CN111927795A - Two-stage axial flow low-noise fan - Google Patents

Two-stage axial flow low-noise fan Download PDF

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Publication number
CN111927795A
CN111927795A CN202010842994.7A CN202010842994A CN111927795A CN 111927795 A CN111927795 A CN 111927795A CN 202010842994 A CN202010842994 A CN 202010842994A CN 111927795 A CN111927795 A CN 111927795A
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CN
China
Prior art keywords
blade
guide vane
stage
impeller
blades
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Pending
Application number
CN202010842994.7A
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Chinese (zh)
Inventor
李诗徉
叶豪杰
蒋洪涛
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Hangzhou Zhixin Electromechanical Design Co.,Ltd.
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Shaoxing Zhixin Electromechanical Technology Co ltd
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Priority to CN202010842994.7A priority Critical patent/CN111927795A/en
Publication of CN111927795A publication Critical patent/CN111927795A/en
Pending legal-status Critical Current

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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D19/00Axial-flow pumps
    • F04D19/002Axial flow fans
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D19/00Axial-flow pumps
    • F04D19/007Axial-flow pumps multistage fans
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D25/00Pumping installations or systems
    • F04D25/02Units comprising pumps and their driving means
    • F04D25/08Units comprising pumps and their driving means the working fluid being air, e.g. for ventilation
    • F04D25/082Units comprising pumps and their driving means the working fluid being air, e.g. for ventilation the unit having provision for cooling the motor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/28Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
    • F04D29/281Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for fans or blowers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/32Rotors specially for elastic fluids for axial flow pumps
    • F04D29/325Rotors specially for elastic fluids for axial flow pumps for axial flow fans
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • F04D29/52Casings; Connections of working fluid for axial pumps
    • F04D29/522Casings; Connections of working fluid for axial pumps especially adapted for elastic fluid pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • F04D29/52Casings; Connections of working fluid for axial pumps
    • F04D29/54Fluid-guiding means, e.g. diffusers
    • F04D29/541Specially adapted for elastic fluid pumps
    • F04D29/542Bladed diffusers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/58Cooling; Heating; Diminishing heat transfer
    • F04D29/5806Cooling the drive system
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/58Cooling; Heating; Diminishing heat transfer
    • F04D29/582Cooling; Heating; Diminishing heat transfer specially adapted for elastic fluid pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/66Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/661Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
    • F04D29/663Sound attenuation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/66Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/661Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
    • F04D29/666Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps by means of rotor construction or layout, e.g. unequal distribution of blades or vanes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/66Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/661Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
    • F04D29/667Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps by influencing the flow pattern, e.g. suppression of turbulence

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

The invention provides a two-stage axial flow low-noise fan, and belongs to the field of low-noise pneumatic design. The low-noise fan comprises a shell, wherein the shell is provided with an air inlet and an air outlet, a rotating structure is arranged in the shell, the rotating structure comprises a mixed-flow type first-stage impeller and an axial-flow type second-stage impeller, a first-stage guide vane used for guiding airflow is arranged between the first-stage impeller and the second-stage impeller, a second-stage guide vane used for guiding airflow is arranged between the second-stage impeller and the air outlet, and a driving device used for driving the rotating structure to rotate is arranged in the first-stage guide vane. The invention has the advantages of low noise and the like.

Description

Two-stage axial flow low-noise fan
Technical Field
The invention belongs to the field of low-noise pneumatic design, and particularly relates to a two-stage axial flow low-noise fan.
Background
The application scenes of the fans on ships are very wide, and fans which need to axially enter and radially flow out are arranged; axial entry, axial exit fans are also required. The existing fan on the ship mostly adopts a single-stage booster fan, the fan can generate great noise when in operation, and the noise and vibration level of the fan are directly related to the concealment of the ship when in navigation. In order to reduce noise, various methods are devised, for example, a low-frequency vibration isolation device, a double-layer vibration isolation device, and the like are adopted, and noise can be reduced by starting with the design of the fan itself. However, compared with the improvement of performance and efficiency, the difficulty of reducing the fan noise is much greater, and even in some fan optimization cases, the aerodynamic efficiency is obviously improved, but the noise level is not changed. When the fan is designed, the full pressure and the flow of the fan are unchanged, so that the noise of the fan is reduced in a crucial way under the condition that the full pressure and the flow of the fan are unchanged.
