PL3447269T3 - Sposób i układ ograniczania mocy silnika turbospalinowego - Google Patents

Sposób i układ ograniczania mocy silnika turbospalinowego

Info

Publication number
PL3447269T3
PL3447269T3 PL18190084.6T PL18190084T PL3447269T3 PL 3447269 T3 PL3447269 T3 PL 3447269T3 PL 18190084 T PL18190084 T PL 18190084T PL 3447269 T3 PL3447269 T3 PL 3447269T3
Authority
PL
Poland
Prior art keywords
gas turbine
turbine engine
limiting power
limiting
power
Prior art date
Application number
PL18190084.6T
Other languages
English (en)
Inventor
Sylvain Lamarre
Simon Lopez
Nicolas DES ROCHES-DIONNE
Michael Conciatori
Original Assignee
Pratt & Whitney Canada Corp.
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 Pratt & Whitney Canada Corp. filed Critical Pratt & Whitney Canada Corp.
Publication of PL3447269T3 publication Critical patent/PL3447269T3/pl

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/76—Control or regulation of thrust reversers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/30—Blade pitch-changing mechanisms
    • B64C11/305—Blade pitch-changing mechanisms characterised by being influenced by other control systems, e.g. fuel supply
    • 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
    • F02C9/44—Control of fuel supply responsive to the speed of aircraft, e.g. Mach number control, optimisation of fuel consumption
    • 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
    • F02C9/48—Control of fuel supply conjointly with another control of the plant
    • F02C9/56—Control of fuel supply conjointly with another control of the plant with power transmission control
    • F02C9/58—Control of fuel supply conjointly with another control of the plant with power transmission control with control of a variable-pitch propeller
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/15—Control or regulation
    • F02K1/16—Control or regulation conjointly with another control
    • F02K1/17—Control or regulation conjointly with another control with control of fuel supply
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/64—Reversing fan flow
    • F02K1/66—Reversing fan flow using reversing fan blades
    • 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
    • F05D2270/05—Purpose of the control system to affect the output of the engine
    • F05D2270/053—Explicitly mentioned power

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Turbines (AREA)
  • Operation Control Of Excavators (AREA)
PL18190084.6T 2017-08-21 2018-08-21 Sposób i układ ograniczania mocy silnika turbospalinowego PL3447269T3 (pl)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US15/681,531 US10823113B2 (en) 2017-08-21 2017-08-21 Method and system for limiting power of an engine

Publications (1)

Publication Number Publication Date
PL3447269T3 true PL3447269T3 (pl) 2024-10-14

Family

ID=63350472

Family Applications (1)

Application Number Title Priority Date Filing Date
PL18190084.6T PL3447269T3 (pl) 2017-08-21 2018-08-21 Sposób i układ ograniczania mocy silnika turbospalinowego

Country Status (4)

Country Link
US (1) US10823113B2 (pl)
EP (1) EP3447269B1 (pl)
CA (1) CA3013601A1 (pl)
PL (1) PL3447269T3 (pl)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11414175B2 (en) * 2019-04-01 2022-08-16 Pratt & Whitney Canada Corp. Method and system for operating an aircraft powerplant
US12078074B2 (en) * 2019-05-13 2024-09-03 Pratt & Whitney Canada Corp. System and method for detecting an uncommanded or uncontrollable high thrust event in an aircraft
US20210070458A1 (en) * 2019-09-06 2021-03-11 Hamilton Sundstrand Corporation Vortex turbines for a hybrid-electric aircraft
US11668253B2 (en) * 2020-10-16 2023-06-06 Pratt & Whitney Canada Corp. System and method for providing in-flight reverse thrust for an aircraft
US11719167B2 (en) * 2021-04-01 2023-08-08 Pratt & Whitney Canada Corp. Operating a turboprop engine for in-flight restart
CN113586277A (zh) * 2021-07-21 2021-11-02 上海外高桥造船有限公司 船上主机功率限制系统及方法
US12006883B2 (en) 2022-02-04 2024-06-11 Pratt & Whitney Canada Corp. Method and system of operating an airplane engine

Family Cites Families (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2640550A (en) * 1948-07-24 1953-06-02 Curtiss Wright Corp Turbine propeller control system
US2737252A (en) * 1950-06-01 1956-03-06 Curtiss Wright Corp Turbine propeller control system
US3936226A (en) 1974-06-07 1976-02-03 United Technologies Corporation Control system for variable pitch fan propulsor with reverse pitch
US4258545A (en) 1978-06-15 1981-03-31 General Electric Company Optimal control for a gas turbine engine
US4958289A (en) * 1988-12-14 1990-09-18 General Electric Company Aircraft propeller speed control
GB0027288D0 (en) 2000-11-08 2000-12-27 Rolls Royce Plc Overthrust protection system and method
US6578794B1 (en) 2000-11-28 2003-06-17 General Electric Co. Methods and systems for jet engine overthrust protection
US6704630B2 (en) 2002-04-04 2004-03-09 Grazyna Balut Ostrom Thrust control malfunction accommodation system and method
DE10302074A1 (de) 2003-01-21 2004-07-29 Rolls-Royce Deutschland Ltd & Co Kg Fehlerdetektionslogik für Triebwerke
US8651811B2 (en) 2005-11-16 2014-02-18 Hamilton Sundstrand Control logic for a propeller system
US8414260B2 (en) 2006-07-25 2013-04-09 Lockheed Martin Corporation Control system for controlling propeller aircraft engine during takeoff
US8954228B2 (en) 2008-12-30 2015-02-10 Rolls-Royce Corporation Gas turbine engine failure detection
GB201201093D0 (en) 2012-01-24 2012-03-07 Rolls Royce Plc Improvements in or relating to control systems for machines
FR2996254B1 (fr) 2012-10-03 2014-09-12 Snecma Methode de surveillance d'un defaut de poussee d'un turboreacteur d'aeronef
GB201301791D0 (en) 2013-02-01 2013-03-20 Rolls Royce Engine Control Systems Ltd Engine fuel control system
GB201313142D0 (en) 2013-07-23 2013-09-04 Rolls Royce Engine Control Systems Ltd Engine Fuel Control System
GB201412189D0 (en) 2014-07-09 2014-08-20 Rolls Royce Plc A nozzle arrangement for a gas turbine engine
EP3018054B1 (en) 2014-11-07 2019-01-02 Airbus Defence and Space, S.A. Method for controlling an aircraft propeller system during thrust reversal
US9494085B2 (en) 2015-01-19 2016-11-15 United Technologies Corporation System and method for load power management in a turboshaft gas turbine engine
US10487752B2 (en) 2015-03-11 2019-11-26 Pratt & Whitney Canada Corp. Overthrust protection system and method
US9932906B2 (en) 2015-09-23 2018-04-03 Honeywell International Inc. Gas turbine engine uncontrolled high thrust detection system and method
US9771878B2 (en) * 2015-10-19 2017-09-26 General Electric Company Thrust scheduling method for variable pitch fan engines and turbo-shaft, turbo-propeller engines
US10279918B2 (en) 2016-08-31 2019-05-07 The Boeing Company Methods and apparatus to control thrust ramping of an aircraft engine

Also Published As

Publication number Publication date
EP3447269A1 (en) 2019-02-27
US20190055901A1 (en) 2019-02-21
CA3013601A1 (en) 2019-02-21
EP3447269B1 (en) 2024-07-31
US10823113B2 (en) 2020-11-03

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