CN111634410A - Convenient small-size rudder cabin interior mounting structure who dismantles - Google Patents
Convenient small-size rudder cabin interior mounting structure who dismantles Download PDFInfo
- Publication number
- CN111634410A CN111634410A CN202010377607.7A CN202010377607A CN111634410A CN 111634410 A CN111634410 A CN 111634410A CN 202010377607 A CN202010377607 A CN 202010377607A CN 111634410 A CN111634410 A CN 111634410A
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- China
- Prior art keywords
- rudder
- rudder shaft
- shell
- shaft sleeve
- mounting structure
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H25/00—Steering; Slowing-down otherwise than by use of propulsive elements; Dynamic anchoring, i.e. positioning vessels by means of main or auxiliary propulsive elements
- B63H25/06—Steering by rudders
- B63H25/38—Rudders
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
- Sealing Devices (AREA)
Abstract
The invention discloses a conveniently-detachable small rudder cabin inner mounting structure which comprises a rudder blade, a rudder shaft, a shell, a lubricating gasket, a rudder shaft sleeve, a steering engine, a rotary grating ring and an O-shaped sealing ring. The lower end surface of the rudder shaft is fixedly connected with the rudder blade and sequentially penetrates through the shell, the lubricating gasket and the rudder shaft sleeve from bottom to top; the rudder blade is tightly attached to the shell, and the rudder shaft is provided with a lubricating and sealing ring structure which is matched with the rudder shaft hole and the sealing groove on the shell to ensure the lubrication and the sealing of the rudder shaft; the lubrication gasket is located between the rudder shaft sleeve and the shell and used for reducing friction between the rudder shaft sleeve and the shell. The tail end of the rudder shaft is a polygonal prism which is matched with a polygonal inner hole of the rudder shaft sleeve, the rudder shaft sleeve and the rudder shaft are fixed by using a countersunk head screw, and the diameter of the rudder shaft sleeve is larger than that of a rudder shaft hole in the shell, so that the rudder shaft is prevented from being separated from the shell. By using the mounting structure in the small rudder cabin, the rudder shaft can be quickly disassembled and assembled in a narrow space, the positioning is accurate, the stability in the using process is ensured, and the strength is reliable.
Description
Technical Field
The invention relates to a conveniently-detachable small rudder cabin mounting structure, and belongs to the technical field of machinery.
Background
The rudder shaft is a transmission device which connects the rudder blade with the steering engine driving mechanism and transmits torque. The traditional rudder shaft adopts a fixing structure of a clamping ring, the mounting process is complex, a large mounting space is needed, and the positioning precision of rudder mounting is reduced by repeated dismounting. Because the installation space of the small rudder is compact and the installation space of the rudder shaft is limited, the traditional snap ring can not meet the requirement. In addition, the ring groove on the rudder shaft can reduce the strength of the rudder shaft and influence the service life of the rudder shaft.
Disclosure of Invention
The technical problem to be solved by the invention is as follows: the small-sized rudder mounting structure overcomes the defects of the prior art, is convenient to detach, has compact structure, simple processing, simple and convenient and fast mounting, accurate positioning and high accuracy, meets the precision requirement of positioning and mounting of the rudder shaft, and effectively avoids the annular groove structure from reducing the strength of the rudder shaft.
The technical solution of the invention is as follows:
a small rudder cabin inner mounting structure convenient to disassemble comprises a rudder blade (1), a rudder shaft (2), a shell (3), a rotating Geleye ring (4), a good type sealing ring (5), a lubricating gasket (7), a rudder shaft sleeve (8), a countersunk screw (9) and a steering engine;
the rudder blade (1) is positioned outside the shell (3), the rudder blade (1) is connected with the rudder shaft (2), the rudder shaft (2) extends into the rudder shaft hole reserved on the shell (3) of the navigation body, sequentially penetrates through the shell (3) and the lubricating gasket (7) and then is connected with the rudder shaft sleeve (8), and the cross section of the inner cavity of the rudder shaft sleeve (8) is consistent with that of the rudder shaft (2);
the upper end surface of the rudder shaft (2) is provided with a threaded hole, and the rudder shaft (2) is tightly connected with a rudder shaft sleeve (8) through a sunk screw (9); the lubricating gasket (7) is positioned between the rudder shaft sleeve (8) and the shell (3), an annular groove (6) is arranged at the position, in contact with the lubricating gasket (7), on the shell (3), the inner diameter of the annular groove (6) is smaller than that of the lubricating gasket (7), the outer diameter of the annular groove (6) is larger than that of the lubricating gasket (7), the surface of the groove is smooth, lubricating grease is filled in the groove, and the lubricating gasket (7) is positioned in the annular groove (6);
the inner wall of the rudder shaft hole of the shell is provided with two annular grooves with different sizes from outside to inside, and a first sealing ring (4) and a second sealing ring (5) are respectively arranged and used for sealing between the rudder shaft (2) and the shell (3); the steering engine is arranged in the shell (3) and drives the rudder shaft sleeve (8) to rotate, torque is transmitted through the rudder shaft (2), and finally the rudder blade (1) is driven to rotate.
