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41results about How to "Reduced risk of cavitation" patented technology

Excavator hydraulic system anti-air-suction controlling method and controlling device and excavator

The invention discloses an excavator hydraulic system anti-air-suction controlling method and controlling device and an excavator. The controlling method comprises the steps that: a pilot pressure value and a main pump pressure value are acquired; whether an excavator hydraulic system is in an air sucking status is judged based on the pilot pressure value and the main pump pressure value; and if the excavator hydraulic system is in the air suck status, compensating current is added to controlling current of a main pump to enable the main pump to adjust output oil amount based on the compensating current. Electric signals replace traditional hydraulic signals in judging whether the hydraulic system is in an air sucking status; the air sucking risk is lowered in a manner that oil supply amount is actively added; and the technical effects that precise judgment on whether the hydraulic system is in an air sucking status can be realized without adding extra controlling components and that the air sucking risk is lowered via linear addition of the oil supply amount to the system.
Owner:WEICHAI POWER CO LTD +1

Oil transportation heat management integrated system for controlling fuel oil temperature rise of high-speed aircraft

The invention provides an oil transportation heat management integrated system for controlling fuel oil temperature rise of a high-speed aircraft. The oil transportation heat management integrated system comprises a main oil tank, a built-in oil tank, an oil pump, a first oil pipe, a second oil pipe, a supporting frame and an air inlet pipe. Oil tank pressurized gas enters the main oil tank from the gas inlet pipe to provide pressure for fuel oil in the main oil tank, so that the fuel oil is conveyed to the built-in oil tank from the main oil tank through the first oil pipe, then is conveyed to the oil pump through the second oil pipe, and finally is supplied to an engine through the oil pump. According to the technical scheme, the built-in oil tank is arranged in the main oil tank, the temperature of fuel oil at the flight tail section of the long-endurance high-speed aircraft can be effectively reduced, and the effects of reducing the cavitation risk of a fuel oil pump, reducing thepressurization pressure of a fuel oil tank, reducing the design difficulty of oil passing equipment, increasing available fuel oil heat sinks of an engine and the like can be achieved. The method canbe applied to high-speed aircrafts such as high-speed aircrafts and aerospace aircrafts.
Owner:BEIJING AEROSPACE TECH INST

Multi-stage throttling labyrinth pressure reducing valve

The invention provides a multi-stage throttling labyrinth pressure reducing valve which comprises a spring cover, a shell and a lower end cover. An adjusting nut is arranged at the upper end of the spring cover, an adjusting spring is arranged between the adjusting nut and a valve element, a return spring is arranged between the valve element and the lower end cover, the valve element is located in a sliding sleeve, the sliding sleeve is fixed in the shell, the shell forms a high-pressure cavity of an inlet and an outlet, a transition cavity is formed in the valve element, the shell and the sliding sleeve form a low-pressure cavity I, the lower end cover and the valve element form a low-pressure cavity II, the sliding sleeve and the valve element are correspondingly provided with upper throttling ports which communicate with the low-pressure cavity I and the transition cavity, the sliding sleeve and the valve element are correspondingly provided with middle throttling ports which communicate with the high-pressure cavity and the transition cavity, and the valve element is provided with a lower throttling port which communicates with the low-pressure cavity II and the transition cavity. The multi-stage throttling labyrinth pressure reducing valve has the advantages that pressure regulation is smooth and accurate, the anti-interference capability of the valve is improved, the structure is simple, maintenance is convenient, the service life is long, the cavitation risk of primary throttling high pressure difference is reduced, medium pressure feedback is more sensitive, and precision is higher.
Owner:HENAN AEROSPACE HYDRAULIC & PNEUMATIC TECH

Pressurization type liquid ring vacuum pump water return system with rotating film and water return method thereof

The invention discloses a pressurization type liquid ring vacuum pump water return system with a rotating film, and relates to the liquid ring vacuum pump water return system applied in the fields of chemical engineering, machinery, exploration, electric power and the like. The liquid ring vacuum pump water return system comprises a vacuum pump body, a vapor-water separator, a feeding pipe, a discharging pipe, a pressurization pump, a rotating film area, a cooling liquid inlet, a vapor-water separation area, a heat exchange area, a commutating area, a flow guide plate, a gas-phase passage and an annular separating plate, wherein a rotating film tube is installed in the rotating film area, and the tube wall of the rotating film tube is provided with rotating film holes; a heat exchange separating plate is installed in the heat exchange area, and a heat exchange liquid inlet communicates with a water inlet of a lower heat exchange pipe; a heat exchange liquid outlet communicates with a water outlet of an upper heat exchange pipe; and the input end of the pressurization pump communicates with a separating liquid outlet, and the output end of the pressurization pump communicates with a water return port and the cooling liquid inlet. By means of the pressurization type liquid ring vacuum pump water return system with the rotating film, water return fluid disturbance can be reduced, and resistance is lowered. The invention further relates to a water return method of the pressurization type liquid ring vacuum pump water return system with the rotating film.
Owner:CENT SOUTHERN CHINA ELECTRIC POWER DESIGN INST CHINA POWER ENG CONSULTING GROUP CORP

