Cabin radiator support device and working method thereof

Abstract

The invention provides a cabin radiator support device and a working method thereof, and relates to the technical field of wind power generation equipment. The cabin radiator support device comprises a rotating track which is rotatably arranged on the top of a cabin; the support module comprises a main supporting rod, and one end of the main supporting rod is hinged to the rotating track; the bracket module has a first state of rotating to a first direction and a second state of rotating to a second direction under the driving of the rotating track; the first diagonal draw bar assembly is hinged to the top of the cabin, in the first state, the first diagonal draw bar assembly is hinged to the main supporting rod, and the inclination angle of the main supporting rod in the first state is adjusted through stretching and retracting of the first diagonal draw bar assembly; and the second diagonal draw bar assembly is hinged to the top of the cabin, in the second state, the second diagonal draw bar assembly is hinged to the main supporting rod, and the inclination angle of the main supporting rod in the second state is adjusted through stretching and retracting of the second diagonal draw bar assembly. According to the cabin radiator support device, height limiting obstruction can be avoided, and disassembly operation is not needed.

Description

Technical Field

[0001] The present application relates to the technical field of wind power generation equipment, and in particular to a cabin radiator bracket device and a working method thereof. Background Art

[0002] The heat dissipation bracket structure designed on the top of the offshore wind turbine nacelle can reduce the number of unit interfaces. At the same time, the air on the top circulates quickly, providing an efficient solution for faster heat dissipation of the unit. Therefore, almost all wind turbine nacelle heat dissipation brackets in the industry are currently designed on the top.

[0003] However, as offshore turbines become larger and larger, the external dimensions of the huge turbine structures have increased significantly, especially the height limit problem for turbine transportation, which has gradually become a common problem in the entire wind power industry.

[0004] In the existing technology, the height limit problem is usually solved by completely removing the top heat dissipation bracket of the wind turbine. However, the overall installation of the top heat dissipation bracket is difficult, especially for large-megawatt offshore units. When installed as a whole, the center of gravity is difficult to accurately align, and it is easy to fall from a high altitude. In addition, the wind load during on-site installation at sea is extremely large, which is extremely dangerous. Summary of the Invention

[0005] In view of the above problems, the present application provides a cabin radiator bracket device and a working method thereof, which are used to solve the problem that the fan top heat dissipation bracket in the prior art is fixed and cannot be adjusted, and is difficult to solve the height limitation problem.

[0006] In order to achieve the above objectives, the embodiments of the present application provide the following technical solutions:

[0007] A first aspect of an embodiment of the present application provides a cabin radiator bracket device, comprising:

[0008] A rotating track is rotatably arranged on the top of the cabin;

[0009] The support module includes a main support rod, one end of which is hinged to the rotating track; the support module is driven by the rotating track to rotate to a first state along a first direction and a second state along a second direction, the first direction and the second direction intersecting;

[0010] a first diagonal tie rod assembly hinged to the top of the nacelle, wherein in a first state, the first diagonal tie rod assembly is hinged to the main strut, and the first diagonal tie rod assembly is telescopically adapted to adjust an inclination angle of the main strut in the first state;

[0011] The second diagonal brace assembly is hinged to the top of the cabin. In the second state, the second diagonal brace assembly is hinged to the main support rod. The second diagonal brace assembly adjusts the inclination angle of the main support rod in the second state by telescoping.

[0012] In a possible implementation, the cabin radiator support device further includes:

[0013] A first support bracket is provided on the top of the nacelle; the first support bracket includes a plurality of first hinged portions, the plurality of first hinged portions are arranged in a row along a first direction; any first hinged portion is used to be hinged to the first inclined rod assembly;

[0014] The second support hanger is arranged on the top of the cabin; the second support hanger includes a plurality of second hinged parts, and the plurality of second hinged parts are arranged in a row along the second direction; any second hinged part is used to be hinged to the second inclined rod assembly.

[0015] In a possible embodiment, the first inclined tie rod assembly includes a first rod body and a first cylinder body, the first rod body is movably disposed in the first cylinder body, and the telescopic length of the first rod body relative to the first cylinder body is adjustable;

[0016] The second inclined rod assembly includes a second rod body and a second cylinder body. The second rod body is movably arranged in the second cylinder body. The telescopic length of the second rod body relative to the second cylinder body is adjustable.

[0017] In a possible implementation, the support module further includes:

[0018] An oblique support rod assembly, one end of which is hinged to the rotating track;

[0019] a first cross bar, one end of the first cross bar being hinged to the main support bar, and the other end of the first cross bar being hinged to an end of the diagonal support bar assembly away from the rotating track;

[0020] The second cross bar has one end hinged to the main support bar and the other end hinged to the diagonal support bar assembly; the diagonal support bar assembly, the first cross bar and the second cross bar are used for auxiliary support of the main support bar.

