Solar panel folding wing for ship
By adopting articulated components and connecting rod driving structures in marine folding wings, the complex and heavy weight of the folding wing power driving mechanism in the prior art is solved, and more efficient solar panel deployment and hull stability are achieved.
Patent Information
- Application Number
- CN202411532536.8
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2024-10-30
- Publication Date
- 2024-12-24
AI Technical Summary
The power drive mechanism of existing marine folding wings is complex, takes up a large space, is heavy in weight, and has a great impact on the stability of the hull during navigation.
A marine solar panel folding wing was designed, using articulated assembly and connecting rod driving structure, and horizontal rotation and stable support of the folding wings are achieved through the folding wing fixing seat, side float and articulated assembly, reducing the volume and weight of the drive assembly, and Maximize the spreading area of the solar panel by the articulated assembly.
With the same driving amplitude, the space and weight of the flap drive assembly is reduced, the passing of the hull and the light receiving area of the solar panel are improved, and the stability and space utilization of the hull are enhanced.
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Figure CN119176223A_ABST
Abstract
Description
Technical Field
[0001] The invention relates to the technical field of ship folding wings, in particular to a ship-used solar panel folding wing. Background Art
[0002] The marine folding wing is a device with special uses on ships. It is usually made of high-strength metal materials or composite materials and has the characteristics of being strong and durable. The marine folding wing mainly includes structures such as foldable wing panels, connecting mechanisms and driving devices. When a ship encounters wind and waves during navigation, unfolding the folding wings can increase the lateral stability of the ship. The lift and resistance generated by the wing panels in the water can offset part of the force of the waves and reduce the roll and pitch of the ship, making the ship travel more smoothly. The folding wings can change the hydrodynamic characteristics of the ship in the water, thereby affecting the maneuverability of the ship. When turning, unfolding the folding wings on one side can increase the resistance on that side and make it easier for the ship to turn. During the docking or transportation of the ship, the folding wings can be folded up to reduce the space occupied, which is very important for ports, docks and ship transportation with limited space. It can improve space utilization and facilitate the parking and transportation of ships. The existing power drive mechanism of the folding wings is relatively complex, occupies more space and has a large weight. Summary of the invention
[0003] In view of the deficiencies of the prior art, the present invention provides a folding wing for a marine solar panel, which reduces the volume and weight of the power drive mechanism of the folding wing, and can unfold the folding lateral wing with the help of a hinge assembly so that the solar panel has a larger unfolding area.
[0004] To achieve the above object, the present invention provides the following technical solutions: A folding wing of a solar panel for a ship comprises a folding wing fixing seat arranged on both sides of a hull and a folding wing hingedly arranged on the folding wing fixing seat, the folding wing horizontally rotates on the folding wing fixing seat to switch between an open state and a folded state, the folding wing fixing seat is also provided with a folding wing driving assembly, and the folding wing is driven to rotate by the folding wing driving assembly; a horizontally rotatable side float is provided at the lower end of the folding wing, a linkage assembly connected to the folding wing fixing seat is provided on the side float, and the linkage assembly is used to keep the folding wing in the same direction as the hull during the opening process, and the unfolded folding wing is supported by the side float and the stability of the hull is maintained; the folding wing comprises a lower folding wing and an upper folding wing, the lower folding wing is connected to the upper folding wing by a hinge assembly, and the hinge assembly makes the upper end surfaces of the lower folding wing and the upper folding wing flush when unfolded, and the upper end surfaces of the lower folding wing and the upper folding wing fit together when closed, and solar panels are arranged on the upper end surfaces of the lower folding wing and the upper folding wing.
[0005] Furthermore, one side of the lower folding wing is connected to a hinge assembly, and the other end of the hinge assembly is connected to an upper folding wing, the lower folding wing includes a lower wing mounting plane and a lower wing curved surface, and the upper folding wing includes an upper wing mounting plane and an upper wing curved surface, when the folding wing is unfolded, the lower wing mounting plane and the upper wing mounting plane are in the same horizontal plane, the lower wing curved surface and the upper wing curved surface are continuous curved surfaces, and when the folding wing is closed, the lower wing mounting plane fits with the upper wing mounting plane.