Furthermore, the number of the rudder blades is multiple, and the rudder blades are uniformly distributed on the outer side of the shell in the circumferential direction and are used for controlling the navigation depth, the course and the rolling of the navigation body; the rudder blades correspond to the rudder shafts one by one.
Furthermore, the rudder blade and the rudder shaft are integrally formed.
Furthermore, the outer diameter of the rudder shaft sleeve (8) is larger than the diameter of a rudder shaft hole reserved on the shell.
Further, the first seal ring (4) adopts a rotary check ring for high-pressure sealing, and the second seal ring (5) adopts a good-quality seal ring for low-pressure sealing.
Furthermore, the inner cavity of the rudder shaft sleeve (8) is processed into a quadrangle, a hexagon or an octagon, and the upper end of the rudder shaft (2) is processed into a corresponding polygonal columnar structure to be tightly matched with the corresponding polygonal columnar structure.
Furthermore, the shape of the rudder shaft sleeve (8) is a polygonal columnar structure and is matched with the groove of the steering engine driving mechanism, and the rudder shaft sleeve (8) is completely embedded into the groove of the steering engine driving mechanism.
Furthermore, the lubricating gasket (7) is made of copper or polytetrafluoroethylene materials and has a self-lubricating effect.
Furthermore, the upper and lower shaft diameters of the rudder shaft (2) are consistent, and no ring groove is formed on the surface.
Further, the different sizes of the annular grooves specifically refer to: the depth of the first sealing ring (4) is larger than that of the second sealing ring (5).
Compared with the prior art, the invention has the beneficial effects that:
(1) the mounting structure in the small rudder cabin is compact in structure, simple to process and convenient to mount, meets the requirement of the mounting accuracy of the rudder shaft, and can be quickly mounted and dismounted in a narrow space.
(2) By using the mounting structure in the small rudder trunk, under the condition of limited space, the mounting and positioning accuracy of the rudder shaft is ensured on one hand, and the bearing capacity and the structure of the whole rudder shaft are ensured to be reliable on the other hand, and the mounting structure has reliable stability and strength in the using process.
(3) The rudder shaft is provided with a lubricating and sealing ring structure which is matched with a rudder shaft hole and a sealing groove on the shell to ensure the lubrication and the sealing of the rudder shaft; the lubrication gasket is located between the rudder shaft sleeve and the shell and used for reducing friction between the rudder shaft sleeve and the shell.
(4) The diameter of the rudder shaft sleeve is larger than that of the rudder shaft hole in the shell, so that the rudder shaft is prevented from being separated from the shell.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a top view of the present invention;
FIG. 3 is a cross-sectional view of FIG. 2A-A;
fig. 4 is a partially enlarged view of fig. 3.
The labels in the figure are: 1. the rudder blade, 2 rudder shafts, 3 shells, 4 rotating check rings, 5O-shaped sealing rings, 6 annular grooves, 7 lubricating gaskets, 8 rudder shaft sleeves and 9 countersunk head screws.
Detailed Description
As shown in figure 1, the invention provides a conveniently-detachable small rudder cabin inner mounting structure which comprises a rudder blade 1, a rudder shaft 2, a shell 3, a rotary grove ring 4, an O-shaped sealing ring 5, a lubricating gasket 7, a rudder shaft sleeve 8, a sunk screw 9 and a steering engine.
