WO1991015664A1 - Space-efficient centrifugal blower - Google Patents

Space-efficient centrifugal blower Download PDF

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Publication number
WO1991015664A1
WO1991015664A1 PCT/US1991/002221 US9102221W WO9115664A1 WO 1991015664 A1 WO1991015664 A1 WO 1991015664A1 US 9102221 W US9102221 W US 9102221W WO 9115664 A1 WO9115664 A1 WO 9115664A1
Authority
WO
WIPO (PCT)
Prior art keywords
plenum
impeller
inlet
centrifugal blower
airfoil
Prior art date
Application number
PCT/US1991/002221
Other languages
French (fr)
Inventor
Martin G. Yapp
Original Assignee
Airflow Research And Manufacturing Corporation
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
Application filed by Airflow Research And Manufacturing Corporation filed Critical Airflow Research And Manufacturing Corporation
Publication of WO1991015664A1 publication Critical patent/WO1991015664A1/en

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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
    • 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
    • F04D29/441Fluid-guiding means, e.g. diffusers especially adapted for elastic fluid pumps
    • F04D29/444Bladed diffusers
    • 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

Definitions

  • This invention is in the general field of centrifugal blowers designed for a compact space, such as those used for automobile interior ventilation.
  • the invention generally features a space efficient centrifugal blower having a plenum connected to the impeller inlet opening.
  • the plenum has at least one plenum inlet positioned to provided airflow from one side of the impeller in a direction generally perpendicular to the impeller axis.
  • a set of airfoil members positioned in the plenum around the impeller inlet have elongated airflow control surfaces extending outwardly from the impeller inlet in a direction generally perpendicular to the impeller axis, so that the airfoil members act on air flowing from the plenum inlet to direct it radially inwardly and to spread the airflow around the impeller inlet.
  • the plenum inlet has an opening positioned within a first quadrant of the plenum, and the directional bias of airflow members in the first quadrant increases as a function of their angular position away from the centerline of the plenum inlet.
  • I mean the angular "turn" effected by a given airfoil member flow control surface, as determined by the change in flow-control angle from the tip to the tail of the airflow member.
  • the directional bias of the airfoil members increases as a function of angular position moving from 0° to 60° and from 0° to -60° (300°), where 0° is the position of the plenum inlet idline as shown in Fig. 3.
  • One particularly preferred embodiment uses a set of airfoil members (a cascade) that has bilateral symmetry (such as the set discussed immediately above) to efficiently control airflow.
  • the airfoil members may be molded as a plastic part, integral with a plenum face.
  • blower is particularly space efficient, and well adapted for use in vehicle (e.g. automotive) cabin ventilation systems. Space efficiency is achieved while minimizing or avoiding trade-offs such as power requirements or noise.
  • Fig. 1 is a sectional view of a blower according to invention.
  • Fig. 2 is a view taken along 2-2 of Fig. 1.
  • Fig. 3 is an enlargement of blades in the cascade of Fig. 2. Structure
  • blower 10 is a centrifugal blower suitable for use in an automotive climate control system.
  • the impeller 30 of blower 10 is driven by motor 11 to draw air in through plenum 50, and axially inwardly through the impeller inlet 39. Since many components of the impeller ar standard, there is no need to refer to them in detail here.
  • the blades 32 impeller 30 of blower 10 may be generally designed according to the design disclosed in commonly owned U.S. Patent 4,900,228, which is hereby incorporated by reference, showing a centrifugal blower with an impeller having variably cambered rearwardly curved blades.
  • the impeller forces air radially outwardly through impeller outlet 35.
  • plenum 50 has inlet 52.
  • Figs. 2 and 3 show cascade 59 diagrammatically, to illustrate the change i bias of members 57 as a function of radial position, where 0° is a radial midline through the operative inlet.
  • Each airfoil member 57 redirects air radially from points around the circumference of inlet 39.
  • the bias angle ⁇ (Fig. 4) of the 53 individual evenly spaced airfoil blades is shown in the following table. Bias angle is defined as the angle between the individual blade nose-tail line and a line connecting the nose to the center of the pattern.
  • blades 7-26 are identical, and blades 28-46 are mirror images of blades 7-26.
  • Fig. 3 is an enlarged diagram of blades 8-11. Also shown in Table is the maximum blade camber f/c for each of the 53 blades. The maximum camber increase linearly with rotational position.
  • a bulkhead is placed in the plenum which isolates the left-hand and right-hand halves, and provides a means of achieving stagnation of the flow at 180°. This improves the efficiency of the device.

