PL3770408T3 - Układ i sposób obsługi silnika turbośmigłowego - Google Patents
Układ i sposób obsługi silnika turbośmigłowegoInfo
- Publication number
- PL3770408T3 PL3770408T3 PL20187537.4T PL20187537T PL3770408T3 PL 3770408 T3 PL3770408 T3 PL 3770408T3 PL 20187537 T PL20187537 T PL 20187537T PL 3770408 T3 PL3770408 T3 PL 3770408T3
- Authority
- PL
- Poland
- Prior art keywords
- operating
- turboprop engine
- turboprop
- engine
- Prior art date
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
- F02C9/48—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
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
- B64D31/02—Initiating means
- B64D31/06—Initiating means actuated automatically
-
- 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
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2270/00—Control
- F05B2270/10—Purpose of the control system
- F05B2270/103—Purpose of the control system to affect the output of the engine
- F05B2270/1031—Thrust
-
- 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
- F05D2270/02—Purpose of the control system to control rotational speed (n)
-
- 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
- F05D2270/051—Thrust
-
- 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
- F05D2270/052—Torque
-
- 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
-
- 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
- F05D2270/304—Spool rotational 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
- F05D2270/30—Control parameters, e.g. input parameters
- F05D2270/335—Output power or torque
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
- Control Of Eletrric Generators (AREA)
- Testing Of Engines (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US201962879066P | 2019-07-26 | 2019-07-26 | |
| US16/551,177 US12435674B2 (en) | 2019-07-26 | 2019-08-26 | System and method for operating a turboprop engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| PL3770408T3 true PL3770408T3 (pl) | 2024-02-12 |
Family
ID=71783974
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PL20187537.4T PL3770408T3 (pl) | 2019-07-26 | 2020-07-23 | Układ i sposób obsługi silnika turbośmigłowego |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US12435674B2 (pl) |
| EP (1) | EP3770408B1 (pl) |
| CA (1) | CA3085690A1 (pl) |
| PL (1) | PL3770408T3 (pl) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| BE1028543B1 (fr) * | 2020-08-14 | 2022-03-14 | Safran Aero Boosters | Méthode et système de régulation de poussée d’une turbomachine d’aéronef |
| US12606313B2 (en) * | 2022-03-29 | 2026-04-21 | Pratt & Whitney Canada Corp. | Aircraft powerplant(s) for an aircraft with electric machine controlled propulsor speed |
Family Cites Families (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4432201A (en) * | 1981-01-14 | 1984-02-21 | Aviation Electric Ltd. | Acceleration limit reset |
| US4625510A (en) * | 1981-04-24 | 1986-12-02 | Bendix Avelex Inc. | Stress limiter apparatus for a gas turbine engine |
| US4958289A (en) * | 1988-12-14 | 1990-09-18 | General Electric Company | Aircraft propeller speed control |
| US8651811B2 (en) * | 2005-11-16 | 2014-02-18 | Hamilton Sundstrand | Control logic for a propeller system |
| FR2986506B1 (fr) * | 2012-02-06 | 2015-06-26 | Eurocopter France | Procede et dispositif pour realiser un controle de sante d'un turbomoteur d'un aeronef pourvu d'au moins un turbomoteur |
| US9494085B2 (en) | 2015-01-19 | 2016-11-15 | United Technologies Corporation | System and method for load power management in a turboshaft gas turbine engine |
| US10040565B2 (en) | 2015-09-22 | 2018-08-07 | Honeywell International Inc. | Single lever turboprop control systems and methods utilizing torque-based and power based scheduling |
| US10584646B2 (en) | 2016-07-29 | 2020-03-10 | Pratt & Whitney Canada Corp. | System and method for control of gas turbine engine |
| US10604268B2 (en) | 2017-02-22 | 2020-03-31 | Pratt & Whitney Canada Corp. | Autothrottle control for turboprop engines |
| US10718231B2 (en) * | 2017-12-15 | 2020-07-21 | General Electric Company | Method and system for mitigating bowed rotor operation of gas turbine engine |
| US11162382B2 (en) * | 2019-02-21 | 2021-11-02 | General Electric Company | Method and system for engine operation |
-
2019
- 2019-08-26 US US16/551,177 patent/US12435674B2/en active Active
-
2020
- 2020-07-03 CA CA3085690A patent/CA3085690A1/en active Pending
- 2020-07-23 EP EP20187537.4A patent/EP3770408B1/en active Active
- 2020-07-23 PL PL20187537.4T patent/PL3770408T3/pl unknown
Also Published As
| Publication number | Publication date |
|---|---|
| US20210025338A1 (en) | 2021-01-28 |
| EP3770408A1 (en) | 2021-01-27 |
| EP3770408B1 (en) | 2023-08-30 |
| CA3085690A1 (en) | 2021-01-26 |
| US12435674B2 (en) | 2025-10-07 |
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