FR3031729B1 - Commande de puissance pour aeronef a turbopropulseurs - Google Patents
Commande de puissance pour aeronef a turbopropulseurs Download PDFInfo
- Publication number
- FR3031729B1 FR3031729B1 FR1650312A FR1650312A FR3031729B1 FR 3031729 B1 FR3031729 B1 FR 3031729B1 FR 1650312 A FR1650312 A FR 1650312A FR 1650312 A FR1650312 A FR 1650312A FR 3031729 B1 FR3031729 B1 FR 3031729B1
- Authority
- FR
- France
- Prior art keywords
- aircraft
- turbo
- power control
- propeller aircraft
- power limit
- 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 - Fee Related
Links
Classifications
-
- 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
-
- 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/04—Aircraft characterised by the type or position of power plants of piston type
-
- 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type
-
- 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
- B64D31/04—Initiating means actuated personally
-
- 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
- B64D43/00—Arrangements or adaptations of instruments
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
- Supercharger (AREA)
Abstract
Procédé (100) de commande de moteur pour aéronef à turbopropulseurs, comportant l'établissement (102) d'une limite initiale de puissance maximale au-dessus de laquelle une puissance de moteur est automatiquement réduite, la limite initiale de puissance maximale étant associée à une poussée maximale admissible pour un aéronef, la réception (104) d'une indication de ce qu'un état prédéterminé de l'aéronef est atteint, et l'établissement (106) d'une limite actualisée de puissance.
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201562103748P | 2015-01-15 | 2015-01-15 | |
US62103748 | 2015-01-15 | ||
US14992465 | 2016-01-11 | ||
US14/992,465 US10112722B2 (en) | 2015-01-15 | 2016-01-11 | Power control for propeller-driven aircraft |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3031729A1 FR3031729A1 (fr) | 2016-07-22 |
FR3031729B1 true FR3031729B1 (fr) | 2020-02-07 |
Family
ID=56293889
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1650312A Expired - Fee Related FR3031729B1 (fr) | 2015-01-15 | 2016-01-15 | Commande de puissance pour aeronef a turbopropulseurs |
Country Status (4)
Country | Link |
---|---|
US (1) | US10112722B2 (fr) |
CA (1) | CA2917565C (fr) |
DE (1) | DE102016100465A1 (fr) |
FR (1) | FR3031729B1 (fr) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3044358B1 (fr) * | 2015-11-27 | 2017-11-24 | Airbus Operations Sas | Procede de controle de la poussee des reacteurs d'un avion pendant la phase de decollage, dispositif de controle et avion correspondant |
US10035609B2 (en) | 2016-03-08 | 2018-07-31 | Harris Corporation | Wireless engine monitoring system for environmental emission control and aircraft networking |
US9862499B2 (en) * | 2016-04-25 | 2018-01-09 | Airbus Operations (S.A.S.) | Human machine interface for displaying information relative to the energy of an aircraft |
US10040564B2 (en) | 2016-11-02 | 2018-08-07 | General Electric Company | Managing an input device |
US10683099B2 (en) | 2017-02-08 | 2020-06-16 | Pratt & Whitney Canada Corp. | Methods and systems for controlling operation of aircraft engines |
US10762726B2 (en) | 2017-06-13 | 2020-09-01 | General Electric Company | Hybrid-electric propulsion system for an aircraft |
US20220258872A1 (en) * | 2021-02-18 | 2022-08-18 | Geoffrey S.M. Hedrick | Pilot interface for aircraft autothrottle control |
EP3650354B1 (fr) * | 2018-11-12 | 2021-11-03 | Ratier-Figeac SAS | Ensemble de commande de poussée |
WO2020180381A1 (fr) * | 2019-03-01 | 2020-09-10 | United Technologies Advanced Projects, Inc. | Indicateurs pour groupes motopropulseurs électriques hybrides |
US11391218B2 (en) * | 2019-03-22 | 2022-07-19 | Pratt & Whitney Canada Corp. | Method and system for setting power of an aircraft engine |
DE102019112387B4 (de) * | 2019-05-13 | 2022-10-20 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Vorrichtung und Verfahren zur Leistungssteuerung von Luftfahrzeugtriebwerken |
Family Cites Families (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3916688A (en) | 1972-02-28 | 1975-11-04 | Sperry Rand Corp | VTOL craft deceleration control system |
US5031102A (en) | 1979-12-03 | 1991-07-09 | The Boeing Company | Method and apparatus for aircraft pitch and thrust axes control |
