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7results about How to "Improve blending efficiency" patented technology

Aero-engine test stand ejection system and adjustment method

PendingCN122505589AAchieving Adaptive MatchingAchieve dynamic compression sealing
The application discloses an aero-engine test stand injection system and a regulating method, relates to the technical field of aero-engine test stands, and solves the problem that the test stand injection system is difficult to adapt to the change of exhaust characteristics and test working conditions of different types of engines. The first-stage injection pipe, the second-stage injection pipe and the third-stage injection pipe are sequentially and slidably arranged on the slide rail, and the distance between the first-stage injection pipe, the second-stage injection pipe and the third-stage injection pipe is adjusted by the distance adjusting device; the inlet end of the first-stage injection pipe is detachably provided with a replaceable flow guide cover, the replaceable flow guide cover is provided with a flow guide block, and the flow guide block is provided with a nozzle; and the inlet end of the second-stage injection pipe and the third-stage injection pipe is provided with a flow guide cover. The application is designed in cooperation with the modular replaceable flow guide cover and the multi-stage dynamic adjustable injection pipe, and realizes the self-adaptive matching of the injection system to different engine exhaust flow, temperature and pressure.
Owner:HARBIN CHENGLIN TECH

Support plate stabilizer structure suitable for afterburner and capable of enhancing fuel atomization

PendingCN121953345AImprove blending efficiencyImprove combustion effectContinuous combustion chamberCombustion chamberJet flow
The invention discloses a support plate stabilizer structure for enhancing fuel oil atomization and suitable for an afterburner, which is used for improving the fuel oil atomization effect and the combustion stability, and comprises two support plate outer edge frames, a support plate tail edge frame, a fuel oil injection rod and the like, and a support plate mixing channel is formed between the two support plate outer edge frames; and a plurality of cooling air cavities are formed in the main body part so as to prevent key parts from being ablated in a high-temperature environment. First fuel oil impacts the fan-shaped channels through the oil injection holes to form an oil film, is further atomized under the shearing action of airflow and is mixed with air, and premixed gas is formed and then enters the concave cavity to be combusted. According to the design, flames in the concave cavity can be kept stable under the extreme conditions of low temperature, low pressure and the like, so that the ignition and flameout boundary of the combustion chamber is widened, meanwhile, high-temperature fuel gas in the concave cavity can heat transverse jet flow of second fuel oil, and the evaporation and mixing efficiency of the second fuel oil is improved. By means of the integrated design, the number of components is reduced, the flow resistance in the non-stress-application state is reduced, and meanwhile the thrust-weight ratio is increased.
Owner:INST OF ENGINEERING THERMOPHYSICS - CHINESE ACAD OF SCI

A radial flame stabilizer with airflow-assisted jet

ActiveCN118009358Bincrease jet velocityImprove evaporation effectContinuous combustion chamberJet flowMechanics
This invention discloses a radial flame stabilizer with airflow-assisted jet, comprising an outer wall and an inner wall. Both the outer and inner wall surfaces have V-shaped cross-sections, including a pointed tip and two tail ends. The two corresponding tail ends of the outer and inner wall surfaces are connected by a flow-rectifying wall. An air-guiding groove is provided at the pointed tip of the outer wall, and several injection holes are provided near the tail ends. The air-guiding groove, the interlayer between the outer and inner wall surfaces, and the injection holes form an airflow channel. A fuel injection extension pipe is provided near the tail ends of the inner wall, extending from the inner wall towards the injection holes. The fuel injection extension pipe guides the fuel injection from the injection holes. By introducing a portion of the incoming flow through the air-guiding groove at the stabilizer head, and utilizing the method of coaxial injection of the introduced incoming gas and fuel, the problem of shallow fuel jet depth and difficult evaporation under high-speed, large-flow conditions is improved, resulting in better fuel evaporation and mixing performance compared to conventional radial flame stabilizers.
Owner:NANJING UNIV OF AERONAUTICS & ASTRONAUTICS

High-precision gas mixing natural gas-hydrogen blending ratio regulating system

This invention discloses a high-precision natural gas-hydrogen blending ratio adjustment system, comprising a natural gas pipeline with a slot on its periphery, a hydrogen pipeline installed at the slot, a first inlet and multiple orifices at the upper and lower ends of the hydrogen pipeline, respectively, and a cylinder rotatably fitted at the middle of the lower end of the hydrogen pipeline. Baffles corresponding to the multiple orifices are installed on the periphery of the cylinder, and a slot is formed inside the lower end of the hydrogen pipeline. This invention, through a designed driving component, can drive multiple teeth to rotate, causing the cylinder to rotate synchronously, thereby driving the multiple baffles to rotate synchronously. This allows for adjustment of the blocking gaps between the multiple orifices as needed, achieving control over the hydrogen flow rate, effectively reducing uneven mixing of natural gas and hydrogen, and improving the blending efficiency of natural gas and hydrogen.
Owner:BEIJING ZHONGQI KUNLUN NEW ENERGY TECHNOLOGY CO LTD

Baijiu blending and stirring device

The utility model relates to the technical field of liquor production equipment, in particular to a liquor blending and stirring device which comprises a support, a barrel, a top cover, a partition plate, a first rotating shaft, a motor, a second rotating shaft and the like. A cylinder body is arranged on the bracket; a top cover is arranged on the cylinder body; a material outlet and a material inlet are formed in the cylinder body; an exhaust hole is formed in the top cover; a first rotating shaft is arranged in the cylinder body; a motor is arranged at the bottom of the barrel; the first rotating shaft penetrates through the barrel and is connected with a motor output end; a plurality of partition plates for separating white spirit are arranged on the first rotating shaft; and a second rotating shaft is arranged on each partition plate. The barrel is divided into four raw material mixing areas through the partition plates, base liquor is separated during liquor blending, the base liquor is stirred through gas blown out of the air blowing opening in the first rotating shaft, the base liquor is fully mixed, the best taste is achieved, follow-up liquor blending is facilitated, and meanwhile the liquor blending efficiency is improved.
Owner:YULIN LAOYULIN LIQUOR CO LTD

Blending hopper, combustion chamber and aircraft engine

ActiveCN118049666Bavoid ablationreduce wall temperatureContinuous combustion chamberAviationCombustion chamber
The application discloses a mixing hopper which is arranged on the wall of a flame tube, and comprises an inner cone part, an outer ring part arranged outside the inner cone part, and a hopper cap used for connecting the wall of the flame tube. The inner cone part and the hopper cap enclose a mixing cavity used for mixing high-temperature gas and cooling gas flow. The inner cone part and the outer ring part enclose a cooling gap used for the flow of the cooling gas flow. Cooling holes are arranged on the inner cone part and are respectively communicated with the mixing cavity and the cooling gap, and are used for introducing the cooling gas flow into the cooling gap to impact cool the outer ring part and form a cooling gas film on the inner cone part. The outer ring part actively uses a small amount of cooling gas flow in cooperation with the cooling holes to effectively reduce the wall temperature of the mixing hopper and prevent the mixing hopper from ablation. Meanwhile, the outer ring part can also shield part of the wall of the inner cone part to prevent the inner cone part from ablation as much as possible, and the cooling effect is good, the service life of the mixing hopper is prolonged, and the mixing hopper can be used in the flame tube for a long time. In addition, the application further discloses a combustion chamber. In addition, the application further discloses an aero-engine.
Owner:AECC HUNAN AVIATION POWERPLANT RES INST