GB2165888A - Air swirl systems for fans - Google Patents

Air swirl systems for fans Download PDF

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Publication number
GB2165888A
GB2165888A GB08426635A GB8426635A GB2165888A GB 2165888 A GB2165888 A GB 2165888A GB 08426635 A GB08426635 A GB 08426635A GB 8426635 A GB8426635 A GB 8426635A GB 2165888 A GB2165888 A GB 2165888A
Authority
GB
United Kingdom
Prior art keywords
fan
inlet tube
inlet
impeller
conduit
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
GB08426635A
Other versions
GB2165888B (en
GB8426635D0 (en
Inventor
Vitold Vitoldovich Pak
Viktoria Ionovna Kovalevskaya
Vitaly Alexandrovich Sidorenko
Margarita Mikhail Kovalevskaya
Valery Prokofievich Peredery
Jury Valerievich Vasiliev
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
DO G PK I EXI KOMPLEXNOI MEK Z
Donetsky Politekhnichesky Institut
Original Assignee
DO G PK I EXI KOMPLEXNOI MEK Z
Donetsky Politekhnichesky Institut
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority to SE8405068A priority Critical patent/SE445061B/en
Application filed by DO G PK I EXI KOMPLEXNOI MEK Z, Donetsky Politekhnichesky Institut filed Critical DO G PK I EXI KOMPLEXNOI MEK Z
Priority to GB08426635A priority patent/GB2165888B/en
Priority to FR8416135A priority patent/FR2572140B1/en
Priority to DE3448204A priority patent/DE3448204C2/en
Priority to DE3439218A priority patent/DE3439218A1/en
Publication of GB8426635D0 publication Critical patent/GB8426635D0/en
Publication of GB2165888A publication Critical patent/GB2165888A/en
Application granted granted Critical
Publication of GB2165888B publication Critical patent/GB2165888B/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F04D29/42Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/4206Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
    • F04D29/4213Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps suction ports
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D27/00Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/002Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids by varying geometry within the pumps, e.g. by adjusting 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
    • F04D29/40Casings; Connections of working fluid
    • F04D29/42Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/44Fluid-guiding means, e.g. diffusers
    • F04D29/46Fluid-guiding means, e.g. diffusers adjustable
    • F04D29/462Fluid-guiding means, e.g. diffusers adjustable especially adapted for elastic fluid pumps
    • F04D29/464Fluid-guiding means, e.g. diffusers adjustable especially adapted for elastic fluid pumps adjusting flow cross-section, otherwise than by using adjustable stator blades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/50Inlet or outlet
    • F05D2250/51Inlet
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/14Preswirling

Landscapes

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

Abstract

The fan comprises an impeller 2 and a system for imparting prerotation swirl to the air flow entering the impeller. The swirl system includes a bypass conduit 6 and an adjustable baffle 9. Normally the baffle blocks the inlet 7 of the conduit 6 so that the entire airflow passes through the inlet box 5 and inlet cone 4 to the impeller. When the baffle is swung away from the inlet 7, the air flow is divided into two streams 10, 11, the stream 11 being swirled due to the tangential direction in which the air is supplied from the conduit 6 to the inlet cone 4. <IMAGE>