[0006] Furthermore, the folding wing also includes a base arranged at the end of the lower folding wing, and the folding wing driving assembly is transmission-connected to the base to drive the folding wing to rotate horizontally; the base includes a rotating base, a power base, a connecting plate and a folding wing mounting plate, the folding wing mounting plate is connected and fixed to the end surface of the lower folding wing, the folding wing mounting plate is provided with a protruding connecting plate, and the connecting plate is provided with a rotating base and a power base; the rotating base is provided on a coaxial hinged seat on the folding wing fixing seat, the base can rotate on the coaxial hinged seat, and the power base is transmission-connected to the folding wing driving assembly.
[0007] Furthermore, the folding wing drive assembly includes a driving rod, a driving block, a limit seat, a support frame and a power cylinder; the support frame is fixedly arranged on the folding wing fixing seat, the limit seat is arranged on the support frame, one end of the driving block is hinged on the limit seat, the other end of the driving block is hinged to the driving rod, and the driving rod is hinged to the power base of the base; the output end of the power cylinder is transmission-connected to the middle part of the driving block, and the driving block is driven by the power cylinder to swing on the limit seat, thereby causing the driving rod to push the base to rotate on the folding wing fixing seat, and the connecting rod structure of the driving rod and the driving block can reduce the size of the power cylinder and reduce the weight.
[0008] Furthermore, a support hole and a vertical long hole are provided on the limit seat, the rotating shaft at one end of the driving block is arranged in the support hole, the hinge hole at the other end of the driving block is hinged to the first hinge part of the driving rod, the second hinge part of the driving rod is hinged to the power base of the base, and the middle part of the driving block is also provided with a laterally extending arc hole; the limit seat is a hollow structure, and the driving block can swing around the rotating shaft in the support hole in the hollow structure, and the arc hole and the vertical long hole have a common passing space, and the power pin on the movable end of the power cylinder is arranged in the common passing space, and when the power cylinder drives the power pin to move linearly along the vertical long hole, the power pin also slides along the arc hole and drives the driving block to swing.
[0009] Furthermore, the side float, buoyancy sheet, bracket, connecting rod assembly and folding wing hinge seat, the upper end of the buoyancy sheet is provided with a bracket, one end of the bracket is rotatably provided on the folding wing hinge seat at the lower end of the lower folding wing, one end of the connecting rod assembly is transmission connected with the bracket, and the other end of the connecting rod assembly is transmission connected with the folding wing fixing seat; when the folding wing swings relative to the folding wing fixing seat, the connecting rod assembly can drive the bracket to rotate on the folding wing hinge seat of the folding wing to ensure that the direction of the buoyancy sheet is consistent with the direction of the hull.
[0010] Furthermore, the connecting rod assembly includes a fixed short rod, a driven long rod, an active long rod and a synchronous short rod; the fixed short rod is fixed to the folding wing fixing seat, one end of the active long rod is rotatably set on the coaxial hinge seat, the other end of the active long rod is fixed on the folding wing hinge seat, and the active long rod can rotate on the coaxial hinge seat synchronously with the folding wing; the synchronous short rod is rotatably set on the folding wing hinge seat, and the synchronous short rod is fixedly connected to the upper end of the bracket, and the two ends of the driven long rod are respectively connected to the fixed short rod and the synchronous short rod.
[0011] Furthermore, a fixed hinge seat is also provided on the folding wing fixing seat, and the two ends of the fixed short rod are respectively mounted on the coaxial hinge seat and the fixed hinge seat, one end of the driven long rod is rotatably arranged on the fixed hinge seat, and the other end of the driven long rod is hinged to the synchronous short rod, and the hinge position of the driven long rod and the synchronous short rod is a free end; when the folding wing driving assembly drives the folding wing to rotate, the folding wing drives the active long rod to rotate synchronously, and the driven long rod makes the synchronous short rod remain parallel to the fixed short rod, thereby making the direction of the buoyancy sheet consistent with the direction of the hull.
