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Fluid systems that include a co-flow jet 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64C-021/08
  • B64C-003/14
  • B64C-021/02
출원번호 US-0255523 (2016-09-02)
등록번호 US-10106246 (2018-10-23)
발명자 / 주소
  • Zha, Gecheng
출원인 / 주소
  • Coflow Jet, LLC
대리인 / 주소
    Buchanan Van Tuinen LLC
인용정보 피인용 횟수 : 0  인용 특허 : 70

초록

Fluid systems are described. An example fluid system has a first body portion, a second body portion, a spacer, and a fluid pressurizer. The first body portion and the second body portion cooperatively define an injection opening, a suction opening, and a channel that extends from the injection open

대표청구항

1. A fluid system comprising: a first body portion having a leading edge, a trailing edge, a first intermediate edge, a second intermediate edge, a front surface, a rear surface, a bottom surface, and a main body defining a recess, an inner surface, a recess base, a first opening, a second opening,

이 특허에 인용된 특허 (70)

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  2. Sammy, Johann Quincy, Adaptive control ducted compound wind turbine.
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  22. Zuck Daniel R. (Sylmar CA), Compound helicopter with no tail rotor.
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  24. Krautheim, Michael S., Compressor casing treatment for gas turbine engine.
  25. Pegram, Barry V., Control-effect enhancement of tiltable aircraft stabilizing member.
  26. Brant H. Maines, Controlled passive porosity systems to mitigate cavitation.
  27. Jonker, Adrianus Stefanus; Bosman, Johannes Jacobus, Controlling the boundary layer of an airfoil.
  28. Rohne Karl-Heinz (Nussbaumen CHX), Device for extending the performances of a radial compressor.
  29. Ladd, Paul Vincent, Directional control and aerofoil system for aircraft.
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  31. Sakurai, Seiya; Fevergeon, Matthew D., Door assembly for laminar flow control system.
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  36. Freeman ; Christopher ; Moritz ; Robert Rudolph, Gas turbine engine with improved compressor casing for permitting higher air flow and pressure ratios before surge.
  37. Cloft, Thomas G.; Wiley, Richard H., Integral suction device with acoustic panel.
  38. Stephen M. Ruffin, Leading edge channel for enhancement of lift/drag ratio and reduction of sonic boom.
  39. Williams Arthur L. (Northridge CA), Leading edge flap for an airfoil.
  40. Rao Dhanvada M. (Yorktown VA), Lift augmentation for highly swept wing aircraft.
  41. Saiz, Manuel Munoz, Lifting arrangement for lateral aircraft surfaces.
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