CN114940251A

CN114940251A - Screw, propeller and equipment on water

Info

Publication number: CN114940251A
Application number: CN202210476036.1A
Authority: CN
Inventors: 唐彪; 李兴
Original assignee: Guangdong ePropulsion Technology Co Ltd
Current assignee: Guangdong ePropulsion Technology Co Ltd
Priority date: 2022-04-29
Filing date: 2022-04-29
Publication date: 2022-08-26

Abstract

The application discloses screw, propeller and equipment on water, wherein the screw includes: a fixing mechanism; one end of the paddle is rotatably connected with the fixing mechanism; the adjusting rod is provided with a first end fixedly connected with the paddle and a second end arranged opposite to the first end, and the extending direction of the adjusting rod is perpendicular to the axial direction of the paddle; the adjusting rod is used for driving the paddle to rotate around the axial direction of the paddle. In this way, the working efficiency can be improved, and the production cost can also be reduced.

Description

Screw, propeller and equipment on water

Technical Field

The application relates to the field of ship equipment, in particular to a propeller, a propeller and water equipment.

Background

The dynamic behavior of screw has very big relation with the screw pitch, in hydrodynamic propulsion field, to the little condition of operating mode change, adopts the fixed pitch screw usually to impel, nevertheless under the big condition of operating mode change, under the different ship circumstances is joined in marriage to standard extra-ship, adopts a model to join in marriage a plurality of screws to adapt to different operating modes usually, has brought inconvenience to the product use like this.

Disclosure of Invention

The application provides a screw, propeller and equipment on water.

Providing a propeller comprising a fixed mechanism; one end of the paddle is rotatably connected with the fixing mechanism; the adjusting rod is provided with a first end fixedly connected with the paddle and a second end arranged opposite to the first end, and the extending direction of the adjusting rod is perpendicular to the axial direction of the paddle; the adjusting rod is used for driving the blades to rotate around the axial direction of the blades.

Wherein, the paddle includes: a blade; the blade root is fixed on the blade root, the blade root is rotatably connected with the fixing mechanism, the first end of the adjusting rod is fixedly connected with the side wall of the blade root, and the axis of the blade root is perpendicular to the adjusting rod; the adjusting rod is used for driving the blade root to rotate so as to drive the blade to rotate.

The fixing mechanism is perpendicular to the axial side wall of the blade, a mounting hole is formed in the axial side wall of the blade, and one end, deviating from the blade, of the blade root is arranged in the mounting hole.

The fixing mechanism comprises a first blade root clamping piece and a second blade root clamping piece stacked with the first blade root clamping piece, wherein a first mounting groove is formed in one end, facing the second blade root clamping piece, of the first blade root clamping piece, and a second mounting groove is formed in one end, facing the first blade root clamping piece, of the second blade root clamping piece; the first mounting groove is spliced with the second mounting groove to form a mounting hole.

The blade comprises a blade root, a blade groove and a blade groove, wherein the inner wall of the mounting hole is provided with an annular sliding groove, the side wall of one end, close to the blade, of the blade root is provided with an annular sliding rail, the annular sliding rail is located in the annular sliding groove, and the annular sliding groove rotates in a rotating plane of the blade relative to the annular sliding rail so that the blade can rotate in the rotating plane.

Wherein, the screw still includes: the adjusting mechanism is rotatably connected with the fixing mechanism and is coaxially arranged with the fixing mechanism, the adjusting mechanism is provided with an adjusting part, the adjusting part is connected with the second end of the adjusting rod, and the adjusting part can drive the second end of the adjusting rod to rotate in the rotating plane of the paddle so that the first end of the adjusting rod drives the paddle to rotate.

The adjusting part is provided with a limiting hole, and the second end of the adjusting rod is embedded in the limiting hole; the adjusting part drives the second end of the adjusting rod arranged in the limiting hole to rotate in the rotating plane of the paddle.

The propeller further comprises a locking piece, and the adjusting mechanism is locked with the fixing mechanism through the locking piece after the adjusting rod is adjusted.

