1920 results about "Fuel injection" patented technology

The invention relates to the technical field of aero-engine combustion chamber outlet temperature field monitoring, and discloses a multi-source data fusion method for an aero-engine combustion chamber outlet temperature field, and the method comprises the steps: unifying a multi-source data space-time reference through a standardized space grid and a precise time synchronization protocol; mapping the data to the same space-time grid by adopting a self-adaptive interpolation algorithm, and embedding a temperature gradient continuity constraint; the confidence coefficient weight is dynamically calculated based on a sensor drift error model and CFD residual feedback, and working condition self-adaptive weighted fusion is realized by using a fuzzy logic rule base; and the interpolation parameters and the weight distribution threshold values are optimized in a distributed mode through a federated learning framework, and fuel injection parameters are adjusted in combination with combustion chamber closed-loop control. The temperature field reconstruction precision and reliability are remarkably improved, the service life of turbine blades can be prolonged, the combustion efficiency can be optimized, and the method is suitable for real-time monitoring and regulation of the combustion state of an aero-engine.

A controller is configured to control an internal combustion engine. The controller is configured to perform a fuel pressure control of adjusting a fuel pressure downstream of an electromagnetic valve in a flow direction of fuel in a fuel passage to a prescribed pressure lower than a fuel pressure upstream of the electromagnetic valve by repeatedly performing opening and closing operations of the electromagnetic valve. The controller includes processing circuitry. The processing circuitry is configured to execute a process of setting opening and closing time points of the electromagnetic valve such that a valve opening period of the electromagnetic valve during execution of the fuel pressure control overlaps with a valve opening period of the fuel injection valve.

A fuel injector is capable of injecting a plurality of different fuels in a single fuel injection event, the fuel injector including: a nozzle at an end of the fuel injector, the nozzle having a tip, openings in the tip of the nozzle through which fuel is configured to be injected, and a check valve member with a tip located within the nozzle, the check valve member being movable between an injection position in which fuel is injected via the openings and a closed position in which the openings are closed. The fuel injector further includes a primary fuel path within the fuel injector, a pilot fuel path within the fuel injector, and a mixing volume connecting the primary fuel path and the pilot fuel path when the check valve member is in the closed position.

A combustor includes a combustion liner that defines a combustion chamber and an outer sleeve spaced apart from the combustion liner, such that an annulus is defined between the combustion liner and the outer sleeve. The combustor further includes a fuel injection assembly having a boss coupled to at least one of the combustion liner and the outer sleeve. The boss includes an inner flange coupled to the combustion liner, an outer flange, and a body extending between the outer flange and the inner flange. The boss defines a cooling circuit having a post-impingement plenum defined in the inner flange between an inner wall of the inner flange and an impingement plate in cooling proximity to the inner wall; and a plurality of film cooling channels that are defined in the inner flange and fluidly couple the post-impingement plenum to the combustion chamber.

The invention discloses a motorcycle emission fuel injector control method, system and equipment and a storage medium, and relates to the technical field of internal combustion engine control. According to the method, the real-time temperature of the fuel injector under the unheated condition is obtained, and the preheating temperature threshold value of the fuel injector is determined based on the difference value between the real-time temperature and the target temperature; acquiring a first temperature change rate of the fuel injector in each preset time period under the condition that the fuel injector is heated by a heat source of the motorcycle according to the preset heat supply amount; the preset heat supply amount is adjusted according to the first temperature change rates, and the target heat supply amount is obtained; a heat source of the motorcycle is controlled to heat a fuel injector according to the target heat supply amount until the real-time temperature reaches the preheating temperature threshold value, and emission parameters of a motorcycle engine are monitored; and the fuel injection amount of the fuel injector is determined based on the emission parameters and the emission parameter standard, and the fuel injector is controlled to inject according to the fuel injection amount. The motorcycle engine has the effect of improving the emission performance of the motorcycle engine.

