172 results about "Ignition system" patented technology

An ignition diagnostic system and method for evaluating and optimizing the ignition performance of internal combustion engines (ICEs), such as those that burn hydrogen (H2) and / or other fuels. According to one example, the ignition diagnostic system and method use an artificial intelligence (AI) model with one or more machine learning (ML) algorithm(s) to identify, predict and / or otherwise evaluate abnormal combustion events, and to provide such information to an electronic control unit (ECU) in real-time. The ECU, in turn, can make combustion-related modifications to one or more components of the ignition system to optimize performance. By integrating the AI model into the ignition diagnostic system and method, a fast and simplified solution is provided that can be implemented across a wide variety of ICEs, including those that burn alternative fuels, where detecting abnormal combustion events and monitoring combustion-related parameters can be important.

According to the system and the control method for improving the sinter quality of the sintering machine, the oxygen concentration in ignition combustion-supporting gas is actively and intelligently adjusted, and traditional passive adaptation is converted into active precise adjustment and control. And the mixing flow of the oxygen-enriched gas is dynamically adjusted according to monitored real-time data, so that the constant optimal ignition intensity is maintained. And then an optimized ignition system matched with oxygen-enriched ignition is designed, and generation of high-strength binding phase calcium ferrite is facilitated. And finally, through safety interlocking, when combustion-supporting air is abnormal, the oxygen content is too high and no coal gas is supplied, an oxygen-enriched pipeline stop valve needs to be closed, so that the system safety is guaranteed. The ignition uniformity and stability are improved, the ore return rate is effectively reduced, and a virtuous cycle is formed.

Road vehicle comprising a powertrain system; an ignition system for the powertrain system comprising in turn a slot integral with the passenger compartment of the road vehicle and configured to receive and accommodate a key for the ignition of the road vehicle; wherein the ignition system comprises a detection system, configured to detect the presence or absence of the key at the slot, and a control unit, which is connected to the detection system and to the powertrain system and is configured to enable the power supply to the powertrain system only when the key is detected at the slot.

A heating system that combusts solid fuel includes a firepot configured to hold the fuel to be combusted therein. The heating system also includes a contactless ignition system including a heating element configured to generate heat sufficient to combust the fuel within the firepot, and an element housing interfaced with the firepot. The element housing is configured to at least partially surround the heating element to prevent the heating element from contacting the fuel within the firepot.

The invention discloses a gas-solid two-phase explosion venting dynamic inhibition experiment system and method, and belongs to the field of explosion venting, and the gas-solid two-phase explosion venting dynamic inhibition experiment system comprises an explosion container, a gas distribution system, a dynamic ignition system, a data acquisition system, a dynamic water mist / powder explosion inhibition system and a computer. The dynamic water mist / powder explosion suppression system comprises a water inlet block which is movably clamped on the inner wall of the upper side of the explosion container, can move along a second strip-shaped hole in the wall and is sealed. The flat plate part is connected with a water inlet pipe (extending out of the container), and a cavity is formed in the flat plate part; and a third rubber ring is arranged at the arc plate part to seal the rotator. The water inlet block is communicated with the rotator through a first through hole and a second through hole respectively, and a water mist / powder sprayer is arranged at the lower end of the rotator. The water inlet block is provided with a support which is provided with a driving structure to enable the rotator to rotate. According to the device and the method, the difference between dynamic explosion suppression and static explosion suppression can be explored, and the coupling effect between dynamic explosion suppression and the explosion source position can be explored.

The present application belongs to the technical field of distributed cooperative control system, and discloses a multi-point high-precision cooperative ignition system for firework display, comprising: a central controller which non-timely distributes delay time stamps to a plurality of distributed ignition modules and broadcasts a content-neutral synchronization event at a starting moment; the distributed ignition module starts a local timer upon detecting the synchronization event and autonomously counts down according to the pre-stored delay time stamp to execute ignition, the present application decentralizes intelligent time decision to the terminal, avoids the interference of signal physical transmission delay on the overall ignition precision of the system, and replaces the complex real-time clock synchronization and delay compensation mechanism in the traditional control system, so that the architecture simplifies the physical design and deployment complexity of the system, and improves the synchronization robustness and scalability when a large number of nodes work cooperatively.

An ignition system for a combustion engine, includes a combustor having an igniter configured to receive a series of electrical current pulses, and, responsive to each electrical pulse, to generate a spark. A sensor is configured to detect each electrical pulse to provide a signal indicative of the electrical pulse to a controller. The controller is configured to determine, prior to an injection of a fuel into the combustor, a spark rate of the igniter, determine whether the spark rate satisfies a spark rate threshold, and in response to a determination that the spark rate satisfies the spark rate threshold, initiate an injection of the fuel into the combustor.

