Patents
Literature
Patsnap Copilot is an intelligent assistant for R&D personnel, combined with Patent DNA, to facilitate innovative research.
Patsnap Copilot

69results about How to "Enhance the dynamic pressure effect" patented technology

Liquid lubricated end face seal structure with cross-scale surface texture characteristic

ActiveCN101696728AImprove throttling effectEnhanced pumping effectEngine sealsPump componentsLubricationMicrometer
The invention discloses a liquid lubricated end face seal structure with a cross-scale surface texture characteristic, which comprises a moving ring and a static ring of a mechanical seal; and one side of an end face of the moving ring/static ring is a high pressure side, namely an upstream, while the other side is a low pressure side, namely a downstream. The liquid lubricated end face seal structure is characterized in that: a plurality of cross-scale texture face grooves are processed on the end face of the moving ring or the static ring of the mechanical seal; each cross-scale texture face groove consists of a millimeter deep groove and micrometer micropores; the deep groove is positioned at the upstream of the end face; the micropores are distributed on the periphery of the deep groove; seal weirs are arranged between the cross-scale texture face grooves; and a downstream of each cross-scale texture face groove is provided with an annular seal dam of a non-opened face groove. The liquid lubricated end face seal structure has the advantages of improving seal lubrication, improving the rigidity of a fluid film and the pressure and heat resistance of the mechanical seal, greatly strengthening the operational reliability, stability and leak tightness of the seal, and prolonging the service life of the seal.
Owner:ZHEJIANG UNIV OF TECH +1

Double-row tilting directional microporous end surface no-leakage mechanical sealing structure

ActiveCN101672364AImproved hydrodynamic effect and tightnessGood start and stop effectEngine sealsDouble rowEngineering
The invention relates to a double-row tilting directional microporous end surface no-leakage mechanical sealing structure, comprising a dynamic ring and a static ring which are sealed mechanically, wherein one side of the end surface of the dynamic ring or the static ring is an high-voltage side, namely an upstream part, and the other side thereof is a low-voltage side, namely an downstream part,the end surface of the dynamic ring or the static ring is provided with an outer microporous ring belt and an inner microporous ring belt; microporous long shafts of the outer microporous ring belt and the inner microporous ring belt are opposite to the direction of a tilting angle of the diameter of the sealing end surface passing through the center of the micropore; the outer microporous ring belt and the inner microporous ring belt are respectively arranged on the upstream part and the downstream part of the end surface; and a continuous ring-shaped sealing dam are respectively arranged between the outer microporous ring belt and the inner microporous ring belt and the downstream part of the inner microporous ring belt. The mechanical sealing structure has the beneficial effects of: realizing no contact, wear resistance and no leakage of sealing, prolonging the service life and improving the sealing reliability.
Owner:ZHEJIANG UNIV OF TECH

Microgroove double-layer composite groove deep end surface mechanical seal structure

The invention discloses a microgroove double-layer composite groove deep end surface mechanical seal structure which comprises a movable ring and a static ring. The movable ring and the static ring are mechanically sealed, a mutual contact surface of the movable ring and the static ring is an end surface, and a microgroove double-layer composite groove deep dynamical pressure groove, a ring groove and a microgroove double-layer composite groove deep pumping groove which are symmetrically distributed along a rotation center are sequentially arranged on the end surface of the movable ring or the static ring from a high pressure side to a low pressure side; the dynamical pressure groove is arranged on the upstream (the high pressure side) of the end surface, the upper layer of the dynamical pressure groove is hollow, and a microgroove shape line on the lower layer of the dynamical pressure groove forms an upstream texture and is same to a dynamical pressure groove shape line on the upper layer; the pumping groove is arranged on the downstream ( the lower pressure side) of the end surface, the upper layer of the pumping groove is hollow, and a microgroove shape line on the lower layer of the pumping groove forms a downstream texture and is same to a shape line on the upper layer of the pumping groove; the upstream texture and the downstream texture are connected through the ring groove; and the inclining direction of the pumping groove is opposite to that of the dynamical pressure groove.
Owner:山东誉中新材料股份有限公司

