GB720956A - Improvements in or relating to centrifugal fan wheels - Google Patents

Improvements in or relating to centrifugal fan wheels

Info

Publication number
GB720956A
GB720956A GB12570/53A GB1257053A GB720956A GB 720956 A GB720956 A GB 720956A GB 12570/53 A GB12570/53 A GB 12570/53A GB 1257053 A GB1257053 A GB 1257053A GB 720956 A GB720956 A GB 720956A
Authority
GB
United Kingdom
Prior art keywords
core
skin
blade
preformed
blades
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
GB12570/53A
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.)
Westinghouse Electric International Co
Original Assignee
Westinghouse Electric International Co
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 Westinghouse Electric International Co filed Critical Westinghouse Electric International Co
Publication of GB720956A publication Critical patent/GB720956A/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
    • F04D29/30Vanes

Landscapes

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

Abstract

720,956. Centrifugal fans. WESTING- HOUSE ELECTRIC INTERNATIONAL CO. May 6, 1953 [June 21, 1952], No. 12570/53. Class 110 (1). In a centrifugal fan impeller comprising aerofoil blades attached at their ends to a back plate and a shroud plate, the blades comprise light-weight sponge-like (i.e. having a large number of interstices with air cells therein) cores within and adhesively bonded to outer skins of sheet metal, preferably aluminium. The impeller may be of the double-inlet type, in which case the back plate is the centre plate of the impeller. The core may be of a plastic composition which is poured into the blade through a hole in the back plate or shroud plate and is subsequently heated to cause it to foam and thus expand to press against and adhere to the inner surface of the blade skin. The plastic composition may be a mixture, such as tolylene diisocyanate plus alkyd resin, which generates its own heat. Alternatively, the heat may be applied externally, in which case the core may comprise pellets of nylon and phenolic rubber, or granular cork mixed with phenolic varnish. As a further alternative, the core is preformed, coated with an adhesive, and slid into an open end of a preformed blade. Or, the blade skin is wrapped around the preformed core with adhesive between them, the trailing edges of the blade skin being secured together in a lock seam. A suitable material for a preformed core is a foamed styrene. Or, a cellular or honeycomb texture may be provided by the use of resin impregnated paper or cloth, aluminium foil or cellular cellulose acetate. Holes 25, Fig. 9, can be pressed inwardly to assist in bonding the core 24 to the skin 23. The core may have a void within it, as shown in Figs. 4 and 8, where a hollow inner skin 26 of aerofoil shape is provided. In the modification shown in Fig. 13, a cellular core 38 is folded over an inner member 37 and then the outer skin 23 is folded around the core, and the trailing edges of the outer skin are joined together by a lock seam. Granular composition 39 is then poured into the vacant space at the trailing end, and heated. Alternatively, the voids may be formed by one or more hollow tubes 27, Fig. 11, passing longitudinally through the core. By expanding the ends of the tubes as shown, the blades are secured in place between the back plate 21 and shroud plate 20. In addition, the blade skin may be welded at 35 to the plates. Figs. 8, 9 and 10 show alternative ways of attaching the blades to the plates. Rivets are shown, but welding may be used instead at the connection to the blade skin. In Fig. 8, angle bars 30, 31 extend around the outside of the blade; and in Fig. 9, channel members 32, 33 are used. In Fig. 10, the use of W-shaped attachment members 34 avoids the use of blind riveting at the connection to the blade skin. Specification 488,781 is referred to.
GB12570/53A 1952-06-21 1953-05-06 Improvements in or relating to centrifugal fan wheels Expired GB720956A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US720956XA 1952-06-21 1952-06-21

Publications (1)

Publication Number Publication Date
GB720956A true GB720956A (en) 1954-12-29

Family

ID=22105532

Family Applications (1)

Application Number Title Priority Date Filing Date
GB12570/53A Expired GB720956A (en) 1952-06-21 1953-05-06 Improvements in or relating to centrifugal fan wheels

Country Status (1)

Country Link
GB (1) GB720956A (en)

Cited By (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2902941A (en) * 1957-08-02 1959-09-08 Continental Plastics Corp Plastic pump impeller
US2916199A (en) * 1958-04-07 1959-12-08 Westinghouse Electric Corp Centrifugal fan wheels
US2970347A (en) * 1957-05-16 1961-02-07 Gen Am Transport Hatch plugs
US3027040A (en) * 1955-07-20 1962-03-27 Electrolux Ab Multi-density expanded plastic-body
US3078202A (en) * 1956-06-01 1963-02-19 August T Bellanca Type of construction
US3096053A (en) * 1960-11-17 1963-07-02 Gen Grid Corp Low density construction material
US3110552A (en) * 1959-09-23 1963-11-12 Walter D Voelker Method of making an inflatable structure
US3128940A (en) * 1964-04-14 Capillary fans
US3144204A (en) * 1962-08-24 1964-08-11 Acme Engineering And Mfg Corp Centrifugal blower wheel
US3166295A (en) * 1959-08-24 1965-01-19 Zakl Mech Im Gen K S Guide wheel for condensing turbines of great and greatest power
US3171586A (en) * 1963-12-31 1965-03-02 Westinghouse Electric Corp Airfoil bladed fans
US3172621A (en) * 1963-07-10 1965-03-09 Gen Electric Airfoil
US3188800A (en) * 1960-05-12 1965-06-15 Thiokol Chemical Corp Helical-type turbojet engine
US3202103A (en) * 1961-12-21 1965-08-24 Western Brass Works Flexible cam actuated impeller pump
US3229935A (en) * 1962-12-06 1966-01-18 August T Bellanca Aircraft wing construction
US3240153A (en) * 1961-12-28 1966-03-15 Rockwell Standard Co Hydrodynamic bladed wheel assemblies
US3273833A (en) * 1965-01-21 1966-09-20 Dow Chemical Co Airfoil structure
US3291382A (en) * 1964-05-08 1966-12-13 Rolls Royce Bladed structure, for example, for a gas turbine engine compressor
US3416756A (en) * 1966-08-03 1968-12-17 Dow Chemical Co Airfoil structure
US3445553A (en) * 1965-04-02 1969-05-20 James S Hardigg Method of making a shock isolator element for cushioned container unit
US3779487A (en) * 1971-04-19 1973-12-18 L Ashton Light weight contoured load carrying structure
US4759690A (en) * 1984-05-24 1988-07-26 Deschamps John A Impeller
GB2240588A (en) * 1990-01-31 1991-08-07 Toshiba Kk Ventilating fan
US5045251A (en) * 1987-06-15 1991-09-03 Ford Motor Company Method of resin transfer molding a composite article
EP1741934A1 (en) * 2005-07-04 2007-01-10 Behr GmbH & Co. KG Rotor
WO2007003416A1 (en) * 2005-07-04 2007-01-11 Behr Gmbh & Co. Kg Blower wheel
DE102006017368A1 (en) * 2006-04-11 2007-10-18 Behr Gmbh & Co. Kg Impeller, in particular double-flow impeller, and method for producing such an impeller
CN102439320A (en) * 2009-05-20 2012-05-02 W&S管理公司 Fan blade
CN103850889A (en) * 2014-02-27 2014-06-11 北京金风科创风电设备有限公司 Blunt trailing edge fan blade and method for fixing vertical face core material of trailing edge of blunt trailing edge fan blade