The application provides an integrated flame stabilizer with a tail edge cavity, which comprises a flame stabilizer, an oil injection rod, a cooling gas inlet pipe and a tail edge wing plate arranged at the rear side of the flame stabilizer, and a stable backflow ignition area is formed in the downstream area of the flame stabilizer; a plurality of cooling channels are arranged on the rear side plate of the flame stabilizer between the two tail edge wing plates, and the airflow direction at the outlet of the cooling channels is inclined to the flow direction, so that a cooling vortex is formed in the tail edge cavity, the flame stabilizer and the backflow ignition area are spaced from each other, the flame stabilizer and the downstream backflow ignition area are isolated from each other to reduce the thermal load of the components such as the flame stabilizer and the fuel injection pipe, the ablation and coking problems are avoided, meanwhile, the flame stabilizing function of the flame stabilizer is not damaged, and the influence on the backflow ignition area behind the stabilizer is small.

A fuel injector is provided. The fuel injector is operable to inject fuel at extremely high pressures which creates very small droplet sizes, allowing for efficient self-ignition of the fuel and allows for clean, efficient combustion due to the small droplet sizes. The fuel injector uses pressure from within a combustion chamber to actuate the spraying of fuel from the injector, thereby solving many problems experienced by typical fuel injectors and eliminating many problem-components of prior art fuel injectors.

A fuel injection system for an engine of a vehicle includes a throttle body and an elastomeric injection manifold coupled to the downstream end of the throttle body. The injection manifold defines a fuel injector socket. The fuel injection system also includes a fuel injector receivable by the fuel injector socket of the injection manifold and a fuel rail fluidly coupled to the fuel injector. The fuel rail supplies fuel to the fuel injector.

The invention relates to the technical field of oil supply assemblies in afterburner components of aero-engines, in particular to a multi-channel distributed series finger-shaped oil supply header pipe and an afterburner. The multi-channel distributed series finger-shaped oil supply header pipe comprises a body, and a plurality of fuel oil channels are formed in the body; the upper end of the fuel oil channel penetrates through the top surface of the body; each fuel oil channel is correspondingly provided with a plurality of main fuel oil injection holes, the main fuel oil injection holes are communicated with the fuel oil channels, and the axes of the main fuel oil injection holes are perpendicular to the central axis of the body; the plurality of main fuel injection holes in each fuel channel are arranged at intervals from top to bottom; a plurality of bypass oil injection holes are formed in the position close to the main oil injection hole, and the bypass oil injection holes are communicated with the main oil injection hole through connecting holes; the main oil injection hole, the bypass oil injection hole and the connecting hole are all formed in the body.

A fuel pressure controller includes processing circuitry that executes a first process, a second process, and a third process as a fuel pressure reduction control. The first process includes closing both a first electromagnetic valve and a second electromagnetic valve. The second process includes adjusting the pressure of the fuel supplied to a fuel injection valve by repeatedly performing an opening and closing operation of the second electromagnetic valve. The third process includes, when the fuel pressure in a fuel pipe between the first electromagnetic valve and the second electromagnetic valve reaches a prescribed pressure, stopping the opening and closing operation of the second electromagnetic valve to maintain the second electromagnetic valve in an open state, and repeatedly performing the opening and closing operation of the first electromagnetic valve to adjust the pressure of the fuel supplied to the fuel injection valve.

Embodiments of the present application disclose a fuel injection parameter adjustment method, device, equipment and storage medium. The fuel injection parameter adjustment method comprises: determining that a vehicle enters a series-parallel hybrid working condition; recording a set of initial fuel injection parameters of an engine; performing fuel injection parameter self-learning, obtaining a plurality of sets of test fuel injection parameters based on the set of initial fuel injection parameters; sequentially using the plurality of sets of test fuel injection parameters to run the engine, and calculating a plurality of test fuel consumptions of the vehicle; wherein each set of test fuel injection parameters corresponds to a test fuel consumption; the running time of each set of test fuel injection parameters is a first self-learning time; based on comparing the plurality of test fuel consumptions, determining an optimal self-learning result from the plurality of sets of test fuel injection parameters; and replacing the initial fuel injection parameters with the self-learning result.