The adjusting mechanism is provided with a first scale mark, the fixing mechanism is provided with a second scale mark corresponding to the first scale mark, and a difference value between the first scale mark and the second scale mark is used for marking the rotating angle of the adjusting mechanism relative to the fixing mechanism so as to mark the self-rotating angle of the blade.

The propeller comprises a fixing piece, and the first blade root clamping piece and the second blade root clamping piece are connected and fixed through the fixing piece.

In order to solve the technical problem, the technical scheme adopted by the application is as follows: a thruster is provided comprising the above-described propeller.

There is provided a water craft comprising a propeller as described above.

The beneficial effects of the embodiment of the application are that: a propeller is provided, which comprises a fixing mechanism, a blade and an adjusting rod. Wherein, it has the first end with paddle fixed connection and holds with the relative second that sets up of first end to adjust the pole, the extending direction who adjusts the pole sets up with the axial vertical of paddle, and the paddle is rotatable coupling with fixed establishment, adopt the screw of above-mentioned technical means, can drive the axial rotation of paddle around the paddle through adjusting the second end of adjusting the pole, with the contained angle between the blade surface of adjustment paddle and the axial plane of perpendicular to fixed establishment, adjust the blade surface of paddle and the contained angle of the rotation plane of screw promptly, thereby it is adjustable to realize the pitch of screw, and then satisfy the operation requirement under the different pitch operating modes, great reduction the manufacturing cost who has saved the screw simultaneously. Meanwhile, the fixing mechanism is rotatably connected with the propeller blades, so that when the pitch of the propeller is adjusted, the propeller blades and the fixing mechanism are not required to be detached, the pitch of the propeller can be adjusted through stirring the second end of the adjusting rod, and the working efficiency is greatly improved.

Drawings

FIG. 1 is a schematic structural view of an embodiment of a propeller of the present application;

FIG. 2 is a schematic view of an exploded view of the propeller of the embodiment of FIG. 1;

FIG. 3 is a schematic structural view of an assembly structure of a blade and an adjusting rod in the propeller of the embodiment of FIG. 1;

FIG. 4 is a schematic view of a cross-sectional structure along the direction B in the embodiment of FIG. 3;

FIG. 5 is a schematic view of a first root clamp of the propeller of the embodiment of FIG. 1;

FIG. 6 is a schematic structural view of a second blade root gripping member of the propeller of the embodiment of FIG. 1;

FIG. 7 is a schematic view of the first and second blade root clamps of the propeller of the embodiment of FIG. 1 assembled together;

FIG. 8 is a schematic diagram of the structure of the adjustment mechanism in the propeller of the embodiment of FIG. 1;

figure 9 is a schematic structural view of an embodiment of the aquatic equipment of the present application.

Detailed Description

The technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the drawings in the embodiments of the present application, and it is obvious that the described embodiments are only a part of the embodiments of the present application, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present application.

The terms "first" and "second" in this application are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. In the description of the present application, "plurality" means at least two, e.g., two, three, etc., unless explicitly specifically limited otherwise. Furthermore, the terms "include" and "have," as well as any variations thereof, are intended to cover an exclusive inclusion. For example, a process, method, system, article, or apparatus that comprises a list of steps or elements is not limited to only those steps or elements listed, but may alternatively include other steps or elements not listed, or inherent to such process, method, article, or apparatus.

The application provides a propeller, as shown in fig. 1 and fig. 2, fig. 1 is a schematic structural diagram of an embodiment of the propeller; FIG. 2 is a schematic diagram of an exploded view of the propeller of the embodiment of FIG. 1; wherein, propeller 100 includes: a fixing mechanism 110, a paddle 120, and an adjusting lever 130.

One end of the paddle 120 is rotatably connected to the fixing mechanism 110.

The adjustment rod 130 has a first end 132 fixedly connected to the blade 120 and a second end 131 disposed opposite to the first end 132, and the adjustment rod 130 extends in a direction perpendicular to the axial direction of the blade 120.

The adjusting rod 130 is used for driving the blades 120 to rotate around the axial direction of the blades 120.