Fuel injection valve sleeve assembly

The invention belongs to the technical field of fuel injectors, and discloses a fuel injection valve sleeve assembly which comprises a valve sleeve body and a throttling sleeve, wherein an operation groove and a control groove are respectively formed at two opposite sides of the valve sleeve body, the operation groove is communicated with the control groove through a first throttling hole, and anoil inlet hole communicated with the outside is formed in the side wall of the operation groove; the throttling sleeve is clamped at the bottom of the operation groove or the control groove, a secondthrottling hole and an inner side counter bore are formed at the two opposite sides of the throttling sleeve respectively, and an opening at one end of the second throttling hole is located in the inner side counter bore; the inner side counter bore is communicated with the first throttling hole, and the hole diameter of the first throttling hole and the hole diameter of the second throttling holeare both smaller than that of the inner side counter bore. According to the fuel injection valve sleeve assembly, because of the split clamping design of the valve sleeve body and the throttling sleeve, the machining and manufacturing difficulty and cost are reduced, and the secondary throttling can be achieved with lower cost.
Owner:FAW JIEFANG AUTOMOTIVE CO

Classified pool-inlet high-dam flood discharge energy dissipater for bottom flow and energy dissipating method

InactiveCN103898882BReduce pulsating loadsAvoid damageBarrages/weirsThree levelEngineering
The invention discloses a classified pool-inlet high-dam flood discharge energy dissipater for bottom flow. The classified pool-inlet high-dam flood discharge energy dissipater comprises a gravity dam and an absorption basin. At least two different elevation positions in a body of the gravity dam are provided with flow discharging channels extending downstream respectively, and falling banks are arranged below outlets of the flow discharging channels, wherein the falling banks are internally provided with ventilation galleries and ventilation holes. At least three levels of steps are sequentially arranged in the absorption basin from the upstream part to the downstream part. When flow passes through the top and the interior of the dam at the same time, the outlets of the flow discharging channels are sequentially located on vertical faces of the steps, with the corresponding level numbers from the upstream part to the downstream part, in the absorption basin from high to low according to the elevation of the outlets. When the flow only passes through the interior of the dam, the outlets of all the flow discharging channels are sequentially located on the vertical face at the starting position of the first-level step in the absorption basin and the vertical faces of the steps with the corresponding level numbers from the upstream part to the downstream part in the absorption basin from high to low according to the elevations of the outlets. With the energy dissipater, water in a reservoir enters the absorption basin from the flow discharging channels at the different elevations or from the top of the gravity dam and the flow discharging channels of the different elevations, and the water is scattered on the faces of the steps with the corresponding level numbers from the upstream part to the downstream part respectively in the absorption basin for energy dissipation.
Owner:SICHUAN UNIV

Oil transportation heat management system design method for controlling temperature rise of fuel oil of high-speed aircraft

The invention provides an oil transportation heat management system design method for controlling the temperature rise of fuel oil of a high-speed aircraft, and the method comprises the steps: building a main oil tank heat transfer model without a built-in oil tank based on a main oil tank structure model; based on the fuel temperature rise curve of the main oil tank heat transfer model without the built-in oil tank, determining the fuel consumption at the fuel target temperature; determining the initial volume of the built-in oil tank based on the fuel consumption at the target fuel temperature; based on the main oil tank structure model and the initial volume of the built-in oil tank, establishing a main oil tank heat transfer model of the built-in oil tank; and determining the final volume of the built-in oil tank based on the highest temperature of the fuel oil temperature rise curve of the main oil tank heat transfer model with the built-in oil tank, the fuel oil target temperature and the initial volume of the built-in oil tank. The method can effectively reduce the temperature of the fuel at the flight tail section of the long-endurance high-speed aircraft, and can achieve the effects of reducing the cavitation risk of a fuel pump, reducing the pressurization pressure of a fuel tank, reducing the design difficulty of fuel passing equipment, increasing the available fuelheat sink of an engine and the like.
Owner:BEIJING AEROSPACE TECH INST

Multi-stage low-temperature centrifugal pump provided with built-in motor

The invention provides a multi-stage low-temperature centrifugal pump provided with a built-in motor. The multi-stage low-temperature centrifugal pump comprises a front shell, a motor shell and a backshell; a forward impeller and a forward guide vane are arranged in the front shell; the motor is arranged in the motor shell; a reverse impeller and a reverse guide vane are arranged in the back shell; the motor shell is located between the front shell and the back shell; an inlet horn pipe is arranged at the end of the front shell; an outlet volute is arranged between the back shell and the motor shell; the forward impeller, a motor rotor and the reverse impeller are connected in series through a rotating shaft assembly; the motor rotor is directly connected with the rotating shaft assemblyfrom the middle to drive the rotating shaft assembly to rotate so as to drive the forward impeller, the reverse impeller and an inducer to rotate. A low-temperature liquid enters a pump body from theinlet horn pipe, is pressurized by the forward impeller and the reverse impeller and is sprayed out of the outlet volute. According to the pump, the motor is arranged internally and is cooled throughthe low-temperature liquid, the overall sealing performance is good, the size is small, the weight is light, the structure is compact, and the pump is particularly applicable to conveying of low-temperature volatile liquids.
Owner:JIANGSU UNIV