The invention provides a carbon tank aging diagnosis method and device, a vehicle and a storage medium, and the method comprises the steps: determining a first theoretical fuel oil vapor adsorption amount of a carbon tank according to the fuel oil basic evaporation amount and evaporation time of fuel oil; when a preset carbon tank desorption condition is met, the carbon tank is controlled to execute desorption operation; in the process that the carbon tank executes desorption operation, the actual fuel steam desorption amount of the carbon tank is determined according to the desorption flow of the carbon tank, the air flow of a throttle valve, the fuel injection amount and the actual air-fuel ratio; and determining a carbon tank aging diagnosis result according to a comparison result of the first theoretical fuel oil steam adsorption amount and the actual fuel oil steam desorption amount. As whether the carbon tank is aged or not is diagnosed, a user can know the aging condition of the carbon tank in time, so that the aged carbon tank can be maintained or replaced in time, and the problem that the emission of evaporative pollutants of a vehicle exceeds the standard is avoided to a certain extent.

An axial fuel stage (AFS) injector includes a mixing member and a high pressure (HP) air-fuel injection member. The injection member includes HP air-fuel injectors including an inner wall defining an inner air jet and an outer wall surrounding and concentric with the inner wall and defining an outer air jet loop therebetween. A spacer member spaces the walls. A plurality of fuel injector passages extends from the outer wall through the spacer member and the inner wall to the inner air jet. Each fuel injector passage has an end including a fuel injector directed into the inner air jet. A fuel plenum is configured to deliver a fuel to each of the fuel injectors. The inner air jets and the air jet loops are configured to direct a high-pressure air flow from a high-pressure air source with the fuel into the inlet of the mixing member.

The invention discloses a dual-fuel engine combustion control method based on hydrogen-ammonia energy ratio and gas distribution overlap angle regulation and control, which comprises the following steps: 1) fuel ratio control: acquiring current operation state parameters of an engine, determining a target AER according to preset mapping, regulating ammonia gas supply quantity and hydrogen supply quantity to enable the actual AER to reach the target AER, and controlling the fuel ratio; the AER is adaptively set according to engine load and combustion stability conditions; 2) valve timing control: adjusting the opening time of an intake valve or the closing time of an exhaust valve through a variable valve timing mechanism so as to change a valve timing overlap angle VOA, wherein the VOA is set to be a negative value, a small overlap angle or a positive overlap angle according to the working condition of an engine; (3) injection time sequence optimization is conducted, specifically, the injection time of ammonia gas and the in-cylinder direct injection time of hydrogen are controlled respectively, and coordinated optimization of a fuel injection strategy and valve timing is achieved; and 4) closed-loop steady-state control: monitoring a combustion state and an emission index in real time, comparing the combustion state and the emission index with a threshold value to serve as a feedback signal, and correcting the target AER and VOA settings in time. According to the dual-fuel engine combustion control method based on regulation and control of the hydrogen-ammonia energy ratio and the gas distribution overlapping angle, the energy ratio of hydrogen fuel and ammonia fuel and the overlapping opening angle of an intake valve and an exhaust valve are dynamically adjusted under different working conditions, so that the combustion reaction rate and temperature are coordinated, and the stable and efficient combustion process is achieved; and harmful emissions of NOx, unburned ammonia and the like are obviously reduced.

The embodiment of the invention relates to the technical field of nuclear reactors, in particular to a gaseous fuel reactor, a reactor and a reactivity adjusting method.The gaseous fuel reactor comprises a reactor body, a containing cavity is formed in the reactor body, the containing cavity is arranged to contain gaseous fuel, and a gaseous fuel injection port is formed in the reactor body; the gaseous fuel injection pipe is arranged at the gaseous fuel injection port, and gaseous fuel is input into the containing cavity through the gaseous fuel injection port and the gaseous fuel injection pipe; the gaseous fuel provides heat and transfers the heat to the heat exchange assembly; the reactivity control assembly is arranged to be capable of changing the volume of the gaseous fuel in the containing cavity. According to the gaseous fuel reactor provided by the embodiment of the invention, the gaseous fuel is adopted as the reactor core fuel of the reactor, and the reactivity of the gaseous fuel reactor is controlled by changing the volume of the gaseous fuel in the accommodating cavity through the reactivity control assembly, so that the redundancy and reliability of reactivity control are improved.