Dynamic-static pressure combined type asymmetrical waviness end face fluid mechanical sealing structure

The invention provides a dynamic-static pressure combined type asymmetrical waviness end face fluid mechanical sealing structure. At least one sealing end face on a moving ring and a stationary seal ring is provided with more than two three-dimensional asymmetrical waviness appearances, the asymmetrical waviness is in a periodical arrangement on the at least one sealing end face, the asymmetrical waviness sealing end face comprises a dam area, a conical surface and a wave crest and a wave trough of the asymmetrical waviness, the dam area is a groove-less parallel annular sealing dam arranged at the low-pressure side, the wave crest and the wave trough are connected through the conical surface, the conical surface is a linear convergence cone formed from the high-pressure side to a low-pressure side and is connected with the dam area, the conical surface can realize sealed non-contact static pressure effect; the conical degree combines with the asymmetrical waviness so that the sealing reliability can be improved, an asymmetrical waviness smooth transition curve can prevent the particles in the sealing fluid from being cumulated, and the dam area can realize static sealing when the axle is stationary. The structure provided by the invention has strong pressure resistance and antijamming capability, the leakage rate is lower at the conditions of high parameters, the fluid has good dynamic pressure effect in the process of start and stop and the fluid bearing capacity is sufficient in the normal operation.
Owner:TSINGHUA UNIV

Non-contact mechanical seal ring with dual-rotating-direction hydrodynamic grooves

The invention provides a non-contact mechanical seal ring with dual-rotating-direction hydrodynamic grooves. Hydrodynamic groove structure units in same forms are arranged on the outer side of a seal end face circumferentially at equal intervals; the hydrodynamic groove structure unit is in a wing-shaped structure formed by a central groove and same wing grooves which are connected to two sides of the central groove respectively and which extend symmetrically in a converged manner; the central groove and two wall edges thereof are two radial extending segments of the seal end face respectively, the wall edge on the inner side is an arc concentric with the seal end face, and the central groove is formed in the circumferential wall of a seal ring body, long side edges of two sides of the wing grooves and short grooves at the converged-extending ends are two radial extending segments of the seal end face; the long side edges of two sides of the wing grooves fit and are connected with the side wall of the central groove where the same located. By the aid of the hydrodynamic groove structure, seal hydrodynamic effect can be improved, seal end face opening force is increased, thickness and strength of the fluid film between the seal end faces are increased, seal leakage is reduced, groove processing difficulty is reduced, and process requirements on seal parts processing and assembling are lowered.
Owner:SICHUAN SUNNY SEAL

Circumferential sectioned helium sealing device for oxygen turbine pump of hydrogen oxygen engine

The invention discloses a circumferential sectioned helium sealing device for an oxygen turbine pump of a hydrogen oxygen engine. According to the circumferential sectioned helium sealing device, a circumferential sectioned sealing ring I and a circumferential sectioned sealing ring II are placed in a cavity formed by a cover plate and a sealing shell; sealing shaft sleeves are placed in rings of the circumferential sectioned sealing ring I and the circumferential sectioned sealing ring II; the circumferential sectioned sealing ring I and the circumferential sectioned sealing ring II are oppositely placed and pre-tensioned by virtue of pre-tensioning springs; and each of the circumferential sectioned sealing ring I and the circumferential sectioned sealing ring II is formed by connecting a plurality of fan-shaped arc sections with the same structure end to end, and constrained on an excircle surface through garter springs. According to the circumferential sectioned helium sealing device, each sealing ring is composed of the plurality of fan-shaped arc sections, a hydrodynamic groove structure is introduced, and a hydrodynamic effect of a sealing clearance fluid is adequately utilized, thus the helium sealing device reliably works under an extremely small clearance, and a low leakage amount is maintained.
Owner:BEIJING AEROSPACE PROPULSION INST

Micro-bulge double-layer composite groove deep end surface mechanical seal structure