[0021] In a possible embodiment, the diagonal support rod assembly includes a third rod body, a third cylinder body and a fourth cylinder body, one end of the third rod body is movably arranged in the third cylinder body, and the other end is movably arranged in the fourth cylinder body, and the telescopic length of the third rod body relative to the third cylinder body and the fourth cylinder body is adjustable, the third cylinder body is hinged to the first cross bar and the second cross bar, and the fourth cylinder body is hinged to the top of the cabin.

[0022] In one possible embodiment, the bracket module includes two bracket units, each bracket unit includes a main support rod, a diagonal support rod assembly, and a first cross rod and a second cross rod hinged between the main support rod and the diagonal support rod assembly;

[0023] A base is provided on the rotating track, and the base is used for being hinged with the main support rod and the diagonal support rod assembly.

[0024] In one possible implementation, the bracket modules are arranged in pairs along the second direction on the top of the cabin;

[0025] The cabin radiator bracket device further includes an adjustment beam, which in the second state is connected between the main struts of the bracket modules arranged in pairs;

[0026] The adjusting beam includes a plurality of third hinged portions, and any third hinged portion is used for being hinged to the main support rod.

[0027] In a possible implementation, the cabin radiator support device further includes a detection module, which is disposed at an end of the main support rod away from the rotating track, and is used to detect a height-limited working condition.

[0028] A second aspect of an embodiment of the present application provides a method for operating the cabin radiator bracket device as described above, comprising:

[0029] Get the height limit condition;

[0030] Determine the required adjustment height of the bracket module based on the height-limited working condition;

[0031] The rotating track is driven to rotate and switch to the state required by the bracket module according to the required adjustment height; the hinge position of the inclined rod assembly on the supporting bracket is selected in the state required by the bracket module; and the telescopic length of the inclined rod assembly is adjusted in the required state.

[0032] In a possible implementation, the operating method of the cabin radiator bracket device further includes:

[0033] Obtain environmental conditions;

[0034] Determine the required adjustment angle of the bracket module based on the environmental conditions;

[0035] The rotating track is driven to rotate according to the adjustment angle required by the bracket module; the hinge position of the inclined rod assembly on the supporting bracket is selected according to the adjustment angle required by the bracket module; and the telescopic length of the inclined rod assembly is adjusted according to the adjustment angle required by the bracket module.

[0036] The cabin radiator bracket device provided in an embodiment of the present application has a rotating track that rotates and drives the bracket module to switch to a first state when the height limit of the passage is H1. In the first state, the main support rod is connected to the top of the cabin via a first diagonal rod assembly. The first diagonal rod assembly flexibly adjusts the main support rod's tilt angle α in the first state by telescoping, so that the main support rod's height can adapt to the passage's height limit H1, thereby avoiding height limit obstruction without requiring disassembly. When the passage's height limit is H2, where H2 is less than or equal to H1, the rotating track rotates and drives the bracket module to switch to a second state. In the second state, the main support rod is connected to the top of the cabin via a second diagonal rod assembly. The second diagonal rod assembly flexibly adjusts the main support rod's tilt angle β in the second state by telescoping, so that the main support rod's height can adapt to the passage's height limit H2, thereby avoiding height limit obstruction without requiring disassembly.

[0037] In addition to the technical problems solved by the embodiments of the present application described above, the technical features that constitute the technical solutions, and the beneficial effects brought about by the technical features of these technical solutions, other technical problems that can be solved by the cabin radiator bracket device and its working method provided by the embodiments of the present application, other technical features included in the technical solutions, and the beneficial effects brought about by these technical features will be further described in detail in the specific implementation methods. BRIEF DESCRIPTION OF THE DRAWINGS

[0038] In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, a brief introduction will be given below to the drawings required for use in the embodiments or the description of the prior art. Obviously, the drawings described below are some embodiments of the present application. For ordinary technicians in this field, other drawings can be obtained based on these drawings without any creative work.

[0039] Figure 1 A perspective view of a cabin radiator bracket device provided by an embodiment of the present application in a first state, wherein the bracket module is an integral structure and the main support rod is in a vertical state;

[0040] Figure 2 A perspective view of a cabin radiator bracket device provided by an embodiment of the present application in a first state, wherein the bracket module is a split structure and the main support rod is in a vertical state;

[0041] Figure 3 A perspective view of the cabin radiator bracket device provided in an embodiment of the present application in a second state;

[0042] Figure 4 A side view of a cabin radiator support device provided by an embodiment of the present application in a first state, wherein the main support rod is in a vertical state;

[0043] Figure 5 for Figure 4 A partial enlarged schematic diagram of point A in the middle;

[0044] Figure 6 A side view of a cabin radiator support device provided by an embodiment of the present application in a first state, wherein the main support rod is arranged at an angle α to the first direction;

[0045] Figure 7 for Figure 6 A partial enlarged schematic diagram of point B in the middle;

[0046] Figure 8 A front view of the cabin radiator support device provided by an embodiment of the present application in a second state, wherein the main support rod is arranged at an angle β to the second direction;

[0047] Figure 9 for Figure 8 A partial enlarged schematic diagram of point C in the middle.

