GB2314383B - Process for regulating a turbojet engine - Google Patents

Process for regulating a turbojet engine

Info

Publication number
GB2314383B
GB2314383B GB9712842A GB9712842A GB2314383B GB 2314383 B GB2314383 B GB 2314383B GB 9712842 A GB9712842 A GB 9712842A GB 9712842 A GB9712842 A GB 9712842A GB 2314383 B GB2314383 B GB 2314383B
Authority
GB
United Kingdom
Prior art keywords
regulating
turbojet engine
turbojet
engine
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 - Lifetime
Application number
GB9712842A
Other versions
GB9712842D0 (en
GB2314383A (en
Inventor
Joachim Dr Kurzke
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.)
MTU Aero Engines GmbH
Original Assignee
MTU Motoren und Turbinen Union Muenchen GmbH
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 MTU Motoren und Turbinen Union Muenchen GmbH filed Critical MTU Motoren und Turbinen Union Muenchen GmbH
Publication of GB9712842D0 publication Critical patent/GB9712842D0/en
Publication of GB2314383A publication Critical patent/GB2314383A/en
Application granted granted Critical
Publication of GB2314383B publication Critical patent/GB2314383B/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/28—Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/11—Purpose of the control system to prolong engine life
    • F05D2270/112—Purpose of the control system to prolong engine life by limiting temperatures
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/303—Temperature
GB9712842A 1996-06-18 1997-06-18 Process for regulating a turbojet engine Expired - Lifetime GB2314383B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE1996124171 DE19624171C1 (en) 1996-06-18 1996-06-18 Process for controlling a turbo jet engine

Publications (3)

Publication Number Publication Date
GB9712842D0 GB9712842D0 (en) 1997-08-20
GB2314383A GB2314383A (en) 1997-12-24
GB2314383B true GB2314383B (en) 2000-01-19

Family

ID=7797192

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9712842A Expired - Lifetime GB2314383B (en) 1996-06-18 1997-06-18 Process for regulating a turbojet engine

Country Status (3)

Country Link
DE (1) DE19624171C1 (en)
FR (1) FR2749884B1 (en)
GB (1) GB2314383B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA2627904C (en) 2005-11-01 2013-08-20 Vestas Wind Systems A/S A method for prolonging and/or controlling the life of one or more heat generating and/or passive components in a wind turbine, a wind turbine, and use hereof

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2175048A (en) * 1985-05-06 1986-11-19 Gen Electric Blade cooling control arrangement

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DD18361A (en) *
GB1228949A (en) * 1968-10-16 1971-04-21
US5197280A (en) * 1989-03-20 1993-03-30 General Electric Company Control system and method for controlling a gas turbine engine
US5267435A (en) * 1992-08-18 1993-12-07 General Electric Company Thrust droop compensation method and system
DE59307747D1 (en) * 1993-09-06 1998-01-08 Asea Brown Boveri Method for controlling a gas turbine group equipped with two combustion chambers
US5596871A (en) * 1995-05-31 1997-01-28 Alliedsignal Inc. Deceleration fuel control system for a turbine engine

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2175048A (en) * 1985-05-06 1986-11-19 Gen Electric Blade cooling control arrangement

Also Published As

Publication number Publication date
GB9712842D0 (en) 1997-08-20
FR2749884A1 (en) 1997-12-19
DE19624171C1 (en) 1998-01-08
FR2749884B1 (en) 2000-07-07
GB2314383A (en) 1997-12-24

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GB2314383B (en) Process for regulating a turbojet engine

Legal Events

Date Code Title Description
PE20 Patent expired after termination of 20 years

Expiry date: 20170617