Engine cooling system and control method thereof

The invention relates to an engine cooling system and a control method thereof. The engine cooling system comprises an engine heat dissipation mechanism and an engine degassing mechanism, wherein theengine heat dissipation mechanism comprises a temperature control valve, an engine water outlet pipeline connected with the temperature control valve, a radiator assembly connected with the engine water outlet pipeline, and an engine water inlet pipeline connected with the radiator assembly; the engine degassing mechanism comprises an engine degassing pipeline, a degassing chamber assembly connected with the engine degassing pipeline, a degassing chamber water outlet pipeline connected with the degassing chamber assembly, and a radiator degassing pipeline connected with a water inlet of the radiator assembly and the degassing chamber assembly; the radiator degassing pipeline is connected with the engine degassing pipeline through a three-way valve; a first stop valve is arranged on the engine water inlet pipeline; and a control valve for preventing reverse flow is arranged on the radiator degassing pipeline. By means of the engine cooling system and the control method thereof, the engine warming speed of an engine can be increased in the low-temperature starting process of the engine and the engine warming stage of the engine.
Owner:DONGFENG MOTOR CORP HUBEI

Fuel injection valve and diesel engine

The invention discloses a fuel injection valve and a diesel engine, and belongs to the field of engine fuel injection valves. A control valve sleeve of the fuel injection valve is provided with an oiloutlet passage, and a throttle orifice plate is provided with a low-pressure oil passage, so that the cavitation risk of a sealing conical surface at the top of the throttle orifice plate is favorably reduced; a first throttling ring belt and a second throttling ring belt are successively formed between a long needle valve and the inner wall of the control valve sleeve in the ascending process ofthe long needle valve, the area of the first throttling ring belt and the area of the second throttling ring belt are gradually increased along with ascending of the long needle valve, and the firstthrottling ring belt and the second throttling ring belt jointly play a throttling role, so that the flow of high-pressure oil flowing into a control cavity from an oil inlet hole is rapidly reduced,the pressure of the control cavity is rapidly reduced, and the opening delay is shortened; and the area of the first throttling ring belt and the area of the second throttling ring belt are graduallydecreased along with descending of the long needle valve, the flow of the high-pressure oil flowing into the control cavity from the oil inlet hole is gradually increased, pressure in the control cavity is rapidly established, the closing speed of the long needle valve is increased, and the closing delay time is shortened.
Owner:FAW JIEFANG AUTOMOTIVE CO

Commercial vehicle blade type variable pump

The invention provides a commercial vehicle blade type variable pump which comprises a pump body, a rotor, blades, a positioning ring, a variable sliding block and a variable spring. An oil inlet, anoil outlet and a rotor cavity are formed in the pump body, and a concave oil suction cavity and a concave oil pressing cavity are formed in the bottom of the rotor cavity. A first groove and a secondgroove which are staggered with the oil inlet and the oil outlet correspondingly are formed in the side wall of the rotor cavity, the variable sliding block is installed in the rotor cavity, a first U-shaped part embedded in the first groove and a second U-shaped part embedded in the second groove are arranged on the peripheral face of the variable sliding block, a feedback oil cavity is formed between the first groove and the first U-shaped part, and a spring cavity is formed between the interior of the second groove and the second U-shaped part and used for installing the variable spring. The positions of the feedback oil cavity and the spring cavity both incline towards the oil suction cavity, and under the action of oil pressure in the feedback oil cavity or the elastic force of the variable spring in the spring cavity, the variable sliding block can move in the rotor cavity in the radial direction, and therefore, the operation reliability of the oil pump can be improved.
Owner:HUNAN OIL PUMP

A multi-stage throttling labyrinth pressure reducing valve

The invention proposes a multi-stage throttling labyrinth pressure reducing valve, which includes a spring cover, a housing and a lower end cover. An adjusting nut is provided on the upper end of the spring cover, and an adjusting spring is provided between the adjusting nut and the valve core. There is a return spring between the covers, the valve core is located in the sliding sleeve, and the sliding sleeve is fixed in the housing, the housing forms a high-pressure chamber for the inlet and outlet, the valve core forms a transition chamber, the housing and the sliding sleeve form a low-pressure chamber I, and the lower end cover The low-pressure chamber II is formed with the spool. The sliding sleeve and the spool are correspondingly provided with an upper throttle port connecting the low-pressure chamber I and the transition chamber, and the sliding sleeve and the spool are correspondingly provided with a middle throttle port connecting the high-pressure chamber and the transition chamber. The spool is provided with a lower throttle port connecting the low-pressure chamber II and the transition chamber. The invention has the advantages of smooth and precise pressure regulation; improved anti-interference ability of the valve; simple structure, convenient maintenance and long service life; reduced cavitation risk of high pressure difference at the first level of throttling; more sensitive feedback medium pressure and higher precision .
Owner:HENAN AEROSPACE HYDRAULIC & PNEUMATIC TECH
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