[0012] Furthermore, the hinge assembly includes a first hinge part, a second hinge part and a hinge assembly connecting the first hinge part and the second hinge part; the first hinge part is installed and fixed to the upper folding wing, and the second hinge part is installed and fixed to the lower folding wing.
[0013] Furthermore, the hinge assembly includes a first link rod and a second link rod, the first link rod and the second link rod have the same structure and are arranged in mirror symmetry, the first through hole of the first link rod is rotatably connected to the connecting shaft of the second link rod, the third through hole of the second link rod is rotatably connected to the hinge shaft on the first mounting tube of the first hinge part, and the other end of the second link rod is connected to the second mounting tube through a sliding hinge part; the first through hole of the first link rod is rotatably connected to the hinge shaft on the second mounting tube, and the sliding hinge part of the first link rod can be slidably arranged in the first slide groove of the first mounting tube.
[0014] Compared with the prior art, the present invention provides a folding wing of a marine solar panel, which has the following beneficial effects: 1. The hull of the present invention is provided with folding wings that can rotate horizontally on both sides, and side floats are provided under the folding wings, which can provide stable support for both sides of the hull, and the folding wing drive assembly is a connecting rod drive structure, which can reduce the occupied space and weight of the folding wing drive assembly under the premise of the same driving amplitude.
[0015] 2. The connecting rod structure on the side float of the present invention can drive the side float to rotate. During the unfolding / folding process of the folding wings, the orientation of the side float and the hull are always kept consistent. The folding wings can be kept at any angle, which increases the lateral occupied space in the hull form and improves the passability of the hull.
[0016] 3. The lower folding wing and the upper folding wing of the folding wing of the present invention are connected by a hinge assembly, which enables the lower folding wing and the upper folding wing to open and close 180 degrees, so that the upper end surfaces of the lower folding wing and the upper folding wing are in contact when closed, which can effectively protect the solar panel set on the upper end surface from collision. At the same time, when opened, the plane of the solar panel installed on the lower folding wing and the upper folding wing is unfolded to the maximum extent to increase the light-receiving area of the solar panel. BRIEF DESCRIPTION OF THE DRAWINGS
[0017] Figure 1 It is a schematic diagram of the overall structure of the marine solar panel of the present invention with the folding wings opened; Figure 2 It is a schematic diagram of the overall structure of the folding wings of the marine solar panel of the present invention in a folded state; Figure 3 It is a structural schematic diagram of the side floating body of the present invention; Figure 4 It is a structural schematic diagram of the folding wing of the present invention; Figure 5 It is a structural schematic diagram of the connecting rod assembly of the present invention; Figure 6 It is a structural schematic diagram of the folding wing drive assembly of the present invention; Figure 7 It is an exploded schematic diagram of the folding wing drive assembly of the present invention; Figure 8 It is an exploded schematic diagram of the folding wing of the present invention; Fig. 9 It is a schematic diagram of the structure of the folding wing and the hinge assembly of the present invention; Fig.10 It is a structural schematic diagram of the hinge assembly of the present invention; Fig.11 It is a structural schematic diagram of the hinge assembly of the present invention; Fig. 12A -C is a schematic diagram of multiple states of the hinge assembly of the present invention; In the figure: Folding wing fixing seat 1, coaxial hinge seat 11, fixed hinge seat 12; Folding wing 2, lower folding wing 21, lower wing mounting plane 211, lower wing arc surface 212, upper folding wing 22, upper wing mounting plane 221, upper wing arc surface 222, base 23, rotating base 231, power base 232, connecting plate 233, folding wing mounting plate 234; Side float 3, buoyancy sheet 31, bracket 32, connecting rod assembly 33, fixed short rod 331, driven long rod 332, active long rod 333, synchronous short rod 334, folding wing hinge seat 34; Solar panel 4; Hull 5; Hinge assembly 6, first hinge part 61, first mounting cylinder 611, first slider 612, hinge shaft 613, first slide groove 614, second hinge part 62, second mounting cylinder 621, second slide groove 622, hinge assembly 60, first link 63, first through hole 631, second through hole 632, sliding hinge part 633, second link 64, connecting shaft 641, third through hole 642; Folding wing drive assembly 7, drive rod 71, first hinge part 711, second hinge part 712, drive block 72, rotating shaft 721, arc hole 722, hinge hole 723, limit seat 73, support hole 731, vertical long hole 732, support frame 74, power cylinder 75, power pin shaft 751. DETAILED DESCRIPTION
[0018] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.
