CN115258109A - Omnidirectional adjustment cycloid propeller - Google Patents
Omnidirectional adjustment cycloid propeller Download PDFInfo
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- CN115258109A CN115258109A CN202210937099.2A CN202210937099A CN115258109A CN 115258109 A CN115258109 A CN 115258109A CN 202210937099 A CN202210937099 A CN 202210937099A CN 115258109 A CN115258109 A CN 115258109A
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- 230000001360 synchronised effect Effects 0.000 abstract description 4
- 238000009434 installation Methods 0.000 description 7
- 230000006978 adaptation Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 238000005265 energy consumption Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H1/00—Propulsive elements directly acting on water
- B63H1/02—Propulsive elements directly acting on water of rotary type
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Abstract
The invention discloses an omnidirectional adjusting cycloid propeller. Belong to cycloid propeller field, including drum, inner skleeve, motor, side direction mount pad, electric cylinder, connecting block, blade, spout, slip road junction, spacing slider, pivot seat, connecting plate, articulated seat, connecting rod, the lower extreme fixedly connected with connection bedplate of pivot seat, and the last An Chakong of having seted up that runs through of connection bedplate, the lower extreme fixedly connected with spacing sleeve of connecting block, be provided with direction adjustment assembly between spacing sleeve and the motor. The problem that the existing cycloid propeller is inconvenient to realize flexible and synchronous omnidirectional adjustment, the distance between blades cannot be adjusted, and the working efficiency of the cycloid propeller is reduced is solved; the cycloid propeller can flexibly and omni-directionally regulate and control the angle, can regulate the angle of each blade and the distance between each blade, obtains different power effects, and has the characteristic of precise regulation.
Description
Technical Field
The invention belongs to the field of cycloid propellers, and relates to an omnidirectional-adjustment cycloid propeller.
Background
In the prior art, cycloidal propellers consist of a set of blades, which are generally arranged in the middle of the hull, extend perpendicularly (at an angle when double-bladed) from the hull into the water and move circumferentially around the centre of the propeller, perpendicular to the axis of the hull. The blade group rotates around the axis of the blade group while making circular motion.
However, the pitch of the blade array distribution of the existing cycloid propeller and the angle between each blade are generally inconvenient to realize flexible synchronous omnidirectional adjustment, although some blades can be adjusted in the prior art, the blade is generally controlled and adjusted independently, that is, each blade is provided with an active adjusting mechanism, so that the cost is increased, the requirement on an operating system is higher, so that the blades can be adjusted accurately and synchronously, in the actual use of the cycloid propeller, the angle between each blade is generally required to be the same as the circumferential tangential angle formed along each blade, and when the blade is different from the tangential angle of the circumferential motion track, the blade angle can increase the resistance in the operation, reduce the working efficiency of the cycloid propeller, and increase the energy consumption. An omnidirectional adjustable cycloid propeller is therefore proposed.
Disclosure of Invention
The purpose of the invention is as follows: the invention aims to provide an omni-directionally adjusted cycloid propeller, and solves the problems that the conventional cycloid propeller is inconvenient to realize flexible and synchronous omni-directional adjustment, the distance between blades cannot be adjusted, and the working efficiency of the cycloid propeller is reduced.
The technical scheme is as follows: the invention relates to an omnidirectional adjustment cycloid propeller which comprises a cylinder, an inner sleeve, a motor, lateral mounting seats, electric cylinders, connecting blocks and blades, wherein chutes are formed in the cylinder in an array mode, chute openings are formed between the inner walls of the upper side and the lower side of each chute and the upper end face and the lower end face of the cylinder in a penetrating mode, limiting sliders are arranged in the chutes in a sliding mode, the upper end and the lower end of each limiting slider are fixedly connected with guide blocks and rotating shaft seats respectively, the output end of each electric cylinder is fixedly connected with a hinged seat, the other end of each electric cylinder is fixedly connected with one end of a supporting seat, the lower end of each rotating shaft seat is fixedly connected with a connecting seat plate, an Chakong penetrates through the connecting seat plate, the lower end of each connecting block is fixedly connected with a limiting sleeve, and a direction adjusting assembly is arranged between each limiting sleeve and the motor.