Disclosure of Invention
The invention aims to solve the problems in the prior art and provides a two-stage axial flow low-noise fan.
The purpose of the invention can be realized by the following technical scheme: the utility model provides a two-stage axial compressor low noise fan, a serial communication port, which comprises an outer shell, the shell be provided with air intake and air outlet, the shell in be provided with rotating-structure, rotating-structure include mixed flow one-level impeller and axial-flow type second grade impeller, one-level impeller and second grade impeller between be provided with the one-level stator that is used for leading the air current, second grade impeller and air outlet between be provided with the second grade stator that is used for leading the air current, the one-level stator in be provided with and be used for driving the rotatory drive arrangement of rotating-structure.
The working principle of the invention is as follows: when the invention works, wind enters from the air inlet, sequentially passes through the primary impeller, the primary guide vane, the secondary impeller and the secondary guide vane, and finally flows out from the air outlet. The invention adopts the structural forms of a primary mixed-flow impeller and a secondary axial-flow impeller, namely, the primary impeller is the mixed-flow impeller, the secondary impeller is the axial-flow impeller, a primary guide vane is adopted between the two stages of impellers for guiding, airflow flowing out from the axial-flow impeller is guided by the secondary guide vane and finally flows out from an air outlet, the driving device is arranged in the primary guide vane, the mechanical noise of the shielding driving device can be effectively reduced, the absolute air speed in the fan can also be effectively reduced, the pneumatic noise is greatly reduced, meanwhile, the structural form can also realize the requirements of axial air inlet and axial air outlet, and the whole structure of the fan is compact.
Preferably, the primary impeller comprises a first wheel disc and first blades uniformly arranged along the circumferential direction of the first wheel disc, the driving device is partially positioned in the first wheel disc, and the driving device is rotatably connected with the first wheel disc through a first rotating shaft.
Preferably, the ratio of the suction diameter of the first vane to the outer diameter of the first vane is between 0.1 and 0.9, the working face exit angle of the first vane is between 10 ° and 90 °, the back face exit angle of the first vane is between 10 ° and 90 °, and the wrap angle of the first vane is between 0 ° and 150 °.
Preferably, the secondary impeller comprises a second wheel disc and second blades uniformly arranged along the circumferential direction of the second wheel disc, and the driving device is rotatably connected with the second wheel disc through a second rotating shaft.
Preferably, the ratio of the suction diameter of the second blade to the outer diameter of the second blade is 1, the working face outlet angle of the second blade is between 10 ° and 90 °, the back face outlet angle of the second blade is between 10 ° and 90 °, and the wrap angle of the second blade is between 0 ° and 150 °.
Preferably, one-level stator include first stator dish and the first stator blade that evenly sets up along the circumferencial direction of first stator dish, drive arrangement be provided with the installed part, the inside of first stator dish be provided with the fixed part, the installed part pass through first connecting piece and fixed part and connect, the installed part evenly be provided with the air current hole along the circumferencial direction, first stator dish and first rim plate and second rim plate between all there is the clearance. In the operation process of the fan, the front end surface and the rear end surface of the first-stage guide vane generate pressure difference, so that air around the driving device flows, and the driving device is taken away to generate heat, thereby achieving the purpose of cooling.
Preferably, the ratio of the suction diameter of the first guide vane blade to the outer diameter of the first guide vane blade is between 1 and 1.5, the working face outlet angle of the first guide vane blade is between 100 and 170 degrees, the back face outlet angle of the first guide vane blade is between 60 and 130 degrees, and the wrap angle of the first guide vane blade is between 0 and 150 degrees. The first-stage guide vane is in a space guide vane form and converts the speed circulation of wind into the pressure potential energy of the wind.
Preferably, the second-stage guide vane comprises a second guide vane disc and second guide vane blades uniformly arranged along the circumferential direction of the second guide vane disc, a gap exists between the second guide vane disc and the second wheel disc, the ratio of the suction diameter of the second guide vane blade to the outer diameter of the second guide vane blade is 1-3, the working face outlet angle of the second guide vane blade is 100-180 degrees, the back face outlet angle of the second guide vane blade is 60-130 degrees, and the wrap angle of the second guide vane blade is 0-150 degrees. The second-stage guide vanes are in a space guide vane form and convert the speed circulation of the wind into the pressure potential energy of the wind.