[0019] The present invention is described in detail below according to the accompanying drawings. The folding wing of the marine solar panel of the present invention comprises a folding wing fixing seat 1 arranged on both sides of the hull 5 and a folding wing 2 hingedly arranged on the folding wing fixing seat 1. The folding wing 2 rotates horizontally on the folding wing fixing seat 1 to switch between an open state and a folded state. The folding wing fixing seat 1 is also provided with a folding wing driving assembly 7, and the folding wing 2 is driven to rotate by the folding wing driving assembly 7; the lower end of the folding wing 2 is provided with a horizontally rotatable side float 3, and the side float 3 is provided with a connection with the folding wing fixing seat 1. The folding wing 2 comprises a lower folding wing 21 and an upper folding wing 22, wherein the lower folding wing 21 is connected to the upper folding wing 22 via a hinge assembly 6, wherein the hinge assembly 6 makes the upper end surfaces of the lower folding wing 21 and the upper folding wing 22 flush when unfolded, and the upper end surfaces of the lower folding wing 21 and the upper folding wing 22 fit when closed, and solar panels 4 are arranged on the upper end surfaces of the lower folding wing 21 and the upper folding wing 22.
[0020] Folding wings 2 that can rotate horizontally are provided on both sides of the hull 5, and side floats 3 are provided under the folding wings 2, which can provide stable support for both sides of the hull. The folding wing drive assembly 7 is a connecting rod drive structure, which can reduce the occupied space and weight of the folding wing drive assembly 7 under the premise of the same driving amplitude.
[0021] See attached Figure 1 and 2 One side of the lower folding wing 21 is connected to the hinge assembly 6, and the other end of the hinge assembly 6 is connected to the upper folding wing 22. The lower folding wing 21 includes a lower wing mounting plane 211 and a lower wing curved surface 212. The upper folding wing 22 includes an upper wing mounting plane 221 and an upper wing curved surface 222. When the folding wing 2 is unfolded, the lower wing mounting plane 211 and the upper wing mounting plane 221 are in the same horizontal plane, the lower wing curved surface 212 and the upper wing curved surface 222 are continuous curved surfaces, and when the folding wing 2 is closed, the lower wing mounting plane 211 is in contact with the upper wing mounting plane 221. More specifically, the planar structure of the upper wing mounting plane 221 and the lower wing mounting plane 211 allows the lower folding wing 21 and the upper folding wing 22 to fit more closely when closed up and down, and can effectively cover the internal solar panel 4. The lower wing curved surface 212 and the upper wing curved surface 222 form a streamlined structure after the folding wing 2 is closed, which can effectively reduce the wind resistance of the folding wing 2.
[0022] The folding wing 2 also includes a base 23 arranged at the end of the lower folding wing 21, and the folding wing driving assembly 7 is transmission-connected with the base 23 to drive the folding wing 2 to rotate horizontally; the base 23 includes a rotating base 231, a power base 232, a connecting plate 233 and a folding wing mounting plate 234, the folding wing mounting plate 234 is connected and fixed to the end surface of the lower folding wing 21, and a protruding connecting plate 233 is provided on the folding wing mounting plate 234, and a rotating base 231 and a power base 232 are provided on the connecting plate 233; the rotating base 231 is provided on the coaxial hinged seat 11 on the folding wing fixing seat 1, and the base 23 can rotate on the coaxial hinged seat 11, and the power base 232 is transmission-connected with the folding wing driving assembly 7.
