Zero calibration device for steering oar

Abstract

The utility model discloses a zero calibration device for a steering oar, and relates to the technical field of zero calibration devices for steering oars. The steering oar comprises a steering oar body, a containing groove is formed in the top face of the steering oar body, a connecting assembly is connected with the interior of the containing groove in a sleeved mode, a connecting column is connected with the interior of the connecting assembly in a sleeved mode, and an identification block is fixedly connected with the top face of the connecting column. According to the zero position calibration device for the steering oar, through the arrangement of the calibration assembly, clamping plates in clamping plates on the side faces of identification blocks are pulled, limiting and fixing of the clamping plates are completed, then a pointer fixed to the side face of a lantern ring is aligned to a gap between the two clamping plates and then connected to the surface of the steering oar in a sleeving mode, and calibration operation on the zero position is completed; therefore, the effects that whether the angle is zero or not does not need to be observed with naked eyes, after the pointer is located between the two clamping plates, the zero position is represented successfully, more convenience and rapidness are achieved, and the zero degree accuracy of the axis included angle is improved are achieved.

Description

Technical Field

[0001] The utility model relates to the technical field of a zero-position calibration device for a steering propeller, in particular to a zero-position calibration device for a steering propeller. Background Art

[0002] The zero-position calibration of the prior art is an important task in the production of rudder propellers. The zero-position calibration is to make the angle between the input axis of the rudder propeller and the output axis of the rudder propeller in the top-view direction zero degree, and calibrate this position so that when the rudder propeller is installed on the ship, it can be used to identify the positive propulsion direction of the rudder propeller relative to the hull. The usual practice is to use a positioning pin. When it is in the zero position, the pin is inserted into the pre-punched zero position hole to determine whether the rudder propeller is in the zero position.

[0003] A zero-position calibration device for a rudder propeller is disclosed in the publication number CN213566426U. Although the zero-position calibration device of the utility model has the advantages of easy installation, safety and reliability, and high calibration accuracy.

[0004] However, the zero-position calibration device for the steering propeller has the following disadvantages:

[0005] (1) When it is necessary to observe whether the axis angle reaches zero, personnel are often required to observe with the naked eye, which will result in a certain deviation and affect the accuracy of the axis angle zero;

[0006] (2) When installing and fixing the zero position calibration, the operation is rather complicated and cannot be installed quickly, which affects work efficiency.

[0007] In view of this, the present utility model is proposed. Utility Model Content

[0008] The technical problem to be solved by the utility model is to overcome the deficiencies of the prior art and provide a zero position calibration device for a rudder propeller, thereby solving the problems raised in the above-mentioned background technology.

[0009] In order to solve the above technical problems, the basic concept of the technical solution adopted by the utility model is:

[0010] A zero position calibration device for a steering propeller, comprising: a steering propeller, a placement groove is provided on the top surface of the steering propeller, a connecting component is sleeved inside the placement groove, a connecting column is sleeved inside the connecting component, a marking block is fixedly connected to the top surface of the connecting column, calibration components are fixedly connected to both sides of the marking block, a collar is sleeved on the surface of the steering propeller, and a pointer is fixedly connected to the side of the collar;

[0011] The calibration component includes a clamping plate which is fixedly connected to the side of the identification block in an axisymmetric manner, a clamping plate is rotatably connected inside the clamping plate, the top and bottom surfaces of the clamping plate are provided with holes, a spring is sleeved inside the holes, the top surface of the spring is fixedly connected to a limiting bean, and the limiting bean is clamped to a clamping block which is fixedly connected to the side of the identification block in an axisymmetric manner.

[0012] Optionally, three slots are sequentially opened on the bottom surface of the card block from left to right, and matching limiting beans are clamped inside the slots. After the limiting beans are clamped in the slots on the surface of the card block, the clamping plate can be effectively limited and fixed.

