• 검색어에 아래의 연산자를 사용하시면 더 정확한 검색결과를 얻을 수 있습니다.
  • 검색연산자
검색연산자 기능 검색시 예
() 우선순위가 가장 높은 연산자 예1) (나노 (기계 | machine))
공백 두 개의 검색어(식)을 모두 포함하고 있는 문서 검색 예1) (나노 기계)
예2) 나노 장영실
| 두 개의 검색어(식) 중 하나 이상 포함하고 있는 문서 검색 예1) (줄기세포 | 면역)
예2) 줄기세포 | 장영실
! NOT 이후에 있는 검색어가 포함된 문서는 제외 예1) (황금 !백금)
예2) !image
* 검색어의 *란에 0개 이상의 임의의 문자가 포함된 문서 검색 예) semi*
"" 따옴표 내의 구문과 완전히 일치하는 문서만 검색 예) "Transform and Quantization"

특허 상세정보

Thermal insulation barrier for an aircraft de-icing heater

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-015/12   
미국특허분류(USC) 244/134D; 244/134A; 244/134B
출원번호 US-0678282 (2012-11-15)
등록번호 US-8998144 (2015-04-07)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Lathrop & Gage LLP
인용정보 피인용 횟수 : 2  인용 특허 : 25

A structure for use with an electrothermal heating element is disclosed comprising a heating element contained in a mat and heater supports attached to one surface of the mat. The heating element is disposed between the skin and internal structure of an aircraft with the heater supports disposed toward the internal structure thereof. The heater supports maintain an insulating layer of air between the mat and the internal structure of the aircraft.


1. An electrothermal heater for a skin of an aircraft, the electrothermal heater comprising: an electrothermal heating element;a mat encasing the electrothermal heating element, the mat comprising a first and a second sheet; anda thermal barrier attached to the second sheet of the mat;wherein the thermal barrier comprises a plurality of rigid support members for maintaining a layer of air between the second sheet and the aircraft. 2. The electrothermal heater of claim 1 wherein the thermal barrier is disposed adjacent to an internal structure of the airc...

이 특허에 인용된 특허 (25)

  1. Chene, Gilles; Gantie, Fabrice; Porte, Alain. Acoustic coating for an aircraft incorporating a frost treatment system by joule effect. USP2012058181900.
  2. Rutherford Robert B. ; Dudman Richard L.. Aircraft de-icing system. USP2001086279856.
  3. Layland, Michael John; Brown, Keith T.. Aircraft engine nacelle inlet having access opening for electrical ice protection system. USP2010037681838.
  4. Atkinson, James William. Bonding of thermoplastics. USP2013098523113.
  5. Swanson ; Everts W. ; Wehrman ; Marvin D.. Boundary layer control system for aircraft. USP1978074099691.
  6. Parente Charles A.. Combined acoustic and anti-ice engine inlet liner. USP1998115841079.
  7. Liang,Rong Chang; Zang,HongMei; Gu,Haiyan. Compositions and assembly process for liquid crystal display. USP2007027182830.
  8. Rauckhorst ; III Richard L. (North Canton OH). Compressible nose dynamic de-icer. USP1994055314145.
  9. Adams Lowell J. (Dayton OH). Deicer assembly utilizing shaped memory metals. USP1996095558304.
  10. Hastings Otis H. (130 E. Crescent Ave. Mahwah NJ 07430) Hastings Otis M. (130 E. Crescent Ave. Mahwah NJ 07430). Electrically conductive laminate for temperature control of aircraft surface. USP1994095344696.
  11. Lardiere ; Jr. Benjamin G. (Milford CT) Goldberg Joshua I. (Woodbridge CT). Electro-expulsive separation apparatus. USP1990014894569.
  12. Manda Leo J. (Florissant MO) Lavorando Michael J. (Chesterfield MO). Energy-exchange system incorporating small-diameter tubes. USP1993075228643.
  13. Lardiere ; Jr. Benjamin G. (Milford CT) Goldberg Joshua I. (Woodbridge CT). Expulsive separation apparatus. USP1991014982121.
  14. Keite-Telgenbüscher, Klaus; Junghans, Monika; Dietz, Bernd; Dominikat, Udo; Domann, Frank; Ellringmann, Ute. Heated planar element and method for its attachment. USP2013028383997.
  15. Caruel, Pierre. Method for making an acoustic panel for the air intake lip of a nacelle. USP2013118584363.
  16. Goldberg Joshua I. (Woodbridge CT). Method of building an expulsive blanket using composite materials and stitched attachment. USP1996075531405.
  17. Kim, Won-Mook. Method of manufacturing multilayer ceramic substrates. USP2013078496770.
  18. Kawabe Shun,JPX ; Sato Keiichi,JPX ; Yamashita Daiya,JPX ; Nakayama Haruo,JPX ; Shiraishi Koji,JPX ; Matsumoto Keizo,JPX. Method of maufacturing a leading edge structure for aircraft. USP1998095807454.
  19. Shatz Solomon (P.O. Box 523 Cupertino CA 94015). Movable sheet for laminar flow and deicing. USP1997015590854.
  20. Leffel Kevin L. (Akron OH) Rauckhorst ; III Richard L. (North Canton OH). Side flex leading edge ice protector. USP1996025489073.
  21. Bardwell, Anthony Edward. Structural bonding arrangement. USP2014058714489.
  22. Gray James B. (San Diego CA) Joyce Robert A. (San Diego CA). System and method for application of internal heating to thermally responsive structures. USP1986014565728.
  23. McLaren Douglas (Seattle WA) Orr William W. (Mercer Island WA). Thermal anti-icing system for aircraft. USP1991045011098.
  24. Alan D. Gardner ; Andrew J. Miller GB; John A. Rolls ; Jeff R. Parkin. Thermoplastic laminate fabric heater and methods for making same. USP2002116483087.
  25. McArdel Richard C. (Kirkland WA). Wing slat anti-ice air duct system with improved slide bearings and air seal. USP1986084603824.