Cited By (34)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3128940A (en) * 1964-04-14 Capillary fans
US3027040A (en) * 1955-07-20 1962-03-27 Electrolux Ab Multi-density expanded plastic-body
US3078202A (en) * 1956-06-01 1963-02-19 August T Bellanca Type of construction
US2970347A (en) * 1957-05-16 1961-02-07 Gen Am Transport Hatch plugs
US2902941A (en) * 1957-08-02 1959-09-08 Continental Plastics Corp Plastic pump impeller
US2916199A (en) * 1958-04-07 1959-12-08 Westinghouse Electric Corp Centrifugal fan wheels
US3166295A (en) * 1959-08-24 1965-01-19 Zakl Mech Im Gen K S Guide wheel for condensing turbines of great and greatest power
US3110552A (en) * 1959-09-23 1963-11-12 Walter D Voelker Method of making an inflatable structure
US3188800A (en) * 1960-05-12 1965-06-15 Thiokol Chemical Corp Helical-type turbojet engine
US3096053A (en) * 1960-11-17 1963-07-02 Gen Grid Corp Low density construction material
US3202103A (en) * 1961-12-21 1965-08-24 Western Brass Works Flexible cam actuated impeller pump
US3240153A (en) * 1961-12-28 1966-03-15 Rockwell Standard Co Hydrodynamic bladed wheel assemblies
US3144204A (en) * 1962-08-24 1964-08-11 Acme Engineering And Mfg Corp Centrifugal blower wheel
US3229935A (en) * 1962-12-06 1966-01-18 August T Bellanca Aircraft wing construction
US3172621A (en) * 1963-07-10 1965-03-09 Gen Electric Airfoil
US3171586A (en) * 1963-12-31 1965-03-02 Westinghouse Electric Corp Airfoil bladed fans
US3291382A (en) * 1964-05-08 1966-12-13 Rolls Royce Bladed structure, for example, for a gas turbine engine compressor
US3273833A (en) * 1965-01-21 1966-09-20 Dow Chemical Co Airfoil structure
US3445553A (en) * 1965-04-02 1969-05-20 James S Hardigg Method of making a shock isolator element for cushioned container unit
US3416756A (en) * 1966-08-03 1968-12-17 Dow Chemical Co Airfoil structure
US3779487A (en) * 1971-04-19 1973-12-18 L Ashton Light weight contoured load carrying structure
US4079903A (en) * 1971-04-19 1978-03-21 Fiber Science, Inc. Lightweight contoured load carrying structure
US4759690A (en) * 1984-05-24 1988-07-26 Deschamps John A Impeller
US5045251A (en) * 1987-06-15 1991-09-03 Ford Motor Company Method of resin transfer molding a composite article
GB2240588A (en) * 1990-01-31 1991-08-07 Toshiba Kk Ventilating fan
GB2240588B (en) * 1990-01-31 1994-08-03 Toshiba Kk Ventilating fan
EP1741934A1 (en) * 2005-07-04 2007-01-10 Behr GmbH & Co. KG Rotor
WO2007003416A1 (en) * 2005-07-04 2007-01-11 Behr Gmbh & Co. Kg Blower wheel
CN101213373B (en) * 2005-07-04 2012-05-09 贝洱两合公司 Impeller
US8337157B2 (en) 2005-07-04 2012-12-25 Behr Gmbh & Co. Kg Blower wheel
DE102006017368A1 (en) * 2006-04-11 2007-10-18 Behr Gmbh & Co. Kg Impeller, in particular double-flow impeller, and method for producing such an impeller
CN102439320A (en) * 2009-05-20 2012-05-02 W&S管理公司 Fan blade
CN103850889A (en) * 2014-02-27 2014-06-11 北京金风科创风电设备有限公司 Blunt trailing edge fan blade and method for fixing vertical face core material of trailing edge of blunt trailing edge fan blade
CN103850889B (en) * 2014-02-27 2016-08-17 北京金风科创风电设备有限公司 Blunt trailing edge fan blade and trailing edge facade core fixing means thereof

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