[0013] Optionally, the connecting component includes a mounting block which is sleeved inside the placement groove, a sliding groove is provided on the surface of the mounting block, a snap structure is slidably connected inside the sliding groove, and a telescopic structure is fixedly connected to the side of the sliding groove in an axially symmetrical manner. After placing the connecting column inside the mounting block, the snap structure is snapped into the inside of the connecting column, so that the calibration component fixed to the connecting column and the top surface can be quickly installed.

[0014] Optionally, the buckle structure includes a slide bracket slidably connected to the inside of the slide groove, and a clamping rod is axially symmetrically sleeved on the surface of the slide bracket.

[0015] Optionally, a socket is axially symmetrically provided on the surface of the connecting column, the inner diameter of the socket matches the outer diameter of the clamping rod, a clamping rod is inserted into the inside of the socket, and the socket of the clamping rod matches the connecting column, so as to effectively clamp and install the clamping rod firmly.

[0016] Optionally, the telescopic structure includes a sleeve fixedly connected to the side of the slide groove, a return spring is sleeved inside the sleeve, one end of the return spring is fixedly connected to a push rod, and the extension and retraction of the return spring can effectively drive the slide to slide, so that it drives the clamping rod to clamp and disengage the connecting column.

[0017] After adopting the above technical solution, the utility model has the following beneficial effects compared with the prior art. Of course, any product implementing the utility model does not necessarily need to achieve all the advantages described below at the same time:

[0018] 1. The zero position calibration device for the steering paddle, through the setting of the calibration component, pulls the clamping plate connected by the gripping inside the clamping plate on the side of the identification block, so that the limiting bean on the surface of the clamping plate is squeezed by the clamping block and shrinks into the inside of the sleeve hole by the limiting bean set on the top surface of the sleeve hole by the spring, and after the clamping plate is moved to a suitable position, the spring rebounds and drives the limiting bean to reset and clamp into the inside of the clamping groove on the bottom surface of the clamping block, so as to complete the limiting fixation of the clamping plate, and then, after the pointer fixed on the side of the ring is aligned with the gap between the two clamping plates, it is sleeved on the surface of the steering paddle to complete the calibration operation of the zero position, so that there is no need to observe whether the angle is zero degree with the naked eye. When the pointer is between the two clamping plates, it means that the zero position is successfully indicated, which is more convenient and quick, and has the effect of improving the accuracy of the zero degree of the axis angle.

[0019] 2. The zero-position calibration device for the rudder propeller, through the setting of the connecting component, presses the slide to move it and drives the push rod reset spring to compress, inserts the connecting column fixedly connected to the bottom surface of the identification block into the interior of the mounting block, and then releases the slide, the reset spring resets and drives the push rod to reset the slide, and the clamping rod sleeved on the surface of the slide is inserted into the interior of the connecting column to complete the clamping installation of the connecting column, so that the calibration component can be quickly installed, thereby achieving the effect of quick installation and improving work efficiency.

[0020] The specific implementation of the utility model is further described in detail below with reference to the accompanying drawings. BRIEF DESCRIPTION OF THE DRAWINGS

[0021] The drawings described below are only some embodiments. For those skilled in the art, other drawings can be obtained based on these drawings without creative work.

[0022] In the figure:

[0023] Figure 1 It is a schematic diagram of the overall structure of the utility model;

[0024] Figure 2 This is a schematic diagram of the structure of the calibration component of the utility model;

[0025] Figure 3 This is a schematic diagram of the structure of the connection assembly of the utility model;

[0026] Figure 4 It is a schematic diagram of the split structure of the utility model.

[0027] In the figure: 1. rudder propeller; 2. connecting assembly; 21. mounting block; 22. snap-fit ​​structure; 221. slide; 222. clamping rod; 23. telescopic structure; 231. sleeve; 232. reset spring; 233. push rod; 3. connecting column; 4. identification block; 5. calibration assembly; 51. splint; 52. clamping plate; 53. spring; 54. limit bean; 55. clamping block; 6. collar; 7. pointer.