Description

SPECIFICATION Fan The present invention relates to devices for producing a current of air, and more specifically concerns fans, especially those centrifugal and axialflow fans as employed in power engineering, mining, metallurgical and chemical industries.
A known type of fan comprises a housing with an inlet tube and suction chamber arranged sequentially; an impeller disposed inside the housing; and a by-pass conduit connected to the chamber and having an air-flow regulator.
The by-pass conduit takes air from the outside.
According to a feature of this earlier invention, if the fan operation should become unstable, a choke of the flow regulator is opened, whereby, because of the influx of air from the outside, the flow rate is increased to result in stable operation of the fan and greater volume flow rate.
However, because of this non-productive suction of air the fan power has to increase and this results in a reduced fan efficiency.
Other known types of fans comprise an impeller disposed in a housing, an inlet tube, and guide vanes for prerotation swirling of the air-flow entering the impeller, arranged either in the inlet tube or in an inlet box. However, reliable adjustment of the operating conditions of such fan is difficult since the guide vane means for prerotation swirling of the air flow have an excessive number of parts arranged in the air flow and this air flow not infrequently carries dust and/or corrosive components.
In addition, the guide vanes provide resistance to the flow, which also affects the overall efficiency of the fan.
The present invention sets out to provide a fan having a construction such as to give increased reliability of adjustment to simplify the fan structurally.
The invention consists in a fan comprising an impeller disposed in a housing; an inlet tube for a current of air drawn in by the fan; and a means for imparting a prerotating swirling of the flow of air entering the impeller; the swirling means comprising at least one bypass conduit an inlet of which is located in the inlet tube of the fan, and an outlet of which is attached tangentially to the inlet tube at a relatively downstream portion closer to the impeller, and a baffle being movably disposed inside the inlet tube to separate the incoming flow into a main flow for the inlet tube and an additional flow entering the by-pass conduit.
The or each by-pass conduit may have the general form of a tube placing a relatively upstream part of the inlet tube of the fan in communication with a suction zone of the impeller. Alternatively, the or each conduit may have the general form of hollow lugs arranged on the walls of the inlet tube of the fan and placing in communication at their tangential outlets a relatively downstream portion of the inlet tube with a relatively upstream portion thereof. In the former case the baffle (which preferably has a height less than the height of the inlet tube in which it is disposed) is usually movable from a position covering the upstream end of the bypass conduit to a position at which it deflects some of the air into the said conduit.In the latter case the baffle is usually movable from a position generally across the inlet tube to a position at which it deflects some of the air into a said conduit.
The examples of the proposed construction as shown in more detail below make it possible to increase fan efficiency, to simplify and make less expensive the fabrication of the fan, and to improve the reliability of fan operation.
The invention will now be described in greater detail with reference to various specific embodiments thereof taken in conjunction with the accompanying drawings, in which: Figure 1 is a diagrammatic illustration of a proposed fan with a tangential air-flow inlet; Figure 2 is a section taken along the line ll-ll in Figure 1; Figure 3 is a section taken along the line Ill-Ill in Figure 1; Figure 4 is a diagrammatic illustration of a modified fan with an axial air-flow inlet; Figure 5 is a section taken along the line V-V in Figure 4; Figure 6 is a section taken along the line VI-VI in Figure 4 and Figure 7 is a part sectional diagrammatic plan view of the modified fan according to Figure 4.
The fan of Figures 1-3 comprises a housing 1 for an impeller 2 disposed inside the housing 1 and secured on a shaft 3. The fan has an inlet cone or tube 4 and an attachable inlet box 5. The inlet box 5 accommodates a means for prerotation swirling of the flow of air entering the impeller 2. This means comprises a by-pass conduit 6, inlet 7 of which is disposed inside the inlet box 5, and outlet 8 (Figure 2) of which is connected tangentially to the inlet cone 4 in proximity to the impeller 2 if viewed along the air inflow. The means for prerotation swirling of the incoming flow of air also comprises a baffle 9 (Figure 1) arranged in the inlet box 5 to separate the incoming air into the main and additional flows indicated by numerals 10 and 11, respectively. The outlet 8 of the bypass conduit 6 is divided by stationary vanes 12 (Figure 2) into several parts.The bypass conduit 6 has the general form of a tube placing a relatively upstream part of the inlet tube in communication with the suction zone of the impeller 2.
The baffle 9 (Figure 3) has a height "h" which is less than the corresponding height "H" of the section of the inlet box 5 in which the baffle 9 is disposed. The value e =H-h amounts to between 0.15 and 0.3 the diameter of the impeller 2 (Figure 1).
Figure 4 shows a modification of the proposed fan but with an axial inlet. In this modification an inlet tube 13 is provided with substantially hollow lugs 14 (Figure 5) outlets 15 of which are connected to the inlet tube 13 such that the additional flow 11 of air passing through the lugs enters the inlet tube 13 tangentially. Inlet holes 16 of the hol low lugs 14 (Figure 6) are connected to the inlet tube 13 upstream of the impeller 2 (Figure 4). Baffles 17 are disposed in the inlet tube 13 between the inlets and outlets 15 and 16 of the hollow lugs 14 (Figure 7). Figure 7 also illustrates by a dashed line an alternative (intermediate) position of the baffle 17.
The proposed fan of Figures 1 to 3 operates in the following manner.
When operating in a mode corresponding to the rated "capacity-pressure characteristic the baffle 9 blocks the inlet 7 of the by-pass passage 6. The air flow is thus fully delivered through the inlet box 5 and inlet cone 4 to the impeller 2.
Adjustment of fan operating conditions is made necessary by swinging the baffle 9 at a required angle for the air flow to divide into two flows, namely the main flow 10 and the additional flow 11. The main flow 10 is conveyed in the same direction as before, axially through the inlet box 5 and inlet cone 4 toward the impeller 2. The additional flow 11 passes through the inlet 7 in the bypass conduit 6 and thereafter flows through the outlet tangentially to the inlet cone 4 thereby swirling the flow entering the impeller 2 to coincide with the direction of rotation of the latter. This results in a drop of pressure developed by the fan, that is, the fan starts operating in conditions corresponding to the adjusted characteristics.
The provision of the gap "4" (Figure 3) between the baffle 9 and the wall of the inlet box 5 enables part of the main flow 10 to be directed along the wall of the inlet box 5, which produces an added swirling of this flow 10.
The proposed fan illustrated in Figures 4 to 7 operates in a manner similar to the aforedescribed one using vanes 17 to deflect at least part of the entering air.
By dispensing with a complicated guide vane apparatus the proposed invention makes it possible: (a) considerably to simplify the construction of the fan, reduce the amount of labour and expenses associated with its manufacture; (b) increase its peak efficiency by eliminating resistance to the flow caused by the prior art guide vanes; (c) expand the range of adjustment through preventing flow separation from the vanes; and the pressure losses associated therewith; and (d) improve the reliability of the flow adjustment means by way of substantially reducing the number of its parts.

