1312 results about "Starter" patented technology

The invention provides a quick connector for an automobile starting motor, and relates to the technical field of starting motor connectors, the quick connector comprises a butt joint A and a butt joint B. A metal plug is installed in the butt joint A, and the metal plug is connected with a wire; the butt joint B is in contact with the butt joint A, a metal insertion cylinder is installed in the butt joint B, the metal insertion cylinder is connected with a wire, and a metal plug is connected with the metal insertion cylinder; and the outer part of the butt joint A is connected with a rotary connecting sleeve. After the metal plug is inserted into the metal insertion cylinder, the end part of the movable head is in close contact with the innermost end of the connecting seat under the thrust influence of the small spring, so that the conductive connection effect between the metal plug and the metal insertion cylinder is ensured, and the occurrence of poor contact is effectively avoided. The invention relates to a connector for an automobile starting motor, which solves the problem that the plug-pull connecting part of the connector is easy to loosen due to vibration when the existing connector for the automobile starting motor is generally fixed by adopting a plug-in matched threaded connection mode and is in a high-strength vibration working condition in an automobile for a long time.

The invention provides a storage battery starting capability prediction method and device, electronic equipment and a medium, and the method comprises the steps: obtaining the change data of the current and voltage of a storage battery when an engine is started this time; determining the moment corresponding to the maximum discharge current, the internal resistance of the starter at the moment and the internal resistance of the storage battery at the current increasing stage in the starting process of the engine based on the change data of the current and the voltage of the storage battery; and inputting the internal resistance of the storage battery and the internal resistance of the starter into a pre-constructed starting capability model to predict the starting voltage which can be provided by the storage battery when the engine is started next time. According to the invention, the prediction accuracy of the starting capability of the storage battery is improved.

The invention discloses a gas generator frequent starting system without a starting motor and an implementation method, and belongs to the technical field of generator control. The gas generator frequent starting system comprises a charging and discharging circuit, a charging control circuit and a discharging control circuit; the storage battery is connected with an inverter and a plurality of super capacitors through a normally open contact of the relay, each super capacitor is connected with a coil of a solid-state relay, the storage battery is further connected with a rectification voltage stabilizer, the inverter and the rectification voltage stabilizer are connected with a coil of a gas generator, the coil of the gas generator is further connected with a coil KMC-0 of an 8 # relay, and the coil KMC-0 of the 8 # relay is connected with the storage battery. A starting mode of directly driving a generator coil is adopted, an external starting motor is not needed, and therefore the problems that a conventional starter slips, cannot be separated and is abraded are solved.

A method and system used to control a rotational speed or a torque of an output drive shaft. The output drive shaft being coupled to a turbine engine. The turbine engine including an engine core and an engine starter assembly. The engine starter assembly including an air turbine starter, an output drive shaft and an electric motor.

A method for controlling gear shifting of a hybrid electric vehicle is applied to a transmission control unit, and includes: transmitting, at an interval of a preset time period and via a vehicle control unit (VCU), a first torque control instruction to a first microcontroller unit (MCU) and a second torque control instruction to a second MCU; transmitting, in response to a difference between a rotational speed of an integrated starter and a rotational speed of the clutch being within a preset speed difference range and via the VCU, a rotational speed control instruction to the first MCU and a gear shift instruction to the second MCU; and transmitting, in response to receiving a TM gear-shifting completion instruction, at an interval of a preset time period and via the VCU, a third torque control instruction to the first MCU and a fourth torque control instruction to the second MCU.

The invention belongs to the technical field of soft starter control, and particularly provides a soft starter control method and system based on dynamic threshold correction and current change prediction, and the method comprises the steps: data collection: collecting the collected data, including the environment temperature, the input current collection and the operation duration of a soft starter; data cleaning and preprocessing; establishing a temperature-time-current threshold correction relation; a soft starter state classification model is constructed based on the long-short-term memory network and used for perfecting the temperature-time-current threshold correction relation constructed in the third step and outputting the soft starter state; soft starter state classification model training optimization and evaluation; and using the trained soft starter state classification model to carry out soft starter operation state discrimination. The method and the system are combined with multi-dimensional data such as temperature and time, a current protection threshold is dynamically adjusted, and the problem that a traditional static constant value is poor in adaptability is solved.