[0028] It should be noted that these drawings and textual descriptions are not intended to limit the conceptual scope of the present invention in any way, but rather to illustrate the concept of the present invention for those skilled in the art by referring to specific embodiments. DETAILED DESCRIPTION

[0029] The utility model will now be further described in detail with reference to the accompanying drawings.

[0030] See also Figure 1-4 As shown, in this embodiment, a zero position calibration device for a steering propeller is provided, including a steering propeller 1, a placement groove is opened on the top surface of the steering propeller 1, a connecting component 2 is sleeved inside the placement groove, a connecting column 3 is sleeved inside the connecting component 2, an identification block 4 is fixedly connected to the top surface of the connecting column 3, calibration components 5 are fixedly connected to both sides of the identification block 4, a ring 6 is sleeved on the surface of the steering propeller 1, and a pointer 7 is fixedly connected to the side of the ring 6.

[0031] Embodiment 1:

[0032] See also Figure 2 As shown, in this embodiment, the calibration component 5 includes a clamping plate 51 which is fixedly connected to the side of the identification block 4 in an axisymmetric manner, a clamping plate 52 is rotatably connected inside the clamping plate 51, the top and bottom surfaces of the clamping plate 52 are provided with sleeve holes, a spring 53 is sleeved inside the sleeve hole, a limiting bean 54 is fixedly connected to the top surface of the spring 53, the limiting bean 54 is clamped to a clamping block 55 which is fixedly connected to the side of the identification block 4 in an axisymmetric manner, and three clamping grooves are sequentially provided on the bottom surface of the clamping block 55 from left to right, and the inside of the clamping groove is clamped with a matching limiting bean 54;

[0033] By setting the calibration component 5, the clamping plate 52 connected to the clamping plate 51 on the side of the identification block 4 is pulled, so that the limiting bean 54 on the surface of the clamping plate 52 set on the top surface of the hole by the spring 53 is squeezed by the clamping block 55 and shrinks into the hole. After the clamping plate 52 is moved to a suitable position, the spring 53 rebounds and drives the limiting bean 54 to reset and clamp in the clamping groove on the bottom surface of the clamping block 55, completing the limiting fixation of the clamping plate 52. Then, after the pointer 7 fixed on the side of the ring 6 is aligned with the gap between the two clamping plates 52, it is sleeved on the surface of the rudder paddle 1 to complete the calibration operation of the zero position, thereby achieving the effect of not needing to observe whether the angle is zero degree with the naked eye. When the pointer 7 is between the two clamping plates 52, it means that the zero position is successfully indicated, which is more convenient and quick, and improves the accuracy of the zero degree of the axis angle.

[0034] Embodiment 2:

[0035] See also Figure 3As shown, in this embodiment, the connecting assembly 2 includes a mounting block 21 sleeved inside the placement groove, a sliding groove is provided on the surface of the mounting block 21, a slide 221 is slidably connected inside the sliding groove, a clamping rod 222 is sleeved on the surface of the slide 221 in an axisymmetric manner, a sleeve 231 is fixedly connected to the side of the sliding groove, a return spring 232 is sleeved inside the sleeve 231, and one end of the return spring 232 is fixedly connected to a push rod 233;

[0036] By setting the connecting component 2, the slide 221 is pressed to move and the return spring 232 of the push rod 233 is compressed. The connecting column 3 fixedly connected to the bottom surface of the identification block 4 is inserted into the interior of the mounting block 21. Then the slide 221 is released, and the return spring 232 is reset to drive the push rod 233 to drive the slide 221 to reset. The clamping rod 222 sleeved on the surface of the slide 221 is inserted into the interior of the connecting column 3 to complete the clamping installation of the connecting column 3, so that the calibration component 5 can be installed quickly, thereby achieving the effect of quick installation and improving work efficiency.