Claims (7)

1. A fan comprising an impeller disposed in a housing; an inlet tube for a current of air drawn in by the fan; and a means for imparting a prerotating swirling of the flow of air entering the impeller; the swirling means comprising at least one by-pass conduit an inlet of which is located in the inlet tube of the fan, and an outlet of which is attached tangentially to the inlet tube at a relatively down stream-portion closer to the impeller, and a baffle being movably disposed inside the inlet tube to separate the incoming flow into a mainflow for the inlet tube and an additional flow entering the bypass conduit.
2. A fan as claimed in claim 1 in which the or each by-pass conduit has the general form of a tube placing a relatively upstream part of the inlet tube of the fan in communication with a suction zone of the impeller;
3. A fan as claimed in claim 1, 2 or 3 in which the baffle is movable from a position covering the upstream end of the bypass conduit to a position at which it deflects some of the air into the said conduit.
4. A fan as claimed in claim 1, 2 or 3 in which the baffle has a height substantially less than the height of the cross-section of the inlet tube in which it is disposed.
5. A fab as claimed in claim 1 in which the or each bypass conduit has the general form of hollow lugs arranged on the walls of the inlet tube of the fan and placing in communication at their tangential outlets a relatively downstream portion of the inlet tube with a relatively upstream portion thereof.
6. A fan as claimed in claim 5 in which the or each baffle is movable from a position generally across the inlet tube to a position at which it deflects some of the air into a said conduit.
7. A fan substantially as described with reference to Figures 1 to 3 or 4 to 7 of the accompanying drawings.
GB08426635A 1984-10-10 1984-10-22 Fan Expired GB2165888B (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
SE8405068A SE445061B (en) 1984-10-10 1984-10-10 FLEET WITH DEVICE FOR ROTATING THE AIR FLOW INCOMING
GB08426635A GB2165888B (en) 1984-10-10 1984-10-22 Fan
FR8416135A FR2572140B1 (en) 1984-10-10 1984-10-22 FAN
DE3448204A DE3448204C2 (en) 1984-10-10 1984-10-26 Fan
DE3439218A DE3439218A1 (en) 1984-10-10 1984-10-26 FAN

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
SE8405068A SE445061B (en) 1984-10-10 1984-10-10 FLEET WITH DEVICE FOR ROTATING THE AIR FLOW INCOMING
GB08426635A GB2165888B (en) 1984-10-10 1984-10-22 Fan
FR8416135A FR2572140B1 (en) 1984-10-10 1984-10-22 FAN
DE3439218A DE3439218A1 (en) 1984-10-10 1984-10-26 FAN

Publications (3)

