GB2067673A - Centrifugal blower impeller - Google Patents

Centrifugal blower impeller Download PDF

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Publication number
GB2067673A
GB2067673A GB8002040A GB8002040A GB2067673A GB 2067673 A GB2067673 A GB 2067673A GB 8002040 A GB8002040 A GB 8002040A GB 8002040 A GB8002040 A GB 8002040A GB 2067673 A GB2067673 A GB 2067673A
Authority
GB
United Kingdom
Prior art keywords
impeller
ring
blades
front plate
blower
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
GB8002040A
Other versions
GB2067673B (en
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.)
Mercantile Oy AB
Original Assignee
Mercantile Oy AB
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 Mercantile Oy AB filed Critical Mercantile Oy AB
Priority to GB8002040A priority Critical patent/GB2067673B/en
Publication of GB2067673A publication Critical patent/GB2067673A/en
Application granted granted Critical
Publication of GB2067673B publication Critical patent/GB2067673B/en
Expired legal-status Critical Current

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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
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/28Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps

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

Abstract

The curved part of the front plate 5 of the impeller is replaced by a conical supporting ring 6, the upper edge or which is attached to the blades 2 and the lower edge to the cylindrical suction ring 7. A guide ring 8 made of thin plate is mounted inwards from the supporting ring. <IMAGE>

Description

SPECIFICATION Impeller in a centrifugal blower, especially a high-pressure blower The present invention relates to an impeller in a centrifugal blower, especially a high-pressure blower.
In order to achieve high efficiency, the impeller of a centrifugal blower must have rounded, aerodynamically correct forms. However, especially the rounding of the front plate of the impeller causes problems in manufacturing techniques, since the thicknesses of material are rather great. The rounding of the front plate is therefore considerably expensive.
The curving part of the front plate can, according to the present invention, be replaced by a conical supporting ring, by means of which loads are transferred to the blades and the cylinder ring of the impeller. The aerodynamically correct form for the supporting ring is achieved by means of a guide ring made of thin plate; the manufacturing cost of this guide ring is low. The characteristics of the invention are given in the accompanying
claim.
The strength of the combined structure according to the invention is higher than the strength of a rounded, i.e. curved, front plate, since the invention eliminates the bending stresses produced in the curved part and the stress peak produced in the curved front plate and the curved part of the blades.
Owing to its flexibility, the guide ring does not receive stresses, but stresses are transferred from the front plate to the suction ring via the supporting cone, which can be manufactured at low cost in, for example, a rounding machine. This eliminates the stress peak otherwise inevitably produced in the center point of the rounding in both the blades and in the suction ring, and a stress level approx. 2030% lower is achieved than by prior known structures. This stress peak is crucial for the dimensioning of the entire impeller.
Thus the essential point is that in the structure according to the invention the aerodynamical design and the strengths design have been carried out separately, whereby a structure is obtained which is optimal both in strength and aerodynamically and less expensive to manufacture than known structures.
The aerodynamically correct form is achieved by means of a guide plate which is made from thin plate and is easy to produce at low cost by compression tools, pressure turning, etc. The radius of curvature is not iimited as is the case in structures produced by turning, and in certain cases this is very important considering the performance of the blower.
The invention can be applied to conventional impellers, but it is especially significant in high-pressure blowers, in which the blades of the impeller extend as far as the hub of the impeller and in which that part of the blades which faces the suction opening has been designed in:an aerodynamically appropriate way.
One embodiment of the invention is described below with reference to the accompanying drawing, but without limiting the invention to this embodiment.
In the embodiment depicted in the drawing the impeller 1 of a high-pressure blower has a structure in which the blades 2 extend as far as the hub 3 of the impeller and in which that part of the blades 2 facing the suction opening 4 has been designed appropriately. The rounded part of the front plate 5 has been replaced by a conical support ring 6; the upper edge of this ring has been attached to the blades 2 and its lower edge to the cylindrical suction ring 7 of the impeller. A guide plate 8 made of thin plate has been mounted inwards from the supporting ring 6; the stress peak of the guide ring 8 is indicated by 9.
CLAIMS 1. An impeller in a centrifugal blower, especially a high-pressure blower, characterized in that the curved part of the front plate (5) of the impeller (1) has been replaced by a conical supporting ring (6) the upper edge of which has been attached to the blades (2) of the impeller (1 ) and the lower edge to the cylindrical suction ring (7) of the impeller, and that a guide ring (8) made of thin plate has been mounted inwards from the supporting ring (6).
2. An impeller in a centrifugal blower, especially a high-pressure blower, constructed and adapted to operate substantially as hereinbefore described, with reference to, and as shown in, the accompanying drawing.
**WARNING** end of DESC field may overlap start of CLMS **.

