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3574 results about "Rotational flow" patented technology

Rotational flow. [rō′tā·shən·əl ′flō] (fluid mechanics) Flow of a fluid in which the curl of the fluid velocity is not zero, so that each minute particle of fluid rotates about its own axis. Also known as rotational motion.

Ecological closed cycle water fish-cultivating method

The present invention belongs to an industrialization aquiculture field, particularly relates to a closed cycle water industrialized fish cultivating system. The system separates solid and liquid in a storage sedimentation basin and a backwater channel sedimentation and rotational flow pool sedimentation, the tiny particulate matter is separated and purified by a sandrock filtering bed of a one level biological filter based on the water particulate matter separation, the water purified by the one level biological filter is feed into a two stage biological filter, the biological film of biologic filling material in the one level and the two stage biological filters is degraded with ammonia nitrogen and azote nitrous acid, the total purifying rate of the water particulate matter reaches more than 99%, the culturing water is added with oxygen mechanically or by liquid oxygen, finally the water is disinfected and sterilized through a ultraviolet ray sterilizer, and the clean ecological water is feed into a fish pool, thus the waste water of the fish pool may be purified and used in repeat. The fish-cultivating system implements completely closed cycle water industrialized fish cultivation, the fish is out of a disease or less, and the fish survival is more than 80%.
Owner:HEBEI NORMAL UNIVERSITY OF SCIENCE AND TECHNOLOGY

Premix and pre-evaporation combustion chamber

The invention discloses a tangential premix and pre-evaporation combustion chamber. The combustion chamber has a single-ring cavity structure; and through a design by adopting a concept of staged combustion, combustion gas is totally supplied by a pre-combustion stage and a main combustion stage, wherein the pre-combustion stage adopts a steady-rotational flow diffusion flame combustion organization mode; and the main combustion stage adopts a premix and pre-evaporation combustion organization mode. The combustion chamber mainly comprises a flow-dividing diffuser, an outer casing of the combustion chamber, an inner casing of the combustion chamber, a fuel nozzle, the pre-combustion stage, the main combustion stage, a flame tube outer wall and a flame tube inner wall, wherein the pre-combustion stage stabilizes the flame by a low-speed return area generated by rotational flow air entering the combustion chamber from a pre-combustion stage swirler assembly; and the fuel needed by the main combustion stage is ejected from a nozzle of the main combustion stage, is atomized to form oil-gas mixed gas under the airflow action of a prefilming air ring of the nozzle of the main combustion stage, flows into a premix and pre-evaporation section to be evaporated, is further doped with the air to form a uniform oil-gas mixed air jet at an opening of the premix and pre-evaporation section to enter the flame tube, and is combusted under the ignition of a pre-combustion stage flame. The tangential premix and pre-evaporation combustion chamber has the advantages of simple structure and capacities of guaranteeing the normal working state of an aircraft engine and effectively reducing pollution discharge simultaneously.
Owner:BEIHANG UNIV

Low-pollution combustion chamber with premixed and pre-evaporated precombustion part

The invention relates to a low-pollution combustion chamber with a premixed and pre-evaporated precombustion part, which adopts a monocylic cavity structure and comprises a pressure diffuser, an outer receiver of a combustion chamber, an outer wall of a flame tube, an inner wall of the flame tube and a combustion chamber head, wherein all air for combustion enters the flame tube from the combustion chamber head, a grade combustion scheme is adopted and comprises a precombustion grade and a main combustion grade ; the main combustion grade adopts a premixed combustion mode, and the precombustion grade adopts a mode of combining diffusion combustion with stable rotational flow and rotational-flow premixed combustion; and the precombustion grade adopts the mode of combining the diffusion combustion and the premixed combustion, and pollutant discharge under a small working condition is reduced without influencing stable combustion. In the invention, the precombustion grade structure is simple, and the pollutant discharge is reduced under a small working condition without influencing the combustion stability so as to ensure that the pollution discharge of the whole landing and take-off (LTO) of an aircraft engine combustion chamber is further reduced.
Owner:BEIHANG UNIV

Layered part premixing low-pollution combustor of main combustion level lean oil premixing

The invention discloses a layered part premixing low-pollution combustor of main combustion level premixing and pre-evaporation. The layered part premixing low-pollution combustor has a pre-heating function. Fuel oil is divided into a main combustion level and an on-duty level. Diffusive combustion is adopted by the on-duty level, lean oil premixed combustion is adopted by the main combustion level, and the premixed combustion of a layered part is achieved through coupling of the diffusive combustion and the lean oil premixed combustion. The on-duty level is composed of a centrifugal atomizing nozzle and first level rotational flow air. The fuel oil of the main combustion level is supplied through multi-point direct-injection type nozzles, and oil and air mixing is enhanced through preheating of second level rotational flow air by combination of transverse jet air and on-duty level flame. The on-duty level is used in part-load conditions such as starting and slow operation, a stable combustion range can be broadened, combustion efficiency can be improved, and emission of CO and UHC is lowered; the on-duty level and the main combustion level work at the same time in the heavy load working condition, the on-duty level provides stable ignition sources for the main combustion level, a main combustion area is in a lean oil state, the temperature is far lower than the adiabatic flame temperature, and emission of NOx of high-load conditions can be reduced remarkably.
Owner:INST OF ENGINEERING THERMOPHYSICS - CHINESE ACAD OF SCI