Abstract

A space efficient centrifugal blower (10) having a plenum (50) connected to the impeller inlet opening (39). The plenum has at least one plenum inlet (52) positioned to provide airflow from one side of the impeller in a direction generally perpendicular to the impeller axis. A set of airfoil members (57) positioned in the plenum around the impeller inlet have elongated airflow control surfaces extending outwardly from the impeller inlet in a direction generally perpendicular to the impeller axis, so that the airfoil members act on air flowing from the plenum inlet to direct it radially inwardly and to spread the airflow around the impeller inlet.

Description

SPACE-EFFICIENT CENTRIFUGAL BLOWER Background of the Invention
This invention is in the general field of centrifugal blowers designed for a compact space, such as those used for automobile interior ventilation.
There are many conflicting and demanding constraints on the design of compact blowers such as those used for automotive interior ventilation systems. One serious constraint is the size of the package available to house the system. Increasingly, automotive designers are driven to use all available cabin space efficiently and to balance conflicting demands for space. Another constraint is noise; excessive noise in the cabin will not be tolerated. Power available to drive fan motors is also limited. Other considerations are ease of molding and manufacturing and cost.
Summary of the Invention
The invention generally features a space efficient centrifugal blower having a plenum connected to the impeller inlet opening. The plenum has at least one plenum inlet positioned to provided airflow from one side of the impeller in a direction generally perpendicular to the impeller axis. A set of airfoil members positioned in the plenum around the impeller inlet have elongated airflow control surfaces extending outwardly from the impeller inlet in a direction generally perpendicular to the impeller axis, so that the airfoil members act on air flowing from the plenum inlet to direct it radially inwardly and to spread the airflow around the impeller inlet.
Preferred embodiments of the invention have the following features. The plenum inlet has an opening positioned within a first quadrant of the plenum, and the directional bias of airflow members in the first quadrant increases as a function of their angular position away from the centerline of the plenum inlet. (By directional bias, I mean the angular "turn" effected by a given airfoil member flow control surface, as determined by the change in flow-control angle from the tip to the tail of the airflow member. These characteristics are described in greater detail below. ) Most preferably, the directional bias of the airfoil members increases as a function of angular position moving from 0° to 60° and from 0° to -60° (300°), where 0° is the position of the plenum inlet idline as shown in Fig. 3. One particularly preferred embodiment uses a set of airfoil members (a cascade) that has bilateral symmetry (such as the set discussed immediately above) to efficiently control airflow. For example, the airfoil members may be molded as a plastic part, integral with a plenum face.
The above-described blower is particularly space efficient, and well adapted for use in vehicle (e.g. automotive) cabin ventilation systems. Space efficiency is achieved while minimizing or avoiding trade-offs such as power requirements or noise.
Description of the Preferred Embodiments Drawings
Fig. 1 is a sectional view of a blower according to invention.
Fig. 2 is a view taken along 2-2 of Fig. 1. Fig. 3 is an enlargement of blades in the cascade of Fig. 2. Structure
In Fig. 1, blower 10 is a centrifugal blower suitable for use in an automotive climate control system. The impeller 30 of blower 10 is driven by motor 11 to draw air in through plenum 50, and axially inwardly through the impeller inlet 39. Since many components of the impeller ar standard, there is no need to refer to them in detail here. For example, the blades 32 impeller 30 of blower 10 may be generally designed according to the design disclosed in commonly owned U.S. Patent 4,900,228, which is hereby incorporated by reference, showing a centrifugal blower with an impeller having variably cambered rearwardly curved blades.
The impeller forces air radially outwardly through impeller outlet 35.
In Fig. 2, plenum 50 has inlet 52. Positioned within plenum 50 is a radially oriented cascade 59 of airfoi members 57 having flow control surfaces 58. Figs. 2 and 3 show cascade 59 diagrammatically, to illustrate the change i bias of members 57 as a function of radial position, where 0° is a radial midline through the operative inlet. Each airfoil member 57 redirects air radially from points around the circumference of inlet 39. The bias angle φ (Fig. 4) of the 53 individual evenly spaced airfoil blades is shown in the following table. Bias angle is defined as the angle between the individual blade nose-tail line and a line connecting the nose to the center of the pattern.
Table
Figure imgf000005_0001
- ώ -
.1152
Bulkhead
-.1152
-.0987
-.0823
-.0658
-.0494
-.0329
Figure imgf000006_0001
-.0165
As the table shows, blades 7-26 are identical, and blades 28-46 are mirror images of blades 7-26. Fig. 3 is an enlarged diagram of blades 8-11. Also shown in Table is the maximum blade camber f/c for each of the 53 blades. The maximum camber increase linearly with rotational position.
Maximum camber is zero for the blade on centerline; .0165 for the first blade; twice .0165 for the second blade, and so on until f/c = .1152 for the 7th through 26th blade. It can be seen from the geometry that some diffusion occurs in the blades 7-26. Increasing maximum camber beyond f/c .115 result in flow separation from the blading and a reduction of efficiency.
A bulkhead is placed in the plenum which isolates the left-hand and right-hand halves, and provides a means of achieving stagnation of the flow at 180°. This improves the efficiency of the device.
Other embodiments are within the following claims.

