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30results about How to "Increase damage tolerance" patented technology

Composite aircraft floor system

InactiveUS20070193146A1Improved structural performanceIncrease damage toleranceBuilding roofsFloorsAirplaneDamage tolerance
An aircraft floor system includes a composite panel which generally includes an inboard layer, an inboard interlock layer, a core layer, an outboard interlock layer and an outboard layer. The advanced sandwich core material may include K-Cor™ or X-Cor™ which is pinned through at least one ply of dry composite reinforcement to provide a mechanical lock between the pins and an inboard and outboard interlock layer. Bonding of the locked-in ply with the inboard and outboard results in improved structural performance and damage tolerance.
Owner:SIKORSKY AIRCRAFT

Preparation method of in-plane isotropic zirconium boride-based ultra-high temperature monolithic structure ceramic with high damage tolerance

ActiveCN109293384ASolve the problem of in-plane anisotropyImprove fracture toughnessInorganic material artificial filamentsBorideFiber
The invention relates to a preparation method of a zirconium boride-based ultra-high temperature monolithic material, in particular to a preparation method of an in-plane isotropic zirconium boride-based ultra-high temperature monolithic structure ceramic with high damage tolerance, and aims to solve the problems that ZrB2-based ultra-high temperature ceramic has poor damage tolerance and seriousin-plane anisotropy exists in ZrB2-based fiber monolithic ceramic. The preparation method includes: dissolving polyether sulfone in N-methylpyrrolidone, and conducting ball milling mixing with ZrB2 powder and SiC powder to obtain a ZrB2-SiC slurry, and subjecting the ZrB2-SiC slurry to extrusion curing to obtain continuous ZrB2-SiC ceramic fiber; dispersing ZrB2 powder, SiC powder and Graphene indeionized water to obtain a ZrB2-SiC-Graphene slurry; coating the continuous ZrB2-SiC ceramic fiber with the ZrB2-SiC-Graphene slurry, performing drying, and conducting prepressing, high temperature glue discharge and hot pressing sintering. The method provided by the invention solves the in-plane anisotropy problem of uniaxially arranged ZrB2-based fiber monolithic ceramic, and improves the damage tolerance. The method provided by the invention is suitable for preparation of zirconium boride-based ultra-high temperature monolithic structure ceramic.
Owner:HARBIN INST OF TECH

Semiconductor element

A drain / drift section (2) is generally equivalent to a portion directly below a p-base region (3a) which is an element active section (21), and is a first parallel pn structure obtained by repeatedly joining in an alternating manner a first n-type region (2a) and a first p-type region (2b). Around the drain / drift section (2) is an element peripheral edge section (22) comprising a second parallel pn structure obtained by repeatedly joining in an alternating manner a second n-type region (12a) and a second p-type region (12b) oriented continuous with the first parallel pn structure. An n-buffer layer (11) is provided between the first and second parallel pn structures and an n+ drain layer (1). A p+ drain region (17) is selectively provided on the interior of the n+ drain layer (1) of the element peripheral edge section (22), the p+ drain region (17) passing through the n+ drain layer (1) in the depth direction. By this means, damage resistance can be improved in a super-junction semiconductor element capable of significantly improving the tradeoff relationship between on resistance and pressure resistance.
Owner:FUJI ELECTRIC CO LTD

Preparation method of multiscale toughened brick-mud structural super high-temperature ceramic material

ActiveCN108249929AReduce anisotropy problemsImproved damage toleranceSpray coatingThermal impact
The invention provides a preparation method of a multiscale toughened brick-mud structural super high-temperature ceramic material, and relates to the field of preparation of structural ceramic materials, in particular to a preparation method of the brick-mud structural super high-temperature ceramic material. The preparation method aims to solve the problem that the anisotropism of multi-component ZrB2-SiC ceramic is severe and the damage resistant tolerance is poor. The preparation method comprises the steps that 1, a ZrB2-SiC ceramic microsphere is prepared through pelleting; 2, the surfaceof the ZrB2-SiC ceramic microsphere is coated with a ZrB2-SiC-Graphene interface layer through a spraying coating method; and 3, the multiscale toughened brick-mud structural super high-temperature ceramic material is prepared through spark plasma sintering. The preparation method is used for preparing the multiscale toughened brick-mud structural super high-temperature ceramic material, the critical crack size and the fracture work of the material reach 161.8 microns and 150.3 J / m2 respectively, and the critical thermal impact temperature difference is as high as 861 DEG C.
Owner:HARBIN INST OF TECH

