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36 results about "Flame structure" patented technology

A flame structure is a type of soft-sediment deformation that forms in unconsolidated sediments. The weight of an overlying bed forces an underlying bed to push up through the overlying bed, generally when both strata are saturated with water. The resulting pattern (in cross section) may resemble flames. In order for the flame structure to occur, the overlying bed must be of a higher density than the underlying bed, or there must be differential pressures in the upper bed.

Synchronous detection method for flow field and flame structures

The invention discloses a synchronous detection method for flow field and flame structures of a hydrocarbon fuel during supersonic combustion. The method employs pulsed schlieren for detection of the flow field structure of a supersonic combustion field and CH-PLIF for detection of the flame structure of the supersonic combustion field. Detection focal planes of the pulsed schlieren and CH-PLIF are respectively focused onto a same detection area in a supersonic combustion chamber and the pulsed schlieren and CH-PLIF are synchronously controlled through a pulse synchronous generator so as to realize synchronous detection of the flow field and flame structures during supersonic combustion of the hydrocarbon fuel. The CH-PLIF image of flame structure without background noise of the combustion chamber is superposed with the schlieren image of the flow field structure so as to obtain a synchronous superposition image of the flow field and flame structures of a same instant during supersonic combustion of the hydrocarbon fuel. According to the invention, an experimental detection method for synchronous acquisition of information about flow field and flame structures in a combustion field at a same instant is provided for research on the interaction mechanism of flowing and chemical reactions during supersonic combustion of hydrocarbon fuels.
Owner:INST OF MECHANICS - CHINESE ACAD OF SCI

Device and method for synchronously or selectively exciting and measuring flame CH groups and NO molecules

ActiveCN110118762ADoes not interfere with flame structureLow costFluorescence/phosphorescenceSelective excitationSignal generator
The invention relates to a device and a method for synchronously or selectively exciting and measuring flame CH groups and NO molecules, belonging to the technical field of combustion component visualization research. A laser, a focusing lens and a space calibration plate arranged at the central plane of a combustor are arranged in order, two ICMOS cameras on the same space focusing plate are arranged towards the combustor, are located at the sides of the combustor and have the same optical distance from the combustor, the cameras are provided with optical filters coaxially arranged and located at the same horizontal height, the pulse signal output end of a pulse signal generator is connected with the laser and the signal input ends of the cameras, and the signal output ends of the camerasare connected with the signal input end of the computer. The device and the method for synchronously or selectively exciting and measuring flame CH groups and NO molecules do not interfere with the flame structure of the combustion field of the combustor, the device is simple, the cost is saved, the synchronous measurement or selective measurement of CH groups and NO molecules in the combustion process is achieved, synchronous excitation or selective excitation of two groups is achieved, and therefore, the device and the method for synchronously or selectively exciting and measuring flame CHgroups and NO molecules have important significance for the combustion mechanism and the control of pollutant NO emission.
Owner:HARBIN INST OF TECH

Experimental device for simulating influence mechanism to flame structure flow field characteristics of bottom cross wind

The invention discloses an experimental device for simulating an influence mechanism to flame structure flow field characteristics of bottom cross wind. The experimental device comprises a combustion box body, a wind tunnel system and a measurement and control system. The bottom of the combustion box body is provided with an open structure, and hollow stainless steel tubes are arranged every 10 cm on the open structure. One side face of the open structure is an observation window, and an operation opening is formed in the middle of the wall face corresponding to the observation window. The wind tunnel system is placed at the bottom of the air tunnel system and comprises a box body, a fan and a rectifying device. The length, the width and the height of the box body are the same as those of the combustion box body. The upper portion of the wind tunnel system is communicated with the bottom of the combustion box body, and the bottom of the wind tunnel system is close to the ground. The fan is placed at one end of the box body, and the other end of the box body is open. The rest two faces are closed by quartz heat insulation plates with the thickness being 8 mm. The experimental device is used for studying the occurrence regularity of internal fires and plume spreading rules in a limited space when the wind is placed at the bottom of a fire source, and a theoretical support is provided for developing related extinguishing methods and control measures.
Owner:CHINA JILIANG UNIV

Experimental device for measuring single-oil-drop combustion temperature and flame structure under low-pressure condition