Claims

Claims 1. A centrifugal blower comprising an impeller that rotates on an axis and a motor connected to rotate the impeller, the impeller comprising blades shaped and oriente to draw air in axially through an impeller inlet opening an to exhaust air radially, the centrifugal blower further comprising, a) a plenum connected to the impeller inlet opening, the plenum having at least one plenum inlet positioned to provide airflow from one side of the impeller in a direction generally perpendicular to the impeller axis, and b) a set of airfoil members positioned in the plenum around the impeller inlet, each airfoil member having an elongated airflow control surface extending outwardly fro the impeller inlet in a direction generally perpendicular to the axis, so as to act on air flowing from the plenum inlet, directing the airflow radially inwardly and spreading it around the impeller inlet.
2. The centrifugal blower of claim 1 in which the plenum inlet has an opening positioned within a first quadrant of the plenum, and the directional bias of the airfoil members in the first quadrant generally increases as a function of angular position of the airfoil member away from the plenum inlet centerline.
3. The centrifugal blower of claim 1 in which the directional bias of said airfoil members generally increases as a function of the angular position of said airfoil member from 0° to 60° and from 0° to -60°.
4. The centrifugal blower of claim 3 in which the airfoil cascade is bilaterally symmetrical.
5. The centrifugal blower of claim 4 in which the airfoil members are molded as an integral plastic part with plenum face.
6. The centrifugal blower of claim 1 in which set of airfoils comprises a bulkhead member positioned at 180° from said plenum inlet.
PCT/US1991/002221 1990-03-30 1991-03-29 Space-efficient centrifugal blower WO1991015664A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US50244090A 1990-03-30 1990-03-30
US502,440 1990-03-30

Publications (1)

Publication Number Publication Date
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Family Applications (1)