[0048] Description of reference numerals:

[0049] 10. Rotating track; 11. Base; 12. Rotating drive module;

[0050] 20. Bracket module; 201. Bracket unit; 21. Main support rod; 22. Diagonal support rod assembly; 221. Third rod body; 222. Third cylinder body; 223. Fourth cylinder body; 23. First crossbar; 24. Second crossbar;

[0051] 31. First inclined rod assembly; 311. First rod body; 312. First cylinder; 32. First support bracket; 321. First hinged portion;

[0052] 41. Second inclined rod assembly; 411. Second rod body; 412. Second cylinder; 42. Second support bracket; 421. Second hinged portion;

[0053] 50. Adjusting beam; 51. Third hinge;

[0054] 60. Detection module;

[0055] 70. Nacelle body;

[0056] X, first direction; Y, second direction; Z, third direction. DETAILED DESCRIPTION

[0057] First, those skilled in the art should understand that these embodiments are merely used to explain the technical principles of this application and are not intended to limit the scope of protection of this application. Those skilled in the art may adjust them as needed to suit specific applications.

[0058] Secondly, it should be noted that in the description of the embodiments of this application, unless otherwise clearly specified or limited, the terms "connected" and "connection" should be understood in a broad sense. For example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection or an indirect connection through an intermediate medium, or it can be internal communication between two components. For those skilled in the art, the specific meanings of the above terms in the embodiments of this application can be understood according to the specific circumstances.

[0059] As described in the background technology, the top heat dissipation bracket of the wind turbine in the related technology faces the problem of height limit during transportation. The inventors have found that there are basically two structural forms of the top heat dissipation bracket structure of the wind turbine in the related technology. One is that the cabin frame and the top heat dissipation bracket are welded into a whole and installed as a whole before leaving the factory. The problem with this design is that if there is a height limit, the top bracket and the cabin frame have to be dismantled as a whole and reinstalled on site. The defects are obvious, and the rainproof sealing problem and the on-site installation efficiency are extremely low; the other is that the cabin frame is a whole and the heat dissipation bracket is a whole. If there is a height limit problem, the top heat dissipation bracket needs to be dismantled as a whole, and after passing the height limit position, it is reconnected with bolts. The defect of this design is that the top bracket is difficult to install as a whole, especially for large-megawatt offshore units. It is difficult to accurately align the center of gravity when installing as a whole, and it is very easy to fall from a high altitude. Generally, the cabin height is more than eight meters, and the wind load for on-site installation at sea is extremely large, which is extremely dangerous.

[0060] In response to the above technical problems, an embodiment of the present application provides a cabin radiator bracket device and a working method thereof, wherein the cabin radiator bracket device includes: a rotating track, which is rotatably set on the top of the cabin; a bracket module, which includes a main support rod, and one end of the main support rod is hinged to the rotating track; driven by the rotating track, the bracket module has a first state of rotating to a first direction and a second state along a second direction, and the first direction intersects with the second direction; a first oblique rod assembly is hinged to the top of the cabin, and in the first state, the first oblique rod assembly is hinged to the main support rod, and the first oblique rod assembly is telescoped to adjust the inclination angle of the main support rod in the first state; a second oblique rod assembly is hinged to the top of the cabin, and in the second state, the second oblique rod assembly is hinged to the main support rod, and the second oblique rod assembly is telescoped to adjust the inclination angle of the main support rod in the second state.

[0061] When the height limit of the passage is H1, the rotating track rotates and drives the bracket module to switch to the first state; in the first state, the main support rod is connected to the top of the cabin via a first diagonal rod assembly. The first diagonal rod assembly flexibly adjusts the main support rod's tilt angle α in the first state by telescoping, so that the main support rod's height can adapt to the passage's height limit H1, thereby avoiding height limit obstruction without requiring disassembly. When the passage's height limit is H2, H2 is less than or equal to H1, and the rotating track rotates and drives the bracket module to switch to the second state; in the second state, the main support rod is connected to the top of the cabin via a second diagonal rod assembly. The second diagonal rod assembly flexibly adjusts the main support rod's tilt angle β in the second state by telescoping, so that the main support rod's height can adapt to the passage's height limit H2, thereby avoiding height limit obstruction without requiring disassembly.

