the drone containing the air-cooled laser needs to turn, the annular part is deflected relative to the plane perpendicular to the axis under the drive of the turning mechanism 10, so that the drone moves in the direction of the deflection and realizes the turning of the drone.

[0088] In this embodiment, the air-cooled component includes a first part 201 connected to the inner wall of the annular portion and a second part 202 connected to the outer wall of the annular portion. The second part 202 is used to drive the drone to rise, fall, and turn, thereby integrating the air-cooled laser into the drone. The drone does not need to be equipped with additional blades 21 for rising, falling, and turning.

[0089] The embodiments of this application have been described in detail above. Specific examples have been used to illustrate the principles and implementation methods of this application. The description of the above embodiments is only for the purpose of helping to understand the method and core ideas of this application. At the same time, for those skilled in the art, there will be changes in the specific implementation methods and application scope based on the ideas of this application. Therefore, the content of this specification should not be construed as a limitation of this application.

Claims

1. An air-cooled laser characterized by, include: The main structure includes at least two substructures arranged along the axial direction of the main structure. Each substructure includes an inner heat dissipation part and an outer heat dissipation part surrounding the inner heat dissipation part. A heat dissipation channel is formed between the inner heat dissipation part and the outer heat dissipation part. The main structure includes a first substructure and a second substructure. The first substructure includes a plurality of first mounting planes arranged sequentially along the circumference. The second substructure is a cylindrical structure. An air supply assembly is connected to the main structure. The air supply assembly is used to drive gas to form an airflow in the heat dissipation channel. and a heating device mounted on the main structure, the heating device including a pump source, the pump source being disposed on the inner wall of the inner heat dissipation part of the first substructure and the first mounting plane of the outer heat dissipation part, the first mounting plane including a first sub-surface and a second sub-surface arranged at intervals, the heating device being disposed on the first sub-surface, the second sub-surface being offset from the heating device, wherein the surface area of ​​the first sub-surface is greater than or equal to the surface area of ​​the second sub-surface; The substructures are detachably connected, and their heat dissipation channels are interconnected. Each heat dissipation channel contains a heat dissipation component connected to the inner heat dissipation section and / or the outer heat dissipation section. The heat dissipation component is located on the back side of the first substructure and is a fin. The density of the fins in the first substructure is greater than the density of the fins in the second substructure. The substructure also includes a third substructure located on the side of the second substructure away from the first substructure along the axial direction. The third substructure includes multiple second mounting planes distributed circumferentially. Each second mounting plane includes a first region and a second region. The heat output of the heating element in the first region is greater than that in the second region. The fins in the third substructure include a first fin and a second fin. The length of the first fin is greater than that of the second fin. The first fin corresponds to the first region, and the second fin corresponds to the second region. The third substructure has an air supply assembly at one end, which includes blades and a motor. The motor is located inside the inner heat dissipation section of the third substructure. The motor drives the blades to rotate. A steering mechanism is connected between the motor and the blades to adjust the rotation direction of the blades. The steering mechanism also includes multiple sub-steering sections, each connected to a blade. The multiple blades are independently arranged. Each blade includes a first part and a second part connected to each other. The blade also includes an annular part. The first part is connected to the inner wall of the annular part, and the second part is connected to the outer wall of the annular part. The first part and the second part rotate around the same center. The first part is aligned with the heat dissipation channel and drives the gas to form an airflow in the heat dissipation channel. The second part is located outside the first part and is used to raise and lower the air-cooled laser. The angle between the second part and the plane perpendicular to the axial direction is less than or equal to the angle between the first part and the plane perpendicular to the axial direction.

2. The air-cooled laser of claim 1, wherein, The heating device includes an optical fiber, which is wound around the outer wall of the outer heat dissipation part of the second substructure.

3. The air-cooled laser of claim 2, wherein, The fins in the first substructure are connected between the outer heat dissipation part and / or the inner heat dissipation part, and the fins in the second substructure are connected to the inner wall of the outer heat dissipation part.

4. The air-cooled laser of claim 3, wherein, The third substructure includes a plurality of second mounting planes arranged sequentially along the circumference. The heating device further includes a power board disposed on the second mounting plane. The power board includes a chip and other components. The power board is disposed on the inner wall of the inner heat dissipation part of the third substructure. The fins are disposed on the outer wall of the inner heat dissipation part and are disposed opposite to the chip. And / or the power board is disposed on the second mounting plane of the third substructure. The fins are disposed on the inner wall of the outer heat dissipation part and are disposed opposite to the chip.

5. The air-cooled laser of claim 3, wherein, The third substructure includes a plurality of second mounting planes distributed sequentially along the circumference. At least one of the second mounting planes of the third substructure is further provided with a plurality of fins of the same length. The second mounting plane includes a central region and an edge region surrounding the central region. The heat generation of the heating device in the central region is greater than the heat generation of the heating device in the edge region, and the arrangement density of the heat sink in the central region is greater than the arrangement density of the heat sink in the edge region.

6. The air-cooled laser of any one of claims 4-5, wherein, The inner and outer heat dissipation parts of the first and third substructures are both multi-faceted prism structures, the inner heat dissipation part of the second substructure is a multi-faceted prism structure, and the outer heat dissipation part of the second substructure is a cylindrical structure.

7. The air-cooled laser of claim 6, wherein, The first mounting plane comprises a first sub-plane and a second sub-plane arranged in a spaced manner, the first sub-plane is provided with the heat generating device, and the second sub-plane is arranged staggered with the heat generating device, wherein the surface area of the first sub-plane is greater than or equal to the surface area of the second sub-plane, and the heat dissipation device is arranged on the back surface of the first sub-plane.

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