CN113525649A - A2B2C type shaftless pump jet propeller fluid module ducted structure technology - Google Patents

A2B2C type shaftless pump jet propeller fluid module ducted structure technology Download PDF

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Publication number
CN113525649A
CN113525649A CN202010233308.6A CN202010233308A CN113525649A CN 113525649 A CN113525649 A CN 113525649A CN 202010233308 A CN202010233308 A CN 202010233308A CN 113525649 A CN113525649 A CN 113525649A
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CN
China
Prior art keywords
stage
guide ring
ring
a2b2c
culvert
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Pending
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CN202010233308.6A
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Chinese (zh)
Inventor
李军
其他发明人请求不公开姓名
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Suzhou Zhenhu Fluid Technology Co ltd
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Suzhou Zhenhu Fluid Technology Co ltd
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Priority to CN202010233308.6A priority Critical patent/CN113525649A/en
Publication of CN113525649A publication Critical patent/CN113525649A/en
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H11/00Marine propulsion by water jets
    • B63H11/02Marine propulsion by water jets the propulsive medium being ambient water
    • B63H11/04Marine propulsion by water jets the propulsive medium being ambient water by means of pumps
    • B63H11/08Marine propulsion by water jets the propulsive medium being ambient water by means of pumps of rotary type
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H11/00Marine propulsion by water jets
    • B63H11/02Marine propulsion by water jets the propulsive medium being ambient water

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Ocean & Marine Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

The invention discloses a fluid module culvert structure technology of an A2B2C type shaftless pump jet propeller, relating to the field of fluid power, in particular to a fluid module culvert structure technology of an A2B2C type shaftless pump jet propeller, which at least comprises a spiral ring, a flow guide ring, a core rod, a rotor culvert inner wall, an input fixing piece and an output fixing piece, wherein a plurality of spiral rings and a plurality of flow guide rings are connected in series, so that the continuous pressurization and pressurization of fluid in the module culvert can be achieved, the low-water-resistance technical design, the product manufacturability engineering design and the product mechanics rationalization structural requirement can be met, and the basic requirement of the reliable work of the underwater propulsion high-speed navigation working condition can be met.