The fixing mechanism 110 has a cylindrical structure as a whole, wherein a plurality of (for example, three paddles 120 are included in fig. 1) the above-mentioned paddles 120 are arranged around the axial direction of the fixing mechanism 110. One end of the blade 120 is rotatably connected to the fixing mechanism 110, and an adjusting rod 130 is disposed at one end of the blade connected to the fixing mechanism 110, the adjusting rod 130 is locked by fixing a second end 131 of the adjusting rod 130, the adjusting rod 130 is prevented from rotating around the blade 120 in the axial direction, so that an included angle between a blade surface of the blade 120 and a plane perpendicular to the axial direction of the fixing mechanism 110 is locked, that is, an included angle between the blade surface of the blade 120 and a rotating plane of the propeller 100 is maintained constant, and the propeller 100 obtains a fixed pitch. Meanwhile, when the pitch of the propeller 100 needs to be adjusted, the second end 131 of the adjusting rod 130 is shifted to enable the adjusting rod 130 to axially rotate around the blade 120, so that the blade 120 is driven to axially rotate around the blade 120, an included angle between the blade surface of the blade 120 and a plane perpendicular to the axial direction of the fixing mechanism 110 is adjusted, that is, an included angle of a rotating plane of the blade-surface propeller 100 of the blade 120 is adjusted, and the pitch of the propeller 100 is adjusted.

Unlike the prior art, the propeller 100 of the present application includes a fixing mechanism 110, blades 120, and an adjusting lever 130. Wherein, the extending direction of the adjusting rod 130 is perpendicular to the axial direction of the blade 120, and the blade 120 is rotatably connected with the fixing mechanism 110, the propeller 100 adopting the above technical means can drive the blade to rotate around the axial direction of the blade by adjusting the second end 131 of the adjusting rod 130, so as to adjust the included angle between the blade surface of the blade 120 and the axial plane perpendicular to the fixing mechanism 110, i.e. adjust the included angle between the blade surface of the blade 120 and the rotating plane of the propeller 100, thereby realizing the adjustable pitch of the propeller 100, and further meeting the use requirements of users under different pitch working conditions while greatly reducing the production cost of the propeller 100. Meanwhile, the fixing mechanism 110 is rotatably connected with the blade 120, so that when the pitch of the propeller is adjusted, the blade 120 and the fixing mechanism 110 do not need to be disassembled, and the pitch of the propeller 100 can be adjusted by stirring the second end 131 of the adjusting rod 130, thereby greatly improving the working efficiency. The pitch of the propeller 100 can be adjusted, so that the propeller 100 can operate under multiple working conditions, the working efficiency is improved, and the cost is reduced.

Optionally, the blade comprises: a blade 121; a blade root 122, the root of which is fixed on the blade root, the blade root 122 is rotatably connected with the fixing mechanism 110, the first end 132 of the adjusting rod 130 is fixedly connected with the side wall of the blade root 122, and the axis of the blade root 122 is perpendicular to the adjusting rod 130; the adjusting rod 130 is used to drive the blade root 122 to rotate, so as to drive the blade 121 to rotate.

Optionally, a mounting hole 190 is disposed on a side wall of the fixing mechanism 110 perpendicular to the axial direction of the blade 120, and an end of the blade root 122 facing away from the blade 121 is disposed in the mounting hole 190.

Fig. 3 is a schematic structural view of an assembly structure of a blade and an adjusting rod in the propeller of fig. 1 according to the embodiment of fig. 3 and 4; FIG. 4 is a schematic view of a cross-sectional structure in the direction B in the embodiment of FIG. 3; the blade 120 includes a blade 121 and a blade root 122, which are disposed opposite to each other, and the blade surface of the blade 120 mentioned in the above is a side surface of the blade 121. The specific structure of the blades 121 can be designed according to practical situations, for example, as shown in fig. 3, the blades 121 are designed to be curved with an umbrella-shaped arc to increase the pitch adjustable range of the propeller 100. It should be noted that the structure of the blade 121 is not limited to the structure shown in fig. 3 and fig. 4, and it may be designed according to specific practical situations, and will not be described in detail herein.