Integrated diffusion oriented combustion chamber

InactiveCN101650038AGuaranteed temperature distributionSimplified matching structureContinuous combustion chamberLow speedCombustion chamber
The invention relates to an integrated diffusion oriented combustion chamber which adopts a full ring combustion chamber structure. The integrated diffusion oriented combustion chamber mainly comprises a crankcase, a combustion liner and an oriented diffuser. The oriented diffuser realizes pneumatic and structural coupling, controls the tangential flow direction and carries out diffusion and speedreduction, and a local return low-speed zone is formed, thereby being good for flame linkage and tangential stable combustion; grading combustion is adopted, and a pre-combustion grade can be selected to work alone and work together with a main pre-combustion grade according to work conditions; the pre-combustion grade utilizes the trapped vortex combustion technology for stable work, goes into amain combustion zone to inflame a main combustion grade through a contraction outlet, and provides a stable ignition source for the main combustion grade; fuel of the main combustion grade is injected to a main combustion grade airflow in the oriented diffuser, atomization evaporation mixing with short distance is realized, and combustible mixture gas with uniform mixing is provided for the maincombustion zone. The invention allows tangential rotational flow of a gas compressor to directly go into the combustion chamber so as to realize tangential highly efficient and stable combustion; in addition, the discharge of pollutants is low, pre-rotation is provided for a turbine, the structure can be simplified, the weight is lightened, and the densification of a gas turbine is realized.
Owner:BEIHANG UNIV

Logistics mixing distribution system

Disclosed is a stream mixing distribution system, and the stream mixing distribution system is composed of a refrigerant pipe (3), a quench box (4), a rectification sieve tray (5) and a distributor disc (6), wherein, the refrigerant pipe (3) is positioned at the upper part of the quench box (4) or positioned in an annular space surrounded by the outer wall of the quench box (4) and the inner wall of a reactor (2), the rectification sieve tray (5) is positioned at the lower part of the quench box (4), the distributor disc (6) is positioned at the lower part of the rectification sieve tray (5), and a plurality of distributors (26) are evenly distributed on the distributor disc (6), and the system is characterized in that each distributor (26) is composed of a bubble cap (27), a center pipe (29), a journal (31) and a rotational flow structure (30), the center pipe (29) is a circular pipe with two open ends, and the bottom part thereof is fixed on the distributor disc, the bubble cap (27) of each distributor is fixed above the center pipe (29) through the journal (31), and the rotational flow structure (30) is fixed at the top part of the center pipe (29) or the outlet of the center pipe (29). The stream mixing distribution system has better mixing distribution effects, and can also save the inner space of the reactor.
Owner:CHINA PETROLEUM & CHEM CORP +1

Aero-engine air rotational flow plasma igniter

InactiveCN103277231AHelps coolingGood for breakdownEngine ignitionMachines/enginesAviationCombustion chamber
Provided is an aero-engine air rotational flow plasma igniter. An insulating sleeve and a supporting sleeve are installed inside a shell, the insulating sleeve is arranged on one side of a separating plate inside the shell, the supporting sleeve is arranged inside the shell, and an air chamber is formed between the outer surface of the supporting sleeve and the inner surface of the shell. An anode sleeve is sleeved at one end, provided with the supporting sleeve, of the shell. A swirler is arranged inside the anode sleeve, and the end surface of the swirler makes contact with the end surface of the supporting sleeve. A cathode installation base is arranged inside the insulating sleeve, and the end surface of the cathode installation base makes contact with a cathode binding post in a coaxial cable. The external thread end of a cathode is fixed inside the cathode installation base and sequentially penetrates through the supporting sleeve and the swirler from top to bottom, and the arc end of the cathode extends out of the lower end surface of the swirler. The aero-engine air rotational flow plasma igniter does not change the structure and the position of an electric spark igniter originally installed in an engine combustor, penetrates through the outer duct of an engine, is installed on the outer wall of the combustor vertically, improves reliability of products, and has the advantages of being small in size, light in weight, simple in structure, and convenient to use and maintain.
Owner:AIR FORCE UNIV PLA

Supporting flow guide plate and separation filtering membrane column device

The invention discloses a supporting flow guide plate and a separation filtering membrane column device. The supporting flow guide plate is a disc with a central circular hole; a plurality of rings of flow blocking salient points are arranged on the disc; a radial rotational flow slit is also formed on the disc; one of two sides of the rotational flow slit of the disc upwarps to be extended into an upwarping part, and the other side is bent downwards to be extended into a lower bending part; and the upwarping part is parallel to the lower bending part. The separation filtering membrane column device comprises the supporting flow guide plate and a membrane; an inner pull rod for fixing the supporting flow guide plate and the membrane and upper and lower stacking plates are also installed in a bearing outer shell; a mounting hole is formed at the center of the membrane; a radial gap aligned with the rotational flow slit is also formed on the membrane; and an outer pull rod for supporting, tensioning and pressing upper and lower end cover flanges is installed outside the bearing outer shell. Compared with a traditional membrane component, the separation filtering membrane column device has the beneficial effects that the pressure loss is reduced by above 70 percent, and the product efficiency is improved. The separation filtering membrane column device is a special device with the advantages of antipollution and low energy consumption and is particularly suitable for an economical treatment process of a high-concentration fluid.
Owner:CHENGDU MEIFUTE MEMBRANE TECHNOLOGY CO LTD