Further, an inner sleeve is arranged at the center of the cylinder, a motor is fixedly mounted on the upper inner wall of the inner sleeve, sliding chutes are formed in the cylinder in an array mode, sliding chute openings formed in the upper inner wall and the lower inner wall of each sliding chute penetrate through the upper end face and the lower end face of the cylinder, and blades are fixedly connected to the lower end of the connecting seat plate.
Furthermore, the lateral surface array of the cylinder is fixedly connected with lateral mounting seats, the upper end surface of each lateral mounting seat is fixedly provided with a connecting rod, and the lower end of each lateral mounting seat is fixedly connected with a connecting block.
Further, the direction adjusting assembly comprises a limiting slide rod, a pin shaft seat, an adjusting plate and an I-shaped rotary drum, wherein the limiting slide rod is sleeved in the limiting sleeve in a sliding mode, the pin shaft seat is installed at one end, close to each other, of the limiting slide rod, the adjusting plate is connected to the pin shaft seat in a rotating mode, the I-shaped rotary drum is fixedly connected to the output end of the motor, and the adjusting plate is connected to the I-shaped rotary drum in a rotating mode.
Furthermore, the limiting slide block is arranged in the sliding groove in a sliding manner, and the guide block and the rotating shaft seat which are fixedly connected with the upper end and the lower end of the limiting slide block respectively are arranged in the sliding way openings which are formed in the upper inner wall and the lower inner wall of the sliding groove in a sliding manner.
Furthermore, the upper end of the guide block passes through the slide way opening and extends above the cylinder, a hinge seat is arranged at the extending end, and one end of the hinge seat is connected with the output end of each electric cylinder on each side. The other end of the electric cylinder is fixedly connected to the supporting seat.
Furthermore, the lower end of the rotating shaft seat penetrates through the slide way opening to extend to the lower side of the cylinder, an adjusting plate is fixedly connected to the extending end of the lower side of the rotating shaft seat, and blades are fixedly mounted at the lower end of each adjusting plate.
Furthermore, the lower end of each connecting block is fixedly connected with a limiting sleeve, one end, close to each other, of a limiting slide rod slidably sleeved in each limiting sleeve extends to one end, close to each limiting sleeve, of each limiting sleeve, and a pin shaft seat is fixedly mounted at the extending end of each limiting slide rod.
Furthermore, adjusting plates are rotatably arranged on the I-shaped rotary drum in an array mode, and one ends, far away from each other, of the adjusting plates are rotatably connected with pin shaft seats on one side of each adjusting plate.
Has the beneficial effects that: compared with the prior art, the invention has the characteristics that: 1. the invention provides an omnidirectional-adjustment cycloid propeller, which is characterized in that each electric cylinder synchronously drives a hinged seat to move left and right, so that each limiting slide block slides in a sliding groove in a manner of approaching or separating from each other, and each blade on the lower side can be driven to gather close to each other or disperse away from each other, thereby obtaining different power effects; 2. the invention provides an omnidirectional-adjustment cycloidal propeller, which drives an I-shaped cylinder to rotate through a motor so as to drive an adjusting plate to rotate, and further, each adjusting plate can rotate to different angles, and simultaneously, a limiting slide rod which is rotatably connected with the outer side of each adjusting plate through a pin shaft seat is pulled to slide in a limiting sleeve, so that a connecting seat plate which is sleeved on the outer side of the adjusting plate through an inserting hole can rotate for a certain angle along the adjusting plate, and further, the angle of each blade along the tangential direction of a circular track of the circumferential motion of the blade is adjusted, and different power effects are obtained.