Preferably, each of the first and second blades is an integer greater than 1; the number of the first guide vane blades and the number of the first blades or the second blades are relatively prime, and the number of the second guide vane blades and the number of the first blades or the second blades are relatively prime.
Preferably, one-level stator still include with first stator blade one side fixed connection's first casing, second grade stator still include with second stator blade one side fixed connection's second casing, the shell including locate the outer first shell of one-level impeller and locate the outer second shell of second grade impeller, first shell, first casing, second shell, second casing loop through the second connecting piece can dismantle the connection. The first guide vane blade and the second guide vane blade not only play a role in guiding airflow, but also play a role in reinforcing ribs.
Preferably, the first casing is provided with a base corresponding to the position of the first-stage guide vane. The purpose of setting up the frame is in order to reduce vibration, noise reduction.
Compared with the prior art, the invention has the following advantages:
1. the invention adopts the structural forms of a primary mixed-flow impeller and a secondary axial-flow impeller, namely, the primary impeller is the mixed-flow impeller, the secondary impeller is the axial-flow impeller, a primary guide vane is adopted between the two stages of impellers for guiding, airflow flowing out from the axial-flow impeller is guided by the secondary guide vane and finally flows out from an air outlet, the driving device is arranged in the primary guide vane, the mechanical noise of the shielding driving device can be effectively reduced, the absolute air speed in the fan can also be effectively reduced, the pneumatic noise is greatly reduced, meanwhile, the structural form can also realize the requirements of axial air inlet and axial air outlet, and the whole structure of the fan is compact.
Drawings
FIG. 1 is a schematic cross-sectional view of the present invention;
FIG. 2 is a schematic structural view of the first and second stage vanes of the present invention;
fig. 3 is a schematic view of the structure of the airflow holes of the present invention.
In the figure, 1, a housing; 101. a first housing; 111. an air inlet; 102. a second housing; 112. an air outlet; 2. a rotating structure; 201. a first-stage impeller; 211. a first wheel disc; 221. a first blade; 202. a secondary impeller; 212. a second wheel disc; 222. a second blade; 3. a first stage guide vane; 301. a first vane disk; 311. a fixed part; 302. a first guide vane blade; 303. a first housing; 4. a drive device; 401. a first rotating shaft; 402. a second rotating shaft; 403. a mounting member; 413. an airflow aperture; 5. a gap; 6. a first connecting member; 7. a second connecting member; 8. a machine base; 9. two-stage guide vanes; 901. a second vane disk; 902. a second guide vane blade; 903. a second housing; 10. a void; 11. a third housing; 12. and a fourth housing.
Detailed Description
The following is a detailed embodiment of the present invention and the accompanying drawings are incorporated to illustrate the technical solution of the present invention
Further, the present invention is not limited to these examples.
As shown in fig. 1 to 3, a two-stage axial flow low noise fan includes a housing 1, the housing 1 includes a second housing 102 and a first housing 101, the housing 1 is provided with an air outlet 112 and an air inlet 111, and the air inlet 111 is located on the first housing 101.
A rotating structure 2 is arranged in the housing 1, and the rotating structure 2 comprises a first-stage impeller 201 and a second-stage impeller 202. A first-stage guide vane 3 is arranged between the first-stage impeller 201 and the second-stage impeller 202, a driving device 4 is arranged inside the first-stage guide vane 3, and the driving device 4 can drive the rotating structure 2 to rotate. A second-stage guide vane 9 is arranged between the second-stage impeller 202 and the air outlet 112. The first-stage guide vane 3 is also provided with a base 8. Wind enters from the air inlet 111, sequentially passes through the first-stage impeller 201, the first-stage guide vanes 3, the second-stage impeller 202 and the second-stage guide vanes 9, and then flows out from the air outlet 112. Air enters axially from the primary impeller 201 and exits axially from the secondary impeller 202.
In further detail, the first-stage impeller 201 is a mixed-flow impeller, the first-stage impeller 201 includes a first disk 211 and a first blade 221, the first blade 221 is fixedly connected with the first disk 211, and the first blade 221 is uniformly arranged along the circumferential direction of the first disk 211. One side of the first blade 221 is fixedly connected with the first wheel disc 211, the other side is fixedly connected with the third shell 11, and the rotation of the first-stage impeller 201 and the first shell 101 do not interfere with each other. The airflow mainly flows from the air inlet 111 into between the third casing 11 and the first disk 211, and then flows to the first stage guide vane 3. The primary impeller 201 performs primary pressurization of the air and causes the air to enter the primary guide vanes 3.