Description

A2B2C type shaftless pump jet propeller fluid module ducted structure technology
Technical Field
The invention relates to the field of fluid power, in particular to a ducted structure technology of an A2B2C type shaftless pump jet propeller fluid module, which can ensure that the fluid propulsion pressure is continuously increased under the condition of high rotor speed, can also meet the requirements of low water resistance technical design, product manufacturability engineering design and product mechanical structure rationalization, and can further meet the basic requirement of the reliable work of the underwater propeller under the high-speed sailing working condition.
Background
Fluid propulsion technical products are more, mainly including centrifugal pumps, reciprocating pumps, screw pumps, gear pumps, axial-flow pumps, propellers and the like, the existing underwater propulsion system mainly comprises the axial-flow pumps and the propellers, but the underwater propulsion system is complex in structure and obviously low in efficiency, and the fundamental reason of the system is negative influence caused by shafting.
Therefore, a technical route of magnetic suspension and spiral ring fluid structures is disclosed in the prior patent CN201210436592.2, and the technical product is approved by the industry through actual test and scene experience, namely the industry is called a linear fluid technology and is commonly called a shaftless pump jet propeller technology, and in the hydrodynamic environments of navigation, spaceflight, industry and agriculture, buildings and civil consumer products, users apply the technology as a key product of future hydrodynamic energy conservation and emission reduction, and the technology is derived from the fact that the fluid propulsion efficiency can be greatly improved, and social resources can be saved by simply realizing the body structure. The realization of the technical function necessarily introduces a plurality of new key technologies.
The comprehensive efficiency of the propeller and the motor of the conventional underwater propeller is about 15-25%, the most important point is that the rotating speed is increased, and the efficiency is reduced more quickly although the navigational speed is also increased. The invention relates to a straight line fluid technology underwater application technology, which is characterized in that the efficiency of a shaftless pump jet propeller product is over 50 percent, the efficiency is not reduced mainly due to the fact that the rotating speed is increased, the navigational speed is increased, and the shaftless pump jet propeller product is simple in process and high in manufacturability.
The shaftless pump-jet propeller is generally divided into three types of ordinary type, rapid type and high-speed propulsion according to the navigational speed capability of underwater propulsion, generally bears lives, comprises that passenger ship propulsion belongs to the ordinary type, the navigational speed is 1-15 knots, the acceleration of the over-rapid navigational speed is not suitable for life bodies, an underwater robot with special purposes needs to quickly react, actively avoid risks and track preys, the navigational speed is 25-35 knots, the faster requirement exceeds 50 knots, and even 150-knot navigational speed propellers in some countries are reported according to information. The requirement of the flow speed of the discharged water of the high-speed shaftless pump jet propeller is very fast, the design of a fluid module of the propeller is obviously different from that of a common propeller, so that the algorithms of the propelled fluid are different, the corresponding structures of the algorithms are also different, and particularly, the bypass structure of the fluid module belongs to a specific technology. Therefore, the inventor group of the patent applicant carries out intensive research on the characteristics to obtain the ducted structure characteristics of the fluid module of the A2B2C type shaftless pump jet propeller, and the results are disclosed and claimed.
The technology of the invention is a key technology introduced by a linear fluid technology in a deep water environment, namely an A2B2C type shaftless pump jet propeller fluid module ducted structure technology, and the traditional underwater propulsion technology does not relate to the technology and has no direct comparison. However, in practice, without this technique, the high-pressure and high-speed propelling function of the shaftless pump jet propeller will be lost.
The technology of the invention is disclosed aiming at the product engineering technology introduced by the linear fluid technology under the high-pressure propelling working condition, and fully discloses the working principle characteristics, the application, the structural characteristics, the actual use method and the key process of the linear fluid technology.
Disclosure of Invention
The invention mainly solves the product engineering key technology of the adaptability of the linear fluid technology under the high pressure working condition, and particularly discloses the key technology of the effective combination of a spiral ring, a flow guide ring, a core rod and an assembly of an A2B2C type shaftless pump jet propeller, and the key technology comprises the product manufacturing characteristics and the basic characteristics obviously possessed by the technology of the invention, and the invention discloses the technical characteristics of a product classification structure suitable for different high pressure working condition ranges.
In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", "axial", "radial", "circumferential", "inner", "outer", etc., indicate orientations or positional relationships based on those shown in the drawings, and are used merely for convenience of description and for simplicity of description, but do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be considered as limiting the present invention. Furthermore, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means two or more unless otherwise specified.
In the description of the present invention, it should be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, e.g., as meaning either a fixed connection, a removable connection, or an integral connection; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.
The method comprises the following specific steps:
the invention relates to a fluid module culvert structure of an A2B2C type shaftless pump jet propeller, which is technically characterized by at least comprising a spiral ring, a flow guide ring, a core rod, a rotor culvert inner wall, an input end fixing piece and an output end fixing piece.
The invention relates to a ducted structure of a fluid module of an A2B2C type shaftless pump jet propeller, which is technically characterized in that at least each spiral ring and each guide ring are axially connected in series and butted, the back of an input end fixing piece corresponds to a first-stage spiral ring first-stage guide ring, the back of the first-stage guide ring is butted with a second-stage spiral ring second-stage guide ring, the back of the second-stage guide ring is butted with a third-stage spiral ring third-stage guide ring, and by analogy, the back of an n-1(n is a natural number) stage guide ring is butted with an n-stage spiral ring and an n-stage guide ring, and the n-stage guide ring corresponds to an output end fixing piece.
The invention relates to a A2B2C type shaftless pump jet propeller fluid module culvert structure, which is characterized in that at least the outer wall of each spiral ring and the inner wall of a rotor culvert keep a synchronous fixed structure, and the inner wall of the rotor culvert and the outer wall of each guide ring relatively keep a freely rotatable structure.
The invention relates to a A2B2C type shaftless pump jet propeller fluid module culvert structure, which is characterized in that at least all guide rings and a core rod have a structure which is synchronously kept immovable, all spiral rings keep a structure which freely rotates relative to the core rod, and the mechanical strength of the core rod cannot bear the torque force transmission of the energy of the whole motive power.
The invention relates to a ducted structure of a fluid module of an A2B2C type shaftless pump jet propeller, which is technically characterized in that the axial width of at least one stage of spiral ring is the largest, the axial width of a second stage of spiral ring is smaller than that of the first stage, and by analogy, the axial width of n stages of spiral rings is the smallest.
The invention relates to a fluid module culvert structure of an A2B2C type shaftless pump jet propeller, which is technically characterized in that at least one stage of guide ring has the largest axial width, the axial width of a second stage of guide ring is smaller than that of the first stage of guide ring, and by analogy, the axial width of n stages of guide rings is the smallest.
Drawings
FIG. 1, A2B2C schematic axial A-A section view of a ducted structure of a shaftless pump jet propeller fluid module
1: first-stage spiral ring
2: two-stage spiral ring
3: three-stage spiral ring
4: four-stage spiral ring
5: five-stage spiral ring
6: six-stage spiral ring
7: output end fixing piece
8: core rod
9: five-stage flow guide ring
10: four-stage flow guide ring
11: three-stage flow guide ring
12: second-level flow guide ring
13: first-level flow guide ring
14: input end fixing piece
15: inner wall of rotor duct
Detailed Description
According to the technical characteristics of the invention, the axial three-dimensional schematic diagram of the A2B2C type shaftless pump jet propeller fluid module duct structure in the attached figure 1 shows that the inner wall of the rotor duct drives all stages of spiral rings to rotate, when fluid medium is pressurized from a first-stage spiral ring (1) entering the duct, the fluid medium enters a first-stage guide ring (13) for pressurization, then is pressurized by a second-stage spiral ring (2), then enters a second-stage guide ring (12) for pressurization, and so on, the fluid medium is pressurized by n stages of guide rings, and is jetted out of the duct after the kinetic energy is pressurized step by step, so that the kinetic energy increasing process of the fluid medium is completed.
According to the technical characteristics of the invention, the axial three-dimensional schematic diagram of the A2B2C type shaftless pump jet propeller fluid module culvert structure in the attached figure 1 shows that when fluid enters the culvert, the core rod is static and motionless relative to the inner wall of the rotor culvert, and the guide ring is static and motionless relative to the inner wall of the rotor culvert due to the synchronous fixing function of the core rod and the guide ring, so that the fluid medium is restrained from rotating radially in the culvert, and the radial energy is converted into axial energy, thereby achieving the effect of forward pressurization of the fluid culvert.
Various applications, modifications, approaches, or similar structures of the devices herein involved, which may occur to those skilled in the art and which are encompassed by the present invention, are deemed to be equivalent to the present invention. Also, other structurally modified push-type products, which may be associated with similar structures and approaches, are also contemplated as being similar to the present invention.

