BE704511A - - Google Patents

Info

Publication number
BE704511A
BE704511A BE704511DA BE704511A BE 704511 A BE704511 A BE 704511A BE 704511D A BE704511D A BE 704511DA BE 704511 A BE704511 A BE 704511A
Authority
BE
Belgium
Application number
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 filed Critical
Publication of BE704511A publication Critical patent/BE704511A/xx

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D27/00Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/02Surge control
    • F04D27/0246Surge control by varying geometry within the pumps, e.g. by adjusting vanes
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/206Flow affected by fluid contact, energy field or coanda effect [e.g., pure fluid device or system]
    • Y10T137/2065Responsive to condition external of system
    • Y10T137/2071And causing change or correction of sensed condition
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/206Flow affected by fluid contact, energy field or coanda effect [e.g., pure fluid device or system]
    • Y10T137/212System comprising plural fluidic devices or stages
    • Y10T137/2125Plural power inputs [e.g., parallel inputs]
    • Y10T137/2147To cascaded plural devices
BE704511D 1967-01-03 1967-09-29 BE704511A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US606757A US3403842A (en) 1967-01-03 1967-01-03 Stall prevention in axial flow compressors

Publications (1)

Publication Number Publication Date
BE704511A true BE704511A (fr) 1968-02-01

Family

ID=24429325

Family Applications (1)

Application Number Title Priority Date Filing Date
BE704511D BE704511A (fr) 1967-01-03 1967-09-29

Country Status (4)

Country Link
US (1) US3403842A (fr)
BE (1) BE704511A (fr)
DE (1) DE1628269A1 (fr)
GB (1) GB1167387A (fr)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3514212A (en) * 1968-06-11 1970-05-26 Us Air Force Incipient stall sensor
US3566900A (en) * 1969-03-03 1971-03-02 Avco Corp Fuel control system and viscosity sensor used therewith
US3677000A (en) * 1970-04-27 1972-07-18 Faulkner C Thomson System for the detection and control of compressor stall
CS175129B1 (fr) * 1975-02-11 1977-04-29
DE2645895C2 (de) * 1976-02-10 1986-06-26 Nordisk Ventilator Co. A/S, Naestved Vorrichtung zur Erkennung des Arbeitens von Axialgebläsen im Abreißgebiet
US4252498A (en) * 1978-03-14 1981-02-24 Rolls-Royce Limited Control systems for multi-stage axial flow compressors
GB2208894A (en) * 1987-08-18 1989-04-19 Rolls Royce Plc Gas turbine engine compressor stall recovery
US7762084B2 (en) * 2004-11-12 2010-07-27 Rolls-Royce Canada, Ltd. System and method for controlling the working line position in a gas turbine engine compressor
US7762078B2 (en) * 2006-09-13 2010-07-27 Aerojet-General Corporation Nozzle with temperature-responsive throat diameter
FR3063782B1 (fr) * 2017-03-07 2021-06-18 Safran Aircraft Engines Procede et dispositif de detection de conditions propices a l'apparition d'un pompage en vue de proteger un compresseur d'une turbomachine d'aeronef

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2455292A (en) * 1944-04-13 1948-11-30 Chrysler Corp Control apparatus
US2390043A (en) * 1944-04-13 1945-12-04 Chrysler Corp Control apparatus
US3248043A (en) * 1963-06-25 1966-04-26 Bendix Corp Fluid pulse surge control indicator
CH419425A (de) * 1964-08-07 1966-08-31 Bbc Brown Boveri & Cie Einrichtung zur Regelung eines Turboverdichters

Also Published As

Publication number Publication date
US3403842A (en) 1968-10-01
GB1167387A (en) 1969-10-15
DE1628269A1 (de) 1971-04-29

Similar Documents

Publication Publication Date Title
AU425114B2 (fr)
AT298283B (fr)
AU416737B2 (fr)
AU2277767A (fr)
AU342066A (fr)
AU610966A (fr)
AU3151267A (fr)
AU1273466A (fr)
AU2116667A (fr)
AU2454867A (fr)
AU2256867A (fr)
AU2528767A (fr)
AU2977667A (fr)
AU3189468A (fr)
AU1868267A (fr)
BE609869A (fr)
AU25066A (fr)
AU34866A (fr)
AU408412B2 (fr)
AU1763766A (fr)
AU1677166A (fr)
AU459699A (fr)
BE692492A (fr)
BE692199A (fr)
AU97666A (fr)