VORTEX GENERATOR, AND FUEL INJECTION SYSTEM OF A GAS TURBINE WITH SUCH VORTEX GENERATOR

• 1. 一种多齿型微涡发生器微涡发生器 [P] . 中国专利： CN213141478U . 2021-05-07
• 2. 一种纵向涡发生器及具有纵向涡发生器的换热器 [P] . 中国专利： CN106017194B . 2018.04.24
• 3. VORTEX GENERATOR, AND FUEL INJECTION SYSTEM OF A GAS TURBINE WITH SUCH VORTEX GENERATOR [P] . 欧洲知识产权局专利： EP3147569A1 . 2017-03-29

  机译： 涡发生器和带有这种涡发生器的燃气轮机燃油喷射系统

• 4. Gas turbine swirler including a vortex generator device and fuel injection openings arranged between adjacent vanes [P] . 美国专利： US9021811B2 . 2015-05-05

  机译： 燃气涡轮旋流器，其包括涡流发生器装置和布置在相邻叶片之间的燃料喷射孔

• 5. Burner of a gas turbine having a vortex generator with fuel lance [P] . 欧洲知识产权局专利： EP2253888B1 . 2013-10-16

  机译： 具有带有燃料喷枪的涡流发生器的燃气轮机的燃烧器

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• 5. A study on vortex generators to improve the mixing rate in the dry sorbent injection process of the flue gas desulfurization system [J] . Jin Do Chung, Jang Woo Kim, Young Moon Park The Korean journal of chemical engineering . 2010,第1期
• 6. A study on vortex generators to improve the mixing rate in the dry sorbent injection process of the flue gas desulfurization system [J] . Jin Do Chung, Jang Woo Kim, Young Moon Park Korean Journal of Chemical Engineering . 2010,第1期
• 7. OPERABILITY LIMITS OF TUBULAR INJECTORS WITH VORTEX GENERATORS FOR A HYDROGEN FUELLED RECUPERATED 100KW CLASS GAS TURBINE [C] . Stefan Bauer, Balbina Hampel, Thomas Sattelmayer ASME turbo expo: turbine technical conference and exposition . 2016
• 8. Endwall shape modification using vortex generators and fences to improve gas turbine cooling and effectiveness. [D] . Gokce, Zeki Ozgur. 2012
• 9. CFD Analysis to Study Effect of Circular Vortex Generator Placed in Inlet Section to Investigate Heat Transfer Aspects of Solar Air Heater [O] . Vipin B. Gawande, A. S. Dhoble, D. B. Zodpe -1
• 10. ANALISIS CFD KARAKTERISTIK AERODINAMIKA PADA SAYAP PESAWAT LSU-05 DENGAN PENAMBAHAN VORTEX GENERATOR (ANALYSIS OF CFD AERODYNAMIC CHARACTERISTICS AT THE WING OF AIRCRAFT LSU-05 WITH THE ADDITION OF VORTEX GENERATOR) [O] . Awalu Romadhon, Dana Herdiana 2017
• 11. Investigation of a High-through-Flow Single-Stage, Axial-Flow Compressor with Tip Clearance Increased 0.020 Inch, Rotor Tip Vortex Generators, and Casing Vortex Generators Configuration B, Configuration 3.1.B. [R] . Wennerstrom, A. J., Law, C. H., DeRose, R. D., 1982

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