SE7709870L - Termiskt kompenserad legesindikator for varierbart turbinmunstycke - Google Patents

Termiskt kompenserad legesindikator for varierbart turbinmunstycke

Info

Publication number
SE7709870L
SE7709870L SE7709870A SE7709870A SE7709870L SE 7709870 L SE7709870 L SE 7709870L SE 7709870 A SE7709870 A SE 7709870A SE 7709870 A SE7709870 A SE 7709870A SE 7709870 L SE7709870 L SE 7709870L
Authority
SE
Sweden
Prior art keywords
rotation
ring gear
vanes
potentiometer
link
Prior art date
Application number
SE7709870A
Other languages
Unknown language ( )
English (en)
Other versions
SE420857B (sv
Inventor
D E Gebhart
E G Meints
B C Smith
Original Assignee
Caterpillar Tractor Co
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 Caterpillar Tractor Co filed Critical Caterpillar Tractor Co
Publication of SE7709870L publication Critical patent/SE7709870L/sv
Publication of SE420857B publication Critical patent/SE420857B/sv

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/162—Final 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
SE7709870A 1976-10-01 1977-09-01 Termiskt kompenserad legesindikator for variebart turbinmunstycke SE420857B (sv)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/728,590 US4067661A (en) 1976-10-01 1976-10-01 Thermally compensated variable turbine nozzle position indicator

Publications (2)

Publication Number Publication Date
SE7709870L true SE7709870L (sv) 1978-04-02
SE420857B SE420857B (sv) 1981-11-02

Family

ID=24927471

Family Applications (1)

Application Number Title Priority Date Filing Date
SE7709870A SE420857B (sv) 1976-10-01 1977-09-01 Termiskt kompenserad legesindikator for variebart turbinmunstycke

Country Status (5)

Country Link
US (1) US4067661A (sv)
JP (1) JPS6056241B2 (sv)
CA (1) CA1062024A (sv)
GB (1) GB1532120A (sv)
SE (1) SE420857B (sv)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4563643A (en) * 1982-07-30 1986-01-07 Westinghouse Electric Corp. Eddy current proximity sensor for use in a hostile turbine environment
US4884944A (en) * 1988-09-07 1989-12-05 Avco Corporation Compressor flow fence
US5279110A (en) * 1992-06-12 1994-01-18 Lin Abraham S Double-rotor rotary engine and turbine
GB2410530A (en) * 2004-01-27 2005-08-03 Rolls Royce Plc Electrically actuated stator vane arrangement
US7137773B1 (en) * 2005-05-16 2006-11-21 Gm Global Technology Operations, Inc. Model-based statistical process to determine diagnostic limits in a sensor position system for a turbocharger
DE102007021483B4 (de) 2006-05-18 2022-08-04 Man Energy Solutions Se Leitapparat für einen Abgasturbolader einer mit Schweröl betriebenen Hubkolben-Brennkraftmaschine und Verfahren zur Funktionssicherung eines solchen Leitapparates
US8382436B2 (en) * 2009-01-06 2013-02-26 General Electric Company Non-integral turbine blade platforms and systems
US8262345B2 (en) * 2009-02-06 2012-09-11 General Electric Company Ceramic matrix composite turbine engine

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2265952A (en) * 1939-04-13 1941-12-09 Allis Chalmers Mfg Co Prime mover control system
BE486585A (sv) * 1948-01-07
US3013771A (en) * 1960-10-18 1961-12-19 Chrysler Corp Adjustable nozzles for gas turbine engine
US3841790A (en) * 1973-11-19 1974-10-15 Avco Corp Compressor flow fence
US3904309A (en) * 1974-08-12 1975-09-09 Caterpillar Tractor Co Variable angle turbine nozzle actuating mechanism
US4003675A (en) * 1975-09-02 1977-01-18 Caterpillar Tractor Co. Actuating mechanism for gas turbine engine nozzles

Also Published As

Publication number Publication date
JPS5344705A (en) 1978-04-21
US4067661A (en) 1978-01-10
JPS6056241B2 (ja) 1985-12-09
GB1532120A (en) 1978-11-15
SE420857B (sv) 1981-11-02
CA1062024A (en) 1979-09-11

Similar Documents

Publication Publication Date Title
US3314651A (en) Sealing device
US2488875A (en) Gas turbine engine
SE7713270L (sv) Turbinmunstycke med variabel geometrisk utformning
GB1345892A (en) Gas turbine engines
GB1466613A (en) Guide vane control for an automobile gas turbine engine
GB1235006A (en) Improvements in or relating to blading arrangements for turbo-machines
JPH03271503A (ja) ブレード先端クリアランス制御装置
SE7709870L (sv) Termiskt kompenserad legesindikator for varierbart turbinmunstycke
US3736070A (en) Variable stator blade assembly for axial flow, fluid expansion engine
GB1453519A (en) Apparatus for varying the stagger angle of the fan blades of a rotor wheel of a gas turbine ducted fan engine
CA1039658A (en) Actuating mechanism for gas turbine engine nozzles
GB1067930A (en) Vane operating mechanism for fluid flow machines
GB1368353A (en) Actuation ring for variable geometry axial flow compressors
KR860003408A (ko) 고압 레이디알 터빈 및 유사장치용 조정가능한 고정자 메카니즘
GB753316A (en) Improvements relating to radial-flow turbines or compressors
US2955744A (en) Compressor
KR930021928A (ko) 축류 터빈
US3030006A (en) Circumferential bleed valve
JPS5813722B2 (ja) タ−ボ機械の調節自在羽根のための作動装置
US2932440A (en) Compressor blade adjustment means
GB737473A (en) Turbines and like machines having adjustable guide blades
US4344736A (en) Sealing device
GB737472A (en) Turbines and like machines having adjustable guide blades
US746388A (en) Steam-turbine.
US760106A (en) Elastic-fluid turbine.

Legal Events

Date Code Title Description
NUG Patent has lapsed

Ref document number: 7709870-5

Effective date: 19930406

Format of ref document f/p: F