[0023] According to the attached Figure 6 and 7 The folding-wing driving assembly 7 includes a driving rod 71, a driving block 72, a limiting seat 73, a support frame 74 and a power cylinder 75; the support frame 74 is fixedly arranged on the folding-wing fixing seat 1, the limiting seat 73 is arranged on the support frame 74, one end of the driving block 72 is hinged on the limiting seat 73, the other end of the driving block 72 is hinged to the driving rod 71, and the driving rod 71 is hinged to the power base 232 of the base 23; the output end of the power cylinder 75 is transmission-connected with the middle part of the driving block 72, and the driving block 72 is driven by the power cylinder 75 to swing on the limiting seat 73, so that the driving rod 71 pushes the base 23 to rotate on the folding-wing fixing seat 1, and the connecting rod structure of the driving rod 71 and the driving block 72 can reduce the size of the power cylinder 75 and reduce the weight. In an embodiment of the present invention, when the folding wing 2 is driven to an approximately vertical state of the hull 5, the driving rod 71 and the driving block 72 are approximately in the same straight line, which can achieve self-locking of the rotation of the folding wing 2, thereby improving the supporting force of the driving rod 71 and the driving block 72 on the folding wing 2 and reducing the squeezing of the power cylinder 75 by the folding wing 2 when subjected to external force.
[0024] The limit seat 73 is provided with a support hole 731 and a vertical long hole 732. The rotating shaft 721 at one end of the driving block 72 is arranged in the support hole 731. The hinge hole 723 at the other end of the driving block 72 is hinged to the first hinge part 711 of the driving rod 71. The second hinge part 712 of the driving rod 71 is hinged to the power base 232 of the base 23. The middle part of the driving block 72 is also provided with a laterally extending arc hole 722. The limit seat 73 is a hollow structure. The moving block 72 can swing around the rotating shaft 721 in the support hole 731 in the hollow structure, and the arc hole 722 and the vertical long hole 732 have a common passing space, and the power pin 751 on the movable end of the power cylinder 75 is arranged in the common passing space. When the power cylinder 75 drives the power pin 751 to move linearly along the vertical long hole 732, the power pin 751 also slides along the arc hole 722 and drives the driving block 72 to swing. Further, the structure of the arc hole 722 of the present invention is an arc extension shape, which reduces the resistance of the power pin 751 sliding in the arc hole 722, and eliminates the situation that the power pin 751 is stuck in the extreme positions at both ends of the arc hole 722, so that the power output of the power cylinder 75 at the extreme position of the folding wing 2 is more stable.
[0025] The side float 3, the buoyancy sheet 31, the bracket 32, the connecting rod assembly 33 and the folding wing hinge seat 34, the upper end of the buoyancy sheet 31 is provided with a bracket 32, one end of the bracket 32 is rotatably arranged on the folding wing hinge seat 34 at the lower end of the lower folding wing 21, one end of the connecting rod assembly 33 is transmission connected with the bracket 32, and the other end of the connecting rod assembly 33 is transmission connected with the folding wing fixing seat 1; when the folding wing 2 swings relative to the folding wing fixing seat 1, the connecting rod assembly 33 can drive the bracket 32 to rotate on the folding wing hinge seat 34 of the folding wing 2 to ensure that the direction of the buoyancy sheet 31 is consistent with the direction of the hull 5.
[0026] The connecting rod structure on the side float 3 can drive the side float 3 to rotate. During the unfolding / folding process of the folding wing 2, the side float 3 and the hull 5 are always kept in the same direction. The folding wing 2 can be stopped at any angle, which increases the lateral occupied space of the hull 5 and improves the passability of the hull 5.