A system includes a gas turbine engine configured to provide propulsion to an aircraft and a starter system configured to start the gas turbine engine. The starter system comprises a motor controller and a closed-loop cooling system configured to cool the motor controller during an emergency in-flight restart operation of the gas turbine engine. The closed-loop cooling system includes a cooling fluid reservoir containing cooling fluid. The cooling fluid is configured to receive thermal energy from the motor controller during the emergency in-flight restart operation of the gas turbine engine.

The invention discloses a compressor assembly, a heat pump system and a clothes dryer. The compressor assembly comprises a reciprocating compressor, a heat pump assembly and a heat pump assembly, the protection shell is arranged on the side, in the first direction, of the reciprocating compressor, the protection shell limits or participates in limiting of a containing cavity, the protection shell is provided with a metal layer and a heat insulation layer, the metal layer is arranged on the outer side of the heat insulation layer, and a wire outlet is formed in the side, in the second direction, of the protection shell. The second direction is perpendicular to the first direction; and the starter is arranged in the accommodating cavity, and a lead wire of the starter is arranged in the wire outlet in a penetrating manner. According to the compressor assembly, the protective shell is provided with the metal layer, so that the risks of melting and overfire are avoided, the structural strength of the protective shell is improved, and the service life of the protective shell is prolonged; in addition, the compressor assembly is small in occupied space, the installation space of other assemblies is not prone to being occupied, and the arrangement difficulty is low.

The utility model relates to the technical field of engine starting, in particular to a starting structure of an in-line piston engine, an engine and an aircraft thereof, which comprises a starting motor, the starting motor is installed on the upper portion of an engine crankshaft box body, and the output end of the starting motor penetrates through the box body and drives a reduction gear assembly through gear meshing. The reduction gear assembly comprises a reduction gear and a driving gear, the reduction gear is formed by laminating a plurality of large gears, the driving gear is meshed with the reduction gear, the large gears are laminated through friction plates and belleville springs, a starting gear is arranged at the front end of the engine crankshaft, and a one-way overrunning clutch assembly is integrally arranged on the starting gear. According to the utility model, the installation position of the starting motor is moved from the end part of the crankcase body to the upper part of the crankcase body, and meanwhile, the number of gears is reduced, so that the miniaturization design of the crankcase body is realized.

A round baler includes a forming belt defining a baling chamber having an inlet through which crop material enters. A belt tensioning system includes a tension arm and a plurality of moveable rollers that move for maintaining tension in a forming belt while allowing a diametric size of the bale to increase during formation. A starter roll is positioned immediately upstream of the inlet relative to a rotational direction of the bale within the baling chamber during formation. The starter roll is moveable during bale formation in a direction at least partially directed toward a central transverse axis of the baling chamber to maintain a constant inward deformation distance into an exterior circumferential surface of the bale as the diametric size of the bale increases during formation.

The invention relates to a low-concentration gas intrinsically safe combustion device, which relates to the technical field of coal resource utilization and comprises a safe ignition unit, a multi-stage backfire prevention unit, a multi-blow-off prevention unit, a combustion chamber, a control unit and an explosion venting unit. The safety ignition unit adopts a staged ignition mode, and the 100% ignition success rate is achieved through a high-energy igniter and a combustion starter; the anti-backfire unit forms three-stage protection through a micro-channel, a quick shut-off valve and an anti-detonation flame arrester, and flame returning is blocked; the anti-blow-off unit is combined with a high-heat-insulation labyrinth type combustion chamber by means of the entrainment effect of a swirler and a flame retention module, so that flame is stable and does not break away; the control unit achieves automatic interlocking control through various sensors, and the explosion venting unit conducts directional explosion venting during overpressure. According to the device, the low-concentration gas with the concentration lower than 30% is subjected to intrinsic safety combustion, and the risks of backfire, blow-off and explosion can be avoided.

The invention provides a turbojet engine starting control method and system based on artificial intelligence. The method comprises the steps that the oil way pressure of an ignition oil way of an engine, the environment temperature of the environment where the engine is located and the internal temperature of the engine are obtained; under the condition that the oil way pressure meets a preset condition and the environment temperature is smaller than or equal to a first temperature threshold value, an igniter is controlled to be started, a gunpowder starter is controlled to be started at a first time point, and the first time point is a time point which is delayed by a preset duration of the time point for controlling the igniter to be started; and under the condition that the oil way pressure meets the preset condition and the environment temperature is larger than a first temperature threshold value, or the oil way pressure meets the preset condition and the internal temperature is larger than a second temperature threshold value, the igniter and the gunpowder starter are controlled to be started at the same time. According to the self-adaptive control method, the starting reliability of the turbojet engine in the low-temperature environment is effectively enhanced, and meanwhile the requirement for quick starting in the normal-temperature or heat engine state is met.