[0062] In order to make the above-mentioned purposes, features and advantages of the embodiments of the present application more obvious and easy to understand, the technical solutions in the embodiments of the present application will be clearly and completely described below in conjunction with the drawings in the embodiments of the present application. Obviously, the described embodiments are only part of the embodiments of the present application, not all of the embodiments. Based on the embodiments in the present application, all other embodiments obtained by ordinary technicians in this field without making creative work are within the scope of protection of this application.

[0063] Please refer to Figures 1-9 According to a first aspect of an embodiment of the present application, a cabin radiator bracket device is provided, comprising:

[0064] The rotating track 10 is rotatably arranged on the top of the cabin;

[0065] The support module 20 includes a main support rod 21, one end of which is hinged to the rotating track 10. Driven by the rotating track 10, the support module 20 has a first state of rotating along a first direction X and a second state of rotating along a second direction Y, where the first direction X and the second direction Y intersect.

[0066] A first diagonal tie rod assembly 31 is hinged to the top of the nacelle. In a first state, the first diagonal tie rod assembly 31 is hinged to the main strut 21. The first diagonal tie rod assembly 31 is telescopic to adjust the inclination angle of the main strut 21 in the first state.

[0067] The second diagonal brace assembly 41 is hinged to the top of the nacelle. In the second state, the second diagonal brace assembly 41 is hinged to the main strut 21. The second diagonal brace assembly 41 is telescopic to adjust the inclination angle of the main strut 21 in the second state.

[0068] Please note that, see Figure 1As shown, the "first direction X" herein refers to the length direction of the cabin body 70; the "second direction Y" herein refers to the width direction of the cabin body 70; the "third direction Z" herein refers to the height direction of the cabin body 70; the first direction X, the second direction Y and the third direction Z intersect with each other.

[0069] In the embodiment of the present application, the rotating track 10 and the top of the cabin can be rotatably connected via a bearing; the rotation drive module 12 includes a motor and a transmission mechanism, and the rotating track 10 and the motor are connected via the transmission mechanism, which can be a gear mechanism. Figure 2 and Figure 3 As shown, the support module 20 is driven by the rotating track 10 to rotate to Figure 2 a first state along a first direction X as shown in FIG, and Figure 3 The second state along the second direction Y is shown in .

[0070] In the embodiment of the present application, the main support rod 21 of the bracket module 20 is the main force-bearing structure.

[0071] In the examples of this application, please see Figure 4 and Figure 5 As shown, when the channel height limit is H1, the rotating track 10 drives the bracket module 20 to switch to the first state by rotating; see Figure 6 and Figure 7 As shown, in the first state, the main strut 21 is connected to the top of the cabin through the first diagonal rod assembly 31. The first diagonal rod assembly 31 flexibly adjusts the inclination angle α of the main strut 21 in the first state by telescoping, so that the height of the main strut 21 can adapt to the height limit H1 of the channel, thereby avoiding height limit obstruction and no disassembly operation is required.

[0072] In the examples of this application, please see Figure 8 and Figure 9 As shown, when the height limit of the channel is H2, H2 is less than or equal to H1, and the rotating track 10 drives the bracket module 20 to switch to the second state by rotating; in the second state, the main support rod 21 is connected to the top of the cabin through the second diagonal rod assembly 41, and the second diagonal rod assembly 41 flexibly adjusts the inclination angle β of the main support rod 21 in the second state by telescoping, so that the height of the main support rod 21 can adapt to the height limit H2 of the channel, thereby avoiding height limit obstacles, and no disassembly operation is required.

[0073] In one possible implementation, see Figure 5 、 Figure 7 and Figure 9 As shown, the cabin radiator support device also includes:

[0074] The first support bracket 32 ​​is provided on the top of the nacelle; the first support bracket 32 ​​includes a plurality of first hinged portions 321, and the plurality of first hinged portions 321 are arranged in a row along the first direction X; any first hinged portion 321 is used to be hinged to the first inclined rod assembly 31;

[0075] The second support mount 42 is provided on the top of the cabin; the second support mount 42 includes a plurality of second hinged portions 421 , which are arranged in a row along the second direction Y; any second hinged portion 421 is used to be hinged to the second diagonal rod assembly 41 .

[0076] In the embodiment of the present application, a first support bracket 32 ​​is provided on the top of the cabin, and the first support bracket 32 ​​includes a plurality of first hinged portions 321 arranged in a row along the first direction X. Figure 5 and Figure 7 As shown, in the first state, one end of the first diagonal rod assembly 31 is hinged to the main support rod 21, and the other end is hinged to one of the multiple first hinge parts 321, so as to preliminarily adjust the inclination angle α of the main support rod 21 in the first state; then, by controlling the telescopic length of the first diagonal rod assembly 31, the inclination angle α of the main support rod 21 in the first state is further adjusted, which can not only expand the adjustment range of the inclination angle α of the main support rod 21, but also ensure the accuracy of the adjustment of the inclination angle α of the main support rod 21.