The invention discloses a precise sensing control method for the combustion state of an internal combustion engine. The method comprises the steps that S1, parameters are collected; s2, establishing a neural network model, training the neural network model, and identifying the running state of the internal combustion engine; s3, a fuzzy language is established, and respective fuzzy adjustment amounts of a fuel injection system, a valve transmission system and an ignition system are obtained; s4, self-adaptive control models of the fuel injection system, the valve transmission system and the ignition system are established respectively, and the self-adaptive adjustment amount of the fuel injection system, the self-adaptive adjustment amount of the valve transmission system and the self-adaptive adjustment amount of the ignition system are obtained; and S5, carrying out weighted fusion on the fuzzy adjustment amount and the adaptive adjustment amount to obtain a final adjustment amount. By collecting multi-dimensional operation parameters in real time, extracting time domain and frequency domain features and combining a deep neural network model, precise recognition and early warning of the operation state of the internal combustion engine are achieved, detection and response can be made in time when the working condition of the internal combustion engine changes slightly, and the problem that a traditional control system is lagged in response is solved.

The invention discloses a heavy duty vehicle pollutant emission correction method in a plateau environment, a storage medium and a PEMS, and the method comprises the steps: obtaining the plain PEMS emission data of a heavy duty vehicle, calculating the specific emission, calculating the window specific emission of NOx in the plateau environment according to the specific emission of the plain NOx, calculating the window specific emission of PN in the plateau environment according to the specific emission of the plain PN, and calculating the window specific emission of the PN in the plateau environment according to the window specific emission of the PN in the plateau environment. The plateau environment comprises correction factors such as altitude, environment temperature, fuel injection quantity, carbon loading quantity, exhaust temperature, exhaust flow, accumulated positive altitude increment and the like. Through verification, the correction method provided by the invention can more accurately estimate the pollutant emission condition in the plateau environment, so that the test efficiency and accuracy are improved.

Disclosed are an apparatus for a simulation test of diesel engine fuel spray in an alpine environment and a test method, the apparatus comprising a fuel storage and pretreatment device, a fuel injection system, an optical visualization system, an environment chamber, and a spray pretreatment system. In alpine environmental conditions, the apparatus can achieve high-pressure injection of liquid, separate injected atomized mist into fine droplets and impinge same on a wall surface by means of a multi-droplet generation apparatus and a wall surface apparatus, and observe and record the whole process by means of an optical visualization path. According to the present invention, the problem of difficulty in distinguishing droplets due to the coalescence of spray into a sheet is avoided, the costs of a traditional spray and droplet test solution can be significantly reduced, and the problem of a high level of dependence on a control program in a constant volume vessel solution is solved. According to the present invention, simulation of spray test in an alpine environment is possible, and the test apparatus has a simple structure. Moreover, it is possible to conduct regular research on free spray, multi-droplet wall impingement, spray wall impingement, and development characteristics thereof under conditions such as different altitudes and different temperatures.

The invention relates to the technical field of vehicles, and discloses an engine intelligent layered thermal management system and method based on multivariable predictive control, and the system comprises a thermal management execution module, an information sensing module and an intelligent control module; the information sensing module is used for collecting real-time information and sending the real-time information to the intelligent control module; the information sensing module comprises a plurality of sensors and a communication interface, the plurality of sensors at least cover a temperature sensor, a pressure sensor and a flow sensor, and the communication interface is used for obtaining engine torque, rotating speed, fuel injection amount, boost pressure and vehicle speed information; the intelligent control module receives the real-time information sent by the information sensing module, performs thermal load prediction and multi-target optimization calculation to obtain an optimal control sequence, and sends the optimal control sequence to the thermal management execution module; and the thermal management execution module receives the optimal control sequence and calls an execution element to execute a thermal management action.

A fuel pre-heating component in a gas turbine engine includes a component housing extending around a central axis from a first end to a second end, wherein the component housing includes walls that define an inner chamber, a heating element positioned inside the inner chamber, and a plurality of internal fuel channels disposed within the component housing and configured to be heated by the heating element.