The invention relates to a combustion experiment technology, and aims to provide an experimental device for measuring a single-oil-drop combustion temperature and a flame structure under a low-pressure condition. The device comprises a low-pressure cavity formed in a movable supporting frame; a bottom sealing cover of the low-pressure cavity is matched with the bottom opening through a flange surface; an observation window and an extraction opening are formed in the side surface; an oil liquid injection opening is arranged in the top cover; the bottom sealing cover is movably connected with aplatform panel of the frame platform through a vertically-arranged central threaded column and a lifting supporting column. A hand wheel is arranged at the lower end part of the central threaded column; and an electric heating wire and a thermocouple are arranged on the fixing piece on the inner side surface of the bottom sealing cover, and a plurality of joints are arranged. The device can be conveniently and quickly moved and fixed; lifting of the low-pressure cavity is adjusted through the hand wheel, continuous measurement is achieved under the condition that the position of the optical measurement system is not changed, and the stability and experiment convenience of the optical measurement system are remarkably improved. The expansibility is high, and internal modules are convenientto maintain and replace. The air tightness is good, and the repeatability of the experiment is good.
Owner:ZHEJIANG UNIV

Steam wet combustion total heat type lifting energy-saving stove

The invention relates to a steam wet combustion total heat type lifting energy-saving stove, which belongs to the technical field of gas stoves, and includes a panel, cooking ranges, a gas supply bracket, a gas supply pipe, a first gas valve, a second gas valve, a main plate, igniters, a pressing plate, a battery holder and a main plate water outlet, wherein each cooking range includes a mixer, a pivot disk, a water storage hearth bottom disk, water storage hearths, a wet combustion back pressure fire cover, a lifting disk, a connecting bracket and bent wanes; the upper end edges of the pivot disks are fixed on the panel through bolts; water storage disk bodies are arranged at the bottom centers inside the pivot disks; the lower ends of the water storage hearths are connected with the water storage hearth bottom disks; communicated lifting disk accommodating holes are arranged at the centers of the water storage hearths and the water storage hearth bottom disks; the lifting disks are positioned inside the lifting disk accommodating holes; and the upper ends of the lifting disks are connected with the wet combustion back pressure fire covers. The steam wet combustion total heat type lifting energy-saving stove is easy to dismount, convenient to clean, has no sanitary dead space, enlarges the combustion area and saves energy source as water vapor in appropriate amount changes the flame structure during combustion, avoids hidden danger caused by bottom combustion of the stoves, and can be suitable for various pot shapes.
Owner:李欣欣

Fan blade type turbulence fire extinguishing device

The invention discloses a fan blade type turbulence fire extinguishing device, and relates to the technical field of fire disaster treatment devices. The fan blade type turbulence fire extinguishing device comprises an air box, connecting plates and partition plates. One side of each connecting plate is fixedly connected with the inner wall of the air box, and one sides of the partition plates are fixedly connected with one sides of the connecting plates. According to a fan blade type vortex flame device, baffles not only play a role in controlling gas circulation and flow velocity, but also play a role in sealing gas through a sliding mode, two to four kinds of gas can be filled for experiments according to the requirements of the experiments, the experiment diversity is increased, and multiple kinds of fire extinguishing gas can be subjected to comparative fire extinguishing performance experiments under the same condition. Three air inlet pipelines are closed, one ventilation pipeline is opened, fire extinguishing gas is introduced, the situation that a firefighter on site can only extinguish fire on one side due to terrain limitation when facing a fire disaster is simulated, guiding significance can be achieved on site fire extinguishing according to experimental data, the gas inlet speed and the air inlet size are dynamically changed, and observation of influences of gas flow velocity changes on characteristics such as a flame structure, a flow field and colors is completed.
Owner:LUOYANG LANGCHAO FIRE SCI & TECH

Assembled turbulent flame extinguishing device

The invention discloses an assembled turbulent flame extinguishing device, whichrelates to the technical field of fire extinguishing devices, and comprises an air box, a partition plate and an arc-shaped plate, wherein one side of the partition plate is fixedly connected with the inner wall of the air box, and one side of the partition plate is fixedly connected with one side of the arc-shaped plate. According to the assembled turbulent flame extinguishing device, the effect of controlling whether air in the air box circulates or not and controlling the flow speed is achieved through the rotating mode of the rotating drum, air entering is quantitatively controlled through the rotating drum, assistance is provided for providing more accurate fuel mass loss efficiency, and two kinds of air are filled into the air box through the vent holes for an experiment; the flow of air on the opposite side can be controlled at the same time only by rotating the rotating drum, the air flow can be controlled more accurately, errors are smaller, experimental data are more accurate, and the influence of air entering the turbulent flame flow field, the flame structure, the flame color and other typical characteristics can be observed while the rotating drum is rotated; a dynamic observation experiment is realized, and the fire extinguishing performance of the water mist and halogenated hydrocarbon fire extinguishing agent can be dynamically observed.
Owner:ZHENGZHOU UNIV