The utility model discloses a deburring device for starter planetary gear production, and belongs to the technical field of gear machining, the deburring device comprises an operation table, the upper surface of the operation table is provided with a polishing assembly and a cleaning assembly, the polishing assembly comprises a supporting plate and a second motor, the supporting plate and the second motor are both arranged on the upper surface of the operation table, and the cleaning assembly is arranged on the upper surface of the operation table. The supporting plate and the second motor are fixedly connected with the operation table, an electric telescopic rod is arranged on the lower surface of the supporting plate, the lower surface of the supporting plate is fixedly connected with the electric telescopic rod, a first motor is arranged at the output end of the electric telescopic rod, and the output end of the electric telescopic rod is fixedly connected with the first motor. A first grinding disc is arranged at the output end of the first motor. Burrs at the upper end and the lower end of the gear are polished through cooperation of the polishing assemblies, the geometric shape symmetry of the gear can be better guaranteed by polishing the two ends, and gravity center shift caused by polishing of one end is reduced.

1. Name of the product in this design: Vehicle-mounted air pump emergency starter power supply unit. 2. Purpose of this product design: An integrated air pump and power supply unit for inflating tires, balls, etc., and for emergency vehicle starting. 3. The key design feature of this product is its shape. 4. The image or photograph that best illustrates the design's key points: a 3D model.

The invention discloses an air turbine starter complete machine containment test platform and method. The air turbine starter complete machine containment test platform comprises a supporting assembly, a verification aluminum cylinder for judging the damage condition of wheel disc trisection fracture impact on the exterior of a starter, a safety protection assembly, a rotating speed control assembly and a high-speed photographing assembly for capturing the impact process. The super-dynamic strain response measuring assembly comprises a plurality of sets of strain gauges arranged on the periphery of the containing ring, and the strain gauges in the sets are arranged in the axial direction and the circumferential direction of the starter respectively. The vibration measurement assembly comprises acceleration sensors which are arranged in multiple groups and are perpendicular to one another in all positions of the shell; the trigger signal assembly comprises a trigger controller and a trigger line arranged on the outer wall of the containing ring, and the trigger controller is electrically connected with the high-speed camera, the super-dynamic strain response measuring assembly, the vibration measuring assembly and the high-pressure air source providing equipment and conducts trigger control on the high-speed camera, the super-dynamic strain response measuring assembly and the vibration measuring assembly. According to the invention, examination of the complete machine containing capacity of the air turbine starter is realized, and the strain of the containing ring, the vibration response of the shell and the impact load transmission in the impact process can be obtained.

The invention discloses an aviation starter generator with an internal cleaning function, and relates to the technical field of starter generators, the aviation starter generator comprises a machine body and a motor shaft, the motor shaft is rotatably mounted in the machine body, a rotor is arranged on the motor shaft, a stator is arranged in the machine body, two air ports are formed in the machine body, and two air filter assemblies are symmetrically arranged in the machine body. The two air filter assemblies are located on the outer sides of the stator and the rotor, the motor shaft is provided with the two sealing assemblies, the two sealing assemblies are located in the two air openings correspondingly, the two sealing assemblies are located on the outer sides of the two air filter assemblies, when the motor shaft operates, the sealing assemblies open the air openings, one air filter assembly extracts external air and guides the filtered air into the machine body, and the other air filter assembly is located on the outer side of the machine body. And the other air filtering assembly discharges air carrying heat out of the machine body from the air port. When the motor shaft rotates in a reversing mode, the wind filtering assembly discharges filtered dust and chippings generated by bearing operation out of the machine body, and cleaning and heat dissipation of the interior of the starting generator are achieved.

The article of this design is a jump starter used to start an automobile engine when the battery is dead.