Method and device for detecting fume denitration catalyst activity

The invention discloses a method and device for detecting fume denitration catalyst activity, belonging to the technical field of air pollution control of environmental engineering. In the method, a numerical control flowmeter is adopted to precisely adjust the main components of stimulated fume which enters a square-shaped stainless-steel reactor provided with the catalyst to be detected after passing through an efficient rotational flow mixer; an opened square three-segment furnace in a cavity structure is adopted to heat at constant temperature; an embedded temperature measuring device is adopted to measure the changes of the fume temperature in real time; and a reductant gas state NH3 is introduced, and the concentration changes of nitric oxide (NO) of the fume before and after the reductant gas state NH3 passes through the reactor are detected by a fume analyzer to obtain the activity of the catalyst. The device provided by the invention has a simple system, and is accurate in parameter adjustment, reliable in operation and high in experimental efficiency; and by the device, the activities of the catalyst can be dynamically stimulated and detected under different operation conditions, and the gap of the detecting technique of the domestic fume denitration catalyst is filled in.
Owner:INST OF URBAN ENVIRONMENT CHINESE ACAD OF SCI

Novel oxygen enrichment tiny-oil ignition and ultralow load stable-combustion combustor

The invention discloses a novel oxygen enrichment tiny-oil ignition and ultralow load stable-combustion combustor. The novel oxygen enrichment tiny-oil ignition and ultralow load stable-combustion combustor comprises an oxygen enrichment guide pipe, a primary air pipe, a cylindrical oil-coal mixed combustion chamber, a secondary air pipe, a secondary air box and a pre-combustion chamber, wherein the central axes of the primary air pipe, the cylindrical oil-coal mixed combustion chamber, the secondary air pipe, the secondary air box and the pre-combustion chamber coincide. A secondary air inlet inclining in the circumferential direction is formed in the pipe wall of the secondary air box; the primary air pipe penetrates through the secondary air box in the axial direction, the oil-coal mixed combustion chamber is coaxially arranged in the primary air pipe, and a high-energy tiny-oil ignition oil gun and the oxygen enrichment guide pipe are arranged in the oil-coal mixed combustion chamber; the secondary air pipe with a rotational flow impeller is coaxially arranged outside the primary air pipe in a sleeved mode and an outlet end is provided with a bluff body; the pre-combustion chamber is arranged in the secondary air box, the inlet end of the pre-combustion chamber is provided with a graded air duct, and a plurality of disturbance air nozzles are installed in an outlet of the combustor. The ignition fuel saving ratio reaches over 90% and the novel oxygen enrichment tiny-oil ignition and ultralow load stable-combustion combustor has the function of low load stable combustion and the function of ultralow load stable combustion; the technologies of oxygen enrichment, coal dust concentration, graded air feeding and the like are adopted, so that the novel oxygen enrichment tiny-oil ignition and ultralow load stable-combustion combustor has the advantages of being high in coal dust burn-off rate, low in NOx discharge and the like.
Owner:CHINA JILIANG UNIV

Low-pollution combustion chamber with main combustion stage adopting single-layer pre-film radial two-grade reverse rotational flow

The invention discloses a low-pollution combustion chamber with a main combustion stage adopting single-layer pre-film radial two-grade reverse rotational flow. The low-pollution combustion chamber adopts a single annular cavity structure, and comprises a diffuser, a combustion outdoor box, a combustion indoor box, a flame cylinder outer wall, a flame cylinder inner wall and a combustion chamber head part; the combustion chamber adopts a classification combustion scheme; the combustion head part is divided into a pre-combustion stage and the main combustion stage; the pre-combustion stage adopts a mode of combining rotational flow-stable diffusion combustion with rotational flow premixing combustion; the combustion mode reduces the pollutant discharge under small working conditions when not influencing stable combustion; and the main combustion stage adopts a premixing pre-evaporation combustion mode to be in favor of uniform combustion. The combustion chamber adopts a center classification structure; the pre-combustion stage is simple in structure; the main combustion grade adopts a two-grade reverse cyclone distributed in the radial direction; and two parts of reverse rotational flows shear an oil film, so that the atomization effect is greatly improved, the atomization of fuel of the main combustion stage and the mixing with air are enhanced, the premixing pre-evaporation of the fuel is reinforced, and the pollution discharge of whole landing and taking-off circulation of an aero-engine combustion chamber is further reduced.
Owner:BEIHANG UNIV
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