JPS5050511A - - Google Patents

Info

Publication number
JPS5050511A
JPS5050511A JP10032173A JP10032173A JPS5050511A JP S5050511 A JPS5050511 A JP S5050511A JP 10032173 A JP10032173 A JP 10032173A JP 10032173 A JP10032173 A JP 10032173A JP S5050511 A JPS5050511 A JP S5050511A
Authority
JP
Japan
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.)
Pending
Application number
JP10032173A
Other languages
Japanese (ja)
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
Priority to JP10032173A priority Critical patent/JPS5050511A/ja
Priority to GB3824974A priority patent/GB1466613A/en
Publication of JPS5050511A publication Critical patent/JPS5050511A/ja
Pending legal-status Critical Current

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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Control Of Turbines (AREA)
  • Supercharger (AREA)
JP10032173A 1973-09-07 1973-09-07 Pending JPS5050511A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
JP10032173A JPS5050511A (en) 1973-09-07 1973-09-07
GB3824974A GB1466613A (en) 1973-09-07 1974-09-02 Guide vane control for an automobile gas turbine engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP10032173A JPS5050511A (en) 1973-09-07 1973-09-07

Publications (1)

Publication Number Publication Date
JPS5050511A true JPS5050511A (en) 1975-05-07

Family

ID=14270906

Family Applications (1)

Application Number Title Priority Date Filing Date
JP10032173A Pending JPS5050511A (en) 1973-09-07 1973-09-07

Country Status (2)

Country Link
JP (1) JPS5050511A (en)
GB (1) GB1466613A (en)

Families Citing this family (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2688827B1 (en) * 1992-03-18 1994-05-06 Snecma VARIABLE SETTING STATOR VANE CONTROL SYSTEM FOR A TURBOREACTOR.
FR2708311B1 (en) * 1993-07-28 1995-09-01 Snecma Turbomachine stator with pivoting vanes and control ring.
GB2301868B (en) * 1995-06-05 1999-08-11 Rolls Royce Plc Improved actuator mechanism for variable angle vane arrays
GB9511269D0 (en) * 1995-06-05 1995-08-02 Rolls Royce Plc Variable angle vane arrays
US5895204A (en) * 1997-08-06 1999-04-20 Carrier Corporation Drive positioning mechanism for a variable pipe diffuser
US5988977A (en) * 1997-08-06 1999-11-23 Carrier Corporation Backlash adjustment mechanism for variable pipe diffuser
US7854112B2 (en) 2004-12-01 2010-12-21 United Technologies Corporation Vectoring transition duct for turbine engine
US8096753B2 (en) 2004-12-01 2012-01-17 United Technologies Corporation Tip turbine engine and operating method with reverse core airflow
EP1825177B1 (en) 2004-12-01 2012-01-25 United Technologies Corporation Inflatable bleed valve for turbine engine and method of controlling bleed air
EP1828683B1 (en) 2004-12-01 2013-04-10 United Technologies Corporation Combustor for turbine engine
DE602004028297D1 (en) 2004-12-01 2010-09-02 United Technologies Corp COMPREHENSIVE COMBUSTION CHAMBER FOR TOP TURBINE ENGINE
WO2006059999A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Plurality of individually controlled inlet guide vanes in a turbofan engine and corresponding controlling method
EP1825116A2 (en) 2004-12-01 2007-08-29 United Technologies Corporation Ejector cooling of outer case for tip turbine engine
WO2006059985A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Axial compressor for tip turbine engine
WO2006059968A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Counter-rotating gearbox for tip turbine engine
DE602004016065D1 (en) 2004-12-01 2008-10-02 United Technologies Corp VARIABLE BULB INLET BUCKET ASSEMBLY, TURBINE ENGINE WITH SUCH AN ARRANGEMENT AND CORRESPONDING STEERING PROCEDURE
EP1825117B1 (en) 2004-12-01 2012-06-13 United Technologies Corporation Turbine engine with differential gear driven fan and compressor
US7934902B2 (en) 2004-12-01 2011-05-03 United Technologies Corporation Compressor variable stage remote actuation for turbine engine
US8967945B2 (en) 2007-05-22 2015-03-03 United Technologies Corporation Individual inlet guide vane control for tip turbine engine
US8240983B2 (en) * 2007-10-22 2012-08-14 United Technologies Corp. Gas turbine engine systems involving gear-driven variable vanes
EP2206891A1 (en) * 2009-01-13 2010-07-14 Siemens Aktiengesellschaft Nozzle vane adjustment device
US9243648B2 (en) 2009-07-20 2016-01-26 Ingersoll-Rand Company Removable throat mounted inlet guide vane
EP2496839B1 (en) 2009-11-03 2017-01-04 Ingersoll-Rand Company Inlet guide vane for a compressor
EP2362071A1 (en) 2010-02-19 2011-08-31 Siemens Aktiengesellschaft Drive device for pivoting adjustable vanes of a turbomachine
EP2362070A1 (en) 2010-02-19 2011-08-31 Siemens Aktiengesellschaft Drive device for pivoting adjustable vanes of a turbomachine
US10329947B2 (en) 2016-03-24 2019-06-25 United Technologies Corporation 35Geared unison ring for multi-stage variable vane actuation
US10443431B2 (en) 2016-03-24 2019-10-15 United Technologies Corporation Idler gear connection for multi-stage variable vane actuation
US10458271B2 (en) 2016-03-24 2019-10-29 United Technologies Corporation Cable drive system for variable vane operation
US10301962B2 (en) 2016-03-24 2019-05-28 United Technologies Corporation Harmonic drive for shaft driving multiple stages of vanes via gears
US10415596B2 (en) 2016-03-24 2019-09-17 United Technologies Corporation Electric actuation for variable vanes
US10294813B2 (en) * 2016-03-24 2019-05-21 United Technologies Corporation Geared unison ring for variable vane actuation
US10190599B2 (en) 2016-03-24 2019-01-29 United Technologies Corporation Drive shaft for remote variable vane actuation
US10288087B2 (en) 2016-03-24 2019-05-14 United Technologies Corporation Off-axis electric actuation for variable vanes
US10443430B2 (en) 2016-03-24 2019-10-15 United Technologies Corporation Variable vane actuation with rotating ring and sliding links
US10329946B2 (en) * 2016-03-24 2019-06-25 United Technologies Corporation Sliding gear actuation for variable vanes

Also Published As

Publication number Publication date
GB1466613A (en) 1977-03-09

Similar Documents

Publication Publication Date Title
AR201758A1 (en)
AU476761B2 (en)
AU465372B2 (en)
AR201235Q (en)
AR201231Q (en)
AU474593B2 (en)
AU474511B2 (en)
AU474838B2 (en)
AU465453B2 (en)
AU471343B2 (en)
AU465434B2 (en)
AU450229B2 (en)
AU476714B2 (en)
AR201229Q (en)
AU466283B2 (en)
AR199451A1 (en)
AU476696B2 (en)
AU472848B2 (en)
AU477823B2 (en)
AR193950A1 (en)
AU476873B1 (en)
AR200256A1 (en)
AU461342B2 (en)
AR210729A1 (en)
AU477824B2 (en)