On board an aircraft, a method is perform in which the following steps are implemented in the following order: measuring a first density value, a first dielectric constant value and a first temperature value of the fuel at a first time, measuring a second density value, a second dielectric constant value and a second temperature value of the fuel, determining parameters of a function for calculating a density from a temperature or a dielectric constant, measuring a volume flow rate value and at least one of a third temperature value and a third dielectric constant value of the fuel in a fuel injection duct in the engine, and determining a density value of the fuel and a mass flow rate of the fuel in the injection line.

The invention relates to the technical field of engine control, in particular to an engine combustion control method, device and system based on double oil sprayers and a computer program product. Comprising the steps that when an engine enters a lean-burn working condition and meets a self-learning condition, self-learning of the injection starting angle and the excess air coefficient of an auxiliary oil injector is conducted; ignition advance angle self-learning of the auxiliary fuel injector is carried out; and fuel injection control over the auxiliary fuel injector is conducted on the basis of the injection starting angle, the excess air coefficient and the ignition advance angle obtained through self-learning. And when refined fuel oil control is carried out to achieve the optimal fuel consumption of the engine, the lowest NOx emission requirement under the lean-burn working condition of the engine is met.

The invention relates to an engine combustion control method and device, computer equipment and a storage medium. The method comprises the following steps: when an engine is in a target state, obtaining calibration data of the engine at a target rotating speed; wherein the calibration data comprises the mapping relation between the total pressure of the air inlet pipe and the air inlet flow and the corresponding circulating oil injection quantities of the engine under different loads; an interpolation algorithm is applied to the calibration data, and the real-time oil consumption and the real-time air inlet flow of the engine are obtained; according to the real-time oil consumption and the real-time air inlet flow, the real-time air-fuel ratio of the engine is obtained through calculation; and comparing the real-time air-fuel ratio with the reference air-fuel ratio to obtain a comparison result, and regulating and controlling the combustion process of the engine according to the comparison result. By the adoption of the method, the air-fuel ratio change under the transient working condition can be responded in real time, the combustion process of the engine is regulated and controlled in real time, the utilization efficiency of fuel oil is optimized, and therefore the overall combustion efficiency is enhanced, pollutant emission is reduced, and the dynamic response is improved.

The invention provides a turbine engine starting processing method and system and a storage medium, and the method comprises the steps: obtaining the rotating speed of a high-pressure rotor, and dividing the high-pressure rotor into a cold operation stage, an ignition stage, an acceleration stage and a slow transition stage which are executed in sequence according to the rotating speed of the high-pressure rotor; a corresponding self-adaptive control process is executed in each stage of the ignition stage, the acceleration stage and the slow transition stage, the self-adaptive control process comprises the steps that environment parameters and stage identification are obtained, and the environment parameters comprise the environment temperature, the flight height and the flight Mach number; processing the environment parameters by using the comprehensive correction logic to obtain a comprehensive environment correction coefficient; determining a target fuel control quantity based on the stage identifier and the comprehensive environment correction coefficient; target fuel injection pressure and target ignition parameters are determined based on the stage identifier, the environment temperature and the flight height; and starting control is executed based on the target fuel control quantity, the target fuel injection pressure and the target ignition parameters. The starting success rate and reliability of the engine can be improved.

A fuel injection valve includes a needle (20) (valve body), a fixed core (13), a movable core (30), a main body (12) (retainer), a non-magnetic member (14) (retainer), and a stopper member (60). The movable core has an inner core (32) that contacts the stopper member, and an outer core (31) that is press-fitted into an outer peripheral surface of the inner core. The outer core has, in a moving direction of the movable core, a press-fit portion (311) that is press-fitted into the outer peripheral surface of the inner core, and a non-press-fit portion (312) that is not press-fitted into the outer peripheral surface of the inner core and is adjacent to the press-fit portion in the moving direction. Between the inner peripheral surface of the main body and the non-magnetic member and the outer peripheral surface of the movable core, the smallest gap in the press-fit portion is larger than the smallest gap in the non-press-fit portion.As a result, variation in fuel injection quantity can be reduced while simultaneously adopting a core boost structure.

