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특허 상세정보

Device for heating an aerofoil

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-015/12    B64D-015/14   
미국특허분류(USC) 244/134D ; 244/134R ; 219/545
출원번호 US-0978045 (1997-11-25)
우선권정보 FR-0014528 (1996-11-27)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Henderson & Sturm
인용정보 피인용 횟수 : 49  인용 특허 : 4
초록

A number of resistive elements are incorporated into the aerofoil in the vicinity of its leading edge. Each of the resistive elements is electrically connected to the other resistive elements at its distal end and is fitted at its proximal end with means of connection to an electrical power supply. The resistive elements are split between a first set that includes at least two resistive elements and a second set that includes at least one resistive element. In service, the resistive of the first set are powered in turn, while each resistive element of th...

대표
청구항

[ We claim:] [1.] A device for heating an aerofoil comprising, incorporated into the aerofoil in the vicinity of a leading edge of the aerofoil, a number of resistive elements which are more or less parallel to the leading edge, each of said resistive elements being fitted at its proximal end with means of connection to an electrical power supply, and the distal ends of the resistive elements being connected electrically to one another, wherein said resistive elements are split between a first set including at least two resistive elements and a second se...

이 특허를 인용한 특허 피인용횟수: 49

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  2. Rutherford Robert B. ; Dudman Richard L.. Aircraft de-icing system. USP2001086279856.
  3. Rutherford Robert B. ; Dudman Richard L.. Aircraft de-icing system. USP2001126330986.
  4. Calder, David Patrick; Opificius, Julian Alexander; Pederson, Erik Thomas; Flosdorf, David Cenit. Aircraft ice protection system and method. USP2016049309001.
  5. Daggett, David L.. Aircraft wing heat exchanger apparatus and method. USP2004036698687.
  6. Hubert,Claude M.; Christy,Daniel P.. Composite ice protection heater and method of producing same. USP2007117291815.
  7. Feeney, Christopher John. Composite laminate having a flexible circuit bridge and method of manufacture thereof. USP2017109793672.
  8. Kismarton,Max U.. Conducting-fiber deicing systems and methods. USP2007017157663.
  9. Rutherford Robert B.. De-ice and anti-ice system and method for aircraft surfaces. USP2001026194685.
  10. Guillermond, Alain; Le Docte, Thierry. De-icing and/or anti-icing system for the leading edge of an aircraft wing. USP2015038991763.
  11. Houlihan, Michael; Flemming, Jr., Robert J.; Daniele, Antonio G.; Budd, Timothy R.; Eisenhauer, Mark P.. Dual-channel deicing system for a rotary wing aircraft. USP2013108550402.
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  13. Euvino, Jr., Frank J.; Vinciquerra, Anthony J.. Electrothermal inlet ice protection system. USP2013028366047.
  14. Hogate, Isaac Jon. Engine inlet ice protection system having embedded variable watt density heaters. USP2012128334486.
  15. Hogate, Isaac Jon. Engine inlet ice protection system with power control by zone. USP2011118049147.
  16. Hindel, James T.; Fahrner, Alan J.; Mullen, James A.. Foil heating element for an electrothermal deicer. USP2010077763833.
  17. Foote, Peter David; Stace, Christopher; Laycock, Leslie Charles. Heat distribution in a distributed lighting apparatus. USP2010087780328.
  18. Vontell, Sr., John Henry; Salisbury, George Alan; Watson, Jr., Charles R.. Heater assembly for deicing and/or anti-icing a component. USP2010097789620.
  19. Brunner,Daniel; Amari,Andr챕. Heater mat made of electrically-conductive fibers. USP2006077078658.
