GB701470A - Improvements relating to gas blowers and compressors - Google Patents

Improvements relating to gas blowers and compressors

Info

Publication number
GB701470A
GB701470A GB22799/51A GB2279951A GB701470A GB 701470 A GB701470 A GB 701470A GB 22799/51 A GB22799/51 A GB 22799/51A GB 2279951 A GB2279951 A GB 2279951A GB 701470 A GB701470 A GB 701470A
Authority
GB
United Kingdom
Prior art keywords
gas
chamber
annular
channel
turbine
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
GB22799/51A
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.)
Sulzer AG
Original Assignee
Sulzer AG
Gebrueder Sulzer AG
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 Sulzer AG, Gebrueder Sulzer AG filed Critical Sulzer AG
Publication of GB701470A publication Critical patent/GB701470A/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
    • F04D29/70—Suction grids; Strainers; Dust separation; Cleaning
    • F04D29/701—Suction grids; Strainers; Dust separation; Cleaning especially adapted for elastic fluid pumps

Abstract

701,470. Centrifugal separators. SULZER FRERES SOC. ANON. Oct. 1, 1951 [Oct. 31, 1950], No. 22799/51. Class 23 [Also in Group XXVI] A gas blower or compressor 1 driven by a gas turbine 15 has in its intake 3 a centrifugal separator comprising means 5 for rotating the gas, an annular channel 2 for the rotating gas, a channel 10 leading the gas towards the axis of rotation, an aperture 12 at the junction of the channels leading particles separated from the rotating gas to a collection chamber 13, and a connection 16 between the chamber and the exhaust pipe 17 of the turbine such that the turbine exhaust gases extract the particles from the chamber. Guide blades 11 are provided in the channel 10 which is annular in form. As shown the aperture and the collection chamber are annular, but a number of apertures may lead to separate collection chambers.
GB22799/51A 1950-10-31 1951-10-01 Improvements relating to gas blowers and compressors Expired GB701470A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH701470X 1950-10-31

Publications (1)

Publication Number Publication Date
GB701470A true GB701470A (en) 1953-12-23

Family

ID=4530059

Family Applications (1)

Application Number Title Priority Date Filing Date
GB22799/51A Expired GB701470A (en) 1950-10-31 1951-10-01 Improvements relating to gas blowers and compressors

Country Status (1)

Country Link
GB (1) GB701470A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1789683B1 (en) * 2004-08-30 2010-06-02 Honeywell International Inc. Compressor and inlet separation system

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1789683B1 (en) * 2004-08-30 2010-06-02 Honeywell International Inc. Compressor and inlet separation system

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