In further detail, the secondary impeller 202 is an axial-flow impeller, the secondary impeller 202 includes a second disk 212 and a second blade 222, the second blade 222 is fixedly connected to the second disk 212, and the second blade 222 is uniformly arranged along the circumferential direction of the second disk 212. One side of the second blade 222 is fixedly connected with the second wheel disc 212, and the other side is fixedly connected with the fourth shell 12, so that the rotation of the secondary impeller 202 and the second shell 102 do not interfere with each other. The air flow mainly flows between the fourth casing 12 and the second disk 212 and then flows to the secondary guide vanes 9, and the secondary impeller 202 performs secondary pressurization on the air and enables the wind energy to axially flow out.
The first-stage impeller 201 and the second-stage impeller 202 both adopt a closed impeller mode, and are high in structural strength, convenient to process and not easy to deform.
In further detail, one-level guide vane 3 includes first guide vane disc 301 and first guide vane blade 302, first guide vane blade 302 one side and first guide vane disc 301 fixed connection, first guide vane blade 302 opposite side fixedly connected with first casing 303, first guide vane blade 302 is located between inboard first guide vane disc 301 and the first casing 303 in the outside promptly, one-level guide vane 3 adopts closed blade mode equally, first guide vane blade 302 has not only played the effect of air current direction, the effect of strengthening rib has been played simultaneously for one-level guide vane 3's structural strength is high.
In further detail, the second-stage guide vane 9 includes a second guide vane disc 901 and a second guide vane blade 902, two sides of the second guide vane blade 902 are fixedly connected to the second guide vane disc 901, the other two sides of the second guide vane blade 902 are fixedly connected to a second casing 903, that is, the second guide vane blade 902 is located between the inner second guide vane disc 901 and the outer second casing 903, the second-stage guide vane 9 also adopts a closed vane mode, the second guide vane blade 902 not only plays a role in guiding airflow, but also plays a role in reinforcing ribs, so that the structural strength of the second-stage guide vane 9 is high. The air outlet 112 is located on the second casing 903.
In more detail, the driving device 4 is a double-output shaft motor, and the driving device 4 is connected with the first wheel disc 211 through a first rotating shaft 401 to drive the first-stage impeller 201 to rotate; the driving device 4 is connected to the second disk 212 via a second rotating shaft 402, and drives the secondary impeller 202 to rotate. The driving device 4 is located inside the first wheel disc 211, the first guide vane disc 301 and the second wheel disc 212, and can effectively reduce the mechanical noise of the motor, and the first wheel disc 211 and the first guide vane disc 301 play a role in shielding the mechanical noise of the motor. The driving device 4 is provided with a mounting part 403, in this embodiment, the mounting part 403 is a flange, a fixing part 311 is arranged inside the first vane wheel 301, the flange is connected with the fixing part 311 through a first connecting part 6, in this embodiment, the first connecting part 6 is a bolt, a plurality of airflow holes 413 are arranged along the circumferential direction of the flange, and a gap 5 exists between the first vane wheel 301 and the first wheel disc 211 and the second wheel disc 212. In the operation process of the fan, the front end surface and the rear end surface of the first-stage guide vane 3 generate pressure difference, wind mainly enters from the air inlet 111, sequentially passes through the first-stage impeller 201, the first-stage guide vane 3, the second-stage impeller 202 and the second-stage guide vane 9, and then flows out from the air outlet 112. However, due to the pressure difference between the front end face and the rear end face of the first-stage guide vane 3, a small part of wind enters the first guide vane disc 301 from the gap 5 between the first guide vane disc 301 and the second wheel disc 212, then flows out of the first guide vane disc 301 from the gap 5 between the first guide vane disc 301 and the first wheel disc 211 through the airflow hole 413, so that the surface of the driving device 4 forms a micro-circulation, as shown by the arrow direction in fig. 2, the heat on the surface of the driving device 4 is taken away, and the purpose of cooling is achieved. The motor of the invention does not need to be provided with a fan, the running of the fan can generate noise, and the motor of the invention cancels the arrangement of the fan, thereby reducing the noise.