Claims (6)

1. The invention relates to a fluid module culvert structure of an A2B2C type shaftless pump jet propeller, which is technically characterized by at least comprising a spiral ring, a flow guide ring, a core rod, a rotor culvert inner wall, an input end fixing piece and an output end fixing piece.
2. The invention relates to a ducted structure of a fluid module of an A2B2C type shaftless pump jet propeller, which is technically characterized in that at least each spiral ring and each guide ring are axially connected in series and butted, the back of an input end fixing piece corresponds to a first-stage spiral ring first-stage guide ring, the back of the first-stage guide ring is butted with a second-stage spiral ring second-stage guide ring, the back of the second-stage guide ring is butted with a third-stage spiral ring third-stage guide ring, and by analogy, the back of an n-1(n is a natural number) stage guide ring is butted with an n-stage spiral ring and an n-stage guide ring, and the n-stage guide ring corresponds to an output end fixing piece.
3. The invention relates to a A2B2C type shaftless pump jet propeller fluid module culvert structure, which is characterized in that at least the outer wall of each spiral ring and the inner wall of a rotor culvert keep a synchronous fixed structure, and the inner wall of the rotor culvert and the outer wall of each guide ring relatively keep a freely rotatable structure.
4. The invention relates to a A2B2C type shaftless pump jet propeller fluid module culvert structure, which is characterized in that at least all guide rings and a core rod have a structure which is synchronously kept immovable, all spiral rings keep a structure which freely rotates relative to the core rod, and the mechanical strength of the core rod cannot bear the torque force transmission of the energy of the whole motive power.
5. The invention relates to a ducted structure of a fluid module of an A2B2C type shaftless pump jet propeller, which is technically characterized in that the axial width of at least one stage of spiral ring is the largest, the axial width of a second stage of spiral ring is smaller than that of the first stage, and by analogy, the axial width of n stages of spiral rings is the smallest.
6. The invention relates to a fluid module culvert structure of an A2B2C type shaftless pump jet propeller, which is technically characterized in that at least one stage of guide ring has the largest axial width, the axial width of a second stage of guide ring is smaller than that of the first stage of guide ring, and by analogy, the axial width of n stages of guide rings is the smallest.
CN202010233308.6A 2020-03-29 2020-03-29 A2B2C type shaftless pump jet propeller fluid module ducted structure technology Pending CN113525649A (en)

