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특허 상세정보

Airfoil anti-icing assembly and method

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-015/04   
미국특허분류(USC) 244/134.B; 060/039.093
출원번호 US-0778178 (2001-02-07)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Goodwin Procter LLP
인용정보 피인용 횟수 : 12  인용 특허 : 13
초록

An anti-icing assembly for an airfoil such as an aircraft wing or slat comprises: (a) an airfoil having an exterior surface and interior wall defining an interior cavity, and bottom, middle and side portions all adjacent to the interior cavity; (b) an inlet plenum integral to the airfoil, wherein the inlet plenum comprises (i) an inlet baffle capable of directing hot gases into the airfoil interior cavity and (ii) a throat section interfacing the inlet plenum and airfoil interior cavity; and (c) an outlet plenum integral to the airfoil, wherein the outle...

대표
청구항

An anti-icing assembly for an airfoil such as an aircraft wing or slat comprises: (a) an airfoil having an exterior surface and interior wall defining an interior cavity, and bottom, middle and side portions all adjacent to the interior cavity; (b) an inlet plenum integral to the airfoil, wherein the inlet plenum comprises (i) an inlet baffle capable of directing hot gases into the airfoil interior cavity and (ii) a throat section interfacing the inlet plenum and airfoil interior cavity; and (c) an outlet plenum integral to the airfoil, wherein the outle...

이 특허를 인용한 특허 피인용횟수: 12

  1. Strobl, Tobias; Storm, Stefan. Actuator mounting method and method for producing an ice protection device as well as mounting device. USP20181110131449.
  2. Johnson, Rick A.; Pham, Victor D.; Gally, Daniel H.; Seydel, Joseph James; Natsui, Edward Charles. Aircraft anti-icing systems having deflector vanes. USP2016119488067.
  3. Saito, Isao; Ishiguro, Tatsuo; Abe, Shigeki; Tanaka, Hideaki; Takasu, Toru; Atsumi, Motohiro; Nakanishi, Masakazu; Kamogari, Minoru. Aircraft ice protection system and aircraft provided with the same. USP2015038967543.
  4. Porte, Alain; Hormiere, Arnaud; Dega, Alain. Aircraft nacelle air intake incorporating optimized ice-treatment hot air injection means. USP2014068757547.
  5. Wollaston, Timothy. Aircraft slat assembly with anti-icing system. USP2013118579236.
  6. Nieman, Ronald J.; Hughes, Jason M.. Anti-icing piccolo tube standoff. USP2012018100364.
  7. Thompson,Robert G.. Inlet muff anti-icing system for an auxiliary power unit. USP2006117137240.
  8. Rocklin, Mark; Karvountzi, Georgia C.; Hummel, Daniel S.. Method and apparatus for aircraft anti-icing. USP2011118061657.
  9. Bernard,Guy. Method and apparatus for inhibiting accretion of airborne material on a surface of an aircraft. USP2007027178760.
  10. Wiberg, Clark George; Mukherjee, Shiladitya. Nozzle and vane system for nacelle anti-icing. USP20190110167085.
  11. Anderson, Morris; Alstad, Shawn. Shielded anti-icing system and methods. USP2018049950799.
  12. Mackin, Steve; Fisher, Robert Earl. Systems and methods for preventing ice formation on portions of an aircraft. USP20190110189572.