The first end 132 of the adjustment rod 130 is fixedly connected to the side wall of the blade root 122, for example, as shown in fig. 3 and 4, the side wall of the blade root 122 is provided with a mounting groove of the adjustment rod 130 along the radial direction thereof, the first end 132 of the adjustment rod 130 is provided with a threaded hole, and while the first end 132 of the adjustment rod is embedded in the mounting groove, the side wall of the blade root 122 is provided with a mounting through hole along the radial direction thereof, so as to use the screw 180 to fix the adjustment rod 130 on the blade 120. It should be noted that the above-mentioned fixed connection manner of the adjusting rod 130 and the blade 120 is only an example, and the adjusting rod 130 may be fixedly connected to the blade root 122 by any other fixed connection manner that does not affect the function of the propeller 100, on the premise that the axial direction of the adjusting rod 130 is perpendicular to the axial direction of the blade 120.

Optionally, as analyzed in conjunction with fig. 5, 6 and 7, fig. 5 is a schematic structural view of a first blade root holder in the propeller of the embodiment of fig. 1; FIG. 6 is a schematic structural view of a second blade root gripping member of the propeller of the embodiment of FIG. 1; FIG. 7 is a schematic view of the assembly of a first root clamp and a second root clamp in the propeller of the embodiment of FIG. 1; the fixing mechanism 110 includes a first blade root clamping piece 111 and a second blade root clamping piece 112 stacked with the first blade root clamping piece 111, wherein a first mounting groove 1111 is formed at one end of the first blade root clamping piece 111 facing the second blade root clamping piece 112, and a second mounting groove 1121 is formed at one end of the second blade root clamping piece 112 facing the first blade root clamping piece 111; the first mounting groove 1111 is spliced with the second mounting groove 1121 to form the mounting hole 190.

Optionally, the propeller 100 includes a fixing member 170, and the first blade root clamping member 111 and the second blade root clamping member 112 are connected and fixed by the fixing member 170.

As will be appreciated with reference to fig. 5 and 6, the securing mechanism 110 specifically includes a first root clamp 111 and a second root clamp 112. The number of the blades 120 on the axial side wall of the first blade root clamping piece 111 perpendicular to the axial direction is equal to that of the blades, and a plurality of first mounting grooves 1111 are uniformly arranged along the radial direction of the second blade root clamping piece 112 (the first mounting grooves 1111 are arranged in a corresponding number according to the number of the blades 120). The number of the second installation grooves 1121 (the number of the second installation grooves corresponding to the number of the blades 120 is set according to the number of the blades 120) is uniformly arranged along the radial direction of the second blade root clamping member 112 on the side wall of one end of the second blade root clamping member 112 perpendicular to the axial direction thereof. Here, an end surface (an end surface perpendicular to the axial direction of the first blade root clamping piece 111) of the first blade root clamping piece 111 provided with the first mounting groove 1111 is connected with an end surface (an end surface perpendicular to the axial direction of the second blade root clamping piece 112) of the second blade root clamping piece 112 provided with the second mounting groove 1121 to assemble the fixing mechanism 110. It is noted that when the first and second

blade root clamps

111, 112 are connected, the first mounting slot 1111 of the first and second

blade root clamps

111, 112 is correspondingly spliced with the second mounting slot 1121 to form the mounting hole 190 for mounting the blade 120.

As shown in fig. 6, on the end surface of the second blade root holding member 112 away from the end surface thereof where the second mounting grooves 1121 are provided, adjusting grooves 1123 are provided corresponding to the positions and the number of the second mounting grooves 1121. When the blade 120 is mounted on the mounting hole 190 of the fixing mechanism 110, a portion of the adjusting rod 130 (i.e., the second end 131 of the adjusting rod 130) is disposed in the mounting hole 190 along with the blade root 122, and the rest of the adjusting rod 130 passes through the adjusting slot 1123, so that the second end 131 of the adjusting rod 130 is located outside the second blade root holder 112, and thus the second end 131 of the adjusting rod 130 is pulled to adjust the pitch of the propeller 100 without being interfered by the second blade root holder 112. Meanwhile, the slotting direction of the adjusting slot 1123 is consistent with the rotation direction of the blades 120, so that the adjusting rod 130 can rotate in the adjusting slot 1123 by a certain angle around the axial direction of the blade root 122, thereby realizing the adjustable pitch of the propeller 100.