The number of the rudder blades is multiple, and the rudder blades are uniformly distributed on the outer side of the shell in the circumferential direction and used for controlling the integral navigation depth, the integral heading and the integral rolling. Each rudder blade drives the rudder blade to rotate through the torque transmitted by the steering engine and the rudder shaft, and all the steering engines are arranged inside the shell. The lower end of the rudder shaft is connected with the rudder blade, and the rudder shaft and the rudder blade are integrally processed. The upper end of the rudder shaft penetrates through the shell and the lubricating gasket respectively and then is connected with the rudder shaft sleeve, the cylindrical structure of the inner cavity of the rudder shaft sleeve is consistent with the cylindrical structure of the upper end of the rudder shaft, and the outer diameter of the rudder shaft sleeve is larger than that of the rudder shaft hole of the shell. The upper end surface of the rudder shaft is provided with a threaded hole which is tightly connected with the rudder shaft sleeve through a sunk screw 9. The position, in contact with the shell, of the lubricating gasket is provided with an annular groove, the inner diameter of the annular groove is slightly smaller than the inner diameter of the lubricating gasket, the outer diameter of the groove is larger than the outer diameter of the lubricating gasket, the surface of the groove is smooth, and lubricating grease is filled in the groove. Two annular grooves with different sizes are arranged at the position of the rudder shaft hole on the shell and are respectively used for installing a rotary check ring and an O-shaped sealing ring.
According to the magnitude of the transmission torque, the inner cavity of the rudder shaft sleeve 8 can be selectively processed into polygonal columnar structures such as quadrangle, hexagon, octagon and the like, and the upper end of the rudder shaft 2 is processed into a corresponding polygonal columnar structure to be tightly matched with the polygonal columnar structure, so that the torque can be reliably transmitted. The upper end face of the rudder shaft 2 is provided with a threaded hole, the rudder shaft sleeve 8 is provided with a corresponding countersunk hole, and the upper part of the rudder shaft sleeve 8 is connected with the rudder shaft 2 through a countersunk screw 9, so that the rudder shaft 2 is tightly attached to the rudder shaft sleeve 8, and the torque is stably transmitted. The shape of the rudder shaft sleeve 8 can also be selectively processed into polygonal columnar structures such as quadrangle, hexagon, octagon and the like.
The examples of the invention are given below:
the rudder shaft sleeve in this embodiment adopts a hexagonal columnar structure, and is installed in cooperation with the steering gear driving mechanism groove, and the rudder shaft sleeve 8 is completely embedded into the steering gear driving mechanism groove, so that the axial installation space can be saved, the structure is compact, and the disassembly is convenient.
The structure realizes effective torque transmission by closely attaching the side surfaces of the inner polygonal columnar structure and the outer polygonal columnar structure, and realizes the tight connection of the rudder shaft 2, the rudder shaft sleeve 8 and the steering engine driving mechanism by screw fastening and axial dimension limiting to ensure reliable torque transmission.
The position of contact of the lubricating gasket 6 and the shell 3 is provided with an annular groove 6, the inner diameter of the annular groove 6 is slightly smaller than the inner diameter of the lubricating gasket 7, the outer diameter of the annular groove 6 is larger than the outer diameter of the lubricating gasket 7, the surface of the annular groove 6 is smooth, and the annular groove 6 is filled with lubricating grease.
The lubricating gasket 7 is made of copper or polytetrafluoroethylene materials, has a self-lubricating effect, and can prevent the rudder shaft sleeve 8 from dry friction with the shell 3.
Two annular grooves with different sizes are arranged at the position of the rudder shaft hole on the shell and are respectively used for installing a rotary check ring 4 and an O-shaped sealing ring 5. The rotary check ring 4 is used as a first seal, can bear water pressure of up to 20MPa, and has excellent low friction and high speed performance. The O-shaped sealing ring 5 is used as a second seal to compensate leakage possibly existing in the check ring during low pressure, and double sealing is more reliable. In this embodiment, the depth of the annular groove of the rotary check ring is greater than the depth of the annular groove of the O-ring.
The mounting structure in the small rudder cabin is simple to process and quick to mount. In the installation process, the rudder shaft 2 is connected with the rudder shaft sleeve 8 after penetrating through the lubricating gasket 7 from the lower end of the shell 3, and the countersunk head screw 9 above the rudder shaft sleeve is fastened. The upper and lower shaft diameters of the rudder shaft 2 are basically consistent, no ring groove is formed, and the strength is reliable. The device structure is axial symmetry, can effectively guarantee the axiality requirement after the rudder axle installation.