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CN202010233308.6A CN113525649A (en) 2020-03-29 2020-03-29 A2B2C type shaftless pump jet propeller fluid module ducted structure technology

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202010233308.6A CN113525649A (en) 2020-03-29 2020-03-29 A2B2C type shaftless pump jet propeller fluid module ducted structure technology

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CN113525649A true CN113525649A (en) 2021-10-22

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Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20030064638A1 (en) * 2001-09-18 2003-04-03 Tomohiro Fuse Water jet propulsion apparatus
US20050148246A1 (en) * 2003-11-25 2005-07-07 Tomohiro Fuse Mounting structure for jet propulsion pump in personal watercraft
CN102114908A (en) * 2011-01-01 2011-07-06 赵明 Pump-jet water propeller system for five-element combined ship
CN106892077A (en) * 2017-04-12 2017-06-27 邓履明 Propeller and propulsion system
CN107336819A (en) * 2017-07-18 2017-11-10 蔡卫忠 Underwater culvert type propeller propulsion plant and its application method
CN206954479U (en) * 2017-04-12 2018-02-02 山东国润船用推进器有限公司 Propeller and propulsion system
CN107972837A (en) * 2017-12-12 2018-05-01 裴睿涛 Combined type pump-jet propulsor
CN108910028A (en) * 2018-07-26 2018-11-30 周庆文 A kind of second level duct power packages and three-level or multistage duct power packages with it
CN109835453A (en) * 2019-04-12 2019-06-04 辽宁工程技术大学 Multistage coil formula pump-jet propulsor
CN110562421A (en) * 2019-07-15 2019-12-13 和近建 Ducted helical drum propeller and lateral control valve system

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20030064638A1 (en) * 2001-09-18 2003-04-03 Tomohiro Fuse Water jet propulsion apparatus
US20050148246A1 (en) * 2003-11-25 2005-07-07 Tomohiro Fuse Mounting structure for jet propulsion pump in personal watercraft
CN102114908A (en) * 2011-01-01 2011-07-06 赵明 Pump-jet water propeller system for five-element combined ship
CN106892077A (en) * 2017-04-12 2017-06-27 邓履明 Propeller and propulsion system
CN206954479U (en) * 2017-04-12 2018-02-02 山东国润船用推进器有限公司 Propeller and propulsion system
CN107336819A (en) * 2017-07-18 2017-11-10 蔡卫忠 Underwater culvert type propeller propulsion plant and its application method
CN107972837A (en) * 2017-12-12 2018-05-01 裴睿涛 Combined type pump-jet propulsor
CN108910028A (en) * 2018-07-26 2018-11-30 周庆文 A kind of second level duct power packages and three-level or multistage duct power packages with it
CN109835453A (en) * 2019-04-12 2019-06-04 辽宁工程技术大学 Multistage coil formula pump-jet propulsor
CN110562421A (en) * 2019-07-15 2019-12-13 和近建 Ducted helical drum propeller and lateral control valve system

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