In more detail, a base 8 corresponding to the position of the first stage guide vane 3 is arranged outside the first casing 303. The base 8 is fixed outside the first housing 303, and the base 8 is fixed on the ground through bolts, so that vibration and noise are reduced. Because the motor can vibrate during operation, the motor and the first guide vane disc 301 are firmly fixed through the flange and the fixing part 311, and then the fan is fixed on the ground through the base 8, so that the overall vibration of the fan is reduced, and the noise is reduced.
In more detail, the first casing 101, the first housing 303, the second casing 102, and the second housing 903 are detachably connected in sequence by the second connecting member 7. In this embodiment, the second connecting member 7 is a bolt. The first casing 101, the first housing 303, the second casing 102, and the second housing 903 of the present invention are detachable from each other. The first-stage impeller 201, the first-stage guide vanes 3, the second-stage impeller 202, the second-stage guide vanes 9, the first casing 101 and the second casing 102, and the driving device 4 can be mutually detached and can enter a hatch door with the diameter of 600 mm. The whole focus of fan is in the motor position, and the center pin of shell 1, the center pin of revolution mechanic 2, the center pin of one-level stator 3, second grade stator 8, the center pin of motor all coincides. A convenient hoisting hanger can be designed on the gravity center vertical line. Iron cores are pre-embedded at the assembly positions of the first-stage impeller 201 and the second-stage impeller 202 and the motor.
When the fan is designed, the total full pressure and the total flow of the fan are not changed, and under the condition that the full pressure and the total flow of the fan are not changed, the two-stage booster fan has lower noise than the existing single-stage booster fan. Because all the flow rates are the same, for example, Q, the total pressure of the fan is Pt. The invention adopts two stages of impellers, the flow of each stage of impeller is still Q, but the full pressure shared by each stage of impeller is smaller than the total full pressure, so that the peripheral speed of each stage of impeller is reduced, and the diameter of each stage of impeller is also reduced. Therefore, the fan adopting the two-stage impeller can effectively reduce the absolute speed inside the fan, thereby reducing the noise of the fan. And the diameter of the impeller blades of each stage is reduced. Therefore, the invention adopts the structural form of the primary mixed-flow impeller and the secondary axial-flow impeller, can effectively reduce the absolute wind speed in the fan, thereby greatly reducing the aerodynamic noise, and the structural form can also realize the requirements of axial air inlet and axial air outlet.
Under the condition of ensuring the pneumatic efficiency, in order to greatly reduce the pneumatic noise, the parameters of the fan provided by the invention need to meet the following conditions:
the full pressure ratio of the first-stage impeller 201 to the second-stage impeller 202 is 1:1-1.5:1, the first-stage impeller 201 is a mixed-flow impeller, the first-stage guide vanes 3 are in the form of space guide vanes, the second-stage impeller 202 is an axial-flow impeller, and the second-stage guide vanes 9 are in the form of space guide vanes. The number of the first-stage impeller 201 and the second-stage impeller 202 is an integer greater than 1, that is, the number of the first blades 221 and the second blades 222 is an integer greater than 1, and the number of the first-stage guide vanes 3 and the second-stage guide vanes 9 is relatively prime to the number of the impeller blades, that is, the number of the first guide vanes 302 and the number of the second guide vanes 902 are both relatively prime to the number of the first blades 221 or the second blades 222.
The distance from the front edge of the flow surface in the middle of the blade to the center of the impeller is called as the suction diameter of the blade D1, the distance from the tail edge of the flow surface in the middle of the blade to the center of the impeller is called as the outer diameter D2 of the long blade, the blade setting angle of the working surface of the blade is the included angle between the tangent of the convex surface of the blade and the circumferential direction, the blade setting angle of the back surface of the blade is the included angle between the tangent of the concave surface of the blade and the circumferential direction, the blade setting angle at the inner diameter of the blade is the inlet angle of the blade. The working surface outlet angle of the blade is beta 1, the back surface outlet angle is beta 2, and the wrap angle of the blade is theta;
first blade 221 parameters of the mixed-flow primary impeller 201: d1 is more than or equal to 0.1, D2 is more than or equal to 0.9, beta 1 is more than or equal to 10 degrees and less than or equal to 90 degrees, beta 2 is more than or equal to 10 degrees and less than or equal to 90 degrees, and theta is more than or equal to 0 degrees and less than or equal to 150 degrees.
