GB191208713A - Improvements in Centrifugal Pumps and Compressors. - Google Patents

Improvements in Centrifugal Pumps and Compressors.

Info

Publication number
GB191208713A
GB191208713A GB191208713DA GB191208713A GB 191208713 A GB191208713 A GB 191208713A GB 191208713D A GB191208713D A GB 191208713DA GB 191208713 A GB191208713 A GB 191208713A
Authority
GB
United Kingdom
Prior art keywords
disk
point
section
blades
line
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
Inventor
Albert Huguenin
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Application granted granted Critical
Publication of GB191208713A publication Critical patent/GB191208713A/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
    • F04D29/18Rotors
    • F04D29/22Rotors specially for centrifugal pumps
    • F04D29/2205Conventional flow pattern
    • F04D29/2216Shape, geometry

Abstract

8713. Huguenin, A. April 12, 1911, [Convention date]. Balancing moving parts.-Rotors for centrifugal pumps and compressors of the type wherein the blades are mounted on one side of the rotor disk are so constructed that the generating-line A B C, Fig. 1, of the medical section of the rotor disk a is oblique to the axis x, x to an extent such that the bending strains due to the action of centrifugal force on the blades b and on the disk a substantially neutralize each other. In small disks and in disks which do not rotate at a very high speed, the generating line ABC is straight, but in high speed disks the medial line A B C is curved away from the side carrying the blades so that the inclination of the line A B C to the normal A C, increases as it approaches the periphery of the disk. The blades b, Fig. 3, are preferably of T section, and may be screwed or riveted to the disk. Considering the centrifugal bending strains produced at any cylindric section y, y of the rotor, let the centre of gravity of that portion of the blade lying outside this cylindric section be at the point S1, and the centre of gravity of that portion of the disk section lying outside the cylindric section be at the point S2. The centrifugal force at unit angular velocity on the portion of blade in question is F1 acting at the point S, and on the portion of the rotor is F2 acting at the point S2, and the inclination of the medial line A B C is such that the moments of the forces above the point B are equal.
GB191208713D 1911-04-12 1912-04-12 Improvements in Centrifugal Pumps and Compressors. Expired GB191208713A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE191208713X 1911-04-12

Publications (1)

Publication Number Publication Date
GB191208713A true GB191208713A (en) 1912-11-21

Family

ID=32604254

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191208713D Expired GB191208713A (en) 1911-04-12 1912-04-12 Improvements in Centrifugal Pumps and Compressors.

Country Status (1)

Country Link
GB (1) GB191208713A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3976396A (en) * 1974-01-07 1976-08-24 Enrico Antogini Device for converting fluid flow into kinetic energy
CN103348142A (en) * 2010-12-03 2013-10-09 Ihc荷兰Ie有限公司 Centrifugal pump and a double bent rotor blade for use in such a centrifugal pump
CN112032105A (en) * 2020-11-05 2020-12-04 中国航发上海商用航空发动机制造有限责任公司 Rotor blade tip clearance control method and rotor blade manufactured by using same

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3976396A (en) * 1974-01-07 1976-08-24 Enrico Antogini Device for converting fluid flow into kinetic energy
CN103348142A (en) * 2010-12-03 2013-10-09 Ihc荷兰Ie有限公司 Centrifugal pump and a double bent rotor blade for use in such a centrifugal pump
CN112032105A (en) * 2020-11-05 2020-12-04 中国航发上海商用航空发动机制造有限责任公司 Rotor blade tip clearance control method and rotor blade manufactured by using same

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