FR1185633A - Perfectionnement aux moteurs à turbine à gaz - Google Patents

Perfectionnement aux moteurs à turbine à gaz

Info

Publication number
FR1185633A
FR1185633A FR1185633DA FR1185633A FR 1185633 A FR1185633 A FR 1185633A FR 1185633D A FR1185633D A FR 1185633DA FR 1185633 A FR1185633 A FR 1185633A
Authority
FR
France
Prior art keywords
development
gas turbine
turbine engines
engines
gas
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
Other languages
English (en)
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Application granted granted Critical
Publication of FR1185633A publication Critical patent/FR1185633A/fr
Expired 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
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
    • F01D21/06—Shutting-down
    • 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
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/14—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to other specific conditions
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/06—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Control Of Turbines (AREA)
FR1185633D 1956-11-08 1957-10-31 Perfectionnement aux moteurs à turbine à gaz Expired FR1185633A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB34217/56A GB837309A (en) 1956-11-08 1956-11-08 Improvements in or relating to gas-turbine engines

Publications (1)

Publication Number Publication Date
FR1185633A true FR1185633A (fr) 1959-08-03

Family

ID=10362852

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1185633D Expired FR1185633A (fr) 1956-11-08 1957-10-31 Perfectionnement aux moteurs à turbine à gaz

Country Status (4)

Country Link
US (1) US2930188A (fr)
DE (1) DE1072014B (fr)
FR (1) FR1185633A (fr)
GB (1) GB837309A (fr)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3159166A (en) * 1961-10-16 1964-12-01 Gen Motors Corp Engine safety control
US3498282A (en) * 1967-12-21 1970-03-03 Donald P Dattilo Mechanism for automatically stopping internal combustion engines
FR2317501A1 (fr) * 1975-07-09 1977-02-04 Snecma Dispositif d'accouplement pour moteur a turbine a gaz
US4389984A (en) * 1981-03-26 1983-06-28 Destrampe Terry G Post-shutdown coolant-supply device
GB2124788B (en) * 1982-06-30 1986-05-21 Rolls Royce Torque-sensitive control of gas turbines
DE4341445A1 (de) * 1993-12-06 1995-06-08 Bmw Rolls Royce Gmbh Mechanisches shut-off-system für eine Gasturbine
US6607349B2 (en) * 2001-11-14 2003-08-19 Honeywell International, Inc. Gas turbine engine broken shaft detection system
US7654093B2 (en) * 2005-09-26 2010-02-02 Pratt & Whitney Canada Corp. Method of adjusting a triggering clearance and a trigger
US8567564B2 (en) * 2008-03-20 2013-10-29 United Technologies Corporation Non-interrupted oil supply for gas turbine engine
CA2760454C (fr) 2010-12-03 2019-02-19 Pratt & Whitney Canada Corp. Element de confinement de rotor turbine a gaz
US10316689B2 (en) 2016-08-22 2019-06-11 Rolls-Royce Corporation Gas turbine engine health monitoring system with shaft-twist sensors
EP3382160B1 (fr) 2017-03-28 2020-10-21 Ge Avio S.r.l. Système de rotation de moteur à turbine à gaz et sa méthode de fonctionnement

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2551429A (en) * 1948-11-19 1951-05-01 Ingersoll Rand Co Safety trip device for motors responsive to temperature, speed, and pressure
US2693248A (en) * 1950-05-03 1954-11-02 Gen Motors Corp Lubrication system
US2676458A (en) * 1951-09-17 1954-04-27 Boeing Co Gas turbine combined lubricating, and fuel supply system having centrifugal means topurify and circulate fuel

Also Published As

Publication number Publication date
US2930188A (en) 1960-03-29
GB837309A (en) 1960-06-09
DE1072014B (fr) 1959-12-24

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