The invention discloses a micro-bulge double-layer composite groove deep end surface mechanical seal structure which comprises a movable ring and a static ring. The movable ring and the static ring are mechanically sealed, a mutual contact surface of the movable ring and the static ring is an end surface, and a micro-bulge double-layer composite groove deep dynamical pressure groove, a sealing dam, a ring groove and a micro-bulge double-layer composite groove deep pumping groove which are symmetrically distributed along a rotation center are sequentially arranged on the end surface of the movable ring or the static ring from a high pressure side to a low pressure side; the dynamical pressure groove is arranged on the upstream (the high pressure side) of the end surface, and a micro-bulge body texture is processed on the lower layer of the dynamical pressure groove; the pumping groove is arranged on the downstream ( the lower pressure side) of the end surface, and a micro-bulge body texture is processed on the lower layer of the pumping groove; the inclining direction of the pumping groove is opposite to that of the dynamical pressure groove; the sealing dam is an unprocessed smooth plane; and the ring groove is communicated with the pumping groove and arranged on the upstream of the pumping groove.
Owner:JINTUO PETROLEUM MACHINERY MANUFACTRING CO LTD

Pulse hydraulic fracturing device and method based on continuous rotary valve

The invention provides a pulse hydraulic fracturing device and method based on a continuous rotary valve. The pulse hydraulic fracturing device based on the continuous rotary valve is composed of a water tank, a water injection pipeline, a water pump, a pressure relief pipeline, the continuous rotary ball valve, a hydraulic motor and the like. According to the pulse hydraulic fracturing method based on the continuous rotary valve, stable pulse water pressure is generated in the water injection pipeline through periodical opening and closing of the continuous rotary ball valve, and a novel technical approach is provided for dynamic hydraulic fracturing of coal rocks. After the continuous rotary ball valve is connected into the water injection pipeline, a valve element of the continuous rotary ball valve is driven by the hydraulic motor to rotate, the valve is opened and closed continuously and stably, the periodical water hammer effect is formed in a water path injected into a coal rock body, and the pulse water pressure is generated; and the continuous rotary ball valve is improved, when the improved continuous rotary ball valve is closed, high-pressure water in the coal rock body can decrease the pressure actively, the vibration amplitude of the pulse water pressure is increased, and the technical effect of hydraulic fracturing is improved.
Owner:CHINA UNIV OF MINING & TECH

Novel active air foil bearing based on PZT and SMA

The invention discloses a novel active air foil bearing based on PZT and SMA. The novel active air foil bearing comprises a shaft sleeve, piezoelectric ceramics (PZT), a memory alloy wire mesh block (SMA block), flexible hinges, a rigid push rod, pre-pressure applying devices, a cooling pipe, a wave foil and a top foil; the PZT and the SMA block are installed in pre-machined through grooves, the corresponding pre-pressure applying devices are designed for the PZT and SMA block, the wave foil is formed by pressing an elastic material, one end of the wave foil is welded, and the other end of thewave foil is free. The top foil overlies the wave foil. Power supply signals of the PZT are controlled, the flexible hinges are coupled, PZT deformation is amplified, the wave foil is supported by the rigid push rod, the wedge-shaped space is enlarged, therefore, the crossed coupling effect is weakened, the dynamic pressure effect of the bearing is enhanced, and the rigidity characteristic of thebearing is improved; by controlling the temperature of the SMA block, the SMA block expands and contracts to generate larger structural damping, and the damping characteristic of the bearing is improved; and finally, the rigidity and damping characteristics of the bearing are actively controlled, and the stability of the system is improved.
Owner:HUNAN UNIV

