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FR3045567B1 - Dispositif de degivrage d'une pale d'helice, pale d'helice munie d'un tel dispositif, helice, turbomachine et aeronef - Google Patents

Dispositif de degivrage d'une pale d'helice, pale d'helice munie d'un tel dispositif, helice, turbomachine et aeronef Download PDF

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Publication number
FR3045567B1
FR3045567B1 FR1563002A FR1563002A FR3045567B1 FR 3045567 B1 FR3045567 B1 FR 3045567B1 FR 1563002 A FR1563002 A FR 1563002A FR 1563002 A FR1563002 A FR 1563002A FR 3045567 B1 FR3045567 B1 FR 3045567B1
Authority
FR
France
Prior art keywords
propeller
propeller blade
turbomachine
defrosting
aircraft
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.)
Active
Application number
FR1563002A
Other languages
English (en)
Other versions
FR3045567A1 (fr
Inventor
Bruno Seminel
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.)
Ratier Figeac SAS
Original Assignee
Ratier Figeac SAS
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 Ratier Figeac SAS filed Critical Ratier Figeac SAS
Priority to FR1563002A priority Critical patent/FR3045567B1/fr
Priority to GB1621524.6A priority patent/GB2547317B/en
Priority to US15/383,173 priority patent/US10457402B2/en
Publication of FR3045567A1 publication Critical patent/FR3045567A1/fr
Application granted granted Critical
Publication of FR3045567B1 publication Critical patent/FR3045567B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • B64D15/12De-icing or preventing icing on exterior surfaces of aircraft by electric heating
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/02De-icing means for engines having icing phenomena
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D80/00Details, components or accessories not provided for in groups F03D1/00 - F03D17/00
    • F03D80/40Ice detection; De-icing means
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05BELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B3/00Ohmic-resistance heating
    • H05B3/0014Devices wherein the heating current flows through particular resistances
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05BELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B2203/00Aspects relating to Ohmic resistive heating covered by group H05B3/00
    • H05B2203/002Heaters using a particular layout for the resistive material or resistive elements
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/70Wind energy
    • Y02E10/72Wind turbines with rotation axis in wind direction
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Control Of Resistance Heating (AREA)
  • Surface Heating Bodies (AREA)
FR1563002A 2015-12-21 2015-12-21 Dispositif de degivrage d'une pale d'helice, pale d'helice munie d'un tel dispositif, helice, turbomachine et aeronef Active FR3045567B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1563002A FR3045567B1 (fr) 2015-12-21 2015-12-21 Dispositif de degivrage d'une pale d'helice, pale d'helice munie d'un tel dispositif, helice, turbomachine et aeronef
GB1621524.6A GB2547317B (en) 2015-12-21 2016-12-16 Device for de-icing a blade of a propeller, blade of a propeller comprising such a device, propeller, Turbomachine and aircraft
US15/383,173 US10457402B2 (en) 2015-12-21 2016-12-19 Device for de-icing a rotor blade, rotor blade provided with such a device, rotor, turbomachine and aircraft

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1563002A FR3045567B1 (fr) 2015-12-21 2015-12-21 Dispositif de degivrage d'une pale d'helice, pale d'helice munie d'un tel dispositif, helice, turbomachine et aeronef
FR1563002 2015-12-21

Publications (2)

Publication Number Publication Date
FR3045567A1 FR3045567A1 (fr) 2017-06-23
FR3045567B1 true FR3045567B1 (fr) 2018-01-19

Family

ID=56068984

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1563002A Active FR3045567B1 (fr) 2015-12-21 2015-12-21 Dispositif de degivrage d'une pale d'helice, pale d'helice munie d'un tel dispositif, helice, turbomachine et aeronef

Country Status (3)

Country Link
US (1) US10457402B2 (fr)
FR (1) FR3045567B1 (fr)
GB (1) GB2547317B (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3125999A1 (fr) 2021-08-03 2023-02-10 Safran Pale dégivrante d’hélice ou de soufflante de turbomachine

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3546364A1 (fr) * 2018-03-28 2019-10-02 Ratier-Figeac SAS Appareil de dégivrage
US11427335B2 (en) * 2018-11-13 2022-08-30 Textron Innovations Inc. Enclosure for contacts of aircraft wing heater blanket
US11655828B2 (en) * 2021-10-27 2023-05-23 General Electric Company Anti-icing systems and airfoils for a fan section of a turbine engine

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2503457A (en) * 1947-04-04 1950-04-11 Curtiss Wright Corp Propeller blade deicing shoe
US2743890A (en) * 1952-07-31 1956-05-01 Goodrich Co B F Electrically heated protective covering for aircraft
US2757273A (en) * 1952-12-12 1956-07-31 Goodyear Tire & Rubber De-icer
US2992317A (en) * 1957-10-14 1961-07-11 Goodrich Co B F Electrically heated ice-removal apparatus
DE1273337B (de) * 1966-05-04 1968-07-18 Hamburger Flugzeugbau G M B H Enteisungsanlage fuer Flugzeuge
CA1069870A (fr) * 1977-03-04 1980-01-15 B.F. Goodrich Company (The) Degrivreur d'helice
EP0459216A3 (en) * 1990-06-01 1993-03-17 The Bfgoodrich Company Electrical heater de-icer
US6279856B1 (en) * 1997-09-22 2001-08-28 Northcoast Technologies Aircraft de-icing system
US6227492B1 (en) * 1999-08-06 2001-05-08 Bell Helicopter Textron Inc. Redundant ice management system for aircraft
US7278610B2 (en) * 2004-03-03 2007-10-09 Goodrich Corporation Aircraft wing with electrothermal deicing and/or anti-icing device
US7763833B2 (en) * 2004-03-12 2010-07-27 Goodrich Corp. Foil heating element for an electrothermal deicer
DE102006031330B4 (de) * 2005-07-14 2014-03-20 Goodrich Corp. Für Eis empfänglicher Abschnitt eines Flugzeugs, insbesondere Flugtriebwerk- Zelleneinlasslippe, umfassend ein Eisschutzsystem, Flugtriebwerk mit einer solchen Einlasslippe sowie ein Verfahren zum Schutz einer solchen Einlasslippe vor Vereisung
CN102783246B (zh) * 2008-10-14 2015-11-25 空中客车营运有限公司 具有至少一个电热加热层的加热系统、具有这种加热层的结构部件、加热方法以及用于制造具有加热装置的部件半成品或者部件的方法
FR2943038B1 (fr) * 2009-03-13 2012-07-27 Aircelle Sa Dispositif de degivrage,notamment pour nacelle d'aeronef
BR112012017396A2 (pt) * 2010-01-14 2016-04-19 Saab Ab sistema multifuncional de descongelamento / anticongelamento
US20130022466A1 (en) * 2010-04-12 2013-01-24 Hans Laurberg Controlling of a heating mat on a blade of a wind turbine
GB201009264D0 (en) * 2010-06-03 2010-07-21 Rolls Royce Plc Heat transfer arrangement for fluid washed surfaces

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3125999A1 (fr) 2021-08-03 2023-02-10 Safran Pale dégivrante d’hélice ou de soufflante de turbomachine

Also Published As

Publication number Publication date
FR3045567A1 (fr) 2017-06-23
GB201621524D0 (en) 2017-02-01
US10457402B2 (en) 2019-10-29
US20170174350A1 (en) 2017-06-22
GB2547317B (en) 2019-07-03
GB2547317A (en) 2017-08-16

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