The invention discloses a method for quickly verifying the capability of an auxiliary power device based on a rack, and the operation environment of the method comprises the steps: carrying out a simulation test on the rack, and simulating an inlet throat of an air turbine starter through a contraction nozzle in the test; before a test, a total pressure recovery coefficient sigma and a conversion inlet area At * of an air turbine starter are calculated, the minimum throat area At'of the shrinkage nozzle is determined, during the test, a test total pressure recovery coefficient sigma'and a conversion area At * 'of the shrinkage nozzle are calculated, and the minimum throat area At'of the shrinkage nozzle is determined by adjusting the test total pressure recovery coefficient sigma' or the minimum area At 'of the shrinkage nozzle. Enabling At * to be equal to At * ', obtaining the required power Pt of the auxiliary power device at the moment, calculating the test power Pt' of the auxiliary power device at the moment, and judging whether the capability of the auxiliary power device meets the requirement or not by comparing Pt with Pt '. Through the method, the verification method and difficulty are simplified, the capability of the auxiliary power device can be rapidly verified under the rack condition, and the verification efficiency is effectively improved.

1. Name of the product of this design: Air Pump Starter Power Supply All-in-One (JN‑8140). 2. Application of this product: used for inflating tires, starting cars, charging, etc. 3. The key point of the design of this product lies in its shape. 4. The picture or photo that best illustrates the design points: three-dimensional picture.

The invention discloses a compressor assembly, a heat pump system and a clothes dryer. The compressor assembly comprises a compressor and a heat pump assembly, the protective shell is arranged on the side, in the first direction, of the compressor, the protective shell is provided with a containing cavity, a wire outlet is formed in the side, in the second direction, of the protective shell, and the second direction is perpendicular to the first direction; and the starter is arranged in the accommodating cavity, and a lead wire of the starter is arranged in the wire outlet in a penetrating manner. According to the compressor assembly, the protective shell and the compressor are arranged in the first direction, the lead is led out of the protective shell in the second direction perpendicular to the first direction, the occupied space of the whole compressor assembly in the first direction can be reduced, and the space of the compressor assembly in the second direction can be fully utilized; all parts of the compressor assembly are arranged more reasonably in the first direction and the second direction, and the utilization rate of the installation space can be improved.

A starting apparatus for a first gas turbine engine of a plurality of gas turbine engines of an aircraft. The apparatus includes an air turbine starter, an electric machine, and a controller. The controller is configured to receive an emergency restart command for the first gas turbine engine while the aircraft is in-flight, determine whether the first gas turbine engine is in operation, determine whether at least a second gas turbine engine of the plurality of gas turbine engines is in operation, and, responsive to receiving the emergency restart command and determining that at least the second gas turbine engine of the plurality of gas turbine engines is in operation and that the first gas turbine engine is not in operation, perform an emergency restart of the first gas turbine engine.

A starting apparatus for a first gas turbine engine of a plurality of gas turbine engines of an aircraft. The apparatus includes an air turbine starter, an electric machine, and a controller. The controller is configured to receive an emergency restart command for the first gas turbine engine while the aircraft is in-flight, determine whether the first gas turbine engine is in operation, determine whether at least a second gas turbine engine of the plurality of gas turbine engines is in operation, and, responsive to receiving the emergency restart command and determining that at least the second gas turbine engine of the plurality of gas turbine engines is in operation and that the first gas turbine engine is not in operation, perform an emergency restart of the first gas turbine engine.

The combined structure of the current type starter and the protector comprises the current type starter and the protector, the current type starter is provided with an S pin and an M pin, the protector is provided with a protector pin, and the combined structure is characterized by further comprising an integrated installation mechanism which comprises a protector pin supporting seat and a protector pin locking cover, the protector pin supporting seat is located on the upward side of a current type starter cover plate of the current type starter and corresponds to the upper portion of the S pin and the upper portion of the M pin across the current type starter cover plate, and the protector pin is supported on the protector pin supporting seat and corresponds to the upper portion between the S pin and the M pin. And the protector pin locking cover is matched with the protector pin supporting seat in an inserting and embedding manner at a position corresponding to the upper part of the protector pin so as to lock the protector pin on the protector pin supporting seat. The method has the advantages that volume increase and obvious cost increase are avoided; assembly process links are reduced, and assembly efficiency is improved; and the reliability and the safety of the three-line column assembled on the refrigeration compressor are ensured.