The utility model discloses a fault frequency counting mechanism for ignition system testing, which belongs to the field of ignition fault testing and is characterized by comprising a body mechanism, a connecting mechanism is mounted at the outer end of the body mechanism, a detection mechanism is mounted at the upper end of the body mechanism, and the connecting mechanism comprises an assembly ring. The assembling ring is located at the outer end of the body mechanism, the inner end of the assembling ring is slidably connected with symmetrically-distributed clamping blocks, the clamping blocks are located at the outer end of the body mechanism, and clamping grooves are formed in the outer ends of the clamping blocks; by arranging the clamping blocks and the positioning rods, when the ignition device needs to be detached from the tester, only the pair of positioning rods needs to be pulled, the positioning blocks release positioning limitation with the clamping blocks, then the clamping blocks are taken out from the interior of the assembly ring at the outer end of the tester, and the ignition device and the tester can be conveniently detached and installed; and the mechanism is more convenient to count and test the number of faults.

This invention discloses a bidirectional controllable heavy-duty gas turbine ignition nozzle, comprising: a cylinder; a bidirectional piston, slidably disposed along the inner wall of the cylinder, dividing the cylinder's air chamber into an upper air chamber and a lower air chamber; an end cap, fixedly connected to one end of the cylinder, the end cap having an interconnected end cap air inlet channel and an end cap high-pressure air nozzle, the end cap high-pressure air nozzle communicating with the upper air chamber; a mounting flange, fixedly connected to the other end of the cylinder, the mounting flange having an interconnected mounting flange air inlet channel and a mounting flange high-pressure air nozzle, the mounting flange high-pressure air nozzle communicating with the lower air chamber, and the mounting flange having a through hole; and an ignition rod, extending and retracting through the end cap into the cylinder and fixedly connected to the bidirectional piston, the ignition rod protruding from the bidirectional piston towards the mounting flange. This reduces the risk of ignition rod ablation.

The invention discloses a solid propellant high-pressure combustion flow field testing device and method based on a particle image velocity measurement technology. The solid propellant high-pressure combustion flow field testing device comprises a visual high-pressure combustion chamber, a solid propellant placement platform, an ignition system, a smoke purging and filtering system, a double-frame high-frequency shooting system and a high-frequency laser system. AlO particles generated by combustion of a solid propellant are used as tracer particles, so that the problem that the tracer particles are difficult to accurately inject in a combustion flow field in a high-pressure environment is solved; strong background radiation caused by combustion of the solid propellant is filtered through a narrow-band filter, and a movement track image of the tracer particles is obtained; by using the smoke purging and filtering system, the removal of AlOparticles during combustion of the solid propellant is realized, and the influence on the observation view and the sheet light source is avoided. The device is convenient to adjust, good in repeatability, low in manufacturing cost and convenient to disassemble and maintain, has high engineering applicability and experiment reliability, and can be suitable for any aluminum-containing solid propellant high-pressure combustion flow field testing experiment.

The utility model discloses a power and lighting system test device, which comprises a rack, a power system, a lighting system and a control system are integrated on the rack, the power system, the lighting system and the control system are connected, the lighting system and the control system are respectively connected with a storage battery, the power system is connected with an oil tank, and the oil tank is connected with the oil tank. The oil tank is connected with the ignition system, and the ignition system is connected with the control system. The device has the advantages that practical operation is carried out on starting, acceleration, deceleration, gear shifting and light switching working conditions of an engine, a gearbox and a light system, and the structure and the working process of vehicle power and light are truly displayed.

1. Name of the designed product: electromagnetic induction instrument. 2. Use of the designed product: for detecting automobile ignition system. 3. Design points of the designed product: combination of shape and pattern. 4. Picture or photo best showing the design points: perspective view.

The invention relates to the technical field of aero-engine fault detection, in particular to a self-detection ignition system for an aero-engine. The invention provides a self-detection ignition system which comprises an ignition exciter, an ignition cable and an ignition electric nozzle. The ignition exciter at least comprises a self-detection module and a fault resistance module. The fault resistor module forms a feedback resistor loop by a plurality of resistors with different resistance values and is used for feeding back a fault state or a normal working state of the ignition exciter; the self-detection module selects a corresponding resistor in the fault resistor module according to a detection result of internal fault information of the ignition exciter to be connected to the feedback resistor loop; and the engine electronic controller identifies and determines a corresponding fault mode according to an acquisition result of the resistance value of the feedback resistance loop. According to the method, the ignition failure reason can be rapidly judged when ignition fails, specific fault components can be accurately positioned when the ignition system breaks down, and the troubleshooting efficiency is improved.