US4633404A (en) | 1983-05-20 | 1986-12-30 | Sperry Corporation | Automatic deceleration of aircraft during descent |
US4750127A (en) | 1985-10-31 | 1988-06-07 | The Boeing Company | Energy compensated target speed for aircraft descent |
US5195700A (en) | 1991-08-28 | 1993-03-23 | United Technologies Corporation | Low speed model following velocity command system for rotary wing aircraft |
US5299765A (en) | 1991-12-23 | 1994-04-05 | The Boeing Company | Apparatus and methods for controlling aircraft thrust during a climb |
US5833177A (en) | 1995-05-15 | 1998-11-10 | The Boeing Company | Autopilot/flight director overspeed protection system |
US6171055B1 (en) | 1998-04-03 | 2001-01-09 | Aurora Flight Sciences Corporation | Single lever power controller for manned and unmanned aircraft |
US6450456B1 (en) | 1999-12-20 | 2002-09-17 | Safe Flight Instrument Corporation | Airborne safe landing power control system and method |
EP1293427B1 (fr) | 2001-09-15 | 2004-10-27 | Pilatus Flugzeugwerke Ag | Aéronef à hélice avec stabilité améliorée autour de son axe de lacet |
US6748744B2 (en) | 2001-11-21 | 2004-06-15 | Pratt & Whitney Canada Corp. | Method and apparatus for the engine control of output shaft speed |
FR2845350B1 (fr) | 2002-10-02 | 2004-12-17 | Airbus France | Procede et dispositif pour commander automatiquement la pousse d'au moins un moteur d'un aeronef lors d'une phase de vol horizontal a vitesse stabilisee |
US6819266B2 (en) | 2002-10-07 | 2004-11-16 | Safe Flight Instrument Corporation | System and method for reducing the speed of an aircraft |
JP4328660B2 (ja) | 2004-04-15 | 2009-09-09 | 富士重工業株式会社 | 航空機の自動離陸装置、自動着陸装置及び自動離着陸装置並びに航空機の自動離陸方法、自動着陸方法及び自動離着陸方法 |
EP1796962A2 (fr) | 2004-09-17 | 2007-06-20 | Aurora Flight Sciences | Commande d'approche destinee a un avion a decollage et a atterrissage vertical de type tail sitter (assis sur la queue) |
US7970501B2 (en) | 2005-03-08 | 2011-06-28 | Honeywell International Inc. | Methods and systems utilizing true airspeed to improve vertical velocity accuracy |
FR2888638B1 (fr) * | 2005-07-18 | 2007-09-28 | Airbus Sas | Indicateur de pilotage pour un aeronef, destine a fournir un parametre de puissance d'au moins un turbopropulseur dudit aeronef |
CA2587835C (fr) | 2005-09-12 | 2010-02-16 | Bell Helicopter Textron Inc. | Systeme de regulation de vitesse automatique pour aeronef |
US7512464B2 (en) | 2005-12-22 | 2009-03-31 | The Boeing Company | System and method for controlling the speed of an aircraft |
US20080228365A1 (en) * | 2006-04-05 | 2008-09-18 | White Steven C | Vehicle power inhibiter |
US8414260B2 (en) * | 2006-07-25 | 2013-04-09 | Lockheed Martin Corporation | Control system for controlling propeller aircraft engine during takeoff |
US8380371B2 (en) | 2007-03-14 | 2013-02-19 | General Electric Company | Method of generating variable thrust cutback during aircraft departure |
US8670881B2 (en) | 2007-03-14 | 2014-03-11 | General Electric Company | Flight management system for generating variable thrust cutback during aircraft departure |
US8615335B2 (en) | 2008-09-17 | 2013-12-24 | The Boeing Company | Progressive takeoff thrust ramp for an aircraft |
NL2002064C (nl) | 2008-10-07 | 2010-04-08 | Robertus Gerardus De Boer | Gedifferentieerde stuwkracht startmethode voor een vliegtuig. |
FR2980454B1 (fr) | 2011-09-27 | 2014-01-31 | Eurocopter France | Procede de regulation de la vitesse de propulsion d'un helicoptere hybride |
-
2016
- 2016-01-11 US US14/992,465 patent/US10112722B2/en active Active
- 2016-01-13 DE DE102016100465.0A patent/DE102016100465A1/de not_active Ceased
- 2016-01-14 CA CA2917565A patent/CA2917565C/fr active Active
- 2016-01-15 FR FR1650312A patent/FR3031729B1/fr not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
US10112722B2 (en) | 2018-10-30 |
DE102016100465A1 (de) | 2016-07-21 |
CA2917565A1 (fr) | 2016-07-15 |
FR3031729A1 (fr) | 2016-07-22 |
US20160207633A1 (en) | 2016-07-21 |
CA2917565C (fr) | 2019-12-31 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 2 |
|
PLFP | Fee payment |
Year of fee payment: 3 |
|
PLFP | Fee payment |
Year of fee payment: 4 |
|
PLSC | Publication of the preliminary search report |
Effective date: 20190201 |
|
PLFP | Fee payment |
Year of fee payment: 5 |
|
ST | Notification of lapse |
Effective date: 20210905 |