Drawings
FIG. 1 is a schematic diagram of the general structure of the present invention;
FIG. 2 is a schematic cross-sectional view of the present invention;
FIG. 3 is a sectional view of the adjusting plate of the present invention;
FIG. 4 is a sectional view of a top view of an adjusting plate according to the present invention;
in the figure: 1. a cylinder; 2. an inner sleeve; 3. a motor; 4. a lateral mounting seat; 5. an electric cylinder; 6. a chute; 7. a gate port; 8. a guide block; 9. a rotating shaft seat; 10. a connecting plate; 11. a supporting seat; 12. a hinged seat; 13. a connecting rod; 14. connecting the seat plate; 15. an Chakong; 16. connecting blocks; 17. a limiting sleeve; 18. a limiting slide bar; 19. a pin shaft seat; 20. an adjusting plate; 21. an I-shaped cylinder; 22. a blade; 23. and a limiting sliding block.
Detailed Description
In order to more clearly illustrate the technical solution of the present invention, the following detailed description is made with reference to the accompanying drawings:
the first embodiment is as follows:
as shown in fig. 1-4, the omnidirectional adjustment cycloid propeller comprises a cylinder 1, an inner sleeve 2, a motor 3, a lateral mounting seat 4, an electric cylinder 5, a connecting block 16 and blades 22, wherein sliding chutes 6 are formed in the cylinder 1 in an array manner, sliding chute ports 7 are formed between the inner walls of the upper side and the lower side of each sliding chute 6 and the upper end surface and the lower end surface of the cylinder 1 in a penetrating manner, a limiting sliding block 23 is arranged in each sliding chute 6 in a sliding manner, the upper end and the lower end of each limiting sliding block 23 are respectively and fixedly connected with a guide block 8 and a rotating shaft seat 9 in a rotating manner, the output end of each electric cylinder 5 is fixedly connected with a hinged seat 12, and the other end of each electric cylinder is fixedly connected with a supporting seat 11; the supporting seat 11 is arranged in the center of the top surface of the cylinder 1, the electric cylinders 5 are fixedly arranged around the supporting seat 11 in an array mode, the output end of each electric cylinder 5 is fixedly connected with a hinged seat 12, the lower end of the rotating shaft seat 9 is fixedly connected with a connecting seat plate 14, an Chakong penetrates through the connecting seat plate 14, the lower end of the connecting block 16 is fixedly connected with a limiting sleeve 17, and a direction adjusting assembly is arranged between the limiting sleeve 17 and the motor 3;
an inner sleeve 2 is arranged in the center of a cylinder 1, a motor 3 is fixedly mounted on the upper inner wall of the inner sleeve 2, sliding chutes 6 are formed in the cylinder 1 in an array mode, sliding chute ports 7 formed in the upper inner wall and the lower inner wall of each sliding chute 6 penetrate through the upper end face and the lower end face of the cylinder 1, blades 22 are fixedly connected to the lower end of a connecting seat plate 14, lateral installation seats 4 are fixedly connected to the outer side face of the cylinder 1 in an array mode, a connecting rod 13 is fixedly mounted on the upper end face of each lateral installation seat, and a connecting block 16 is fixedly connected to the lower end of each lateral installation seat; the direction adjusting assembly comprises limiting slide rods 18, pin shaft seats 19, adjusting plates 20 and I-shaped rotary drums 21, wherein the limiting slide rods 18 are sleeved in each limiting sleeve 17 in a sliding mode, the pin shaft seats 19 are mounted at the mutually close ends of the limiting slide rods 18, the adjusting plates 20 are connected to the pin shaft seats 19 in a rotating mode, I-shaped rotary drums 21 are fixedly connected to the output ends of the lower sides of the motors 3, each adjusting plate 20 is connected to the I-shaped rotary drums 21 in a rotating mode, limiting slide blocks 23 are arranged in the sliding grooves 6 in a sliding mode, guide blocks 8 fixedly connected to the upper ends and the lower ends of the limiting slide blocks 23 respectively and rotating shaft seats 9 in a rotating mode are arranged in sliding mode in slide way openings 7 formed in the upper inner wall and the lower inner wall of the sliding grooves 6 respectively, the upper ends of the guide blocks 8 penetrate through the slide way openings 7 to extend above the rotary drums 1, hinged seats 12 are mounted at extending ends, the mutually close ends of the hinged seats 12 are connected with the output ends of the electric cylinders 5 on the respective sides, and the other ends of the electric cylinders 5 on the respective sides are fixedly connected to the supporting seats 11;
