PL2979980T3 - Sposób i urządzenie do wykrywania podczas lotu statku powietrznego stanów oblodzenia - Google Patents

Sposób i urządzenie do wykrywania podczas lotu statku powietrznego stanów oblodzenia

Info

Publication number
PL2979980T3
PL2979980T3 PL15175834.9T PL15175834T PL2979980T3 PL 2979980 T3 PL2979980 T3 PL 2979980T3 PL 15175834 T PL15175834 T PL 15175834T PL 2979980 T3 PL2979980 T3 PL 2979980T3
Authority
PL
Poland
Prior art keywords
detecting
icing conditions
aircraft flies
flies
aircraft
Prior art date
Application number
PL15175834.9T
Other languages
English (en)
Inventor
Régis Rossotto
Emmanuel Camhi
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 filed Critical
Publication of PL2979980T3 publication Critical patent/PL2979980T3/pl

Links

Classifications

    • GPHYSICS
    • G08SIGNALLING
    • G08BSIGNALLING OR CALLING SYSTEMS; ORDER TELEGRAPHS; ALARM SYSTEMS
    • G08B19/00Alarms responsive to two or more different undesired or abnormal conditions, e.g. burglary and fire, abnormal temperature and abnormal rate of flow
    • G08B19/02Alarm responsive to formation or anticipated formation of ice
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D15/00De-icing or preventing icing on exterior surfaces of aircraft
    • B64D15/20Means for detecting icing or initiating de-icing

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
  • Control Of Turbines (AREA)
  • Measuring Fluid Pressure (AREA)
PL15175834.9T 2014-07-29 2015-07-08 Sposób i urządzenie do wykrywania podczas lotu statku powietrznego stanów oblodzenia PL2979980T3 (pl)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1401738A FR3024434B1 (fr) 2014-07-29 2014-07-29 Procede et dispositif de detection de givrage d'une entree d'air d'un turbomoteur

Publications (1)

Publication Number Publication Date
PL2979980T3 true PL2979980T3 (pl) 2016-12-30

Family

ID=51688122

Family Applications (1)

Application Number Title Priority Date Filing Date
PL15175834.9T PL2979980T3 (pl) 2014-07-29 2015-07-08 Sposób i urządzenie do wykrywania podczas lotu statku powietrznego stanów oblodzenia

Country Status (7)

Country Link
US (1) US9666051B2 (pl)
EP (1) EP2979980B1 (pl)
CN (1) CN105314117B (pl)
CA (1) CA2896695C (pl)
FR (1) FR3024434B1 (pl)
PL (1) PL2979980T3 (pl)
RU (1) RU2608990C1 (pl)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10184405B1 (en) * 2016-04-15 2019-01-22 The United States Of America As Represented By The Administrator Of National Aeronautics And Space Administration Aircraft engine icing event avoidance and mitigation through real-time simulation and controls
DE102016111902A1 (de) * 2016-06-29 2018-01-04 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verfahren und Assistenzsystem zur Detektion einer Flugleistungsdegradierung
GB201612021D0 (en) * 2016-07-11 2016-08-24 Rolls-Royce Ltd A method of operating a gas turbine engine
GB2565842B (en) * 2017-08-25 2020-04-01 Ge Aviat Systems Ltd Method and apparatus for predicting conditions favorable for icing
FR3077059B1 (fr) * 2018-01-24 2020-01-31 Airbus Operations Methode de detection de conditions givrantes pour un aeronef par apprentissage automatique supervise
FR3095196B1 (fr) * 2019-04-17 2021-12-03 Airbus Helicopters Procédé et dispositif pour estimer la santé d’une installation motrice d’un aéronef pourvu d’au moins un moteur et d’un filtre colmatable filtrant de l’air en amont du moteur
US11667392B2 (en) * 2019-06-20 2023-06-06 Pratt & Whitney Canada Corp. Method and system for operating a rotorcraft engine
FR3111947B1 (fr) * 2020-06-30 2022-05-27 Airbus Helicopters système et procédé de filtration d’air à media filtrant autonettoyant pour un moteur d’un aéronef
US11897619B2 (en) * 2021-11-22 2024-02-13 Rosemount Aerospace Inc. Heating prognostics system for ice protection system

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2046690B (en) * 1979-02-01 1982-12-08 Secr Defence Instrumentation apparatus
FR2681310B1 (fr) * 1991-09-18 1993-12-17 Sextant Avionique Dispositif pour la detection du givrage des pales d'un rotor d'aeronef.
US5354015A (en) * 1993-08-10 1994-10-11 Meador Robert H System for warning the flight crew on board an aircraft of pre-flight aircraft icing
US6304194B1 (en) * 1998-12-11 2001-10-16 Continuum Dynamics, Inc. Aircraft icing detection system
RU2200860C2 (ru) * 2000-12-26 2003-03-20 Летно-исследовательский институт им. М.М. Громова Устройство для автономного определения наличия условий обледенения входных устройств газоперекачивающих агрегатов
US7487029B2 (en) * 2004-05-21 2009-02-03 Pratt & Whitney Canada Method of monitoring gas turbine engine operation
FR2888287B1 (fr) * 2005-07-07 2011-04-08 Eurocopter France Procede d'optimisation de l'enveloppe de perfomances d'un turbomoteur.
US7374404B2 (en) 2005-09-22 2008-05-20 General Electric Company Methods and apparatus for gas turbine engines
NO324138B1 (no) * 2006-05-08 2007-09-03 Norsk Miljokraft Forskning Og Fremgangsmate og anordning for styring av effekt til en utrustning for a motvirke isdannelse eller fjerning av sno/is pa en konstruksjonsdel
FR2902407B1 (fr) * 2006-06-16 2009-04-17 Eurocopter France Procede et dispositif pour determiner le parametre limitant d'un turbomoteur.
WO2008138846A2 (en) 2007-05-09 2008-11-20 Dalsgaard Nielsen Aps A method for warning of engine icing conditions and application of runup procedures for a jet engine
US8049147B2 (en) 2008-03-28 2011-11-01 United Technologies Corporation Engine inlet ice protection system with power control by zone
US20090260341A1 (en) 2008-04-16 2009-10-22 United Technologies Corporation Distributed zoning for engine inlet ice protection
US8068997B2 (en) * 2009-02-06 2011-11-29 Honeywell International Inc. Continuous performance analysis system and method
FR2986505B1 (fr) 2012-02-06 2015-06-26 Eurocopter France Procede d'optimisation de performances d'un aeronef, dispositif et aeronef
EP2657133A3 (en) 2012-04-27 2016-08-03 Goodrich Corporation Aircraft ice protection system with operation optimization based on ice-detection input
US8720258B2 (en) * 2012-09-28 2014-05-13 United Technologies Corporation Model based engine inlet condition estimation

Also Published As

Publication number Publication date
EP2979980A1 (fr) 2016-02-03
CN105314117B (zh) 2017-08-25
CA2896695A1 (fr) 2016-01-29
EP2979980B1 (fr) 2016-08-24
RU2608990C1 (ru) 2017-01-30
FR3024434B1 (fr) 2016-08-05
RU2015131173A (ru) 2017-02-02
CA2896695C (fr) 2017-03-28
US20160035203A1 (en) 2016-02-04
FR3024434A1 (fr) 2016-02-05
US9666051B2 (en) 2017-05-30
CN105314117A (zh) 2016-02-10

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