The utility model relates to the field of oil and gas exploitation, in particular to a blowout pool for a sulfur-containing gas well, which comprises a combustion cylinder, an ignition system and a spraying system. And the combustion cylinder is arranged in the blowout pool body and is communicated with the tail end of the blowout pipeline. The ignition system comprises a spark plug, and the spark plug is located above the combustion cylinder. The spraying system comprises a spraying pipe, the spraying pipe is located above the open flow pool body, the spraying pipe is used for spraying alkaline liquid, and the spraying range of the spraying pipe can cover the whole open flow pool body. The spraying system capable of spraying the alkaline liquid is arranged above the blowout pool body, so that the alkaline liquid and hydrogen sulfide gas leaked from the combustion cylinder are subjected to neutralization reaction, and leakage and diffusion of the hydrogen sulfide gas can be effectively reduced.

The invention provides an oil injection control method of an ignition system, a storage medium and a vehicle, and belongs to the technical field of vehicles. The method comprises the steps that the current working condition type of an engine is determined based on the engine rotating speed and driver demand torque; an oil injection strategy corresponding to the current working condition type is determined; and based on the fuel injection strategy, the first fuel injector and the second fuel injector are controlled to conduct fuel injection operation. According to the embodiment of the invention, the distances among the first fuel injector, the second fuel injector and the sparking plug are reasonably arranged, and meanwhile, according to the current working condition type of the engine, a proper fuel injection strategy is specifically matched to control the first fuel injector and the second fuel injector to carry out fuel injection matching, so that mixed gas can be distributed more reasonably and ignited more easily; no matter what working condition the engine is in, stable ignition of the engine and stable combustion of flames can be achieved, and meanwhile the lean combustion effect is improved.

A first vehicle configured to jump start a second vehicle is disclosed. The first vehicle may include a first energy storage system, a second energy storage system, and a converter. The first vehicle may further include a switch between the second energy storage system and the converter, and a control unit. The control unit may obtain a user request to activate a jump start mode of the first vehicle, deactivate a vehicle load in the first vehicle, and cause the switch to operate in the ON state. The control unit may further cause the second energy storage system to supply a first amount of current to pre-charge a battery of the second vehicle for a predefined time duration, and cause the second energy storage system to supply a second amount of current to the battery to start a second vehicle ignition system when the battery is pre-charged.

An engine ignition system, an ignition method, an engine, a vehicle and a transport, relating to the technical field of vehicle parts. The ignition system comprises: an ignition member, the ignition member being suitable to be mounted in a combustion chamber of an engine; and a heating device, the heating device being connected to the ignition member and used for heating the ignition member to a set temperature, so that fuel sprayed into the combustion chamber is heated and combusted, the set temperature being greater than or equal to the auto-ignition temperature of the fuel in the combustion chamber.

This invention discloses a fuel-fired cascade heating device for the primary air duct of a boiler coal mill, relating to the technical field of boiler auxiliary systems in thermal power plants. The device includes a large-capacity oil gun (1), a small-capacity oil gun (2), a primary air duct heating section (3), an oil gun flame detection device (4), a combustion air system (5), and a local control cabinet (6). The large-capacity oil gun (1) and the small-capacity oil gun (2) have different rated fuel consumption. Both are installed on the primary air duct heating section (3), using compressed air atomization to atomize the fuel and burn it within the duct. The combustion air system (5) draws combustion air from the boiler's sealed air main pipe and sends it into the primary air duct heating section (3). The local control cabinet (6) has a built-in PLC controller, which performs cascade heating control on the large-capacity oil gun (1) and the small-capacity oil gun (2) according to a four-stage sequence: "simultaneous activation of both guns—stopping the small gun—switching between large and small guns—stopping all oil guns," gradually raising the primary air temperature from ambient temperature to a target temperature range of 180–220°C. This invention solves the problem of insufficient heating capacity of steam heat exchangers under cold start conditions, which leads to insufficient drying output of coal mills. It achieves an engineering-feasible trade-off between fuel consumption and heating rate, and can also serve as an auxiliary heat source for plasma oil-free ignition systems.

The invention discloses an ignition device for semiconductor tail gas treatment. The ignition device comprises a collection cavity, a storage cavity, a mixing cavity and a combustion cavity which are connected in sequence, and an ignition system. The ignition system comprises a sensing module, a fuel gas conditioning module, a control module and an igniter. High-concentration tail gas is collected through the storage cavity and released when the concentration is low, the stored tail gas or auxiliary fuel is sprayed into the mixing cavity for dynamic mixing through a mixing execution unit in the fuel gas conditioning module, the mixing proportion is actively adjusted through the control module based on real-time data of the sensing module and a built-in prediction model, and the fuel gas conditioning efficiency is improved. And stable combustible mixed gas is ensured to be formed and is finally ignited reliably by the igniter. The device effectively solves the problem of combustion interruption caused by severe fluctuation of semiconductor process tail gas concentration, and realizes efficient, stable and safe treatment of the tail gas.