in the embodiment, the cylinder 1 is provided with the sliding chutes 6 in an array manner, sliding chute ports 7 are formed between the upper inner wall and the lower inner wall of each sliding chute 6 and the upper end surface and the lower end surface of the cylinder in a penetrating manner, the sliding chutes 6 are provided with the limiting sliding blocks 23 in a sliding manner, the upper end and the lower end of each limiting sliding block 23 are respectively fixedly connected with the guide block 8 and the rotating sleeve is provided with the rotating shaft seat 9, the guide blocks 8 are arranged in the sliding chute ports 7 in a sliding manner and extend above the cylinder 1, the outer side surface of the cylinder 1 is fixedly connected with the lateral mounting seat 4 in an array manner, the upper end surface of the lateral mounting seat is fixedly provided with the connecting rod 13, and the lower end of the lateral mounting seat is fixedly connected with the connecting block 16; the articulated seat 12 of the equal fixedly connected with of output of each electric cylinder 5, other end fixed connection is in supporting seat (11), the articulated seat 12 of upside extension fixed mounting of every guide block 8, and install connection base plate 14 on the pivot seat 9 of downside, and the lower terminal surface fixed mounting who connects base plate 14 has blade 22, can control like this through the articulated seat 12 of each electric cylinder 5 synchronous drive, and then make each stop block 23 be close to or keep away from mutually slide in spout 6, and then can drive the dispersion that each blade 22 of downside was close to mutually and is gathered together or keep away from mutually, and obtain different power effects.
Example two:
as shown in fig. 1 to 4, on the basis of the first embodiment, another technical solution provided by the present invention is: the lower end of the rotating shaft seat 9 penetrates through the slide way opening 7 to extend to the lower side of the cylinder 1, an adjusting plate 14 is fixedly connected to the extending end of the lower side, blades 22 are fixedly mounted at the lower end of each adjusting plate 14, a limiting sleeve 17 is fixedly connected to the lower end of each connecting block 16, the mutually close ends of limiting slide rods 18 slidably sleeved in the limiting sleeves 17 extend to the mutually close ends of the limiting sleeves 17, shaft seat pin shafts 19 are fixedly mounted at the extending ends of the limiting slide rods 18, adjusting plates 20 are rotatably mounted on the I-shaped rotary drum 21 in an array mode, and the mutually far ends of the adjusting plates 20 are rotatably connected with the pin shaft seats 19 on one side of each adjusting plate 20;
in this embodiment, the connection seat plate 14 is provided with the insertion holes 15, the lower end surface of each lateral installation seat 4 is fixedly connected with a limit sleeve 17 through a connection block, a limit slide bar 18 is sleeved in the limit sleeve 17 in a sliding manner, the end of each limit slide bar 18 close to each other passes through the corresponding limit sleeve 17 and extends to one side of each limit sleeve 17 close to each other, a pin shaft seat 19 is fixedly installed at the extending end, the center of the cylinder 1 is provided with the inner sleeve 2, the upper inner wall of the inner sleeve 2 is fixedly provided with the motor 3, the output end of the lower side of the motor 3 is fixedly connected with the i-shaped cylinder 21, the outer side surface of the i-shaped cylinder 21 is rotatably provided with the adjusting plates 20, one end of each adjusting plate 20 far away from the i-shaped cylinder is rotatably connected with the pin shaft seat 19 at each side, and further the i-shaped cylinder 21 can be driven to rotate by the motor 3, the adjusting plate 20 is driven to rotate, so that each adjusting plate 20 can rotate to different angles, the limiting slide rods 18 which are respectively and rotatably connected with each other through the pin shaft seats 19 are pulled to slide in the limiting sleeves 17, the connecting seat plate 14 which is sleeved on the outer side of the adjusting plate through the inserting holes 15 can rotate for a certain angle along the adjusting plate 20, and further the angle of each blade 22 in the tangential direction of the circular track of the circumferential motion of the blade can be adjusted, so that different power effects are obtained, and when each limiting slide block 23 is at different positions in the sliding groove 6, the adjusting plate can drive the blade 22 to rotate for adjusting the angle possibly to be different, so that the experiment can be carried out in advance through the existing computer data simulation pole technology, and then the data intelligent control is carried out between the experiment, so that when the limiting slide blocks 23 are at different positions in the sliding groove 6, the angle of the blade 22 can be precisely adjusted by the driving of the motor 3, and the motor 2 adopts a servo motor for improving the precision.