[0077] In the embodiment of the present application, a second support bracket 42 is provided on the top of the cabin, and the second support bracket 42 includes a plurality of second hinged portions 421 arranged in a row along the second direction Y. Figure 9 As shown, in the second state, one end of the second diagonal rod assembly 41 is hinged to the main support rod 21, and the other end is hinged to one of the multiple second hinge parts 421, so as to preliminarily adjust the inclination angle β of the main support rod 21 in the second state; and then by controlling the telescopic length of the second diagonal rod assembly 41, the inclination angle β of the main support rod 21 in the second state is further adjusted, which can not only expand the adjustment range of the inclination angle β of the main support rod 21, but also ensure the accuracy of the adjustment of the inclination angle β of the main support rod 21.

[0078] Furthermore, the first support hanger 32 and the second support hanger 42 can be installed by nesting or bolt connection, so as to facilitate disassembly. When the tilt angle adjustment of the bracket module 20 cannot meet the height limit, it can be used as an emergency backup plan.

[0079] In one possible implementation, see Figure 5 As shown, the first inclined rod assembly 31 includes a first rod body 311 and a first cylinder body 312. The first rod body 311 is movably disposed in the first cylinder body 312. The telescopic length of the first rod body 311 relative to the first cylinder body 312 is adjustable.

[0080] See Figure 9 As shown, the second inclined rod assembly 41 includes a second rod body 411 and a second cylinder body 412 . The second rod body 411 is movably disposed in the second cylinder body 412 , and the telescopic length of the second rod body 411 relative to the second cylinder body 412 is adjustable.

[0081] It should be noted that the first oblique rod assembly 31 and the second oblique rod assembly 41 can be configured as electric push rods or hydraulic cylinders, so as to realize the extension and retraction of the first oblique rod assembly 31 and the second oblique rod assembly 41, and then adjust the inclination angle of the main support rod 21; the first oblique rod assembly 31 and the second oblique rod assembly 41 further have a self-locking function, so as to keep the inclination angle in the specified state unchanged.

[0082] In the embodiment of the present application, by adjusting the telescopic length of the first rod body 311 relative to the first cylinder 312, the length of the first diagonal rod assembly 31 is adjusted, and then the inclination angle α of the main support rod 21 in the first state is adjusted; by adjusting the telescopic length of the second rod body 411 relative to the second cylinder 412, the length of the second diagonal rod assembly 41 is adjusted, and then the inclination angle β of the main support rod 21 in the second state is adjusted, thereby achieving the adjustment of the pitch angle of the bracket module 20.

[0083] In one possible implementation, see Figure 5 As shown, the bracket module 20 also includes:

[0084] An oblique support rod assembly 22, one end of the oblique support rod assembly 22 is hinged to the rotating track 10;

[0085] A first cross bar 23, one end of the first cross bar 23 is hinged to the main support bar 21, and the other end is hinged to the end of the diagonal support bar assembly 22 away from the rotating track 10;

[0086] The second cross bar 24 has one end hinged to the main support bar 21 and the other end hinged to the diagonal support bar assembly 22 ; the diagonal support bar assembly 22 , the first cross bar 23 and the second cross bar 24 are used to provide auxiliary support to the main support bar 21 .

[0087] In the embodiment of the present application, the main support rod 21 is connected with the diagonal support rod assembly 22, the first cross bar 23 and the second cross bar 24 to form a quadrilateral linkage mechanism. During the pitch adjustment process of the bracket module 20, the diagonal support rod assembly 22, the first cross bar 23 and the second cross bar 24 can provide auxiliary support to the main support rod 21, which can not only enhance the overall mechanical stability of the bracket module 20, but also facilitate the pitch adjustment of the bracket module 20.

[0088] In one possible implementation, see Figure 5As shown, the diagonal support rod assembly 22 includes a third rod body 221, a third cylinder body 222 and a fourth cylinder body 223. One end of the third rod body 221 is movably set in the third cylinder body 222, and the other end is movably set in the fourth cylinder body 223. The telescopic length of the third rod body 221 relative to the third cylinder body 222 and the fourth cylinder body 223 is adjustable. The third cylinder body 222 is hinged to the first cross bar 23 and the second cross bar 24, and the fourth cylinder body 223 is hinged to the top of the cabin.

[0089] In an embodiment of the present application, during the pitch adjustment of the bracket module 20, the diagonal support rod assembly 22 can adjust the telescopic length of the third rod body 221 relative to the third cylinder body 222 and the fourth cylinder body 223 in real time, thereby providing auxiliary support to the main support rod 21 and adjusting and adapting the length of the diagonal support rod assembly 22 along with the pitch of the bracket module 20.