[0027] According to the attached Figure 3-5The connecting rod assembly 33 includes a fixed short rod 331, a driven long rod 332, an active long rod 333 and a synchronous short rod 334; the fixed short rod 331 is fixed on the folding wing fixing seat 1, one end of the active long rod 333 is rotatably set on the coaxial hinge seat 11, and the other end of the active long rod 333 is fixed on the folding wing hinge seat 34, and the active long rod 333 can rotate on the coaxial hinge seat 11 synchronously with the folding wing 2; the synchronous short rod 334 is rotatably set on the folding wing hinge seat 34, and the synchronous short rod 334 is fixedly connected to the upper end of the bracket 32, and the two ends of the driven long rod 332 are respectively connected to the fixed short rod 331 and the synchronous short rod 334.
[0028] The folding wing fixing seat 1 is also provided with a fixed hinge seat 12, and the two ends of the fixed short rod 331 are respectively mounted on the coaxial hinge seat 11 and the fixed hinge seat 12, and one end of the driven long rod 332 is rotatably arranged on the fixed hinge seat 12, and the other end of the driven long rod 332 is hinged to the synchronous short rod 334, and the hinge position of the driven long rod 332 and the synchronous short rod 334 is a free end; when the folding wing driving assembly 7 drives the folding wing 2 to rotate, the folding wing 2 drives the active long rod 333 to rotate synchronously, and the driven long rod 332 makes the synchronous short rod 334 remain parallel to the fixed short rod 331, thereby making the direction of the buoyancy sheet 31 consistent with the direction of the hull 5.
[0029] According to the attached Figure 9-11 , attached Fig. 12A , 12B, 12C, the hinge assembly 6 includes a first hinge portion 61, a second hinge portion 62 and a hinge assembly 60 connecting the first hinge portion 61 and the second hinge portion 62; the first hinge portion 61 is mounted and fixed to the upper folding wing 22, and the second hinge portion 62 is mounted and fixed to the lower folding wing 21. In an embodiment of the present invention, a plurality of hinge assemblies 6 are arranged side by side between the lower folding wing 21 and the upper folding wing 22, and the connecting rod structure of the hinge assembly 60 can provide a more stable supporting force when the first hinge portion 61 and the second hinge portion 62 are opened in a horizontal state, so that the lower folding wing 21 and the upper folding wing 22 are stably maintained in a horizontal state.
[0030] The lower folding wing 21 and the upper folding wing 22 of the folding wing 2 are connected by a hinge assembly 6, and the hinge assembly 6 allows the lower folding wing 21 and the upper folding wing 22 to be opened and closed 180 degrees, so that the upper end surfaces of the lower folding wing 21 and the upper folding wing 22 are in contact when closed, which can effectively protect the solar panel 4 set on the upper end surface from collision. At the same time, when opened, the plane of the solar panel 4 installed on the lower folding wing 21 and the upper folding wing 22 is unfolded to the maximum extent to increase the light-receiving area of the solar panel 4.
[0031] The hinge assembly 60 includes a first link rod 63 and a second link rod 64. The first link rod 63 and the second link rod 64 have the same structure and are arranged in mirror symmetry. The first through hole 631 of the first link rod 63 is rotatably connected to the connecting shaft 641 of the second link rod 64. The third through hole 642 of the second link rod 64 is rotatably connected to the hinge shaft 613 on the first mounting tube 611 of the first hinged portion 61. The other end of the second link rod 64 is connected to the second mounting tube 621 through a sliding hinge. The first through hole 631 of the first link rod 63 is rotatably connected to the hinge shaft on the second mounting tube 621. The sliding hinge portion 633 of the first link rod 63 can be slidably arranged in the first slide groove 614 of the first mounting tube 611.
[0032] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.
