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특허 상세정보

Nozzle structure with notches

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-021/04   
미국특허분류(USC) 244/211 ; 239/26519 ; 239/566 ; 239/601
출원번호 US-0968226 (1978-12-11)
우선권정보 CA-0316697 (1978-11-22)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 20  인용 특허 : 0

A nozzle for a jet stream in which the rear edge of the nozzle has a number of notches spaced therealong to widen the jet stream while directing the jet stream rearwardly of the nozzle. Each notch has a narrow front apex and a rear opening substantially wider than the apex, and each notch widens substantially smoothly and progressively from its apex to its rear opening, each notch having sides which at least over a major portion of their length diverge from each other at an angle of at least 60 degrees, and preferably at least 90 degrees. The nozzle will...


In an aircraft, a lift and/or propulsion system for said aircraft, said system comprising: supply means for supplying pressurized gas, a nozzle connected with said supply means for receiving said gas and producing a jet stream, said nozzle having a nozzle exit surface having a rear edge, said rear edge having a plurality of notches formed therein and spaced along said rear edge for spreading said jet stream while directing said jet stream rearwardly of said nozzle, each notch having a narrow front apex and a rear opening substantially wider than said ape...

이 특허를 인용한 특허 피인용횟수: 20

  1. Tse, Man-Chun. Aero-engine exhaust jet noise reduction assembly. USP2003116640537.
  2. Dodd, Daniel; Cathelain, Francois. Aircraft wing. USP2013018353483.
  3. Narayanan, Satish; Simonich, John; Schlinker, Robert Hans. Asymmetric serrated nozzle for exhaust noise reduction. USP2009047520124.
  4. John F. Brausch ; Bangalore A. Janardan ; John W. Barter, IV ; Gregory E. Hoff. Chevron exhaust nozzle for a gas turbine engine. USP2002036360528.
  5. Kelber Charles C. (2081 Snowden Ave. Long Beach CA 90815). Combination lift thrust device. USP1987054666104.
  6. Evulet, Andrei. Fluidic propulsive system and thrust and lift generator for aerial vehicles. USP20190210207812.
  7. Huzzard Cunningham, Mark. Gas turbine engine exhaust mixer including circumferentially spaced-apart radial rows of tabs extending downstream on the radial walls, crests and troughs. USP2014018635875.
  8. Papamoschou,Dimitri. Jet engine noise suppressor. USP2007117293401.
  9. Sylla, Amadou André; Huber, Jérôme; Pelagatti, Olivier; Prat, Damien; Debatin, Klaus. Noise control chevron for a nozzle, and nozzle and turboshaft engine provided with such a chevron. USP2014118887489.
  10. Raether, Thomas D.. Nozzle arrangements and method for cleaning filter elements. USP2015109162234.
  11. Bevilaqua Paul M. (Dublin OH) Dehart John H. (Powell OH). Nozzle system. USP1987024645140.
  12. Lansing James P. (St. Cloud MN). Portable room air filter. USP1990024900344.
  13. Balzer,Ronald L.. Segmented mixing device for jet engines and aircraft. USP2006067065957.
  14. Balzer, Ronald L.. Segmented mixing device having chevrons for exhaust noise reduction in jet engines. USP2004096786037.
  15. Balzer, Ronald L.. Segmented mixing device having chevrons for exhaust noise reduction in jet engines. USP2003096612106.
  16. Martens, Steven. Shelf truncated chevron exhaust nozzle for reduction of exhaust noise and infrared (IR) signature. USP2003036532729.
  17. Schmid Rene,DEX ; Lepper Joachim,DEX ; Planck Wolfgang,DEX ; Kurmann Ludger,DEX. Suction jet pump having an inlet diffuser with an elliptical inflow cone. USP2001106296454.
  18. Campbell, Christian X.. Vane assembly with metal trailing edge segment. USP2010117837438.
  19. Campbell,Christian X.. Vane assembly with metal trailing edge segment. USP2008017316539.
  20. Dorsett, Kenneth M.. Vortex generation. USP2016119505485.