First vane blade 302 parameters of stage one vane 3: d1 is more than or equal to 1, D2 is more than or equal to 1.5, beta 1 is more than or equal to 100 degrees and less than or equal to 170 degrees, beta 2 is more than or equal to 60 degrees and less than or equal to 130 degrees, and theta is more than or equal to 0 degrees and less than or equal to 150 degrees.
Second blade 222 parameters of the axial flow two-stage impeller 202: d1, D2=1, beta 1 is more than or equal to 10 degrees and less than or equal to 90 degrees, beta 2 is more than or equal to 10 degrees and less than or equal to 90 degrees, and theta is more than or equal to 0 degrees and less than or equal to 150 degrees.
Second guide vane blade 902 parameters of the second stage guide vane 9: d1 is more than or equal to 1, D2 is more than or equal to 3, beta 1 is more than or equal to 100 degrees and less than or equal to 180 degrees, beta 2 is more than or equal to 60 degrees and less than or equal to 130 degrees, and theta is more than or equal to 0 degrees and less than or equal to 150 degrees.
Example 1
The full pressure ratio shared by the first-stage impeller 201 and the second-stage impeller 202 is 1.2: 1.
first blade 221 parameters of the mixed-flow primary impeller 201: the number is 7, D1=310mm, D2=510mm, β 1=25 °, β 2=35 °, θ =80 °.
First vane blade 302 parameters of stage one vane 3: the number was 17, D1=500mm, D2=500mm, β 1=130 °, β 2=100 °, θ =25 °.
Second blade 222 parameters of the axial flow two-stage impeller 202: the number is 7, D1=500mm, D2=500mm, β 1=40 °, β 2=30 °, θ =50 °.
Second guide vane blade 902 parameters of the second stage guide vane 9: 17 tablets in number, D1=500mm, D2=380mm, β 1=120 °, β 2=100 °, θ =40 °;
the decibel noise of example 2 was measured to be 60 decibels.
The specific embodiments described herein are merely illustrative of the spirit of the invention. Various modifications or additions may be made to the described embodiments or alternatives may be employed by those skilled in the art without departing from the spirit or ambit of the invention as defined in the appended claims.
Although terms are used more often herein, the possibility of using other terms is not excluded. These terms are used merely to more conveniently describe and explain the nature of the present invention; they are to be construed as being without limitation to any additional limitations that may be imposed by the spirit of the present invention.

Claims (10)

1. The utility model provides a two-stage axial flow low noise fan, a serial communication port, including shell (1), shell (1) be provided with air intake (111) and air outlet (112), shell (1) in be provided with rotating-structure (2), rotating-structure (2) including mixed flow type one-level impeller (201) and axial-flow type second grade impeller (202), one-level impeller (201) and second grade impeller (202) between be provided with one-level stator (3) that are used for leading the air current, second grade impeller (202) and air outlet (112) between be provided with second grade stator (9) that are used for leading the air current, one-level stator (3) in be provided with and be used for driving rotating-structure (2) rotatory drive arrangement (4).
2. A two-stage axial flow low noise blower according to claim 1 wherein said one-stage impeller (201) comprises a first disk (211) and first blades (221) uniformly arranged along the circumferential direction of the first disk (211), said driving means (4) is partially located in the first disk (211), and said driving means (4) and the first disk (211) are rotatably connected by a first rotating shaft (401).
3. A two-stage axial flow low noise fan according to claim 2, wherein the ratio of the suction diameter of said first blade (221) to the outer diameter of the first blade (221) is between 0.1-0.9, the working face exit angle of said first blade (221) is between 10 ° -90 °, the back face exit angle of said first blade (221) is between 10 ° -90 °, and the wrap angle of said first blade (221) is between 0 ° -150 °.
4. A two-stage axial flow low noise blower according to claim 2 wherein said secondary impeller (202) comprises a second disk (212) and second blades (222) uniformly arranged along the circumferential direction of said second disk (212), said driving means (4) and said second disk (212) being rotatably connected by a second rotating shaft (402).