[0090] In one possible implementation, see Figure 2 、 Figure 3 and Figure 5 As shown, the bracket module 20 includes two bracket units 201, each bracket unit 201 includes a main support rod 21, an oblique support rod assembly 22, and a first cross rod 23 and a second cross rod 24 hinged between the main support rod 21 and the oblique support rod assembly 22;

[0091] A base 11 is provided on the rotating track 10 , and the base 11 is used to be hinged to the main support rod 21 and the diagonal support rod assembly 22 .

[0092] In an embodiment of the present application, four bases 11 can be set on the rotating track 10; each bracket module 20 includes two bracket units 201, and the main support rod 21 and the diagonal support rod assembly 22 of each bracket unit 201 are hinged to the base 11. The four bases 11 are all set on the rotating track 10. The bracket unit 201 can be designed as a universal structure. Not only does it not need to design a separate bracket for each model, but it is also easy to disassemble and replace separately, without the need to disassemble the bracket or cabin as a whole, which greatly reduces the maintenance workload and downtime, thereby reducing production and maintenance costs.

[0093] In one possible implementation, see Figure 8 As shown, the bracket modules 20 are arranged in pairs along the second direction Y on the top of the cabin;

[0094] The cabin radiator support device further comprises an adjustment beam 50 , which in the second state is connected between the main struts 21 of the support modules 20 arranged in pairs;

[0095] The adjusting beam 50 includes a plurality of third hinged portions 51 , and any third hinged portion 51 is configured to be hinged to the main support rod 21 .

[0096] In an embodiment of the present application, the bracket modules 20 are arranged in pairs along the second direction Y on the top of the cabin. The bracket modules 20 adopt a split modular structure to adapt to wind turbines of different power levels across models, reducing the need for customized structures. At the same time, the universal characteristics across models can realize large-scale production and reduce material and manufacturing costs; in the second state, the adjustment beam 50 can connect the main support rods 21 of two bracket modules 20 that are relatively arranged along the second direction Y. The adjustment beam 50 includes a plurality of third hinged parts 51, so that the third hinged parts 51 can be hinged to the main support rod 21 according to the inclination angle β of the main support rod 21. Not only can the inclination angle β of the main support rod 21 in the second state be flexibly adjusted, but also the stability and reliability of the overall structure of the cabin radiator bracket device can be ensured.

[0097] In one possible implementation, see Figure 5 As shown, the cabin radiator support device further includes a detection module 60 , which is disposed at one end of the main support rod 21 away from the rotating track 10 , and is used to detect a height-limited working condition.

[0098] It should be noted that the detection module 60 may include a laser height detector to measure the height difference feedback during the transportation process, and the detection module 60 is electrically connected to the control center.

[0099] In an embodiment of the present application, the height limit working condition is detected by the detection module 60 to accurately detect the height limit distance ahead, and the control center selects the first state or the second state of the bracket module 20 according to the detection result, and determines the tilt angle of the bracket module 20.

[0100] The cabin radiator bracket device of the present application can be applied to direct-drive units, medium-speed permanent magnet units or doubly fed units, and can be adapted to different models.

[0101] The present application also provides a method for operating the cabin radiator bracket device as described above, including:

[0102] Get the height limit condition;

[0103] Determine the required adjustment height of the bracket module 20 based on the height-limited working condition;

[0104] According to the required adjustment height, the rotating track 10 is driven to rotate and switch to the required state of the bracket module 20; in the required state of the bracket module 20, the hinge position of the diagonal rod assembly on the supporting bracket is selected; and in the required state, the telescopic length of the diagonal rod assembly is adjusted.

[0105] In the embodiment of the present application, m1<H2≤H1 is set, and m1 is the height of the cabin body 70 along the third direction Z. The height limit working condition of the passage is obtained by the detection module 60, and the required adjustment height of the bracket module 20 is determined based on the height limit working condition.

[0106] When the height limit of the channel is H1, the rotating track 10 drives the bracket module 20 to switch to the first state by rotating; one end of the first inclined rod assembly 31 is hinged to the main support rod 21, and the other end is selectively hinged to one of the multiple first hinge parts 321, thereby preliminarily adjusting the inclination angle α of the main support rod 21 in the first state. Figure 5 and Figure 7 As shown, the closer the first hinged portion 321 to which the first diagonal brace assembly 31 is hinged is to the main strut 21 along the first direction X, the smaller the inclination angle α, the greater the inclination degree of the main strut 21, and the smaller the height of the main strut 21 along the third direction Z; by adjusting the telescopic length of the first diagonal brace assembly 31, the inclination angle α of the main strut 21 in the first state can be further adjusted.

