FR2284521A1 - Thermoelectric device for helicopter rotor blades - has heating element net works along leading edges and protective skin - Google Patents

Thermoelectric device for helicopter rotor blades - has heating element net works along leading edges and protective skin

Info

Publication number
FR2284521A1
FR2284521A1 FR7430971A FR7430971A FR2284521A1 FR 2284521 A1 FR2284521 A1 FR 2284521A1 FR 7430971 A FR7430971 A FR 7430971A FR 7430971 A FR7430971 A FR 7430971A FR 2284521 A1 FR2284521 A1 FR 2284521A1
Authority
FR
France
Prior art keywords
heating element
rotor blades
thermoelectric device
leading edges
helicopter rotor
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.)
Granted
Application number
FR7430971A
Other languages
French (fr)
Other versions
FR2284521B3 (en
Inventor
Guy Gaudart
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.)
Pneumatiques Caoutchouc Manufacture et Plastiques Kleber Colombes SA
Original Assignee
Pneumatiques Caoutchouc Manufacture et Plastiques Kleber Colombes SA
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 Pneumatiques Caoutchouc Manufacture et Plastiques Kleber Colombes SA filed Critical Pneumatiques Caoutchouc Manufacture et Plastiques Kleber Colombes SA
Priority to FR7430971A priority Critical patent/FR2284521A1/en
Publication of FR2284521A1 publication Critical patent/FR2284521A1/en
Application granted granted Critical
Publication of FR2284521B3 publication Critical patent/FR2284521B3/fr
Granted legal-status Critical Current

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
    • B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
    • B64D15/12—De-icing or preventing icing on exterior surfaces of aircraft by electric heating

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Resistance Heating (AREA)
  • Steering Controls (AREA)
  • Surface Heating Bodies (AREA)

Abstract

The helicopter blade de-icer consists of a heating network which runs the length and both sides of the leading edge of each blade. An external anti-abrasive and anti-corrosive skin consists stainless steel strips covering the leading edge, their adjoining edges forming transverse joints. The heating network is divided into several elements electrically connected to one another by bridges crossing joints only in the vicinity of the leading edge. The bridges connecting the elements are made of slightly undulating metal cables.
FR7430971A 1974-09-12 1974-09-12 Thermoelectric device for helicopter rotor blades - has heating element net works along leading edges and protective skin Granted FR2284521A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR7430971A FR2284521A1 (en) 1974-09-12 1974-09-12 Thermoelectric device for helicopter rotor blades - has heating element net works along leading edges and protective skin

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7430971A FR2284521A1 (en) 1974-09-12 1974-09-12 Thermoelectric device for helicopter rotor blades - has heating element net works along leading edges and protective skin

Publications (2)

Publication Number Publication Date
FR2284521A1 true FR2284521A1 (en) 1976-04-09
FR2284521B3 FR2284521B3 (en) 1977-06-17

Family

ID=9143039

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7430971A Granted FR2284521A1 (en) 1974-09-12 1974-09-12 Thermoelectric device for helicopter rotor blades - has heating element net works along leading edges and protective skin

Country Status (1)

Country Link
FR (1) FR2284521A1 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2719182A1 (en) * 1990-11-21 1995-10-27 Onera (Off Nat Aerospatiale) Electrical de-icing system, e.g. for helicopter rotor blades
FR2730597A1 (en) * 1995-02-15 1996-08-14 Dunlop Ltd DEVICE FOR PROTECTING AGAINST ICE FORMATION
FR2744872A1 (en) * 1996-02-08 1997-08-14 Eurocopter France Electric de-icing heater for serofoil leading edge

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110481793A (en) * 2019-07-12 2019-11-22 中国人民解放军空军工程大学 A kind of new electrically heating ice shape regulation method and anti-freeze type aircraft

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2719182A1 (en) * 1990-11-21 1995-10-27 Onera (Off Nat Aerospatiale) Electrical de-icing system, e.g. for helicopter rotor blades
FR2730597A1 (en) * 1995-02-15 1996-08-14 Dunlop Ltd DEVICE FOR PROTECTING AGAINST ICE FORMATION
US5765779A (en) * 1995-02-15 1998-06-16 Dunlop Limited Ice protection device
FR2744872A1 (en) * 1996-02-08 1997-08-14 Eurocopter France Electric de-icing heater for serofoil leading edge
US6031214A (en) * 1996-02-08 2000-02-29 Eurocopter Device for heating an aerofoil

Also Published As

Publication number Publication date
FR2284521B3 (en) 1977-06-17

Similar Documents

Publication Publication Date Title
DK153241C (en) Windmill with rotary blade with variable blade angle
IT7851692A0 (en) IMPROVEMENT IN HEATING SYSTEMS AND PROCEDURES INCLUDING HEAT PUMPS
NL7703060A (en) RAZOR BLADE WITH PROTECTIVE EQUIPMENT ON THE CUTTING EDGE.
NL177988B (en) RAZOR UNIT WITH CUT PROTECTION FRAME AND TWO BLADES.
BR7906331A (en) CLEANER BLADE AND METHOD TO PRODUCE A CLEANER BLADE
IL48606A0 (en) Lightning protected composite helicopter blade
IT7950016A0 (en) INTEGRATED ELECTRIC GENERATOR AND ACTUATOR SYSTEM PARTICULARLY FOR AIRCRAFT
DE2907989A1 (en) UNDULATOR WITH ADJUSTABLE WAVE SHAPE
IT1089443B (en) COMPOSITE ROTOR SHOVEL FOR TURBOMACHINES
IT1035748B (en) IMPROVEMENT IN THE STRUCTURES OF EPR HELICOPTER BLADE
DK586078A (en) KNIFE WITH INDIVIDUAL BLADE
NO834230L (en) ROTOR WITH A PIECE AND BLADES IN ONE PIECE AND PROCEDURE FOR PRODUCING THE SAME
IT1086932B (en) ROTOR, WITHOUT BATTING AND ORIENTATION JOINTS, FOR ROTARY WING AIRCRAFT
DE3480864D1 (en) FLOW MEASURING SYSTEM WITH COUNTER-ROTATING MULTIPLE TURBINES.
IT1149344B (en) ACCEPTANCE TEST PLANT FOR AIRCRAFT CALCULATORS, AND RELATED EQUIPMENT CALCULATOR
FR2284521A1 (en) Thermoelectric device for helicopter rotor blades - has heating element net works along leading edges and protective skin
IT7825774A0 (en) AIRCRAFT ROTOR WITHOUT BEATING AND ORIENTATION JOINTS.
FI823935A0 (en) FARTYGSPROPELLER MED TVAO ELLER FLERA PERFORERADE, IHAOLIGA BLAD
NL7513220A (en) ELECTRIC BLADE.
IT1078483B (en) WING SURFACE IN PARTICULAR HELICOPTER WING EQUIPPED WITH ANTI-ICE SYSTEMS
NL185949B (en) ANGLE JOINT IN COMBINATION WITH EDGES.
IT7947701A0 (en) IMPROVEMENT IN CONNECTING RODS FOR ICE ENGINES
IT7851623A0 (en) IMPROVEMENT IN THREE-PHASE WAVY SYSTEMS
DK220075A (en) SAFETY EQUIPMENT IN CONNECTION WITH AIRCRAFT BRIDGES
GB1542529A (en) Shearing machine with adjustable angle between blades

Legal Events

Date Code Title Description
ST Notification of lapse