5. A two-stage axial flow low noise fan according to claim 4, wherein the ratio of the suction diameter of the second blade (222) to the outer diameter of the second blade (222) is 1, the working face exit angle of the second blade (222) is between 10 ° and 90 °, the back face exit angle of the second blade (222) is between 10 ° and 90 °, and the wrap angle of the second blade (222) is between 0 ° and 150 °.
6. A two-stage axial flow low noise fan according to claim 4, wherein the one-stage guide vane (3) comprises a first guide vane disc (301) and first guide vane blades (302) uniformly arranged along the circumferential direction of the first guide vane disc (301), the driving device (4) is provided with a mounting member (403), a fixing portion (311) is arranged inside the first guide vane disc (301), the mounting member (403) is connected with the fixing portion (311) through a first connecting member (6), the mounting member (403) is uniformly provided with air flow holes (413) along the circumferential direction, and a gap (5) is formed between the first guide vane disc (301) and the first and second wheel discs (211, 212).
7. A two-stage axial flow low noise fan according to claim 6, wherein the ratio of the suction diameter of the first vane blade (302) to the outer diameter of the first vane blade (302) is between 1-1.5, the working face exit angle of the first vane blade (302) is between 100 ° -170 °, the back face exit angle of the first vane blade (302) is between 60 ° -130 °, and the wrap angle of the first vane blade (302) is between 0 ° -150 °.
8. A two-stage axial flow low noise fan according to claim 6, characterized in that said two-stage guide vanes (9) comprise a second guide vane disc (901) and second guide vane blades (902) uniformly arranged along the circumferential direction of the second guide vane disc (901), a gap (10) exists between the second guide vane disc (901) and the second wheel disc (212), the ratio of the suction diameter of the second guide vane blade (902) to the outer diameter of the second guide vane blade (902) is between 1 and 3, the working face exit angle of the second guide vane blade (902) is between 100 ° and 180 °, the back face exit angle of the second guide vane blade (902) is between 60 ° and 130 °, and the wrap angle of the second guide vane blade (902) is between 0 ° and 150 °.
9. A two-stage axial flow low noise fan according to claim 8, wherein said first blade (221) and said second blade (222) are both integers greater than 1; the number of the first guide vane blades (302) is coprime to the number of the first blades (221) or the second blades (222), and the number of the second guide vane blades (902) is coprime to the number of the first blades (221) or the second blades (222).
10. The two-stage axial flow low-noise fan according to claim 8, wherein the one-stage guide vane (3) further comprises a first casing (303) fixedly connected with one side of the first guide vane blade (302), the two-stage guide vane (9) further comprises a second casing (903) fixedly connected with one side of the second guide vane blade (902), the casing (1) comprises a first casing (101) arranged outside the one-stage impeller (201) and a second casing (102) arranged outside the two-stage impeller (202), and the first casing (101), the first casing (303), the second casing (102) and the second casing (903) are detachably connected through the second connecting member (7) in sequence.
CN202010842994.7A 2020-08-20 2020-08-20 Two-stage axial flow low-noise fan Pending CN111927795A (en)

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114680706A (en) * 2020-12-25 2022-07-01 广东美的白色家电技术创新中心有限公司 Fan assembly and dust collector
CN115492794A (en) * 2022-09-09 2022-12-20 续新技术(深圳)集团有限公司 Motor and fan
CN116624430A (en) * 2023-05-19 2023-08-22 东莞市旭恒电子有限公司 A Diagonal Flow Duct Fan
CN117905712A (en) * 2024-03-20 2024-04-19 绍兴智新机电科技有限公司 Two-stage variable-speed low-noise axial flow fan