A vehicle security and ignition authorization system comprising a hybrid tracker control unit connected to a GPS module, a GSM communication module, a Bluetooth authentication module, and a driver presence sensor. The GPS module determines the geographic location of a vehicle. The GSM communication module transmits vehicle data to a remote monitoring platform. The Bluetooth authentication module detects and authenticates a registered Bluetooth device associated with a user. The driver presence sensor detects the physical presence of a driver within the vehicle. The hybrid tracker control unit receives signals from the Bluetooth authentication module and the driver presence sensor and transmits an authorization signal to an ignition interface connected to the vehicle ignition system.

The application relates to the technical field of aviation engine ignition material preparation, in particular to a SiC semiconductor ignition material and a preparation method thereof, which comprises the following raw material components in percentage by mass: 60-80% of SiC semiconductor composite powder, 0.05-0.35% of isobutylene maleic anhydride copolymer, 0.5-2.5% of dispersant, 0.1-0.5% of defoaming agent, 15.65-39.25% of water and 0.1-1% of pH value regulator; the SiC semiconductor composite powder comprises the following components: 4-8% of Re2Si2O7 powder, 3-6% of SiO2 powder, 1-5% of Y2O3 powder, 1-3% of SrO powder, 40-70% of SiC powder, 15-35% of Al2O3 powder and 5-20% of ZrO2 powder, and the Re is a rare earth element. The ignition material uses rare earth silicate compounds as corrosion-resistant phases and is used in cooperation with other powders, so that the SiC semiconductor ignition material can resist a temperature of 1300 DEG C or above, has excellent high-temperature stability, high-temperature resistance and thermal shock resistance. The problems that the SiC semiconductor ignition material has poor temperature resistance and cannot meet the requirements of an aviation engine ignition system are solved.

The invention relates to the technical field of engine flameout control methods, in particular to a flameout line breakage detection protection method and system applied to garden machine.The method comprises the steps that in the full operation stage of an engine, the electrical connection state of a flameout line is continuously obtained through a controller; when the flameout line is in the open circuit state, a corresponding safety protection instruction is determined based on the current operation stage of the engine; the safety protection instruction is used for controlling the engine to enter a non-starting state or execute active flameout; executing the safety protection instruction, and synchronously triggering the instrument to carry out fault alarm; and when the safety protection instruction is to execute active flameout, the controller selects and executes a corresponding active flameout mode according to a preset engine ignition system type. The flameout line detection method has the effect of improving the defects that an existing flameout line detection mode is single in function and cannot actively intervene in protection in the driving process.

The present application relates to a powder chamber for a hybrid gas generator comprising a tube body (60) and a first (1) and a second (2) partition element. The first partition element has a through hole (5) forming an ignition channel for an ignition system (10). Between the two partition elements a first chamber (6) for accommodating a powder (4) is formed. The second partition element has a peripheral portion (11) and a central portion (12) connected to the peripheral portion extending at least partially tapered in axial direction of the tube body towards the first partition element. The central portion has a wall around the longitudinal axis of the tube body enclosing a second chamber (7), in which wall a plurality of exhaust holes (13) is provided configured such that reaction gas mixes with compressed gas stored in the tube body through the exhaust holes. The present application also relates to a hybrid gas generator and to a safety airbag.

The invention discloses a light-weight torch ignition system and method. The light-weight torch ignition system comprises an oxidant supply unit, a fuel supply unit, a thrust chamber and an igniter. The oxidant supply unit and the fuel supply unit are both communicated with the thrust chamber so as to supply an oxidant and fuel into the thrust chamber; the oxidant supply unit is sequentially connected with an oxygen pump and an oxygen main valve through a pipeline; the oxygen main valve is connected with the thrust chamber; the fuel supply unit is sequentially connected with a fuel pump and a fuel main valve through a pipeline; the fuel main valve is connected with the thrust chamber; the igniter is mounted on the thrust chamber; an oxygen inlet and a fuel inlet are formed in the igniter; the pipeline between the oxygen pump and the oxygen main valve is communicated through a first auxiliary pipeline; the first auxiliary pipeline is connected with an igniter oxygen valve; the pipeline between the fuel pump and the fuel main valve is communicated through a second auxiliary pipeline; and an igniter oxygen valve is arranged on the first auxiliary pipeline. According to the torch ignition system, infinite ignition can be achieved, and the mass and the size of the torch ignition system are greatly reduced.