Novel active air foil bearing based on PZTs and flexible hinges

The invention discloses a novel active air foil bearing. The bearing comprises a shaft sleeve, the PZTs, the flexible hinges, rigid push rods, precompression exertion devices, wave foil and top foil; the shaft sleeve is machined through wire cutting, three PZT mounting through grooves circumferentially and evenly distributed, the corresponding flexible hinges and the corresponding rigid push rods are obtained, the top ends of the rigid push rods are flush with the inner cylindrical face of the shaft sleeve, the PZTs are mounted in the through grooves, the corresponding precompression exertion devices are designed for the PZTs, the wave foil is formed by pressing of elastic materials, and is arranged on the shaft sleeve and the inner cylindrical faces of the rigid push rods, one end of the wave foil is welded to the inner round face of the shaft sleeve, and the other end of the wave foil is free. The top foil is arranged on the wave foil in a covering manner. Through control over power supply signals of the PZTs, the PZTs mechanically deform, the flexible hinges are enlarged to deform, and are supported through the rigid push rods to be attached to the wave foil on the push rods and the inner wall of the shaft sleeve, a gap between a bearing and a supporting rotor is changed, the wedge space is increased, the crossed coupling effect is weakened, the bearing dynamic pressure effect is enhanced, the rigid characteristic of the bearing is improved, and finally the aims of actively controlling the rigidity characteristics of the bearing and improving the stability of the bearing are achieved.
Owner:HUNAN UNIV

Gas-lubricated bird-wing-shaped groove end face seal structure

A gas lubrication bird-wing-shape-imitation v groove end face sealing structure comprises two sealing rings with sealed end faces; the two sealing rings comprise a movable ring and a static ring; the end face of at least one of the movable ring and the static ring is provided with a plurality of bird-wing-shape-imitation v grooves; each bird-wing-shape-imitation v groove is composed of a tail-feather-shape-imitation v groove body and a flight-feather-shape-imitation v groove body; the tail-feather-shape-imitation v groove bodies are provided with swallow-tail-shaped furcal tails; the flight-feather-shape-imitation v groove bodies are roughly in a bull horn shape with the thick ends and the tail tip ends; the tail-feather-shape-imitation v groove bodies are transversely arranged at the thick ends of the flight-feather-shape-imitation v groove bodies; the thick segments of the flight-feather-shape-imitation v groove bodies and the thick ends of the tail-feather-shape-imitation v groove bodies are toward airflow; the bird-wing-shape-imitation v grooves are arranged to be bird-wing-shape-imitation v groove annular belts; secondary annular sealing dams are arranged between the bird-wing-shape-imitation v groove annular belts; annular main sealing dams are arranged on the low-pressure sides of the end faces; drainage grooves are arranged on the high-pressure sides of the end faces; the drainage grooves and the bird-wing-shape-imitation v grooves are shallow grooves of the micrometer scale; the depths of the flight-feather-shape-imitation v groove bodies are gradually decreased in the airflow direction. The sealing structure has the advantages of being good in stability and long in service life, and resisting abrasion.
Owner:ZHEJIANG UNIV OF TECH

Intelligent hybrid bearing based on negative-poisson-ratio structure

The invention discloses an intelligent hybric bearing based on a negative-poisson-ratio structure. The intelligent hybric bearing comprises a main shaft, a bearing body and an oil inlet device. The bearing body is arranged on the main shaft in a sleeving manner. An installation hole is formed in the bearing body. The oil inlet device is installed in the installation hole. A first static pressure cavity and a second static pressure cavity which communicate with each other are formed in a bearing face of the bearing body. The oil inlet device is connected with the second static pressure cavity through an oil inlet formed in the bottom of the installation hole. The negative-poisson-ratio structure is adopted in the oil inlet device for achieving oil supply adjustment. According to the intelligent hybric bearing based on the negative-poisson-ratio structure, a specific stretching effect of the negative-poisson-ratio structure is utilized, bearing vibration and eccentricity can be effectively reduced, and therefore the movement precision is improved; and meanwhile, the dependency on bearing clearances under the high-speed work condition is lowered, and the problems that a traditional high-precision hybrid bearing is difficult to machine and likely to be blocked are solved.
Owner:洛阳神实轴承科技有限公司

End-surface mechanical seal structure with sharkskin-imitated surface three-dimensional shape