Claims
1. A folding wing of a solar panel for a ship, comprising folding wing fixing seats (1) arranged on both sides of a hull (5) and folding wings (2) hingedly arranged on the folding wing fixing seats (1), characterized in that: The folding wing (2) rotates horizontally on the folding wing fixing seat (1) to switch between an open state and a folded state. The folding wing fixing seat (1) is also provided with a folding wing driving assembly (7), and the folding wing (2) is driven to rotate by the folding wing driving assembly (7); A horizontally rotatable side float (3) is provided at the lower end of the folding wing (2), and a linkage assembly connected to the folding wing fixing seat (1) is provided on the side float (3). The linkage assembly enables the folding wing (2) to maintain the same orientation as the hull (5) during the unfolding process, and the unfolded folding wing (2) is supported by the side float (3) and the stability of the hull (5); The folding wing (2) comprises a lower folding wing (21) and an upper folding wing (22); the lower folding wing (21) is connected to the upper folding wing (22) via a hinge assembly (6); the hinge assembly (6) enables the upper end surfaces of the lower folding wing (21) and the upper folding wing (22) to be flush when unfolded, and to fit the upper end surfaces of the lower folding wing (21) and the upper folding wing (22) when closed; and solar panels (4) are arranged on the upper end surfaces of the lower folding wing (21) and the upper folding wing (22).
2. The folding wing of a marine solar panel according to claim 1, characterized in that: One side of the lower folding wing (21) is connected to the hinge assembly (6), and the other end of the hinge assembly (6) is connected to the upper folding wing (22); the lower folding wing (21) comprises a lower wing mounting plane (211) and a lower wing curved surface (212); the upper folding wing (22) comprises an upper wing mounting plane (221) and an upper wing curved surface (222); when the folding wing (2) is unfolded, the lower wing mounting plane (211) and the upper wing mounting plane (221) are in the same horizontal plane; the lower wing curved surface (212) and the upper wing curved surface (222) are continuous curved surfaces; when the folding wing (2) is closed, the lower wing mounting plane (211) and the upper wing mounting plane (221) are in contact with each other.
3. The folding wing of the marine solar panel according to claim 2, characterized in that: The folding wing (2) further comprises a base (23) arranged at the end of the lower folding wing (21); the folding wing driving assembly (7) is transmission-connected to the base (23) to drive the folding wing (2) to rotate horizontally; the base (23) comprises a rotating base (231), a power base (232), a connecting plate (233) and a folding wing mounting plate (234); the folding wing mounting plate (234) is connected and fixed to the end surface of the lower folding wing (21); a protruding connecting plate (233) is arranged on the folding wing mounting plate (234); and the rotating base (231) and the power base (232) are arranged on the connecting plate (233); The rotating base (231) is arranged on a coaxial hinge seat (11) on the folding wing fixing seat (1); the base (23) is capable of rotating on the coaxial hinge seat (11); and the power base (232) is in transmission connection with the folding wing driving assembly (7).
4. The folding wing of the marine solar panel according to claim 3, characterized in that: The folding wing drive assembly (7) comprises a drive rod (71), a drive block (72), a limit seat (73), a support frame (74) and a power cylinder (75); The support frame (74) is fixedly arranged on the folding wing fixing seat (1), the limiting seat (73) is arranged on the support frame (74), one end of the driving block (72) is hinged on the limiting seat (73), the other end of the driving block (72) is hinged to the driving rod (71), and the driving rod (71) is hinged to the power base (232) of the base (23); The output end of the power cylinder (75) is transmission-connected to the middle of the driving block (72), and the power cylinder (75) drives the driving block (72) to swing on the limit seat (73), thereby causing the driving rod (71) to push the base (23) to rotate on the folding wing fixing seat (1). The connecting rod structure of the driving rod (71) and the driving block (72) can reduce the size of the power cylinder (75) and reduce the weight.
5. The folding wing of the marine solar panel according to claim 4, characterized in that: The limiting seat (73) is provided with a support hole (731) and a vertical long hole (732); a rotating shaft (721) at one end of the driving block (72) is arranged in the support hole (731); a hinge hole (723) at the other end of the driving block (72) is hinged to a first hinge portion (711) of the driving rod (71); a second hinge portion (712) of the driving rod (71) is hinged to a power base (232) of the base (23); and a laterally extending arc hole (722) is further provided in the middle of the driving block (72); The limit seat (73) is a hollow structure, and the driving block (72) can swing around the rotating shaft (721) in the support hole (731) in the hollow structure, so that the arc hole (722) and the vertical long hole (732) have a common passing space, and the power pin shaft (751) on the movable end of the power cylinder (75) is arranged in the common passing space. When the power cylinder (75) drives the power pin shaft (751) to move linearly along the vertical long hole (732), the power pin shaft (751) also slides along the arc hole (722) and drives the driving block (72) to swing.