Steel reinforced concrete column-steel beam joint locally adopting fiber reinforced concrete

The invention discloses a steel reinforced concrete column-steel beam joint locally adopting fiber reinforced concrete. The steel reinforced concrete column-steel beam joint comprises core profile steel, the fiber reinforced concrete, a first steel beam, a second steel beam, a third steel beam and a fourth steel beam; the core profile steel comprises a first profile steel web and a second profilesteel web which are welded to form cross-shaped profile steel, the two ends of the first profile steel web are correspondingly provided with a first profile steel flange and a second profile steel flange, and the two ends of the second profile steel web are correspondingly provided with a third profile steel flange and a fourth profile steel flange; and the first profile steel flange, the second profile steel flange, the third profile steel flange and the fourth profile steel flange are correspondingly connected with the first steel beam, the second steel beam, the third steel beam and the fourth steel beam. The steel reinforced concrete column-steel beam joint locally adopting the fiber reinforced concrete has the characteristics that the fiber reinforced concrete is adopted at a joint core zone, the using amount of stirrups in the core zone can be reduced or even eliminated, the shear resistance capacity of the joint, the rotating capability of the joint and the energy dissipation capability can be remarkably improved, and meanwhile, construction complexity is reduced.
Owner:CHANGAN UNIV

Preparation method of mullite whisker low-temperature growth toughening type aluminum-phosphate-based high-temperature adhesive

The invention provides a preparation method of mullite whisker low-temperature growth toughening type aluminum-phosphate-based high-temperature adhesive. The preparation method comprises the steps ofusing aluminium hydroxide powder, kaolinite powder and an ammonium molybdate tetrahydrate powder prefabricated whisker growth precursor to mix aluminum oxide powder, silicon powder, boron carbide powder and glass powder to prepare a filler, taking a reaction solution of aluminum hydroxide and phosphoric acid as a glue solution, and finally preparing an adhesive by mixing the precursor, the fillerand the glue solution. The preparation method has the effects that the high-temperature adhesive can grow mullite whiskers in situ at 700 DEG C to be strengthened and toughened, and the bonding performance of the high-temperature adhesive can be greatly improved within the range of 700 DEG C to1300 DEG C. Especially after treatment at 1100 DEG C, the adhesive shows excellent bonding effect, compared with a blank sample without whisker growth, the adhesive strength of the adhesive is increased by 79.88% and reaches 49 MPa, and fracture displacement is increased by nearly 164%. In addition, thehigh-temperature adhesive also shows high damage resistant tolerance, and it is fully shown that the high-temperature adhesive has high use safety.
Owner:CIVIL AVIATION UNIV OF CHINA

Power amplifier module

Provided is a power amplifier module having high efficiency and high damage resistance, and at the same time having a function of protecting an amplifying device from being damaged from a standing wave generated by reflection from an antenna end or the like when a load fluctuates. By detecting and canceling the base overcurrent of the last-stage amplified GaAs-HBT and limiting it, the increase of the collector current can be prevented to prevent damage. In addition, by using both the function of stepping down the reactive current corresponding to the increase of the power supply voltage and the clipping function of the diode connected in parallel with the output stage GaAs-HBT, it is possible to prevent the output stage GaAs-HBT from receiving more than necessary voltage and current. In addition, it is highly resistant to manufacturing variations and temperature fluctuations of the GaAs-HBT and the base current supply source, and the cost is low.
Owner:RENESAS ELECTRONICS CORP