ActiveCN106838323APrevent adhesionTo achieve the effect of enhanced heat dissipationEngine sealsThree dimensional shapeEngineering
The invention discloses an end-surface mechanical seal structure with a sharkskin-imitated surface three-dimensional shape. The end-surface mechanical seal structure comprises a moving ring or a fixed ring as mechanical seal, wherein the outer ends of the seal end surfaces of the moving ring and the fixed ring are taken as high-pressure sides, namely upstream parts, and the inner ends of the seal end surfaces are taken as low-pressure sides, namely downstream parts; a circle of closed seal dam is arranged at the upstream high-pressure side of at least one seal end surface in the moving ring or the fixed ring, a plurality of upstream pump grooves are uniformly arranged on the circumference of the surface of the seal end surface, a first end of each upstream pump groove extends to the high-pressure side of the seal end surface, and a second end extends to the low-pressure side of the seal end surface; an area between two adjacent upstream pump grooves is a seal weir; micro convex body clusters with the sharkskin-imitated surface shape are processed on the bottoms of the grooves and the surfaces of the seal weirs; the micro convex body clusters are arranged in a staggered manner until the micro convex body clusters uniformly bestrew the whole seal weirs and the bottoms of the upstream pump grooves; and the micro convex body clusters are formed by a plurality of parallel micro convex body units. The end-surface mechanical seal structure has the beneficial effects that attachment, drag reduction, wear resistance and enhanced heat dissipation of marine fouling organisms are prevented through the sharkskin-imitated surface three-dimensional shape.
Owner:ZHEJIANG UNIV OF TECH

Two-way rotating gas dynamic/static pressure mechanical seal type bird wing-shaped groove structure

The invention discloses a two-way rotating gas dynamic / static pressure mechanical seal type bird wing-shaped groove structure. The structure comprises two mechanically sealed sealing rings-a dynamic ring and a static ring. The structure is characterized in that a plurality of bird wing-shaped grooves are formed in the end surface of at least one sealing ring of the dynamic ring and the static ring; the bird wing-shaped grooves are shallow grooves in micrometer scale, and consist of tail feather-shaped grooves and flight feather-shaped grooves; the tail feather-shaped grooves have swallow tail-shaped furcal tails; the flight feather-shaped grooves substantially take the shape of ox horns with thick ends and tail tip ends; the tail feather-shaped grooves are transversely arranged at the thick ends of the flight feather-shaped grooves; every two bird wing-shaped grooves form groove pairs in a splayed shape; multiple groove pairs are evenly arranged peripherally to form a bird wing-shaped groove ring belt; the bird wing-shaped groove ring belt is arranged at the high-pressure side of the end surface; and the depths of the flight feather-shaped grooves are gradually decreased in the airflow direction. The structure has the characteristics of two-way rotation, excellent opening character, good stability, wear resistance and long service life.
Owner:ZHEJIANG UNIV OF TECH

Micro-hole end face mechanical seal structure with air inlet grooves

A micro-hole end face mechanical seal structure with air inlet grooves comprises two end faces for mechanical sealing, namely a moving ring and a stationary ring, wherein one end face is sequentially provided with micro-hole groups and annular sealing dams which are symmetrically distributed relative to the rotation center from the high-pressure side to the low-pressure side. Multiple rows of micro-hole groups are distributed on the high-pressure side of the end face and comprise the linear air inlet grooves and multiple elliptic micro-holes, the centers of the micro-holes are located on the air inlet grooves, included angles formed by long shafts of the micro-holes and the air inlet grooves are identical, and one end of each micro-hole facing air flows is located on the high-pressure side of the end face. A straight line where the air inlet grooves are located is located on the radius of the end face. The low-pressure side of the end face is provided with the annular sealing dams with smooth faces. The micro-hole end face mechanical seal structure has the advantages that the opening performance under the high-pressure frequent start-stop condition is improved; the problem of poor hydrodynamic effect of the end faces caused by the air negative pressure effect is solved; the solid particle preventing capacity and the advantages of the micro-holes are fully played; the hydrodynamic effect and the disturbance-resisting performance are enhanced, the service life is prolonged, and the stability of the end faces is improved.
Owner:ZHEJIANG UNIV OF TECH