1. Name of the designed product: combined frequency starter (mine explosion-proof and intrinsically safe type). 2. Use of the designed product: used for controlling explosion-proof motor in coal mine. 3. Design points of the designed product: combination of shape and pattern. 4. Picture or photo best indicating the design points: front view.

The present invention discloses a multi-purpose ground test bench, comprising: a test bench system, a measurement and control system, a measuring system, an intake system, and an exhaust system disposed on the test bench system. The test bench system is detachably configured to accommodate the installation of various types of test machines, including prototypes and models, and to adaptably connect to the intake and exhaust systems after installation. The measurement and control system is used to measure the output speed and torque of the test machine and adjust the output speed, thereby enabling the prototype machine to realistically simulate its actual operating state. The outlet of the intake system is connected to the test machine to supply the test machine with compressed air of a certain pressure, temperature, and flow rate required for the test. The intake end of the exhaust system is also connected to the intake system and the test machine. The present invention can meet the requirements of ground test benches for various types of air turbine starters, while also taking into account small-power model turbine testing, thereby improving the comprehensive utilization rate of the test bench and reducing testing costs.

The present application relates to digital display press technical field, and disclose four position drive end cover press lock mouth machine, including platform base, the top of platform base is equipped with workpiece conveying device, the top of platform base is equipped with first work position, second work position, third work position and fourth work position which are annularly and equidistantly distributed. The four position drive end cover press lock mouth machine has the advantages of high efficiency, labor saving, high press-in progress, etc. It solves the problems of low efficiency, high labor intensity, poor press-in accuracy, lack of statistical function and poor adaptability in the existing starter drive end cover assembly which mostly adopts manual operation.

A vehicle includes an engine, an intake manifold, a starter motor, a battery, and a control apparatus. The intake manifold is coupled to the engine. The starter motor is configured to start up the engine. The battery is configured to drive the starter motor. The control apparatus includes one or more processors, and one or more memories coupled to the one or more processors. The one or more processors are configured to execute idle reduction control, and execute, during execution of the idle reduction control and before cancelling the idle reduction control, adjustment control of adjusting an internal pressure of the intake manifold and causing the internal pressure of the intake manifold to be lower as a voltage of the battery is lower.

The utility model discloses a control system for soft start of a motor in the papermaking industry, which comprises a soft starter RQ, a terminal 7 and a terminal 10 of the soft starter RQ are in short circuit, a terminal 8 and a terminal 9 of the soft starter RQ are in short circuit, the terminal 8 and the terminal 9 of the soft starter RQ are both connected with one end of a normally open contact of a relay KA, and the other end of the normally open contact of the relay KA is connected with the terminal 7 and the terminal 10; and the terminals L11, L12 and L13 of the soft starter RQ are connected with one end of a contact of a contactor 2KM, and the other end of the contact of the contactor 2KM is connected with a motor M. The soft starter has the following advantages that the motor can continuously operate under the condition that the soft starter misreports a fault, and after the fault is misreported, the motor can still continuously operate and has circuit break protection, so that the condition that components are damaged cannot occur.

This application belongs to the field of aero-engine design and presents a design method for high-altitude starting fuel supply patterns based on the low-altitude starting fuel supply patterns. It involves first conducting high-altitude bench tests on the starter to obtain the power reduction characteristics of the starter at different altitudes. Then, based on the power balance equation, the acceleration time of the starter from rotor standstill to idle speed is determined. Finally, based on the acceleration time of the starter from rotor standstill to idle speed, the time allocation of the three starting stages of the starting process—starter engagement, starter disengagement, and engine starting—is performed to obtain the high-altitude starting fuel supply pattern. This method enables rapid and accurate design of the high-altitude fuel supply pattern, taking into account the engine's stability margin design in high-altitude areas, starter power characteristics, and the attenuation characteristics of starter power with increasing altitude, thus avoiding abnormal phenomena such as engine cold suspension and overheating. Furthermore, it can be based on ground starting data statistics, achieving better design compatibility and reducing debugging work.

1. Name of the product in this design: Emergency Starter Power Supply (YTJ-B3-01). 2. Purpose of this design: To inflate and replenish the air in all types of inflatable products, including bicycle tires, motorcycle tires, electric vehicle tires, wheelchairs, balance bikes, and car tires. It also has lighting and emergency power functions. 3. The key design feature of this product is its shape. 4. The image or photograph that best illustrates the design's key points: a 3D model.