Wherein the first and second blade root clamps 111, 112 connected in the above manner are fixed by at least three fixtures 170. At least three fixing members 170 are symmetrically disposed around the axial direction of the fixing mechanism 110, respectively, so as to fixedly connect the first blade root clamping member 111 and the second blade root clamping member 112. Specifically, the fixing member 170 may be a standard member such as a long screw.

Optionally, as shown in fig. 5, 6 and 7, an annular sliding groove 191 is formed in an inner wall of the mounting hole 190, an annular sliding rail 1221 is formed in a side wall of one end of the blade root 122 close to the blade 121, the annular sliding rail 1221 is located in the annular sliding groove 191, and the annular sliding groove 191 rotates relative to the annular sliding rail 1221 in a rotation plane of the blade 120, so that the blade 120 rotates in the rotation plane.

Specifically, as shown in fig. 5 and 6, a first sliding groove 1112 and a second sliding groove 1122 are respectively disposed on the inner walls of the first mounting groove 1111 and the second mounting groove 1121, wherein after the first blade root clamping piece 111 and the second blade root clamping piece 112 are connected in the above manner, the first sliding groove 1112 and the second sliding groove 1122 are butted to form an annular sliding groove 191 on the inner wall of the mounting hole 190. As shown in fig. 3, an annular sliding track 1221 surrounding the axial direction of the blade root is disposed on the side wall of the blade root 122, wherein when the blade root 122 is disposed in the mounting hole 190, the annular sliding track 1221 is slidably engaged with the annular sliding slot 191, so that when the second end 131 of the adjusting rod 130 is pulled, the blade 120 can rotate around the axial direction of the annular sliding slot 191, thereby adjusting the pitch of the propeller 100. Meanwhile, the sliding fit of the annular slide rail 1221 and the annular slide groove 191 can limit the degree of freedom of the blade 120 in moving along the axial direction thereof, so as to connect and fix the blade 120 and the fixing mechanism 110.

Optionally, as shown in fig. 1, 2 and 8, fig. 8 is a schematic structural diagram of an adjusting mechanism in the propeller of the embodiment of fig. 1; the propeller 100 further includes: the adjusting mechanism 140, the adjusting mechanism 140 is rotatably connected to the fixing mechanism 110 and coaxially disposed with the fixing mechanism 110, the adjusting mechanism 140 has an adjusting portion 144, the adjusting portion 144 is connected to the second end 131 of the adjusting rod 130, and the adjusting portion 144 can drive the second end 131 of the adjusting rod 130 to rotate in the rotation plane of the blade 120, so that the first end 132 of the adjusting rod 130 drives the blade 120 to rotate.

Optionally, the adjusting portion 144 is provided with a limiting hole 141, and the second end 131 of the adjusting rod 130 is embedded in the limiting hole 141; the adjusting portion 144 drives the second end 131 of the adjusting rod 130 disposed in the limiting hole 141 to rotate in the rotation plane of the blade 120.

Optionally, as shown in fig. 1 and 2, the propeller 100 further includes a locking member 150, and the adjusting mechanism 140 is locked with the fixing mechanism 110 by the locking member 150 after the adjusting lever 130 is adjusted.

