GB251659A - Improvements in blades for centrifugal compressors - Google Patents

Improvements in blades for centrifugal compressors

Info

Publication number
GB251659A
GB251659A GB11456/26A GB1145626A GB251659A GB 251659 A GB251659 A GB 251659A GB 11456/26 A GB11456/26 A GB 11456/26A GB 1145626 A GB1145626 A GB 1145626A GB 251659 A GB251659 A GB 251659A
Authority
GB
United Kingdom
Prior art keywords
blades
centrifugal compressors
secured
blade
ribs
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
GB11456/26A
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.)
BBC Brown Boveri AG Germany
BBC Brown Boveri France SA
Original Assignee
Brown Boveri und Cie AG Germany
BBC Brown Boveri France SA
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 Brown Boveri und Cie AG Germany, BBC Brown Boveri France SA filed Critical Brown Boveri und Cie AG Germany
Publication of GB251659A publication Critical patent/GB251659A/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
    • F04D29/30—Vanes

Landscapes

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

Abstract

251,659. Akt.-Ges. Brown, Boveri, et Cie. May 2, 1925, [Convention date]. Impeller blades.-Blades 1 for the rotor wheels of centrifugal compressors have transverse and longitudinal ribs 5, 6 and are secured to the rotor discs by rivets 3. The ribs are provided only on the side of the blade facing the centre of the wheel, and they are covered with a sheet 17 of metal bent round the inner edge of the blade and secured by a rivet 19. The blades are composed of light metal and may be made in sections which can be arranged to form passages of any desired shape.
GB11456/26A 1925-05-02 1926-04-30 Improvements in blades for centrifugal compressors Expired GB251659A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE251659X 1925-05-02

Publications (1)

Publication Number Publication Date
GB251659A true GB251659A (en) 1926-06-10

Family

ID=5944042

Family Applications (1)

Application Number Title Priority Date Filing Date
GB11456/26A Expired GB251659A (en) 1925-05-02 1926-04-30 Improvements in blades for centrifugal compressors

Country Status (1)

Country Link
GB (1) GB251659A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2254892A (en) * 1991-04-16 1992-10-21 Gen Electric Hollow airfoil.
US5253824A (en) * 1991-04-16 1993-10-19 General Electric Company Hollow core airfoil

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2254892A (en) * 1991-04-16 1992-10-21 Gen Electric Hollow airfoil.
US5253824A (en) * 1991-04-16 1993-10-19 General Electric Company Hollow core airfoil

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