Claims (2)

**WARNING** start of CLMS field may overlap end of DESC **. SPECIFICATION Impeller in a centrifugal blower, especially a high-pressure blower The present invention relates to an impeller in a centrifugal blower, especially a high-pressure blower. In order to achieve high efficiency, the impeller of a centrifugal blower must have rounded, aerodynamically correct forms. However, especially the rounding of the front plate of the impeller causes problems in manufacturing techniques, since the thicknesses of material are rather great. The rounding of the front plate is therefore considerably expensive. The curving part of the front plate can, according to the present invention, be replaced by a conical supporting ring, by means of which loads are transferred to the blades and the cylinder ring of the impeller. The aerodynamically correct form for the supporting ring is achieved by means of a guide ring made of thin plate; the manufacturing cost of this guide ring is low. The characteristics of the invention are given in the accompanying claim. The strength of the combined structure according to the invention is higher than the strength of a rounded, i.e. curved, front plate, since the invention eliminates the bending stresses produced in the curved part and the stress peak produced in the curved front plate and the curved part of the blades. Owing to its flexibility, the guide ring does not receive stresses, but stresses are transferred from the front plate to the suction ring via the supporting cone, which can be manufactured at low cost in, for example, a rounding machine. This eliminates the stress peak otherwise inevitably produced in the center point of the rounding in both the blades and in the suction ring, and a stress level approx. 2030% lower is achieved than by prior known structures. This stress peak is crucial for the dimensioning of the entire impeller. Thus the essential point is that in the structure according to the invention the aerodynamical design and the strengths design have been carried out separately, whereby a structure is obtained which is optimal both in strength and aerodynamically and less expensive to manufacture than known structures. The aerodynamically correct form is achieved by means of a guide plate which is made from thin plate and is easy to produce at low cost by compression tools, pressure turning, etc. The radius of curvature is not iimited as is the case in structures produced by turning, and in certain cases this is very important considering the performance of the blower. The invention can be applied to conventional impellers, but it is especially significant in high-pressure blowers, in which the blades of the impeller extend as far as the hub of the impeller and in which that part of the blades which faces the suction opening has been designed in:an aerodynamically appropriate way. One embodiment of the invention is described below with reference to the accompanying drawing, but without limiting the invention to this embodiment. In the embodiment depicted in the drawing the impeller 1 of a high-pressure blower has a structure in which the blades 2 extend as far as the hub 3 of the impeller and in which that part of the blades 2 facing the suction opening 4 has been designed appropriately. The rounded part of the front plate 5 has been replaced by a conical support ring 6; the upper edge of this ring has been attached to the blades 2 and its lower edge to the cylindrical suction ring 7 of the impeller. A guide plate 8 made of thin plate has been mounted inwards from the supporting ring 6; the stress peak of the guide ring 8 is indicated by 9. CLAIMS
1. An impeller in a centrifugal blower, especially a high-pressure blower, characterized in that the curved part of the front plate (5) of the impeller (1) has been replaced by a conical supporting ring (6) the upper edge of which has been attached to the blades (2) of the impeller (1 ) and the lower edge to the cylindrical suction ring (7) of the impeller, and that a guide ring (8) made of thin plate has been mounted inwards from the supporting ring (6).
2. An impeller in a centrifugal blower, especially a high-pressure blower, constructed and adapted to operate substantially as hereinbefore described, with reference to, and as shown in, the accompanying drawing.
GB8002040A 1980-01-22 1980-01-22 Centrifugal blower impeller Expired GB2067673B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB8002040A GB2067673B (en) 1980-01-22 1980-01-22 Centrifugal blower impeller

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8002040A GB2067673B (en) 1980-01-22 1980-01-22 Centrifugal blower impeller

Publications (2)

Publication Number Publication Date
GB2067673A true GB2067673A (en) 1981-07-30
GB2067673B GB2067673B (en) 1983-08-24

Family

ID=10510794

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8002040A Expired GB2067673B (en) 1980-01-22 1980-01-22 Centrifugal blower impeller

Country Status (1)

Country Link
GB (1) GB2067673B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5082425A (en) * 1987-09-17 1992-01-21 Ksb Aktiengesellschaft Centrifugal pump impeller

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5082425A (en) * 1987-09-17 1992-01-21 Ksb Aktiengesellschaft Centrifugal pump impeller

Also Published As

Publication number Publication date
GB2067673B (en) 1983-08-24

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Legal Events

Date Code Title Description
732 Registration of transactions, instruments or events in the register (sect. 32/1977)
732 Registration of transactions, instruments or events in the register (sect. 32/1977)
PE20 Patent expired after termination of 20 years

Effective date: 20000121