DE1809621U - AXIAL FLOW CIRCULATION COMPRESSOR. - Google Patents

AXIAL FLOW CIRCULATION COMPRESSOR.

Info

Publication number
DE1809621U
DE1809621U DEB36965U DEB0036965U DE1809621U DE 1809621 U DE1809621 U DE 1809621U DE B36965 U DEB36965 U DE B36965U DE B0036965 U DEB0036965 U DE B0036965U DE 1809621 U DE1809621 U DE 1809621U
Authority
DE
Germany
Prior art keywords
axial flow
flow circulation
circulation compressor
compressor
axial
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
DEB36965U
Other languages
German (de)
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.)
BRISTOL AERO ENGINES Ltd
Original Assignee
BRISTOL AERO ENGINES Ltd
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
Priority to GB9764/58A priority Critical patent/GB894826A/en
Application filed by BRISTOL AERO ENGINES Ltd filed Critical BRISTOL AERO ENGINES Ltd
Publication of DE1809621U publication Critical patent/DE1809621U/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00Regulating or controlling by varying flow
    • F01D17/10Final actuators
    • F01D17/12Final actuators arranged in stator parts
    • F01D17/14Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/162Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line
    • 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
    • F04D29/40Casings; Connections of working fluid
    • F04D29/52Casings; Connections of working fluid for axial pumps
    • F04D29/54Fluid-guiding means, e.g. diffusers
    • F04D29/56Fluid-guiding means, e.g. diffusers adjustable
    • F04D29/563Fluid-guiding means, e.g. diffusers adjustable specially adapted for elastic fluid pumps
DEB36965U 1958-03-26 1959-03-25 AXIAL FLOW CIRCULATION COMPRESSOR. Expired DE1809621U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB9764/58A GB894826A (en) 1958-03-26 1958-03-26 Improvements in or relating to adjustable pitch guide blades in axial-flow compressors

Publications (1)

Publication Number Publication Date
DE1809621U true DE1809621U (en) 1960-04-14

Family

ID=9878340

Family Applications (1)

Application Number Title Priority Date Filing Date
DEB36965U Expired DE1809621U (en) 1958-03-26 1959-03-25 AXIAL FLOW CIRCULATION COMPRESSOR.

Country Status (4)

Country Link
US (1) US3056541A (en)
DE (1) DE1809621U (en)
FR (1) FR1229053A (en)
GB (1) GB894826A (en)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3271949A (en) * 1963-04-26 1966-09-13 Williams Res Corp Gas turbine
US3314595A (en) * 1965-06-09 1967-04-18 Gen Electric Adjustment mechanism for axial flow compressors
US4439983A (en) * 1978-11-13 1984-04-03 Gertz David C Inlet turbine powered exhaust extractor for internal combustion engines
US4299535A (en) * 1980-11-24 1981-11-10 The Trane Company Fan inlet guide vane assembly
US4718819A (en) * 1983-02-25 1988-01-12 Teledyne Industries, Inc. Variable geometry device for turbine compressor outlet
DE3722253C2 (en) * 1987-07-06 1989-09-21 Aktiengesellschaft Kuehnle, Kopp & Kausch, 6710 Frankenthal, De
GB8722714D0 (en) * 1987-09-26 1987-11-04 Rolls Royce Plc Variable guide vane arrangement for compressor
DE4117025A1 (en) * 1991-05-24 1992-11-26 Halberg Maschbau Gmbh & Co SWIRL REGULATOR FOR CENTRIFUGAL PUMPS
FR2890136B1 (en) * 2005-08-30 2007-11-09 Snecma Rod with an evolving length in operation
US20140314549A1 (en) * 2013-04-17 2014-10-23 General Electric Company Flow manipulating arrangement for a turbine exhaust diffuser
FR3031772B1 (en) * 2015-01-19 2017-01-13 Snecma VARIABLE TIMING AUB CONTROL SYSTEM FOR TURBOMACHINE
US20160258438A1 (en) * 2015-03-05 2016-09-08 Regal Beloit America, Inc. Assembly, blower and associated method
DE102016203025A1 (en) * 2016-02-26 2017-08-31 Bosch Mahle Turbo Systems Gmbh & Co. Kg Variable turbine geometry

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2393042A (en) * 1943-01-16 1946-01-15 B F Sturtevant Co Axial flow fan
US2388208A (en) * 1943-05-27 1945-10-30 B F Sturtevant Co Control vanes for fans
US2435092A (en) * 1944-11-01 1948-01-27 American Blower Corp Inlet vane control apparatus with vanes set at an angle
US2857092A (en) * 1951-05-25 1958-10-21 Gen Motors Corp Variable compressor vanes
US2793804A (en) * 1954-09-28 1957-05-28 Westinghouse Electric Corp Fans with spin vanes
US2858062A (en) * 1955-01-24 1958-10-28 Gen Electric Variable stator mechanism

Also Published As

Publication number Publication date
US3056541A (en) 1962-10-02
GB894826A (en) 1962-04-26
FR1229053A (en) 1960-09-02

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