An aircraft flame guiding structure

ActiveCN105235919BAddressing ablative effectsSolve the gap outflowCosmonautic thermal protectionFuselage insulationFiberFlight vehicle
The invention relates to a flame piloting structure for an aircraft. The structure is positioned behind an air inlet exhaust nozzle of an engine; a transitional section exists behind the air inlet exhaust nozzle of the engine; and the transitional section is used for connecting the flame piloting structure and an aircraft body. The transitional section comprises a first connecting piece and a second connecting piece; the space between the first connecting piece and the aircraft body is filled with a piece of high-temperature-resistant heat insulating felt; a groove is formed in the jointed part of the first connecting piece and the second connecting piece; a sealing piece is placed in the groove; the sealing piece comprises high-temperature cotton, a flexible spring and a ceramic fiber cloth from inside to outside, wherein the flexible spring is made of high-temperature metal; the ceramic fiber cloth coats the flexible spring; the space between the sealing piece and the groove is filled with a sealing adhesive; one layer of ceramic fiber cloth is also arranged between the first connecting piece and the second connecting piece; the second connecting piece is connected with a flame piloting groove; the flame piloting groove is made of a high-temperature-resistant C / C composite material; a shunting structure is arranged in the flame piloting groove; and tail flame ejected by the engine passes through the transitional section along an air inlet and is shunted by the shunting structure in the flame piloting groove to be ejected out from the two sides of the exterior of the flame piloting groove.
Owner:CHINA ACAD OF LAUNCH VEHICLE TECH

Preparation method and production device of large-particle spherical glass

ActiveCN113754252AGuaranteed low temperature kinetic energyColor stableGlass shaping apparatusFurnace temperatureGlass ball
The invention discloses a preparation method and a production device of large-particle spherical glass, a gas-material co-spraying balling process is adopted, in the balling process of the glass, the glass does not make contact with other materials, the surface is smooth, and secondary treatment and cleaning are not needed. And the outlet of a high-temperature furnace adopts a trumpet-shaped flame structure, so that the static pressure of a high-temperature section is increased on the basis of ensuring the low-temperature kinetic energy of the frit, and the high-temperature separation of gas and solid glass balls is strengthened while the frit is fully heated. Oxygen-enriched combustion flames are adopted, so that the rigidity of the flames is improved, the atmosphere in the combustion process is ensured, and the color of the glass is stable. And a gas and furnace temperature linkage control technology is adopted, so that the product quality is ensured, and the production cost is reduced. A furnace body structure step-by-step heat preservation technology is adopted, so that the high temperature is not reduced, the low temperature is not increased, meanwhile, the cost is saved, and the production efficiency is improved. And the top cover is cooled by water, so that the service life of the equipment is fully prolonged while environmental protection is realized.
Owner:SHAANXI UNIV OF SCI & TECH

Measuring device and measuring method for combustion field double-component synchronous excitation

ActiveCN112255213ADoes not interfere with flame structureOvercoming overlapping issuesPhase-affecting property measurementsScattering properties measurementsLaser transmitterCombustion instability
The invention discloses a measuring device and a measuring method for combustion field double-component synchronous excitation, and belongs to the technical field of combustion component visualization. A combustor is arranged in the middle of two laser transmitters, a light beam modulation system and a focusing lens are sequentially arranged between each laser transmitter and the combustor in thelaser transmitting direction, and each light beam modulation system and the corresponding focusing lens are confocal with a combustion field of the combustor. An ICMOS camera is additionally providedwith an interference filter, and the interference filter is matched with the combustion field of the combustor; a pulse signal generator is in signal transmission connection with the two laser transmitters, and a computer is in signal transmission connection with the ICMOS camera. Non-contact measurement is achieved, a flame structure is not interfered, the problem that fluorescence spectral linesof a CH group and an OH group are overlapped under the high-frequency excitation condition is solved, complete synchronization can be achieved in time sequence, the device is simple, cost is saved, and the flame structure and heat release data which can be used for combustion instability mechanism analysis and prediction are provided.
Owner:HARBIN INST OF TECH

