A Supersonic Atomizing Nozzle Combining Two-stage Laval and Hartmann Structures
An atomization nozzle, supersonic technology, applied in the field of supersonic atomization nozzle, can solve the problems such as no nozzle, achieve high atomization efficiency, fine atomization particles, narrow particle size distribution effect
Active Publication Date: 2015-11-25
TONGJI UNIV
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Problems solved by technology
However, judging from the domestic and foreign research reports that have been consulted, there is no nozzle style with both structures
Method used
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Embodiment 1
[0030] A supersonic atomizing nozzle with two-stage laval and hartmann structure fusion, such as figure 1 As shown, the liquid guide cavity 1 is included. A nozzle port 2 is provided below the liquid guide cavity 1, and an annular high pressure air inlet cavity 3 is surrounded by the liquid guide cavity 1, and an air inlet passage is provided on the inner side wall of the high pressure air inlet cavity 3 4. The high-pressure air inlet chamber 3 communicates with the nozzle opening 2 through the air inlet channel 4, and the number of air inlet channels 4 is greater than 18.
[0031] reference figure 1 , figure 2 , The intake passage 4 is a crossed Hartmann double-stage resonance tube structure formed by the communication of the inlet duct 5, the outlet duct 6, the primary resonance tube 7 and the secondary resonance tube 8, wherein the inlet duct 5 and the primary resonance tube 7 are located Same as a straight line, the outlet duct 6 and the secondary resonance tube 8 are on the ...
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The invention relates to a supersonic atomizing nozzle with a two-stage laval and hartmann combined structure. The supersonic atomizing nozzle comprises a liquid guide cavity, wherein a nozzle orifice is formed in the lower part of the liquid guide cavity; an annular high-pressure air inlet cavity surrounds the liquid guide cavity; an air inlet passage is formed in the inner side wall of the annular high-pressure air inflow cavity; the annular high-pressure air inflow cavity is communicated with the nozzle orifice through the air inlet passage; the air inlet passage is of a cross hartmann two-stage resonance tube structure which is formed by communicating an inlet guide pipe, an outlet guide pipe, a first-stage resonance tube and a second-stage resonance tube; the inlet guide pipe and the first-stage resonance tube are arranged on the same straight line; the outlet guide pipe and the second-stage resonance tube are arranged on the same straight line; the tail ends of the first-stage resonance tube and the second-stage resonance tube are sealed; the inlet guide pipe and the outlet guide pipe are reducer pipes with characteristics of a laval pipe. Compared with the prior art, the supersonic atomizing nozzle disclosed by the invention has the advantages that the characteristics of the laval pipe and the cross hartmann resonance tubes are combined to form the air inlet passage with the annular ring structure, so as to obviously improve the nozzle atomizing efficiency, lower the diameter of the atomized particles and narrow the particle size distribution.
Description
Technical field [0001] The invention relates to an atomizing nozzle, in particular to a supersonic atomizing nozzle with a two-stage laval and hartmann structure fusion. Background technique [0002] At present, with the development of modern powder metallurgy technology and high-performance powder metallurgy materials, as well as the development of advanced preparation technologies such as ball grid array packaging, metal injection molding, thermal spraying, and metal rapid prototyping 3D printing, more demanding requirements have been placed on metal powders. Requirements, such as powder particle size and uniformity, fluidity, etc. At present, most of the powder market and technology applicable to these advanced preparation technologies are monopolized by foreign powder product companies, such as titanium alloy powder, aluminum alloy powder, magnesium alloy powder, stainless steel powder, etc., and their prices are as high as conventional powders. Metallurgy requires more than...
Claims
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IPC IPC(8): B22F9/08
Inventor 严彪严鹏飞孙启阮成宇张庆
Owner TONGJI UNIV