The working principle of the invention is as follows: when the device is installed and used, the sliding grooves 6 are formed in the cylinder 1 in an array mode, sliding channel openings 7 are formed in the positions, penetrating through the upper inner wall and the lower inner wall of each sliding groove 6 and the upper end face and the lower end face of the cylinder, limiting sliding blocks 23 are arranged in the sliding grooves 6 in a sliding mode, the upper end ends and the lower end ends of the limiting sliding blocks 23 are respectively fixedly connected with guide blocks 8 and rotating shaft seats 9 in a sleeved mode, the guide blocks 8 are arranged in the sliding channel openings 7 in a sliding mode and extend above the cylinder 1, lateral installation seats 4 are fixedly connected to the outer side face of the cylinder 1 in an array mode, and connecting rods 13 are fixedly installed on the upper end face of each lateral installation seat 4; the output end of each electric cylinder 5 is fixedly connected with a hinged seat 12, the other end of each electric cylinder is fixedly connected with a supporting seat 11, the upper extending end of each guide block 8 is fixedly provided with the hinged seat 12, the rotating shaft seat 9 at the lower side is provided with a connecting seat plate 14, and the lower end face of the connecting seat plate 14 is fixedly provided with a blade 22, so that the hinged seats 12 can be synchronously driven to move left and right through each electric cylinder 5, each limiting slide block 23 can slide in the sliding groove 6 when approaching or separating from each other, and each blade 22 at the lower side can be driven to gather together or separate from each other, thereby obtaining different power effects; the installation holes 15 are arranged on the connecting seat plate 14, the lower end surface of each lateral mounting seat 4 is fixedly connected with a limiting sleeve 17 through a connecting block, a limiting slide rod 18 is sleeved in the limiting sleeve 17 in a sliding mode, one end, close to each other, of each limiting slide rod 18 penetrates through the corresponding limiting sleeve 17 and extends to one side, close to each limiting sleeve 17, a pin shaft seat 19 is fixedly installed at an extending end, an inner sleeve 2 is arranged at the center of the cylinder 1, a motor 3 is fixedly installed on the upper inner wall of the inner sleeve 2, an I-shaped cylinder 21 is fixedly connected to the output end of the lower side of the motor 3, an adjusting plate 20 is rotatably installed on the outer side surface array of the I-shaped cylinder 21, one end, far away from the I-shaped cylinder, of each adjusting plate 20 is rotatably connected with the pin shaft seat 19 on the corresponding side, the I-shaped cylinder 21 can be driven to rotate by the motor 3, the adjusting plate 20 is driven to rotate to different angles, the adjusting plates 20 can be rotated to different angles, meanwhile, the limiting slide rods 18 rotatably connected to the corresponding to the limiting slide in the limiting sleeves 17, the limiting slide plates 22, the adjusting grooves can be driven by different rotation angles of the connecting seat plate 15, and the sliding grooves 6 of the adjusting plate can be controlled by different rotation directions of the rotating speed data of the existing adjusting mechanism, and the sliding grooves 6, so that the sliding grooves 6 can be calculated in advance when the sliding grooves of the sliding block, and the sliding chute 6 of the sliding block can be controlled by different rotation of the sliding chute, the sliding block, the sliding mechanism, to precisely adjust the angle of the vane 22, and to improve the accuracy, the motor 2 employs a servo motor.