Forming mold and preparation technology for laminated solid propellant

The invention discloses a forming mold and a preparation technology for a laminated solid propellant. The forming mold for the laminated solid propellant compacts ammonium perchlorate slices by usingthe cooperation of a groove mold with different specifications with a press mold, so the production efficiency of the prepared slices is improved. A vacuum box is vacuumized before curing, so a largeamount of air bubbles is effectively prevented from remaining in the adhesive layer of the propellant. The thickness of the adhesive layer is controlled by a height control plate; and when the laminated propellant is cured, a zigzag curing plate is used to prevent the propellant from sticking to the curing plate, so the problem of easy breakage during peeling of the propellant on the curing platebonded to the curing plate is solved. A gap between the adhesive layer and the ammonium perchlorate flakes after vacuumizing is eliminated by arranging a weight on the height control plate. The preparation technology can significantly improve the molding preparation efficiency of the solid propellant, and provides the laminated propellant with different specifications for the observation and research of the propellant flame structure; and the preparation technology has the advantages of simplicity in operation, high molding rate and time saving.
Owner:NORTHWESTERN POLYTECHNICAL UNIV

Steam wet combustion total heat type lifting energy-saving stove

The invention relates to a steam wet combustion total heat type lifting energy-saving stove, which belongs to the technical field of gas stoves, and includes a panel, cooking ranges, a gas supply bracket, a gas supply pipe, a first gas valve, a second gas valve, a main plate, igniters, a pressing plate, a battery holder and a main plate water outlet, wherein each cooking range includes a mixer, a pivot disk, a water storage hearth bottom disk, water storage hearths, a wet combustion back pressure fire cover, a lifting disk, a connecting bracket and bent wanes; the upper end edges of the pivot disks are fixed on the panel through bolts; water storage disk bodies are arranged at the bottom centers inside the pivot disks; the lower ends of the water storage hearths are connected with the water storage hearth bottom disks; communicated lifting disk accommodating holes are arranged at the centers of the water storage hearths and the water storage hearth bottom disks; the lifting disks are positioned inside the lifting disk accommodating holes; and the upper ends of the lifting disks are connected with the wet combustion back pressure fire covers. The steam wet combustion total heat type lifting energy-saving stove is easy to dismount, convenient to clean, has no sanitary dead space, enlarges the combustion area and saves energy source as water vapor in appropriate amount changes the flame structure during combustion, avoids hidden danger caused by bottom combustion of the stoves, and can be suitable for various pot shapes.
Owner:李欣欣

A Synchronous Detection Method of Flow Field and Flame Structure

The invention discloses a synchronous detection method for flow field and flame structures of a hydrocarbon fuel during supersonic combustion. The method employs pulsed schlieren for detection of the flow field structure of a supersonic combustion field and CH-PLIF for detection of the flame structure of the supersonic combustion field. Detection focal planes of the pulsed schlieren and CH-PLIF are respectively focused onto a same detection area in a supersonic combustion chamber and the pulsed schlieren and CH-PLIF are synchronously controlled through a pulse synchronous generator so as to realize synchronous detection of the flow field and flame structures during supersonic combustion of the hydrocarbon fuel. The CH-PLIF image of flame structure without background noise of the combustion chamber is superposed with the schlieren image of the flow field structure so as to obtain a synchronous superposition image of the flow field and flame structures of a same instant during supersonic combustion of the hydrocarbon fuel. According to the invention, an experimental detection method for synchronous acquisition of information about flow field and flame structures in a combustion field at a same instant is provided for research on the interaction mechanism of flowing and chemical reactions during supersonic combustion of hydrocarbon fuels.
Owner:INST OF MECHANICS - CHINESE ACAD OF SCI

Experimental device for analyzing influences of volume force on flame characteristics

The invention discloses an experimental device for analyzing influences of volume force on flame characteristics. The experimental device comprises an experiment table body, two glass partition plates, a draught fan, five sets of pulleys, weights, a tray, a steel wire, a candle, a trolley, a wind screen and a camera. The trolley is arranged on a trolley rail of the experiment table body. The candle and the wind screen are fixed to the trolley. One end of the steel wire is hooked to the front end of the trolley, and the other end of the steel wire is wound around the five sets of pulleys and hooks the tray. The weights are arranged in the tray. The two glass partition plates are mounted in the middle of the experiment table body horizontally. Openings are formed in the two ends of the experiment table body in the length direction. The draught fan is located beside the opening of one end of the experiment table body. The camera is used for shooting the experiment process. The experimental device for analyzing the influences of volume force on the flame characteristics is simple in structure and flexible in operation, and obtained experiment data are true and reliable. The static characteristics and the dynamic characteristics of a diffusion flame structure of a movable combustion source can be researched, and an experiment foundation is laid for researching of the intrinsic physical essence and laws of the flame structure of the movable combustion source.
Owner:SOUTH CHINA UNIV OF TECH
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