In conclusion, the small rudder cabin mounting structure is compact in structure, convenient to machine and simple to mount, meets the requirement of the mounting accuracy of the rudder shaft 2, and can be quickly mounted and dismounted in a narrow space. By using the small rudder mounting structure, under the condition of limited space, the mounting and positioning accuracy of the rudder shaft 2 is ensured, and the bearing capacity and the structure of the whole rudder shaft 2 are ensured to be reliable, and the stability and the strength in the using process are ensured to be reliable.
The following describes embodiments of the present invention in further detail with reference to the accompanying drawings.
Claims (10)
1. The utility model provides a convenient interior mounting structure of small-size rudder cabin who dismantles which characterized in that: the rudder comprises a rudder blade (1), a rudder shaft (2), a shell (3), a rotary grove ring (4), an O-shaped sealing ring (5), a lubricating gasket (7), a rudder shaft sleeve (8), a sunk screw (9) and a steering engine;
the rudder blade (1) is positioned outside the shell (3), the rudder blade (1) is connected with the rudder shaft (2), the rudder shaft (2) extends into the rudder shaft hole reserved on the shell (3) of the navigation body, sequentially penetrates through the shell (3) and the lubricating gasket (7) and then is connected with the rudder shaft sleeve (8), and the cross section of the inner cavity of the rudder shaft sleeve (8) is consistent with that of the rudder shaft (2);
the upper end surface of the rudder shaft (2) is provided with a threaded hole, and the rudder shaft (2) is tightly connected with a rudder shaft sleeve (8) through a sunk screw (9); the lubricating gasket (7) is positioned between the rudder shaft sleeve (8) and the shell (3), an annular groove (6) is arranged at the position, in contact with the lubricating gasket (7), on the shell (3), the inner diameter of the annular groove (6) is smaller than that of the lubricating gasket (7), the outer diameter of the annular groove (6) is larger than that of the lubricating gasket (7), the surface of the groove is smooth, lubricating grease is filled in the groove, and the lubricating gasket (7) is positioned in the annular groove (6);
the inner wall of the rudder shaft hole of the shell is provided with two annular grooves with different sizes from outside to inside, and a first sealing ring (4) and a second sealing ring (5) are respectively arranged and used for sealing between the rudder shaft (2) and the shell (3); the steering engine is arranged in the shell (3) and drives the rudder shaft sleeve (8) to rotate, torque is transmitted through the rudder shaft (2), and finally the rudder blade (1) is driven to rotate.
2. The conveniently detachable mini rudder trunk internal mounting structure according to claim 1, wherein: the number of the rudder blades is multiple, the rudder blades are circumferentially and uniformly distributed on the outer side of the shell and are used for controlling the navigation depth, the course and the roll of the navigation body; the rudder blades correspond to the rudder shafts one by one.
3. An easily detachable mini rudder trunk internal mounting structure according to claim 1 or 2, wherein: the rudder blade and the rudder shaft are integrally formed.
4. The conveniently detachable mini rudder trunk internal mounting structure according to claim 1, wherein: the outer diameter of the rudder shaft sleeve (8) is larger than the diameter of a rudder shaft hole reserved on the shell.
5. The conveniently detachable mini rudder trunk internal mounting structure according to claim 1, wherein: the first sealing ring (4) adopts a rotary check ring for high-pressure sealing, and the second sealing ring (5) adopts a good-quality sealing ring for low-pressure sealing.
6. The conveniently detachable mini rudder trunk internal mounting structure according to claim 1, wherein: the inner cavity of the rudder shaft sleeve (8) is processed into a quadrangle, a hexagon or an octagon, and the upper end of the rudder shaft (2) is processed into a corresponding polygonal columnar structure to be tightly matched with the corresponding polygonal columnar structure.
7. The conveniently disassembled mini rudder trunk internal mounting structure provided by claim 6, wherein: the rudder shaft sleeve (8) is of a polygonal columnar structure and is installed in a matching mode with the steering engine driving mechanism groove, and the rudder shaft sleeve (8) is completely embedded into the steering engine driving mechanism groove.
8. The conveniently detachable mini rudder trunk internal mounting structure according to claim 1, wherein: the lubricating gasket (7) is made of copper or polytetrafluoroethylene materials and has a self-lubricating effect.