  20. Patrice Rauch FR; Jean-Cyril Bauchet FR. Heating device with resistive elements for an aerodynamic profile. USP2002016338455.
  21. Voss Timothy H. ; Messersmith Maurice L. ; Ed Darryl K.. Helicopter deicing and anti-icing system and method. USP2001076264142.
  22. Petrenko,Victor F.; Sullivan,Charles R.. High-frequency de-icing of cableways. USP2007017164100.
  23. Petrenko,Victor F.. High-frequency melting of interfacial ice. USP2006087087876.
  24. Chow,Philip S.; Derouineau,Jean Luc. Hybrid electrical ice protection system and method including an energy saving mode. USP2006107124983.
  25. Mullen, James; Schroeder, Gregory. Ice protection system. USP2014098827207.
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  27. Scheibert, Tobias. Icing protection system for an aircraft and method for operating an icing protection system. USP2016029267715.
  28. Kruckenberg, Teresa M.; Pujar, Vijay V.. Lightning strike protection. USP2013108561934.
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  30. Stoner,Paul; Christy,Daniel P.; Sweet,David B.. Low power, pulsed, electro-thermal ice protection system. USP2007077246773.
  31. Vauchel, Guy Bernard; Gerome, Marc; Lemains, Laurence. Method for making deicing system on a nacelle panel. USP2015028959768.
  32. Brittingham, David L.; Prybyla, Stanley G.; Christy, Daniel P.. Methods of protecting an aircraft component from ice formation. USP2014068752279.
  33. Bourjac, Didier; Cuadrado, Gerard. Modular anti-icing/de-icing device for an aerodynamic surface. USP2009047523889.
  34. Kruckenberg, Teresa M.; Hill, Valerie A.. Nacelles and nacelle components containing nanoreinforced carbon fiber composite material. USP2010117832983.
  35. Petrenko, Victor. Pulse electrothermal and heat-storage ice detachment apparatus and methods. USP2009127638735.
  36. Petrenko, Victor F.; Martinez, Gabriel; Lee, Tae Hee; Park, Hong Hee; Oh, Joon Hwan; Suh, Kwang Ha. Pulse electrothermal mold release icemaker with safety baffles for refrigerator. USP2013038405002.
  37. Petrenko, Victor. Pulse systems and methods for detaching ice. USP2010047703300.
  38. Schellhase Ernst Calvin ; Eisenhauer Mark P. ; Miller Richard Dean ; Pappas John Peter ; Froman Gary Scott ; Aubert Roger Jacques Michel. Redundant ice management system for aircraft. USP2001056227492.
  39. Petrenko, Victor F.; Petrenko, Fedor F.. Refrigerant evaporators with pulse-electrothermal defrosting. USP2013048424324.
  40. Mukherji, Tapas K.; Araujo, Robert J.. Refurbishing method and system for a main rotor blade spar. USP2014088800145.
  41. Yu, Jia; Chien, Eugene W.. Sound-absorbing exhaust nozzle center plug. USP2010087784283.
  42. Stewart,John R.. Stretch forming method for a sheet metal skin segment having compound curvatures. USP2008037340933.
  43. Vauchel, Guy Bernard. Structure for an air inlet lip of an electric de-icing pod comprising an acoustic attenuation zone. USP2012088240982.
  44. Petrenko, Victor F.; Chen, Cheng; Petrenko, Fedor V.. System and method for energy-saving inductive heating of evaporators and other heat-exchangers. USP2015018931296.
  45. Petrenko, Victor. Systems and methods for modifying an ice-to-object interface. USP2009127629558.
  46. Petrenko, Victor. Systems and methods for modifying an ice-to-object interface. USP2005036870139.
  47. Loewe, Astrid; Renschler, Oskar; Rindt, Philipp. Wind turbine rotor blade having a heating element and a method of making the same. USP2016089410533.
  48. Loewe, Astrid; Renschler, Oskar; Rindt, Philipp. Wind turbine rotor blade having an electrical heating arrangement and method of making the same. USP2016119482208.
  49. Rutherford Robert B. ; Dudman Richard L.. Zoned aircraft de-icing system and method. USP2001056237874.