GB1001153A - Improvements relating to rotors for flow machines - Google Patents

Improvements relating to rotors for flow machines

Info

Publication number
GB1001153A
GB1001153A GB3216561A GB3216561A GB1001153A GB 1001153 A GB1001153 A GB 1001153A GB 3216561 A GB3216561 A GB 3216561A GB 3216561 A GB3216561 A GB 3216561A GB 1001153 A GB1001153 A GB 1001153A
Authority
GB
United Kingdom
Prior art keywords
blades
component
support member
holes
disc
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.)
Expired
Application number
GB3216561A
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.)
Firth Cleveland Ltd
Original Assignee
Firth Cleveland Ltd
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 Firth Cleveland Ltd filed Critical Firth Cleveland Ltd
Publication of GB1001153A publication Critical patent/GB1001153A/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
    • F04D29/26Rotors 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
    • F04D29/282Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for fans or blowers the leading edge of each vane being substantially parallel to the rotation axis
    • F04D29/283Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for fans or blowers the leading edge of each vane being substantially parallel to the rotation axis rotors of the squirrel-cage type

Landscapes

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

Abstract

1,001,153. Transverse-flow machines. FIRTH CLEVELAND Ltd. Sept. 7, 1961 [Sept. 8, 1960], No. 32165/61. Heading F1C. A rotor for a transverse-flow machine comprises at least two axially-aligned interconnected moulded components, each component having a support member of circular periphery and a series of blades moulded integrally with and extending from the support member parallel to the rotor axis and in a ring thereabout, and an additional support member of circular periphery, the ends of the blades of at least one component remote from the support member thereof being interengaged with another of the support members, the last-mentioned support member having, in the completed rotor, blades extending from that support member to opposite sides thereof with the blades on one side in staggered relationship with the blades on the other side. The rotor component 31 shown in Fig. 1a comprises an end disc 30 integral with blades 32 having projections 33 which can be glued into holes 34, Fig. 1b, in an intermediate disc (or ring) 35. The disc 35 has a further set of holes 34 intercalated with the first-mentioned holes, to receive the blade projections 33<SP>1</SP>, Fig. 1c, of a further rotor component 37 having blades 38, 38<SP>1</SP> projecting from opposite sides of a central disc 36. Further discs 35 and components 37 may be added, and the final component may be similar to the component 31 but of opposite hand. Alternatively, an end disc 44, Fig. I e (not shown), having holes for engagement with blade projections and provided with a hub for connection to a shaft, may be used. An annular weakened portion around the hub permits flexure to compensate for misalignment between the shaft and the rotor axis. A similar provision is made at 31<SP>1</SP> in the end disc 30. A further component which may be used in addition to, or in place of, components 37 and discs 35 comprises a plain disc 42, Fig. 1d (not shown), provided with blades at one side only, holes similar to the holes 34 being provided intermediate the blades. All components may be moulded from plastics material. Specification 876,611 is referred to.
GB3216561A 1960-09-08 1961-09-07 Improvements relating to rotors for flow machines Expired GB1001153A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEL0006997 1960-09-08

Publications (1)

Publication Number Publication Date
GB1001153A true GB1001153A (en) 1965-08-11

Family

ID=7257195

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3216561A Expired GB1001153A (en) 1960-09-08 1961-09-07 Improvements relating to rotors for flow machines

Country Status (1)

Country Link
GB (1) GB1001153A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0348846A2 (en) * 1988-06-30 1990-01-03 Siemens Aktiengesellschaft Balanced-fan rotor and method and apparatus for realising the balancing
GB2292190A (en) * 1994-08-09 1996-02-14 Toshiba Kk Transverse fan, method of manufacture, and moulding apparatus
GB2324836A (en) * 1994-08-09 1998-11-04 Toshiba Kk A method of manufacturing a transverse fan having moulded impeller components
WO2005017363A1 (en) * 2003-07-31 2005-02-24 Silentum Ab A device comprising a shaft with a plurality of fan bodies provided thereto and a method for mounting the device as well as a use of the device
GB2416568A (en) * 2004-07-24 2006-02-01 Rolls Royce Plc Aerofoil with support member
CN111664117A (en) * 2020-06-08 2020-09-15 华帝股份有限公司 Intelligent adjustment's impeller device, fan and range hood

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0348846A2 (en) * 1988-06-30 1990-01-03 Siemens Aktiengesellschaft Balanced-fan rotor and method and apparatus for realising the balancing
EP0348846A3 (en) * 1988-06-30 1990-04-18 Siemens Aktiengesellschaft Balanced-fan rotor and method and apparatus for realising the balancing
GB2292190A (en) * 1994-08-09 1996-02-14 Toshiba Kk Transverse fan, method of manufacture, and moulding apparatus
US5827046A (en) * 1994-08-09 1998-10-27 Kabushiki Kaisha Toshiba Transverse fan, method of manufacturing the same and apparatus therefor
GB2324836A (en) * 1994-08-09 1998-11-04 Toshiba Kk A method of manufacturing a transverse fan having moulded impeller components
GB2292190B (en) * 1994-08-09 1999-03-10 Toshiba Kk Transverse fan
GB2324836B (en) * 1994-08-09 1999-03-10 Toshiba Kk Method of manufacturing a transverse fan
WO2005017363A1 (en) * 2003-07-31 2005-02-24 Silentum Ab A device comprising a shaft with a plurality of fan bodies provided thereto and a method for mounting the device as well as a use of the device
US7357617B2 (en) 2003-07-31 2008-04-15 Johan Haga Fan including a plurality of spaced fan bodies
GB2416568A (en) * 2004-07-24 2006-02-01 Rolls Royce Plc Aerofoil with support member
CN111664117A (en) * 2020-06-08 2020-09-15 华帝股份有限公司 Intelligent adjustment's impeller device, fan and range hood

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