9. The conveniently detachable mini rudder trunk internal mounting structure according to claim 1, wherein: the upper and lower shaft diameters of the rudder shaft (2) are consistent, and no ring groove is formed on the surface.
10. The conveniently detachable mini rudder trunk internal mounting structure according to claim 1, wherein: the annular grooves with different sizes specifically refer to: the depth of the first sealing ring (4) is larger than that of the second sealing ring (5).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010377607.7A CN111634410A (en) | 2020-05-07 | 2020-05-07 | Convenient small-size rudder cabin interior mounting structure who dismantles |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010377607.7A CN111634410A (en) | 2020-05-07 | 2020-05-07 | Convenient small-size rudder cabin interior mounting structure who dismantles |
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| Publication Number | Publication Date |
|---|---|
| CN111634410A true CN111634410A (en) | 2020-09-08 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202010377607.7A Pending CN111634410A (en) | 2020-05-07 | 2020-05-07 | Convenient small-size rudder cabin interior mounting structure who dismantles |
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| CN (1) | CN111634410A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113492967A (en) * | 2021-07-23 | 2021-10-12 | 航天时代飞鹏有限公司 | Device and method for quickly disassembling steering engine of freight unmanned aerial vehicle |
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| CN101074050A (en) * | 2007-06-25 | 2007-11-21 | 哈尔滨工程大学 | Modular steering engine of ship underwater |
| CN201099351Y (en) * | 2007-06-25 | 2008-08-13 | 哈尔滨工程大学 | Underwater navigation body modularized steering engine |
| KR20090015248A (en) * | 2007-08-08 | 2009-02-12 | 한국해양연구원 | Small autonomous underwater vehicle test-bed |
| KR101504949B1 (en) * | 2011-08-17 | 2015-03-23 | 티센크루프 마린 시스템즈 게엠베하 | A rudder device for a water vehicle |
| CN104512542A (en) * | 2013-10-01 | 2015-04-15 | 达门科技（控股）有限公司 | Rudder for ships |
| CN206243431U (en) * | 2016-12-02 | 2017-06-13 | 长兴大河造船有限公司 | A kind of shipping rudder system structure |
| CN207617947U (en) * | 2017-10-12 | 2018-07-17 | 中国船舶重工集团公司第七一九研究所 | Three rudder formula tail integration structures of micro-unmanned submariner device |
| CN208010626U (en) * | 2018-03-15 | 2018-10-26 | 珠海格力电器股份有限公司 | Fan assembly and air conditioner with it |
| CN109250056A (en) * | 2018-10-11 | 2019-01-22 | 交通运输部天津水运工程科学研究所 | A kind of submarine navigation device tail vane |
| CN209795815U (en) * | 2019-03-29 | 2019-12-17 | 成都云鼎智控科技有限公司 | Steering engine for aircraft |
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2020
- 2020-05-07 CN CN202010377607.7A patent/CN111634410A/en active Pending
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101074050A (en) * | 2007-06-25 | 2007-11-21 | 哈尔滨工程大学 | Modular steering engine of ship underwater |
| CN201099351Y (en) * | 2007-06-25 | 2008-08-13 | 哈尔滨工程大学 | Underwater navigation body modularized steering engine |
| KR20090015248A (en) * | 2007-08-08 | 2009-02-12 | 한국해양연구원 | Small autonomous underwater vehicle test-bed |
| KR101504949B1 (en) * | 2011-08-17 | 2015-03-23 | 티센크루프 마린 시스템즈 게엠베하 | A rudder device for a water vehicle |
| CN104512542A (en) * | 2013-10-01 | 2015-04-15 | 达门科技（控股）有限公司 | Rudder for ships |
| CN206243431U (en) * | 2016-12-02 | 2017-06-13 | 长兴大河造船有限公司 | A kind of shipping rudder system structure |
| CN207617947U (en) * | 2017-10-12 | 2018-07-17 | 中国船舶重工集团公司第七一九研究所 | Three rudder formula tail integration structures of micro-unmanned submariner device |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113492967A (en) * | 2021-07-23 | 2021-10-12 | 航天时代飞鹏有限公司 | Device and method for quickly disassembling steering engine of freight unmanned aerial vehicle |
| CN113492967B (en) * | 2021-07-23 | 2023-02-17 | 航天时代飞鹏有限公司 | Freight unmanned aerial vehicle steering engine quick-release device and method |
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Application publication date: 20200908 |
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