Specifically, the adjusting mechanism 140 is a disk-shaped structure, one end of the adjusting mechanism 140 is connected to an end surface of the second blade root clamping element 112, which is away from the end provided with the second mounting groove 1121, and the adjusting mechanism 140 is coaxial with the fixing mechanism 110 in the axial direction. A plurality of limiting holes 141 are uniformly arranged on the adjusting mechanism 140 along the axial direction thereof, and the number of the limiting holes 141 corresponds to the number of the paddles 120 (i.e., several paddles correspond to several limiting holes 141). The limiting hole 141 is a concrete structure embodiment of the adjusting portion 144 on the adjusting mechanism 140. As described above, the second end 131 of the adjustment rod 130 is embedded in the limiting hole 141, and the adjustment mechanism 140 is rotated around the axial direction of the fixing mechanism 110, so that the inner wall 143 of the limiting hole 141 pushes the second end of the adjustment rod 130 while the limiting hole 141 rotates along with the adjustment mechanism 140, so that the adjustment rod 130 rotates around the axial direction of the blade 120 as a rotation axis. The adjusting mechanism 140 is rotated in the above manner, so that the adjusting rods 130 can be simultaneously driven to rotate around the axial direction of the blades 120 as a rotating axis at one time, and the blades 120 are driven to rotate around the axial direction, so as to adjust the pitch of the propeller 100. The adjusting mechanism 140 is rotatable about its axial direction relative to the fixing mechanism 110 during pitch adjustment of the propeller 100, so that the pitch of the propeller 100 can be adjusted by rotating the adjusting mechanism 140 during pitch adjustment of the propeller 100.

The adjusting mechanism 140 is further provided with a plurality of (at least three) third sliding grooves 142 uniformly arranged around the axial direction thereof, wherein a plurality of locking members 150 corresponding to the number of the third sliding grooves 142 respectively pass through the third sliding grooves 142, and press-lock the adjusting mechanism 140 on the fixing mechanism 110 along the fixing mechanism 110. Specifically, for example, as shown in fig. 1, 2, 5 and 6, the locking member 150 has a locking cap 151 and a threaded connection column 152, the first blade root clamping member 111 and the second blade root clamping member 112 are respectively provided with a threaded hole 1113 and a positioning through hole 1124 which are matched with the locking member, wherein the connection columns 152 of the three locking members 150 pass through the third sliding groove 142 and the positioning through hole 1124 and are in threaded fit with the threaded hole 1113 to coaxially and radially fix the adjusting mechanism 140, the first blade root clamping member 111 and the second blade root clamping member 112 so as to prevent the two from moving relative to each other along the radial direction thereof, and meanwhile, the brim of the locking cap 151 of the locking member 150 abuts against the end surface of the adjusting mechanism 140 which is away from the end connected with the second blade root clamping member 112 to provide an abutting force for the adjusting mechanism 140, so as to lock the adjusting mechanism 140 on the fixing mechanism 110, at this time, the adjusting mechanism 140 is acted by the abutting force, such that adjustment mechanism 140 is neither axially movable along the fixation mechanism relative to fixation mechanism 110 nor axially rotatable about fixation mechanism 110. The abutting force applied by the locking cap 151 to the adjusting mechanism 140 can be adjusted by adjusting the degree of the threaded fit between the connecting column 152 and the threaded hole 1113.

It should be noted that the third sliding slot 142 allows the adjusting mechanism 140 to rotate relatively to the locking member 150 in the axial direction around the fixing mechanism 110 (i.e. the adjusting mechanism 140 can rotate around its own axis), in other words, the locking member 150 serves to connect the fixing adjusting mechanism 140 and the fixing mechanism 110 (i.e. the above description), on the one hand, and on the other hand, the locking member 150 provides a guiding function for the adjusting mechanism 140 to rotate around its own axis. Specifically, for example, when the propeller 100 needs to adjust the pitch, the abutting force can be reduced or eliminated by adjusting the degree of matching between the locking member 150 and the threaded hole 1113 (at this time, the locking member 150 still coaxially and radially fixes the adjusting mechanism 140, the first blade root clamping member 111 and the second blade root clamping member 112), so that the adjusting mechanism 140 can rotate around its own axial direction relative to the fixing mechanism 110, wherein the third sliding slot 142 corresponds to the guiding slot, and the locking member 150 corresponds to the guiding rail, and when the adjusting mechanism 140 rotates, while the third sliding slot 142 rotates along with the adjusting mechanism 140, since the plurality of locking members 150 radially pass through the corresponding third sliding slots 142, the inner wall of the third sliding slot 142 is always subjected to the guiding force provided by the locking member 150, which is radially perpendicular to the adjusting mechanism 140, and acts on the axial center of the adjusting mechanism 140, so that the adjusting mechanism 140 can relatively rotate around the axial direction of the fixing mechanism 110 relative to the locking member 150 and the fixing mechanism 110 .