The above is only a preferred embodiment of the present invention, and the protection scope of the present invention is not limited to the above-mentioned embodiments, and all technical solutions belonging to the idea of the present invention belong to the protection scope of the present invention. It should be noted that several modifications and adaptations without departing from the principles of the present invention are intended to be within the scope of the present invention.
Claims (9)
1. An omnidirectional adjustment cycloid propeller comprises a cylinder (1), a motor (3), an electric cylinder (5), a chute (6), a slideway port (7), a guide block (8), a rotating shaft seat (9), a supporting seat (11), a hinged seat (12), a connecting seat plate (14), an inserting hole (15), a connecting block (16), a limiting sleeve (17) and blades (22),
the device is characterized in that sliding chutes (6) are arranged in the cylinder (1) in an array manner, and sliding chute openings (7) are formed between the inner walls of the upper side and the lower side of each sliding chute (6) and the upper end face and the lower end face of the cylinder (1) in a penetrating manner;
limiting sliding blocks (23) are arranged in the sliding grooves (6) in a sliding mode, and the upper end and the lower end of each limiting sliding block (23) are fixedly connected with a guide block (8) and a rotating shaft seat (9) respectively;
the output end of each electric cylinder (5) is fixedly connected with a hinge seat (12), the other end of each hinge seat is fixedly connected with one end of the support seat (11), and one end of each hinge seat (12) is connected with the output end of the electric cylinder (5) on the side of the hinge seat;
a connecting seat plate (14) is fixedly connected to the lower end of the rotating shaft seat (9), and An Chakong (15) penetrates through the connecting seat plate (14);
the lower end of the connecting block (16) is fixedly connected with a limiting sleeve (17), and a direction adjusting assembly is arranged between the limiting sleeve (17) and the motor (3).
2. The omni-directionally regulated cycloidal propeller of claim 1,
an inner sleeve (2) is arranged at the center of the cylinder (1), a motor (3) is fixedly arranged on the upper inner wall of the inner sleeve (2), and an I-shaped cylinder (21) is fixedly connected to the output end of the lower side of the motor (3);
the arranged slideway ports (7) penetrate through the upper end surface and the lower end surface of the cylinder (1);
the lower end of the connecting seat plate (14) is fixedly connected with a blade (22).
3. An omni-directionally regulated cycloidal propeller as claimed in claim 1,
a lateral mounting seat (4) is fixedly connected to the outer side surface array of the cylinder (1),
and the upper end surface of each lateral mounting seat (4) is fixedly provided with a connecting rod (13), and the lower end of each lateral mounting seat is fixedly connected with a connecting block (16).
4. An omni-directionally regulated cycloidal propeller as claimed in claim 2,
the direction adjusting component comprises a limiting slide rod (18), a pin shaft seat (19), an adjusting plate (20) and an I-shaped rotary drum (21);
limiting slide rods (18) are slidably sleeved in each limiting sleeve (17), a pin shaft seat (19) is arranged at one end, close to each other, of each limiting slide rod (18), and an adjusting plate (20) is rotatably connected to the pin shaft seat (19);
each adjusting plate (20) is rotatably connected to the I-shaped cylinder (21).
5. The omni-directionally regulated cycloidal propeller of claim 1,
the limiting slide block (23) is arranged in the sliding groove (6) in a sliding mode, and the guide block (8) fixedly connected with the upper end and the lower end of the limiting slide block (23) and the rotating shaft seat (9) sleeved with the limiting slide block in a rotating mode are arranged in the sliding way opening (7) formed in the upper inner wall and the lower inner wall of the sliding groove (6) in a sliding mode.
6. The omni-directionally regulated cycloidal propeller of claim 1,
the upper end of the guide block (8) passes through the slideway port (7) and extends above the cylinder (1), and a hinge seat (12) is arranged at the extending end;
one end of each hinged seat (12) is connected with the output end of the electric cylinder (5) on each side.