Method for producing a core composite with double-sided surface layers

The invention relates to a method for manufacturing flat, single or double curved core composites 1, 23 with at least one folded honeycomb core 4, 19. Prior to applying the initially not yet hardened cover layers 2, 3, 13, 22 a curable and later removable core filler material 15, 16 is introduced into full-length drainage-enabling channels 5, 6 of the folded honeycomb core 4, 19 in order to prevent telegraphing of the cover layers 2, 3, 13, 22 into the channels 5, 6 of the folded honeycomb core when arranging and / or hardening the cover layers 2, 3, 13, 22 and to produce edge-free and polygon-free surfaces of the core composite 1, 23. The core composites 1, 23 made according to the method have optimum structural mechanical properties, an ideal surface quality from the aerodynamic and aesthetic point of view, whereby a direct reprocessing of the core composites 1, 23 is possible without the need for further time and cost-intensive as well as in some circumstances weight-increasing finishing steps. With the method it is possible to manufacture in particular one-piece fuselage sections with wound core composites 1, 23 with a folded honeycomb 4, 19 as well as shell segments with laid cover layers 2, 3, 13, 22 for longitudinally divided (segmented) fuselage sections for large aircraft.
Owner:AIRBUS OPERATIONS GMBH

A method for preparing in-plane isotropic zirconium boride-based ultra-high temperature monolithic ceramics with high damage tolerance

The invention relates to a preparation method of a zirconium boride-based ultra-high temperature monolithic material, in particular to a preparation method of an in-plane isotropic zirconium boride-based ultra-high temperature monolithic structure ceramic with high damage tolerance, and aims to solve the problems that ZrB2-based ultra-high temperature ceramic has poor damage tolerance and seriousin-plane anisotropy exists in ZrB2-based fiber monolithic ceramic. The preparation method includes: dissolving polyether sulfone in N-methylpyrrolidone, and conducting ball milling mixing with ZrB2 powder and SiC powder to obtain a ZrB2-SiC slurry, and subjecting the ZrB2-SiC slurry to extrusion curing to obtain continuous ZrB2-SiC ceramic fiber; dispersing ZrB2 powder, SiC powder and Graphene indeionized water to obtain a ZrB2-SiC-Graphene slurry; coating the continuous ZrB2-SiC ceramic fiber with the ZrB2-SiC-Graphene slurry, performing drying, and conducting prepressing, high temperature glue discharge and hot pressing sintering. The method provided by the invention solves the in-plane anisotropy problem of uniaxially arranged ZrB2-based fiber monolithic ceramic, and improves the damage tolerance. The method provided by the invention is suitable for preparation of zirconium boride-based ultra-high temperature monolithic structure ceramic.
Owner:HARBIN INST OF TECH

Multi-level micro-nano mechanical structure for enhancing damage resistance of functional surface

The invention discloses a multi-level micro-nano mechanical structure for enhancing damage resistance of a functional surface. The multi-level micro-nano mechanical structure comprises a micro-nano composite structure functional layer, an interconnection network structure functional layer and a mechanical artificial structure functional layer which are connected; the micro-nano composite structure functional layer is of a micro-column array structure which plays a surface function, the interconnection network structure functional layer is of a hard phase and soft interconnection structure, the hard phases are connected through soft phase materials to form an unstable parallelogram, and under the action of plane stress at the tail ends of micro-columns, spontaneous rotation or reconstruction is achieved, and apparent numerical values of stress and strain at the tail ends of the micro-columns are reduced; the mechanical artificial structure functional layer is of an array structure composed of reconfigurable artificial lattices with mechanical properties, and through time-space domain reconstruction of the artificial lattices, a stress transfer path and strain energy density are optimized, and stress concentration of a functional surface is reduced. According to the invention, a dynamic structure is introduced, the damage tolerance of the surface functional layer is improved, the service cycle of the functional surface is prolonged, and the performance of the functional surface is guaranteed.
Owner:XI AN JIAOTONG UNIV

Semiconductor device

A semiconductor device having a high withstand voltage is provided. An activation groove (22a) is composed of a long and narrow main groove part (26) and a sub-groove part (27) which is connected with a side plane in a longitudinal direction of the main groove part. On a bottom plane of the main groove part (26), a second conductivity type embedding region (24) having a height lower than a bottom plane of a second conductivity type base diffusion region (32a) is arranged, and in the sub-groove part (27), a second conductivity type activation groove filling region (25) contacting the base diffusion region (32a) is arranged. The embedding region (24) is brought into contact with the base diffusion region (32a) through the activation groove filling region (25). In the one activation groove (22a), since one gate groove (83) is formed at a part upper than the embedding region (24), a gate electrode plug (48) is not interrupted and an electrode pattern is simplified.
Owner:SHINDENGEN ELECTRIC MFG CO LTD
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