In other words, the plurality of locking members 150 are respectively engaged with the plurality of third sliding grooves 142, and as the adjusting mechanism 140 rotates relative to the fixing mechanism 110, the end of the locking member 150 slides in the third sliding groove 142, so that the relative rotation between the adjusting mechanism 140 and the locking member 150 always rotates around the central axis of the plurality of third sliding grooves 142, that is, when the adjusting mechanism 140 is adjusted, the adjusting mechanism 140 always rotates around the axial direction thereof, thereby driving the plurality of adjusting rods 130 to rotate (for example, the three adjusting rods 130 shown in fig. 1), and further adjusting the pitch of the propeller 100. After the pitch of the propeller 100 is adjusted, the adjusting mechanism 140 and the fixing mechanism 110 can be fixed only by adjusting the degree of the thread fit between the connecting column 152 of the locking member 150 and the threaded hole 1113 to increase the abutting force, so as to restrict the rotation of the adjusting rod 130, and further fix the blades 120, so that the included angle of the blade surface of the blade 121 with respect to the axial vertical end surface of the fixing mechanism 110 is unchanged, and the pitch of the propeller 100 is kept unchanged.

Optionally, as analyzed with reference to fig. 1, fig. 6, and fig. 8, a first scale mark 162 is disposed on the adjusting mechanism 140, a second scale mark 161 corresponding to the first scale mark 162 is disposed on the fixing mechanism 110, and a difference between the first scale mark 162 and the second scale mark 161 is used to mark a rotation angle of the adjusting mechanism 140 relative to the fixing mechanism, so as to mark a rotation angle of the blade 120.

Specifically, the second scale mark 161 and the first scale mark 162 are respectively arranged on the side wall of the connection end of the adjusting mechanism 140 and the second blade root clamping member 112, for example, the second scale mark 161 is used as a scale pointer, the first scale mark 162 is a scale value, when the adjusting mechanism 140 rotates relative to the fixing mechanism 110, the second scale mark 161 points to the scale value corresponding to the first scale mark 162 on the fixing mechanism 110, so as to obtain the specific rotation angle of the adjusting mechanism 140 relative to the fixing mechanism 110, so as to determine the pitch adjustment value of the propeller 100, and further greatly improve the pitch adjustment accuracy of the propeller 100.

In summary, unlike the prior art, the propeller 100 of the present application includes a fixing mechanism 110, a blade 120, and an adjusting rod 130. The propeller 100 adopting the technical means can drive the blades to rotate around the axial direction of the blades by adjusting the second ends 131 of the adjusting rods 130 so as to adjust an included angle between the blade surfaces of the blades 120 and a plane perpendicular to the axial direction of the fixing mechanism 110, namely, adjust an included angle between the blade surfaces of the blades 120 and a rotating plane of the propeller 100, thereby realizing the adjustment of the pitch of the propeller 100, further meeting the use requirements of users under different pitch working conditions and greatly reducing the production cost of the propeller 100. Meanwhile, the fixing mechanism 110 is rotatably connected with the blade 120, so that when the pitch of the propeller is adjusted, the blade 120 and the fixing mechanism 110 do not need to be disassembled, and the pitch of the propeller 100 can be adjusted by stirring the second end 131 of the adjusting rod 130, thereby greatly improving the working efficiency. Wherein, propeller 100 still includes adjustment mechanism 140 and locking piece 150, through the adjustment mechanism 140 and the locking piece 150 of above-mentioned relation of connection, propeller 100 can be through adjusting adjustment mechanism 140 and then the quick pitch of adjusting propeller 100 to lock through locking piece 150, thereby make propeller 100's pitch regulation more high-efficient, and then promoted user's work efficiency greatly. In addition, the propeller 100 is further provided with a first scale mark 162 and a second scale mark 161, so that a user can more accurately adjust the pitch of the propeller 100 required by the user, and the pitch adjustment precision of the propeller 100 is greatly improved.