7. An omni-directionally regulated cycloidal propeller as claimed in claim 1,
the lower end of the rotating shaft seat (9) passes through the slide way port (7) and extends to the lower side of the cylinder (1), and an adjusting plate (14) is fixedly connected to the extending end of the lower side;
and the lower end of each adjusting plate (14) is fixedly provided with a blade (22).
8. An omni-directionally regulated cycloidal propeller as claimed in claim 3,
the lower end of each connecting block (16) is fixedly connected with a limiting sleeve (17), one end, close to each other, of a limiting slide rod (18) slidably sleeved in the limiting sleeve (17) extends to one end, close to each limiting sleeve (17), of each limiting slide rod, and a pin shaft seat (19) is fixedly mounted at the extending end of each limiting slide rod (18).
9. An omni-directionally regulated cycloidal propeller as claimed in claim 2,
adjusting plates (20) are rotatably arranged on the I-shaped rotary drum (21) in an array mode, and one ends, far away from each other, of the adjusting plates (20) are rotatably connected with pin shaft seats (19) on one side of each adjusting plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210937099.2A CN115258109A (en) | 2022-08-05 | 2022-08-05 | Omnidirectional adjustment cycloid propeller |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210937099.2A CN115258109A (en) | 2022-08-05 | 2022-08-05 | Omnidirectional adjustment cycloid propeller |
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| Publication Number | Publication Date |
|---|---|
| CN115258109A true CN115258109A (en) | 2022-11-01 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202210937099.2A Pending CN115258109A (en) | 2022-08-05 | 2022-08-05 | Omnidirectional adjustment cycloid propeller |
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Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1205836A (en) * | 1956-08-10 | 1960-02-04 | Voith Gmbh J M | Cycloidal nautical thruster |
| DE102009026382A1 (en) * | 2009-07-17 | 2011-02-03 | Nescholta, Friedhelm, Dipl.-Ing. | Method for positioning of rotating paddles on paddle wheel, involves bringing paddles in position perpendicular to water surface by positioning device directly by immersing into water |
| CN103723259A (en) * | 2013-12-31 | 2014-04-16 | 浙江大学 | Blade swing mechanism and marine cycloidal propeller comprising blade swing mechanism |
| CN205186489U (en) * | 2015-12-11 | 2016-04-27 | 浙江大学 | Slider -crank formula blade swing mechanism and including straight wing propeller of this mechanism |
| WO2020120824A1 (en) * | 2018-12-14 | 2020-06-18 | Abb Oy | A cycloidal marine propulsion unit and a marine vessel equipped therewith |
| CN113086149A (en) * | 2021-05-13 | 2021-07-09 | 鸿蒙海工(大庆)科技有限公司 | Multi-link mechanism based on VSP novel cycloidal propeller |
-
2022
- 2022-08-05 CN CN202210937099.2A patent/CN115258109A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1205836A (en) * | 1956-08-10 | 1960-02-04 | Voith Gmbh J M | Cycloidal nautical thruster |
| DE102009026382A1 (en) * | 2009-07-17 | 2011-02-03 | Nescholta, Friedhelm, Dipl.-Ing. | Method for positioning of rotating paddles on paddle wheel, involves bringing paddles in position perpendicular to water surface by positioning device directly by immersing into water |
| CN103723259A (en) * | 2013-12-31 | 2014-04-16 | 浙江大学 | Blade swing mechanism and marine cycloidal propeller comprising blade swing mechanism |
| CN205186489U (en) * | 2015-12-11 | 2016-04-27 | 浙江大学 | Slider -crank formula blade swing mechanism and including straight wing propeller of this mechanism |
| WO2020120824A1 (en) * | 2018-12-14 | 2020-06-18 | Abb Oy | A cycloidal marine propulsion unit and a marine vessel equipped therewith |
| CN113086149A (en) * | 2021-05-13 | 2021-07-09 | 鸿蒙海工(大庆)科技有限公司 | Multi-link mechanism based on VSP novel cycloidal propeller |
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