The utility model relates to a carbon dioxide enriched lime calcining system, which is a lime shaft kiln. A calcining chamber is arranged in the lime shaft kiln, the calcining chamber is sequentially divided into a plurality of combustion areas which are connected in series from top to bottom, and fuel injection combustion mechanisms are respectively and independently arranged in the combustion areas. According to the lime calcining system enriched with carbon dioxide, the calcining chamber is sequentially divided into a plurality of combustion areas connected in series from top to bottom, fuel and combustion-supporting gas are introduced into the calcining chamber in a segmented mode, the concentration of CO2 is controlled to be in a distribution mode that the concentration of CO2 is gradually increased from top to bottom, the inhibition effect of high-concentration CO2 on decomposition of CaCO3 is reduced, and the decomposition efficiency of CaCO3 is improved. The oxygen concentration of the middle-upper part of the calcining chamber is improved, and the burn-off rate and the utilization rate of fuel are improved.

The invention discloses a low-temperature starting control method and system for an aero-engine, and the method comprises the following steps: S1, collecting the operation parameters and basic total fuel injection quantity of the engine, the operation parameters comprising the environment temperature of the engine; s2, determining injection parameters of a combustion improver according to the collected environment temperature, and performing combustion improver injection, wherein the injection parameters of the combustion improver comprise the injection starting time and the injection duration of the combustion improver; and S3, secondary injection parameters of fuel oil are determined according to the collected environment temperature, and fuel oil injection is conducted. According to the invention, direct starting of the aero-engine in a low-temperature environment of-50 DEG C can be realized under the condition of starting without the help of an external auxiliary combustion-supporting structure through cooperation of secondary injection of the combustion improver and the fuel oil, so that on one hand, the structural arrangement of the aero-engine can be simplified; and on the other hand, the use scene of the aero-engine can be expanded to a great extent.

A fuel supply device for an internal combustion engine includes a tank, a fuel injection valve, a fuel passage, a second shut-off valve to open and close the fuel passage, a variable volume mechanism configured to vary the volume of a downstream-side fuel passage, which is a section of the fuel passage that is connected to a downstream side of the electromagnetic valve, and a controller that executes a fuel pressure control. In the fuel pressure control, the second shut-off valve is repeatedly opened and closed such that the fuel pressure in the downstream-side fuel passage falls within a range defined by an upper limit value and a lower limit value. The controller executes a volume increasing process that operates the variable volume mechanism to increase the volume of the downstream-side fuel passage during the execution of the fuel pressure control.

A fuel supply device for an internal combustion engine includes a tank that stores gas fuel, a fuel injection valve that supplies gas fuel to a cylinder, a fuel pipe that supplies gas fuel in the tank to the fuel injection valve, a pressure reducing valve provided downstream of the tank in the fuel pipe, a second shut-off valve as an electromagnetic valve that is provided downstream of the pressure reducing valve in the fuel pipe so as to open and close the fuel pipe, and a controller. A pressure reduced by the pressure reducing valve is defined as an outlet-side pressure. The pressure reducing valve includes a valve member that opens and closes in accordance with an increase and a decrease in the outlet-side pressure. The controller executes a valve closing process of closing the second shut-off valve when a stop condition for stopping fuel injection of the fuel injection valve is met.

The invention discloses a combustion chamber fuel injection and oil-gas mixing system suitable for a low-temperature environment, and belongs to the field of combustion chambers of gas turbines, the combustion chamber fuel injection and oil-gas mixing system comprises a flame tube, a centrifugal nozzle and a two-stage cyclone which are coaxially arranged, after fuel is atomized through the centrifugal nozzle and enters, the fuel is further atomized through rotational flow of an inner ring of the two-stage cyclone and enters the flame tube, and the fuel is injected into the combustion chamber through the centrifugal nozzle. External high-pressure air is swirled through the outer ring of the two-stage swirler to form swirling air, and internal fuel spray is crushed, atomized and mixed; a venturi tube is arranged at the end, close to the flame tube, of the inner ring of the two-stage cyclone, vortex generators are evenly arranged on the inner wall of the expansion section of the venturi tube in the circumferential direction, and oil mist with the small and even particle size is formed after the atomized mist is acted. Through multi-stage rotational flow, oil mist with fine and uniform granularity is formed, the atomization effect is optimized, and the fuel oil atomization quality and combustion stability in a low-temperature environment are improved.