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1998017918A1 (en) * 1996-10-18 1998-04-30 New Philadelphia Fan Company Fan inlet flow controller
US6092988A (en) * 1998-07-06 2000-07-25 Ford Motor Company Centrifugal blower assembly with a pre-swirler for an automotive vehicle
FR2859251A1 (en) * 2003-08-28 2005-03-04 Valeo Climatisation Pulser for heating, ventilation and/or air conditioning apparatus, has intermediate piece mounted on engine support and placed in upstream of vaned rotor, where piece and support have radial ribs to spin air in rotor direction
EP2424082A1 (en) * 2010-08-24 2012-02-29 Alstom Technology Ltd Electric machine with coolant intake chamber
EP3161322B1 (en) * 2014-06-26 2023-10-04 General Electric Company Turbomachine inlet nozzle for asymmetric flow, with vanes of different shapes

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1900144A (en) * 1930-09-02 1933-03-07 William M White Hydraulic machine
US2210155A (en) * 1936-07-16 1940-08-06 Szydlowski Josef Machine for the displacement and compression of fluids
US2320733A (en) * 1938-01-07 1943-06-01 Macard Screws Ltd Screw type fluid propelling apparatus
US2438246A (en) * 1945-03-27 1948-03-23 American Molded Products Co Facial analysis chart
US2811303A (en) * 1948-12-28 1957-10-29 Joy Mfg Co Impeller for axial flow fans
US4566166A (en) * 1984-10-03 1986-01-28 Allis-Chalmers Corporation Method for manufacturing a stay ring bearing stationary guide vanes for a nongated turbine
US4799857A (en) * 1986-11-29 1989-01-24 Klein, Schanzlin & Becker Aktiengesellschaft Casing for fluid flow machines
US4900228A (en) * 1989-02-14 1990-02-13 Airflow Research And Manufacturing Corporation Centrifugal fan with variably cambered blades

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1900144A (en) * 1930-09-02 1933-03-07 William M White Hydraulic machine
US2210155A (en) * 1936-07-16 1940-08-06 Szydlowski Josef Machine for the displacement and compression of fluids
US2320733A (en) * 1938-01-07 1943-06-01 Macard Screws Ltd Screw type fluid propelling apparatus
US2438246A (en) * 1945-03-27 1948-03-23 American Molded Products Co Facial analysis chart
US2811303A (en) * 1948-12-28 1957-10-29 Joy Mfg Co Impeller for axial flow fans
US4566166A (en) * 1984-10-03 1986-01-28 Allis-Chalmers Corporation Method for manufacturing a stay ring bearing stationary guide vanes for a nongated turbine
US4799857A (en) * 1986-11-29 1989-01-24 Klein, Schanzlin & Becker Aktiengesellschaft Casing for fluid flow machines
US4900228A (en) * 1989-02-14 1990-02-13 Airflow Research And Manufacturing Corporation Centrifugal fan with variably cambered blades

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1998017918A1 (en) * 1996-10-18 1998-04-30 New Philadelphia Fan Company Fan inlet flow controller
US5979595A (en) * 1996-10-18 1999-11-09 New Philadelphia Fan Company Fan inlet flow controller
US6148954A (en) * 1996-10-18 2000-11-21 Joy Mm Delaware, Inc. Fan inlet flow controller
US6193011B1 (en) 1996-10-18 2001-02-27 New Philadelphia Fan Company Fan inlet flow controller
EP1172564A3 (en) * 1996-10-18 2002-11-13 Howden Buffalo Inc. Fan inlet flow controller
US6092988A (en) * 1998-07-06 2000-07-25 Ford Motor Company Centrifugal blower assembly with a pre-swirler for an automotive vehicle
FR2859251A1 (en) * 2003-08-28 2005-03-04 Valeo Climatisation Pulser for heating, ventilation and/or air conditioning apparatus, has intermediate piece mounted on engine support and placed in upstream of vaned rotor, where piece and support have radial ribs to spin air in rotor direction
EP2424082A1 (en) * 2010-08-24 2012-02-29 Alstom Technology Ltd Electric machine with coolant intake chamber
EP3161322B1 (en) * 2014-06-26 2023-10-04 General Electric Company Turbomachine inlet nozzle for asymmetric flow, with vanes of different shapes

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