[0107] When the height limit of the channel is H2, the rotating track 10 drives the bracket module 20 to switch to the second state by rotating; one end of the second inclined rod assembly 41 is hinged to the main support rod 21, and the other end is selectively hinged to one of the multiple second hinge parts 421, so as to preliminarily adjust the inclination angle β of the main support rod 21 in the second state. Figure 9 As shown, the smaller the inclination angle β is, the greater the inclination of the main support rod 21 is, and the smaller the height of the main support rod 21 along the third direction Z is; by adjusting the telescopic length of the second diagonal tie rod assembly 41, the inclination angle β of the main support rod 21 in the second state is further adjusted.

[0108] Furthermore, when the height limit of the channel is H2, if the transport channel only has a height limit requirement, the rotating track 10 drives the bracket module 20 to switch to the second state by rotating, and the inclination directions of multiple bracket modules 20 along the second direction Y can be opposite to enhance the balance and stability of the overall transportation of the equipment; if the transport channel also has a width limit requirement, the rotating track 10 drives the bracket module 20 to switch to the second state by rotating; the inclination directions of the bracket modules 20 along the second direction Y are the same, for example, along the second direction Y, they can be biased to the left or to the right at the same time.

[0109] In a possible implementation, the operating method of the cabin radiator bracket device further includes:

[0110] Obtain environmental conditions;

[0111] Determining the required adjustment angle of the bracket module 20 based on the environmental conditions;

[0112] The rotating track 10 is driven to rotate according to the adjustment angle required by the bracket module 20; the hinge position of the diagonal rod assembly on the support bracket is selected according to the adjustment angle required by the bracket module 20; the telescopic length of the diagonal rod assembly is adjusted according to the adjustment angle required by the bracket module 20.

[0113] In some embodiments, the environmental working conditions under different wind speed conditions can be obtained, and the heat dissipation efficiency and aerodynamic performance can be optimized by adjusting the rotation angle of the rotating track 10 and adjusting the pitch angle of the bracket module 20. At low wind speeds, the windward area is increased to improve the heat dissipation effect; at high wind speeds, the windward area is reduced to reduce the impact of wind load on the unit, thereby avoiding the problem of insufficient heat dissipation or structural overload caused by wind speed fluctuations in traditional fixed brackets, and improving the adaptability of the unit to changing environments. For example, before the onset of extreme weather (such as a typhoon), the wind load can be reduced by adjusting the pitch angle of the bracket module 20 to avoid structural damage caused by the bracket module 20 exceeding the rated wind load range.

[0114] In some embodiments, the environmental conditions of different application scenarios can be determined by adjusting the rotation angle of the rotating track 10 and the pitch angle of the bracket module 20 to adapt to different installation angles (such as mountainous areas, offshore areas, and other special scenarios), ensuring that the bracket module 20 is always in optimal working condition. For example, in a floating offshore wind farm, pitch adjustment can be used to cope with the angular deviation of the bracket module 20 caused by wave turbulence, thereby maintaining stable heat dissipation efficiency.

[0115] The various embodiments or implementation methods in this specification are described in a progressive manner. Each embodiment focuses on the differences from other embodiments, and the same or similar parts between the various embodiments can be referenced to each other.

[0116] It should be noted that references in this specification to "one embodiment," "an embodiment," "an exemplary embodiment," "some embodiments," and the like indicate that the described embodiment may include a particular feature, structure, or characteristic, but not necessarily every embodiment includes that particular feature, structure, or characteristic. Furthermore, such phrases do not necessarily refer to the same embodiment. Furthermore, when a particular feature, structure, or characteristic is described in conjunction with an embodiment, it is within the knowledge of those skilled in the art to implement such feature, structure, or characteristic in conjunction with other embodiments, whether explicitly described or not.

[0117] Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of the present application, rather than to limit them. Although the present application has been described in detail with reference to the aforementioned embodiments, those skilled in the art should understand that they can still modify the technical solutions described in the aforementioned embodiments, or make equivalent replacements for some or all of the technical features therein. These modifications or replacements do not deviate the essence of the corresponding technical solutions from the scope of the technical solutions of the embodiments of the present application.

Claims

1. A cabin radiator bracket device, characterized in that: include: A rotating track (10) is rotatably arranged on the top of the cabin; The support module (20) comprises a main support rod (21), one end of which is hinged to the rotating track (10); the support module (20) is driven by the rotating track (10) to rotate to a first state along a first direction (X) and a second state along a second direction (Y), wherein the first direction (X) intersects with the second direction (Y); A first inclined rod assembly (31) is hinged to the top of the cabin, and in the first state, the first inclined rod assembly (31) is hinged to the main support rod (21), and the first inclined rod assembly (31) is telescopic to adjust the inclination angle of the main support rod (21) in the first state; The second inclined rod assembly (41) is hinged to the top of the cabin. In the second state, the second inclined rod assembly (41) is hinged to the main support rod (21). The second inclined rod assembly (41) is telescopic to adjust the inclination angle of the main support rod (21) in the second state.