The invention relates to a shock tube detonation test visualization device and a test method thereof, and the device comprises a shock tube which is sequentially divided into a premixing section, a detonation section, a development section and a measurement section along the axial direction, and the measurement section is provided with a plurality of optical visualization windows; the gas distribution ignition system is used for filling combustible premixed gas into the shock tube and generating a controllable ignition source at the detonation section; the synchronous signal acquisition system is used for acquiring a flame front position signal in the shock tube in real time; the schlieren system is used for acquiring a two-dimensional transient density gradient field of the shock wave and the flame front; the laser-induced fluorescence system is used for carrying out two-dimensional plane laser-induced fluorescence imaging on the flame reaction area; the high-speed photographing system is used for recording the overall propagation process of the flame in the shock tube; and the smoke grain acquisition unit is used for forming a smoke film on the inner wall of the measurement section to capture and retain the detonation cell structure. Compared with the prior art, the detonation wave three-dimensional structure and array surface change characteristics can be captured and observed at the same time through one detonation test.

An ignition system for an internal combustion system has a power source for passing a DC voltage, a push-pull isolating transformer connected to the power source so as to increase the voltage from the power source and convert the DC voltage to AC voltage, a high-voltage transformer having a primary winding connected to an output of the push-pull isolating transformer, and a spark plug connected to a secondary winding of the high-voltage transformer. The high-voltage transformer increases the voltage from the push-pull isolating transformer to a voltage that fires the spark plug.

An ignition system including an injection member configured to deliver fuel to an ignition zone within a combustion chamber, an ignition element configured to ignite fuel within the ignition zone, and a control unit configured to operate the injection member and the ignition element in a first ignition phase including ignition of a first delivery of fuel provided to the combustion chamber by the injection member and a second ignition phase including ignition of a second delivery of fuel provided to the combustion chamber by the injection member.

The utility model discloses a kind of coke oven automatic diffusion ignition systems, belong to coke oven automatic diffusion ignition system technical field, including controller, control module and monitoring module, the controller is connected with pressure transmitter, the pressure transmitter is equipped with gas collector, the gas collector is connected with diffusion pipe, the controller is connected with diffusion control valve, the controller is connected with high-energy igniter, the controller is connected with flame detection device;The utility model, over setting monitoring module and soft and hard combination module, when needing to query which hardware or software of coke oven automatic diffusion ignition system specific appears fault, monitoring module can monitor the working procedure under the interactivity of modularization and hardware, under the interactivity of modularization and hardware, relevant information can be acquired quickly, accurately to complete relevant operation instruction, to be able to automatically, quickly, accurately realize the automatic diffusion ignition function of coke oven.

A prechamber device for facilitating a combustion reaction within a combustion chamber of an internal combustion spark-ignition gasoline engine includes a prechamber body, first and second electrodes, an insulation, first and second electrode terminals, a spark plug, and a prechamber head. The prechamber body includes orifices and at least partially contains the combustion reaction. The insulation insulates the first electrode and the second electrode from the prechamber body. The first electrode terminal receives a first amount of power and the second electrode terminal receives a second amount of power from an energy storage device. The first and second electrode terminals deliver the power to the first electrode and the second electrode that generate the electric field. The spark plug generates an ignition arc to initiate the combustion reaction. The prechamber head retains a position of the spark plug and closes off a first end of the prechamber body.

The application discloses a kind of double-opposed-piston quick compressor ignition experimental device, comprising: combustion system, including combustion chamber and piston, the both ends of combustion chamber are provided with opening, the opening is connected with the pipeline where piston is located, and the front opening of combustion chamber is provided with window;Gas pressure system, comprising: gas pressure storehouse and quick compressor, gas pressure storehouse is double-opposed structure;Quick compressor can compress air to 10 atmosphere pressure;Sample introduction and exhaust system, comprising: gas cylinder;Mixing gas tank;Vacuum pump, gas in gas cylinder is filled into mixing gas tank by pipeline, vacuum pump is connected combustion chamber and gas pressure storehouse by air extraction pipe, for the vacuum state of combustion chamber and gas pressure storehouse is extracted, premixed gas is stored in mixing gas tank, for premixed gas is filled into combustion chamber by pipeline;Oil pressure system, comprising: oil pressure storehouse and oil pressure pump.The double-opposed-piston quick compressor ignition experimental device can reasonably arrange ignition system, inhibit the occurrence of knock, so that combustion is fully carried out.