[0037] One aspect of the application of this embodiment is that the working steps of the device are as follows:

[0038] First, the clamping plate 52 connected to the clamping plate 51 on the side of the identification block 4 is pulled, so that the limiting bean 54 set on the top surface of the sleeve hole by the spring 53 on the surface of the clamping plate 52 is squeezed by the clamping block 55 and shrinks into the sleeve hole. After the clamping plate 52 is moved to a suitable position, the spring 53 rebounds and drives the limiting bean 54 to reset and clamp it in the clamping groove on the bottom surface of the clamping block 55, completing the limiting fixation of the clamping plate 52. Then, after aligning the pointer 7 fixed on the side of the ring 6 with the gap between the two clamping plates 52, the sleeve is connected. On the surface of the rudder propeller 1, complete the calibration operation of the zero position, and finally, press the slide 221 to move it while driving the top rod 233 to compress the reset spring 232, insert the connection column 3 fixedly connected to the bottom surface of the identification block 4 into the interior of the installation block 21, and then release the slide 221, the reset spring 232 resets and drives the top rod 233 to drive the slide 221 to reset, and the clamping rod 222 sleeved on the surface of the slide 221 is inserted into the interior of the connection column 3, completing the clamping installation of the connection column 3, so that the calibration component 5 can be quickly installed. It should be noted that all electrical equipment involved in this application can be powered by batteries or external power supplies.

[0039] The present invention is not limited to the above-mentioned implementation modes. Anyone should be aware of the structural changes made under the inspiration of the present invention. Any technical solution that is the same or similar to the present invention falls within the protection scope of the present invention. The technology, shape, and structure that are not described in detail in the present invention are all known technologies.

Claims

1. A zero position calibration device for a rudder propeller, characterized in that: include: A steering paddle (1), wherein a placement groove is provided on the top surface of the steering paddle (1), a connecting component (2) is sleeved inside the placement groove, a connecting column (3) is sleeved inside the connecting component (2), an identification block (4) is fixedly connected to the top surface of the connecting column (3), both sides of the identification block (4) are fixedly connected to calibration components (5), a collar (6) is sleeved on the surface of the steering paddle (1), and a pointer (7) is fixedly connected to the side of the collar (6); The calibration component (5) comprises a clamping plate (51) fixedly connected to the side of the identification block (4) in an axisymmetric manner, a clamping plate (52) rotatably connected inside the clamping plate (51), a sleeve hole is provided on the top and bottom surfaces of the clamping plate (52), a spring (53) is sleeved inside the sleeve hole, a limit bean (54) is fixedly connected to the top surface of the spring (53), and the limit bean (54) is clamped to a clamping block (55) fixedly connected to the side of the identification block (4) in an axisymmetric manner.

2. A zero position calibration device for a rudder propeller according to claim 1, characterized in that: The bottom surface of the clamping block (55) is provided with three clamping grooves in sequence from left to right, the inner diameter of the clamping grooves matches the outer diameter of the limiting bean (54), and the limiting bean (54) is clamped inside the clamping grooves.

3. A zero position calibration device for a rudder propeller according to claim 1, characterized in that: The connection assembly (2) comprises a mounting block (21) sleeved inside the placement groove, a sliding groove is provided on the surface of the mounting block (21), a buckle structure (22) is slidably connected inside the sliding groove, and a telescopic structure (23) is fixedly connected to the side of the sliding groove in an axisymmetric manner.

4. A zero position calibration device for a rudder propeller according to claim 3, characterized in that: The buckle structure (22) comprises a slide frame (221) slidably connected to the inside of the slide groove, and a clamping rod (222) is sleeved on the surface of the slide frame (221) in an axisymmetric manner.

5. A zero position calibration device for a rudder propeller according to claim 1, characterized in that: The surface of the connecting column (3) is provided with an insertion hole in an axisymmetric manner, the inner diameter of the insertion hole matches the outer diameter of the clamping rod (222), and the clamping rod (222) is inserted into the interior of the insertion hole.

6. A zero position calibration device for a rudder propeller according to claim 3, characterized in that: The telescopic structure (23) comprises a sleeve (231) fixedly connected to the side of the slide groove, a return spring (232) is sleeved inside the sleeve (231), and one end of the return spring (232) is fixedly connected to a push rod (233).

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