CN119755110A (en) * 2025-03-05 2025-04-04 绍兴智新机电科技有限公司 Low-noise multistage axial flow fan

Citations (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4511308A (en) * 1980-12-03 1985-04-16 James Howden Australia Pty. Limited Axial and mixed flow fans and blowers
CN201013672Y (en) * 2007-04-04 2008-01-30 陈泽民 Refrigerating mechanism used for double stage axial-flow draught fan
CN201050495Y (en) * 2007-04-04 2008-04-23 陈泽民 Two-stage axial-flow draught fan
CN101975177A (en) * 2010-11-18 2011-02-16 王涤生 Built-in turbo shaft flow motor type strong fan
CN103161608A (en) * 2013-02-07 2013-06-19 南京凌日星能源科技有限公司 Single rotor minitype turbofan engine adopting axial flow oblique flow serial composite compressing system
CN105317716A (en) * 2015-12-08 2016-02-10 中车大连机车研究所有限公司 Compound cooling ventilator with interior self-adaption cooling circulation
CN205101247U (en) * 2015-10-30 2016-03-23 中南大学 Oblique flow ventilation blower
CN205101263U (en) * 2015-10-30 2016-03-23 中南大学 Bilobed wheel axial -flow blower
CN105443417A (en) * 2015-12-31 2016-03-30 株洲联诚集团有限责任公司 Compound cooling fan
CN205592162U (en) * 2016-04-21 2016-09-21 株洲联诚集团有限责任公司 Standardized EMUs are axial -flow type cooling ventilation machine for transformer
CN108240344A (en) * 2016-12-23 2018-07-03 华中科技大学 A kind of two-stage diagonal flow fan
CN208348164U (en) * 2018-04-09 2019-01-08 浙江理工大学上虞工业技术研究院有限公司 The second level axial flow blower of efficient anti-surging
CN109236702A (en) * 2018-11-15 2019-01-18 海明(江苏)环境科技有限公司 A kind of enclosed blower peculiar to vessel
CN210509738U (en) * 2019-08-02 2020-05-12 珠海格力电器股份有限公司 Air duct assembly and air conditioner with same

Patent Citations (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4511308A (en) * 1980-12-03 1985-04-16 James Howden Australia Pty. Limited Axial and mixed flow fans and blowers
CN201013672Y (en) * 2007-04-04 2008-01-30 陈泽民 Refrigerating mechanism used for double stage axial-flow draught fan
CN201050495Y (en) * 2007-04-04 2008-04-23 陈泽民 Two-stage axial-flow draught fan
CN101975177A (en) * 2010-11-18 2011-02-16 王涤生 Built-in turbo shaft flow motor type strong fan
CN103161608A (en) * 2013-02-07 2013-06-19 南京凌日星能源科技有限公司 Single rotor minitype turbofan engine adopting axial flow oblique flow serial composite compressing system
CN205101247U (en) * 2015-10-30 2016-03-23 中南大学 Oblique flow ventilation blower
CN205101263U (en) * 2015-10-30 2016-03-23 中南大学 Bilobed wheel axial -flow blower
CN105317716A (en) * 2015-12-08 2016-02-10 中车大连机车研究所有限公司 Compound cooling ventilator with interior self-adaption cooling circulation
CN105443417A (en) * 2015-12-31 2016-03-30 株洲联诚集团有限责任公司 Compound cooling fan
CN205592162U (en) * 2016-04-21 2016-09-21 株洲联诚集团有限责任公司 Standardized EMUs are axial -flow type cooling ventilation machine for transformer
CN108240344A (en) * 2016-12-23 2018-07-03 华中科技大学 A kind of two-stage diagonal flow fan
CN208348164U (en) * 2018-04-09 2019-01-08 浙江理工大学上虞工业技术研究院有限公司 The second level axial flow blower of efficient anti-surging
CN109236702A (en) * 2018-11-15 2019-01-18 海明(江苏)环境科技有限公司 A kind of enclosed blower peculiar to vessel
CN210509738U (en) * 2019-08-02 2020-05-12 珠海格力电器股份有限公司 Air duct assembly and air conditioner with same

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114680706A (en) * 2020-12-25 2022-07-01 广东美的白色家电技术创新中心有限公司 Fan assembly and dust collector
CN115492794A (en) * 2022-09-09 2022-12-20 续新技术(深圳)集团有限公司 Motor and fan
CN116624430A (en) * 2023-05-19 2023-08-22 东莞市旭恒电子有限公司 A Diagonal Flow Duct Fan
CN117905712A (en) * 2024-03-20 2024-04-19 绍兴智新机电科技有限公司 Two-stage variable-speed low-noise axial flow fan
CN117905712B (en) * 2024-03-20 2024-06-04 绍兴智新机电科技有限公司 Two-stage variable-speed low-noise axial flow fan
CN119755110A (en) * 2025-03-05 2025-04-04 绍兴智新机电科技有限公司 Low-noise multistage axial flow fan

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Application publication date: 20201113