6. The folding wing of a marine solar panel according to claim 5, characterized in that: The side float (3), the buoyancy sheet (31), the bracket (32), the connecting rod assembly (33) and the folding wing hinge seat (34), wherein the upper end of the buoyancy sheet (31) is provided with the bracket (32), one end of the bracket (32) is rotatably arranged on the folding wing hinge seat (34) at the lower end of the lower folding wing (21), one end of the connecting rod assembly (33) is transmission-connected to the bracket (32), and the other end of the connecting rod assembly (33) is transmission-connected to the folding wing fixing seat (1); When the folding wing (2) swings relative to the folding wing fixing seat (1), the connecting rod assembly (33) can drive the bracket (32) to rotate on the folding wing hinge seat (34) of the folding wing (2), so as to ensure that the orientation of the buoyancy sheet (31) is consistent with the orientation of the hull (5).
7. The folding wing of a marine solar panel according to claim 6, characterized in that: The connecting rod assembly (33) comprises a fixed short rod (331), a driven long rod (332), an active long rod (333) and a synchronous short rod (334); The fixed short rod (331) is fixed on the folding wing fixing seat (1), one end of the active long rod (333) is rotatably arranged on the coaxial hinge seat (11), the other end of the active long rod (333) is fixed on the folding wing hinge seat (34), and the active long rod (333) can rotate on the coaxial hinge seat (11) synchronously with the folding wing (2); The synchronous short rod (334) is rotatably arranged on the folding wing hinge seat (34), and the synchronous short rod (334) is fixedly connected to the upper end of the bracket (32), and the two ends of the driven long rod (332) are respectively connected to the fixed short rod (331) and the synchronous short rod (334).
8. The folding wing of a marine solar panel according to claim 7, characterized in that: The folding wing fixing seat (1) is also provided with a fixed hinge seat (12), the two ends of the fixed short rod (331) are respectively sleeved on the coaxial hinge seat (11) and the fixed hinge seat (12), one end of the driven long rod (332) is rotatably provided on the fixed hinge seat (12), the other end of the driven long rod (332) is hinged to the synchronous short rod (334), and the hinged position between the driven long rod (332) and the synchronous short rod (334) is a free end; When the folding wing driving assembly (7) drives the folding wing (2) to rotate, the folding wing (2) drives the active long rod (333) to rotate synchronously, and the driven long rod (332) causes the synchronous short rod (334) to remain parallel to the fixed short rod (331), thereby making the orientation of the buoyancy sheet (31) consistent with the orientation of the hull (5).
9. The folding wing of a marine solar panel according to claim 8, characterized in that: The hinge assembly (6) comprises a first hinge portion (61), a second hinge portion (62), and a hinge assembly (60) connecting the first hinge portion (61) and the second hinge portion (62); The first hinged portion (61) is mounted and fixed to the upper folding wing (22), and the second hinged portion (62) is mounted and fixed to the lower folding wing (21).
10. The folding wing of a marine solar panel according to claim 9, characterized in that: The hinge assembly (60) comprises a first link (63) and a second link (64); the first link (63) and the second link (64) have the same structure and are arranged in mirror symmetry; the first through hole (631) of the first link (63) is rotatably connected to the connecting shaft (641) of the second link (64); the third through hole (642) of the second link (64) is rotatably connected to the hinge shaft (613) on the first mounting cylinder (611) of the first hinged portion (61); and the other end of the second link (64) is connected to the second mounting cylinder (621) via a sliding hinged portion; The first through hole (631) of the first chain rod (63) is rotatably connected to the hinge shaft on the second mounting tube (621), and the sliding hinge portion (633) of the first chain rod (63) is slidably arranged in the first sliding groove (614) of the first mounting tube (611).