The present application provides a propeller, as shown in fig. 9, fig. 9 is a schematic structural view of an embodiment of the aquatic equipment of the present application; the propeller 200 includes the propeller 100 described above.

The present application also provides a water device, as shown in figure 9, the water device 300 comprising the propeller 200 described above.

It should be noted that the drawings are only for showing the structural relationship and connection relationship of the product of the invention of the present application, and do not limit the specific structural dimensions of the product of the invention of the present application.

The above description is only an embodiment of the present invention, and is not intended to limit the scope of the present invention, and all equivalent structures or equivalent processes performed by the present specification and the attached drawings, or directly or indirectly applied to other related technical fields, are included in the scope of the present invention.

Claims

1. A propeller, comprising:

a fixing mechanism;

the paddle is rotatably connected with the fixing mechanism at one end;

the adjusting rod is provided with a first end fixedly connected with the paddle and a second end arranged opposite to the first end, and the extending direction of the adjusting rod is perpendicular to the axial direction of the paddle;

the adjusting rod is used for driving the paddle to rotate around the axial direction of the paddle.

2. The propeller of claim 1, wherein the blade comprises:

a blade;

the root of the blade is fixed on the blade root, the blade root is rotatably connected with the fixing mechanism, the first end of the adjusting rod is fixedly connected with the side wall of the blade root, and the axis of the blade root is perpendicular to the adjusting rod;

the adjusting rod is used for driving the blade root to rotate so as to drive the blades to rotate.

3. The propeller of claim 2 wherein the side wall of the attachment means perpendicular to the axial direction of the blade is provided with a mounting hole, and the end of the blade root facing away from the blade is provided in the mounting hole.

4. The propeller of claim 3, wherein the securing mechanism comprises a first root clamp and a second root clamp stacked with the first root clamp, the first root clamp having a first mounting slot at an end toward the second root clamp, the second root clamp having a second mounting slot at an end toward the first root clamp;

the first mounting groove is spliced with the second mounting groove to form the mounting hole.

5. The propeller as claimed in claim 3, wherein the inner wall of the mounting hole is provided with an annular sliding groove, the side wall of the blade root near one end of the blade is provided with an annular sliding rail, the annular sliding rail is positioned in the annular sliding groove, and the annular sliding groove rotates relative to the annular sliding rail in the rotating plane of the blade so as to enable the blade to rotate in the rotating plane.

6. The propeller of claim 1, further comprising: the adjusting mechanism is rotatably connected with the fixing mechanism and coaxially arranged with the fixing mechanism, the adjusting mechanism is provided with an adjusting part, the adjusting part is connected with the second end of the adjusting rod, and the adjusting part can drive the second end of the adjusting rod to rotate in the rotating plane of the paddle, so that the first end of the adjusting rod drives the paddle to rotate.

7. The propeller as recited in claim 6, wherein the adjusting portion is provided with a limiting hole, and the second end of the adjusting rod is embedded in the limiting hole;

the adjusting part drives the second end of the adjusting rod arranged in the limiting hole to rotate in the rotating plane of the paddle.

8. The propeller of claim 6, further comprising a locking member, wherein the adjusting mechanism is locked with the fixing mechanism by the locking member after completion of the adjustment of the adjusting rod.

9. The propeller as claimed in claim 6, wherein a first scale mark is provided on the adjusting mechanism, a second scale mark corresponding to the first scale mark is provided on the fixing mechanism, and a difference value between the first scale mark and the second scale mark is used for marking a rotation angle of the adjusting mechanism relative to the fixing mechanism so as to mark a rotation angle of the blade.

10. The propeller of claim 4 wherein the propeller includes a mount, the first and second blade root clamps being secured in connection by the mount.

11. A propeller comprising a propeller as claimed in any one of claims 1 to 10.

12. A water device comprising a propeller as claimed in claim 11.