2. The cabin radiator bracket device according to claim 1, characterized in that: The cabin radiator bracket device also includes: A first support hanger (32) is provided on the top of the cabin; the first support hanger (32) comprises a plurality of first hinged portions (321), the plurality of first hinged portions (321) being arranged in a row along a first direction (X); any of the first hinged portions (321) is used to be hinged to the first inclined rod assembly (31); A second support hanger (42) is arranged on the top of the cabin; the second support hanger (42) includes a plurality of second hinged parts (421), and the plurality of second hinged parts (421) are arranged in a row along a second direction (Y); any second hinged part (421) is used to be hinged to the second inclined rod assembly (41).

3. The cabin radiator bracket device according to claim 2, characterized in that: The first inclined rod assembly (31) comprises a first rod body (311) and a first cylinder body (312); the first rod body (311) is movably disposed in the first cylinder body (312); and the telescopic length of the first rod body (311) relative to the first cylinder body (312) is adjustable; The second inclined rod assembly (41) comprises a second rod body (411) and a second cylinder body (412); the second rod body (411) is movably arranged in the second cylinder body (412); and the telescopic length of the second rod body (411) relative to the second cylinder body (412) is adjustable.

4. The cabin radiator bracket device according to any one of claims 1 to 3, characterized in that: The support module (20) further comprises: An oblique support rod assembly (22), one end of which is hinged to the rotating track (10); a first cross bar (23), one end of the first cross bar (23) being hinged to the main support bar (21), and the other end of the first cross bar (23) being hinged to an end of the diagonal support bar assembly (22) away from the rotating track (10); A second cross bar (24), one end of the second cross bar (24) is hinged to the main support bar (21), and the other end is hinged to the diagonal support bar assembly (22); the diagonal support bar assembly (22), the first cross bar (23), and the second cross bar (24) are used to assist in supporting the main support bar (21).

5. The cabin radiator support device according to claim 4, characterized in that: The diagonal brace assembly (22) comprises a third rod body (221), a third cylinder body (222) and a fourth cylinder body (223); one end of the third rod body (221) is movably arranged in the third cylinder body (222), and the other end is movably arranged in the fourth cylinder body (223); the telescopic length of the third rod body (221) relative to the third cylinder body (222) and the fourth cylinder body (223) is adjustable; the third cylinder body (222) is hinged to the first cross bar (23) and the second cross bar (24); and the fourth cylinder body (223) is hinged to the top of the cabin.

6. The cabin radiator support device according to claim 4, characterized in that: The support module (20) comprises two support units (201), each of the support units (201) comprises the main support rod (21), the diagonal support rod assembly (22), and the first cross rod (23) and the second cross rod (24) hinged between the main support rod (21) and the diagonal support rod assembly (22); A base (11) is provided on the rotating track (10), and the base (11) is used to be hinged with the main support rod (21) and the diagonal support rod assembly (22).

7. The cabin radiator bracket device according to any one of claims 1 to 3, characterized in that: The bracket modules (20) are arranged in pairs along a second direction (Y) on the top of the cabin; The cabin radiator bracket device further comprises an adjusting beam (50), wherein in the second state, the adjusting beam (50) is connected between the main support rods (21) of the bracket modules (20) arranged in pairs; The adjusting beam (50) comprises a plurality of third hinged portions (51), and any of the third hinged portions (51) is used for being hinged to the main support rod (21).

8. The cabin radiator bracket device according to any one of claims 1 to 3, characterized in that: The cabin radiator support device further comprises a detection module (60), wherein the detection module (60) is arranged at an end of the main support rod (21) away from the rotating track (10), and the detection module (60) is used to detect a height-limited working condition.

9. A method for operating a cabin radiator support device according to any one of claims 1 to 8, characterized in that: include: Get the height limit condition; Determining the required adjustment height of the bracket module (20) based on the height-limited working condition; The rotating track (10) is driven to rotate and switch to a state required by the bracket module (20) according to the required adjustment height; the hinge position of the inclined tie rod assembly on the supporting hanger is selected in the required state of the bracket module (20); and the telescopic length of the inclined tie rod assembly is adjusted in the required state.

10. The operating method of the cabin radiator bracket device according to claim 9, characterized in that: The operating method of the cabin radiator bracket device also includes: Obtain environmental conditions; Determining a required adjustment angle of the support module (20) based on environmental conditions; The rotating track (10) is driven to rotate according to the adjustment angle required by the bracket module (20); the hinge position of the inclined tie rod assembly on the support hanger is selected according to the adjustment angle required by the bracket module (20); and the telescopic length of the inclined tie rod assembly is adjusted according to the adjustment angle required by the bracket module (20).

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