End face mechanical seal structure with air inlet grooves and micropores

An end face mechanical seal structure with air inlet grooves and micropores comprises two end faces for mechanical seal. The two end faces are a moving ring and a static ring. Micropore groups in symmetrical distribution according to the rotation center and a ring-shaped seal dam are sequentially arranged on one end face from the high-pressure side to the low-pressure side; a plurality of micropore groups are distributed on the high-pressure side of the end face, every micropore group comprises a straight-line-shaped air inlet groove and a plurality of oval micropores, wherein the centers of the micropores are located on the air inlet groove, included angles of the long axis of every micropore and the air inlet groove are identical, and one end of every micropore facing to air flow is located on the high-pressure side of the end face. Straight lines where the air inlet grooves are located are obliquely crossed with the radius of the end face, and the shiny side ring-shaped seal dam is arranged on the low-pressure side of the end face. The end face mechanical seal structure has the advantages that starting performance under high-pressure frequent starting and shutdown working conditions is improved; the problem that the end face dynamic pressure effect is weak due to gas negative pressure effect is solved; the capability and the advantages of the micropore in stopping solid particles are brought into full play; the dynamic pressure effect and disturbance resistance are enhanced, the service life is prolonged, and end face stability is improved.
Owner:ZHEJIANG UNIV OF TECH

Transcritical main shaft system design method based on multi-scale interface regulation and control

The invention belongs to the technical field of main shaft system design, and discloses a transcritical main shaft system design method based on multi-scale interface regulation and control. The method comprises the following steps: giving multi-scale interface parameters; establishing a film thickness equation to obtain a film thickness value of each point of the liquid film; calculating the pressure value of each point of the liquid film to obtain oil film force; calculating a stiffness matrix and a damping matrix of the bearing; solving the axis trajectory motion equation to obtain a spindle vibration quantity; judging whether the spindle vibration quantity meets requirements or not; if not, giving a value interval of the multi-scale interface parameters, resetting the parameters in the given value interval of the multi-scale interface parameters, and performing iterative calculation again; and if yes, outputting the parameters of the multi-scale interface. Through collaborative optimization of deep and shallow cavity interfaces and texture interfaces of the bearing, a functionalized multi-scale interface is formed, the dynamic stability of a main shaft system can be remarkably improved, vibration of the main shaft system is restrained, and the main shaft system can safely and stably work in a critical rotating speed range.
Owner:TIANJIN UNIV

Dynamic-static pressure combined type asymmetrical waviness end face fluid mechanical sealing structure

The invention provides a dynamic-static pressure combined type asymmetrical waviness end face fluid mechanical sealing structure. At least one sealing end face on a moving ring and a stationary seal ring is provided with more than two three-dimensional asymmetrical waviness appearances, the asymmetrical waviness is in a periodical arrangement on the at least one sealing end face, the asymmetrical waviness sealing end face comprises a dam area, a conical surface and a wave crest and a wave trough of the asymmetrical waviness, the dam area is a groove-less parallel annular sealing dam arranged at the low-pressure side, the wave crest and the wave trough are connected through the conical surface, the conical surface is a linear convergence cone formed from the high-pressure side to a low-pressure side and is connected with the dam area, the conical surface can realize sealed non-contact static pressure effect; the conical degree combines with the asymmetrical waviness so that the sealing reliability can be improved, an asymmetrical waviness smooth transition curve can prevent the particles in the sealing fluid from being cumulated, and the dam area can realize static sealing when the axle is stationary. The structure provided by the invention has strong pressure resistance and antijamming capability, the leakage rate is lower at the conditions of high parameters, the fluid has good dynamic pressure effect in the process of start and stop and the fluid bearing capacity is sufficient in the normal operation.
Owner:TSINGHUA UNIV
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products