GB586836A - Elastic fluid pumps and turbines - Google Patents

Elastic fluid pumps and turbines

Info

Publication number
GB586836A
GB586836A GB706543A GB706543A GB586836A GB 586836 A GB586836 A GB 586836A GB 706543 A GB706543 A GB 706543A GB 706543 A GB706543 A GB 706543A GB 586836 A GB586836 A GB 586836A
Authority
GB
United Kingdom
Prior art keywords
vanes
divided
parts
rotor
vibration
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
GB706543A
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.)
TURBO ENGINEERING CORP
Original Assignee
TURBO ENGINEERING CORP
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 TURBO ENGINEERING CORP filed Critical TURBO ENGINEERING CORP
Priority to GB706543A priority Critical patent/GB586836A/en
Publication of GB586836A publication Critical patent/GB586836A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/28—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
    • F04D29/284—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for compressors
    • F04D29/285—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for compressors the compressor wheel comprising a pair of rotatable bladed hub portions axially aligned and clamped together
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/04—Blade-carrying members, e.g. rotors for radial-flow machines or engines
    • F01D5/043—Blade-carrying members, e.g. rotors for radial-flow machines or engines of the axial inlet- radial outlet, or vice versa, type
    • F01D5/045—Blade-carrying members, e.g. rotors for radial-flow machines or engines of the axial inlet- radial outlet, or vice versa, type the wheel comprising two adjacent bladed wheel portions, e.g. with interengaging blades for damping vibrations
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/661—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
    • F04D29/668—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps damping or preventing mechanical vibrations

Abstract

586,836. Centrifugal pumps. NEWTON, E. P. (Turbo Engineering Corporation). May 4, 1943, No. 7065. [Classes 110 (i) and 110 (iii)] [Also in Group XXXII] To reduce vibration in the blades of centrifugal pumps and the like, the rotor is divided by a radial plane into parts 158,160, Fig 15, so that the natural vibration of the two blade parts have different periods. Frictional contact between the tips of the blade parts is secured by a slight undercut 162 ; the closing pressure may be provided by the fluid being pumped. A disc 166 may provide a damping friction on the discharge ends of the blades. Instead of the undercut, the rotor portions may be divided by thin inserts of an artificial resin, or be linked by small steel balls housed in complementary recesses in the meeting faces of the vanes. In another form, the rotor is not divided and small bodies such as rivets or clips, are attached with a slight play to non-nodal parts of the vanes. To reduce the cause of vibration, supports or vanes in the inlet and outlet channels, for example, the vanes 12, Fig, 2, are arranged out of line with the vanes 6.
GB706543A 1943-05-04 1943-05-04 Elastic fluid pumps and turbines Expired GB586836A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB706543A GB586836A (en) 1943-05-04 1943-05-04 Elastic fluid pumps and turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB706543A GB586836A (en) 1943-05-04 1943-05-04 Elastic fluid pumps and turbines

Publications (1)

Publication Number Publication Date
GB586836A true GB586836A (en) 1947-04-02

Family

ID=9825949

Family Applications (1)

Application Number Title Priority Date Filing Date
GB706543A Expired GB586836A (en) 1943-05-04 1943-05-04 Elastic fluid pumps and turbines

Country Status (1)

Country Link
GB (1) GB586836A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2913221A (en) * 1955-12-12 1959-11-17 Gen Electric Damping turbine buckets
FR2561339A1 (en) * 1984-03-14 1985-09-20 Paris & Du Rhone Ventilator mounting for electrical machine
DE3519125A1 (en) * 1985-05-28 1986-12-04 Siemens AG, 1000 Berlin und 8000 München Fan arrangement having radially extending fan blades
DE9017417U1 (en) * 1990-12-22 1991-03-14 Behr Gmbh & Co, 7000 Stuttgart, De
EP2072758A3 (en) * 2007-12-18 2012-10-24 Hamilton Sundstrand Corporation Method of modifying the natural frequency of an airfoil for a gas turbine engine and the corresponding airfoil
EP2484867A3 (en) * 2011-02-03 2014-06-18 General Electric Company Rotating component of a turbine engine
EP2612989A3 (en) * 2012-01-05 2014-06-18 General Electric Company System and method for reducing stress in a rotor

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2913221A (en) * 1955-12-12 1959-11-17 Gen Electric Damping turbine buckets
FR2561339A1 (en) * 1984-03-14 1985-09-20 Paris & Du Rhone Ventilator mounting for electrical machine
DE3519125A1 (en) * 1985-05-28 1986-12-04 Siemens AG, 1000 Berlin und 8000 München Fan arrangement having radially extending fan blades
DE9017417U1 (en) * 1990-12-22 1991-03-14 Behr Gmbh & Co, 7000 Stuttgart, De
EP2072758A3 (en) * 2007-12-18 2012-10-24 Hamilton Sundstrand Corporation Method of modifying the natural frequency of an airfoil for a gas turbine engine and the corresponding airfoil
EP2484867A3 (en) * 2011-02-03 2014-06-18 General Electric Company Rotating component of a turbine engine
EP2612989A3 (en) * 2012-01-05 2014-06-18 General Electric Company System and method for reducing stress in a rotor

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