Publication Number Publication Date
GB8426635D0 GB8426635D0 (en) 1984-11-28
GB2165888A true GB2165888A (en) 1986-04-23
GB2165888B GB2165888B (en) 1988-12-21

Family

ID=27433221

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08426635A Expired GB2165888B (en) 1984-10-10 1984-10-22 Fan

Country Status (4)

Country Link
DE (1) DE3439218A1 (en)
FR (1) FR2572140B1 (en)
GB (1) GB2165888B (en)
SE (1) SE445061B (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2224076A (en) * 1988-08-03 1990-04-25 Atomic Energy Authority Uk Controlling pumps
US5807073A (en) * 1996-01-31 1998-09-15 Grundfos A/S Inline centrifugal pump
FR2878914A1 (en) * 2004-12-03 2006-06-09 Inst Francais Du Petrole Air compressor for supercharged internal combustion engine, has butterfly valve moved between full open and close positions, and annular chamber, disposed around suction pipeline, to spin fresh air before its introduction in pipeline
CN112253494A (en) * 2020-09-11 2021-01-22 宁波方太厨具有限公司 Fan system, range hood applying fan system and control method of range hood

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE9400035U1 (en) * 1994-01-03 1994-03-10 NKF-Leichtmetallbau Kurt Hodermann GmbH & Co, 12277 Berlin Blower for a sweeper or suction vehicle
CN106015092A (en) * 2016-07-13 2016-10-12 重庆沃亚机械有限公司 High-efficiency energy-saving fan

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB455512A (en) * 1935-05-29 1936-10-22 Davidson & Co Ltd Improvements in or relating to the control of centrifugal fans, pumps and the like
GB464844A (en) * 1935-10-30 1937-04-26 Davidson & Co Ltd Improvements in or relating to the control of centrifugal fans, pumps and the like
GB803422A (en) * 1954-01-27 1958-10-22 Bruno Eck Radial flow blower for conveying gases with a high dust content
GB1480871A (en) * 1974-03-18 1977-07-27 Wallace Murray Corp Compressor installation for a turbocharger

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB408325A (en) * 1932-10-08 1934-04-09 Robert Ernest Workman Improvements in or relating to rotary fans
US2336010A (en) * 1942-09-17 1943-12-07 Fairchild Engine & Airplane Supercharger
CH252875A (en) * 1945-07-14 1948-01-31 Sulzer Ag Centrifugal hoist.
US3019963A (en) * 1955-07-08 1962-02-06 Eck Bruno Christian Radial blower for gases with high dust content

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB455512A (en) * 1935-05-29 1936-10-22 Davidson & Co Ltd Improvements in or relating to the control of centrifugal fans, pumps and the like
GB464844A (en) * 1935-10-30 1937-04-26 Davidson & Co Ltd Improvements in or relating to the control of centrifugal fans, pumps and the like
GB803422A (en) * 1954-01-27 1958-10-22 Bruno Eck Radial flow blower for conveying gases with a high dust content
GB1480871A (en) * 1974-03-18 1977-07-27 Wallace Murray Corp Compressor installation for a turbocharger

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2224076A (en) * 1988-08-03 1990-04-25 Atomic Energy Authority Uk Controlling pumps
US5807073A (en) * 1996-01-31 1998-09-15 Grundfos A/S Inline centrifugal pump
FR2878914A1 (en) * 2004-12-03 2006-06-09 Inst Francais Du Petrole Air compressor for supercharged internal combustion engine, has butterfly valve moved between full open and close positions, and annular chamber, disposed around suction pipeline, to spin fresh air before its introduction in pipeline
CN112253494A (en) * 2020-09-11 2021-01-22 宁波方太厨具有限公司 Fan system, range hood applying fan system and control method of range hood
CN112253494B (en) * 2020-09-11 2022-04-19 宁波方太厨具有限公司 Fan system, range hood applying fan system and control method of range hood

Also Published As

Publication number Publication date
GB2165888B (en) 1988-12-21
GB8426635D0 (en) 1984-11-28
FR2572140B1 (en) 1987-02-27
DE3439218C2 (en) 1988-01-14
SE8405068L (en) 1986-04-11
SE445061B (en) 1986-05-26
DE3439218A1 (en) 1986-05-07
SE8405068D0 (en) 1984-10-10
FR2572140A1 (en) 1986-04-25

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19921022