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52results about How to "High technical efficiency" patented technology

Titanium alloy surface high temperature oxidation resistance and wear resistance oxide gradient coat, and preparation method thereof

ActiveCN102732832ADense tissueSolve the problem of poor high temperature oxidation resistanceVacuum evaporation coatingSputtering coatingAntioxidant capacityCoated surface
The invention relates to a titanium alloy surface high temperature oxidation resistance and wear resistance oxide gradient coat. According to the coat, the surface of the coat is an oxide film layer comprising Al2O3, Cr2O3 and NiO2, wherein the thickness is 4-6 mum; the middle of the coat is an Al-Cr-Ni alloy layer, wherein the thickness is 2-4 mum; and an Al-Cr-Ni-Ti interdiffusion layer is arranged between the coat and a substrate to achieve metallurgical collection, wherein the thickness of the Al-Cr-Ni-Ti interdiffusion layer is 4-6 mum. According to the present invention, the oxide film layer on the surface of the coat has characteristics of compactness, flatness and strong antioxidant capacity; the Al-Cr-Ni alloy layer in the middle of the coat has characteristics of compact structure and high hardness so as to greatly improve wear resistance of the titanium alloy; the metallurgical collection of the coat and the substrate is achieved through the Al-Cr-Ni-Ti interdiffusion layer, and the combination strength is high; and a double glow plasma surface metallurgy technology is adopted to prepare the Al-Cr-Ni alloy layer on the surface of the titanium alloy, and then a plasma oxygen permeation treatment is performed on the Al-Cr-Ni alloy layer to prepare the high temperature oxidation resistance and wear resistance coat, such that the efficiency is high, and the process is simple.
Owner:NANJING UNIV OF AERONAUTICS & ASTRONAUTICS

Titanium aluminum alloy surface high temperature oxidation and hot corrosion resistant Al-Cr coating and preparation method thereof

The present invention discloses a titanium aluminum alloy surface high temperature oxidation and hot corrosion resistant Al-Cr coating; an Al-rich deposition layer, an Al-Cr alloy layer and a Cr diffusion layer are successively arranged from surface to a titanium aluminum alloy substrate. The content of Al in the Al-rich deposition layer remains the same. The content of Al in the Al-Cr alloy layer gradually reduces outside-to-inside to 70%-100% of the content of Al in the titanium aluminum alloy substrate, and the rest in the Al-Cr alloy layer is Cr. The contents of Cr and Al in the Cr diffusion layer respectively gradually reduces outside-to-inside to same as the contents of Cr and Al in the titanium aluminum alloy substrate, and the rest in the Cr diffusion layer is other elements in the titanium aluminum alloy substrate, and the contents of other elements in the Cr diffusion layer respectively gradually rise to same as the contents of the other elements in the titanium aluminum alloy substrate from zero. The invention also discloses a preparation method of the titanium aluminum alloy surface high temperature oxidation and hot corrosion resistant Al-Cr coating; the titanium aluminum alloy surface high temperature oxidation and hot corrosion resistant Al-Cr coating can give titanium aluminum alloy excellent oxidation resistance and heat resistance corrosion performance under high temperature and long term service conditions, and due to the presence of the diffusion layer of the gradient components, the reliable binding strength and excellent thermal shock resistance can be realized.
Owner:NANJING UNIV OF AERONAUTICS & ASTRONAUTICS

Gamma-TiAl alloy surface high temperature oxidation resistance and wear resistance coat, and preparation method thereof

The invention relates to a gamma-TiAl alloy surface high temperature oxidation resistance and wear resistance coat. According to the coat, the surface of the coat is an oxide film layer comprising Cr2O3 and NiO2, wherein the thickness is 2-3 mum; the middle of the coat is a Cr-Ni alloy layer, wherein the thickness is 2-4 mum; and a Cr-Ni-Ti-Al interdiffusion layer is arranged between the coat and a substrate to achieve metallurgical collection, wherein the thickness of the Cr-Ni-Ti-Al interdiffusion layer is 4-6 mum. According to the present invention, the Cr2O3 and NiO2 oxide film on the surface of the coat has characteristics of compact structure and strong antioxidant capacity; the Cr-Ni alloy layer in the middle of the coat has characteristics of uniform structure and high hardness so as to greatly improve wear resistance of the gamma-TiAl alloy; the metallurgical collection of the coat and the substrate is achieved through the Cr-Ni-Ti-Al interdiffusion layer, and the combination strength is high; and a double glow plasma surface metallurgy technology and a plasma oxygen permeation technology are firstly combined in the coat preparation process of the present invention, special plasma oxygen permeation equipment is not required, the coat can be directly prepared in 5 hours by adopting double glow plasma surface metallurgy equipment, the process is simple, and the efficiency is high.
Owner:NANJING UNIV OF AERONAUTICS & ASTRONAUTICS

High-temperature-oxidation-resistant and abrasion-resistant AlCrN coating on surface of titanium-aluminum alloy and preparation method thereof

InactiveCN105839049AImprove wear resistanceThe surface of the coating is smooth and denseVacuum evaporation coatingSputtering coatingOxidation resistantGlow plasma
The invention discloses a high-temperature-oxidation-resistant and abrasion-resistant AlCrN coating on the surface of a titanium-aluminum alloy and a preparation method thereof. The coating is deposited on the surface of a titanium-aluminum alloy workpiece through the double glow plasma surface technology, an AlCrN deposited layer is located on the surface of the coating and is 5-10 micrometers thick, and a compact oxidized layer rich in Al2O3 and Cr oxide is formed by the AlCrN deposited layer at a high temperature; an AlCrN diffused layer is arranged in the coating and is 12-15 micrometers thick; the hardness of the obtained coating is 30-37 GPa, the room temperature friction coefficient of the coating is 0.3-0.33, and the high-temperature friction coefficient of the coating is 0.47-0.49. The preparation method includes the steps of charging, vacuumizing, workpiece surface activation, plasma permeation of the AlCrN coating, cooling and discharging. The obtained AlCrN coating solves the problem that the titanium-aluminum alloy is poor in high-temperature-oxidation resistance; meanwhile, the gradient structure of the diffused layer achieves metallurgical bonding of the coating and a substrate, and good high-temperature-oxidation resistance and good abrasion resistance are achieved.
Owner:NANJING UNIV OF AERONAUTICS & ASTRONAUTICS

High temperature oxidation resistant composite gradient coating on Ti2AlNb alloy surface and preparation method thereof

The invention relates to a high temperature oxidation resistant composite gradient coating on a Ti2AlNb alloy surface and a preparation method thereof. The composite gradient coating sequentially comprises a pure Al layer, an Al-Ti alloy layer and an Al-Ti-Nb mutual diffusion layer from the surface to a substrate; the Al content of the Al-Ti alloy layer is decreased in a slow gradient manner from the surface of an Al-Ti seeping layer from outside to inside, the Ti content is slowly increased, and component mutation is avoided; and Al content of the Al-Ti-Nb mutual diffusion layer is decreased in a gradient manner from the surface of a diffusion layer from outside to inside, and the Ti content and the Nb content are increased from outside to inside in a gradient manner from the surface of the diffusion layer. The preparation method comprises the steps as follows: Ti2AlNb base alloy is taken as a workpiece electrode, an Al-Ti alloy target material is taken as a source electrode, the Al-Ti alloy layer is prepared by adopting an arc-glow plasma surface metallurgy technology, and then a pure Al target material is taken as the source electrode to prepare the pure Al layer on the Al-Ti alloy layer. The technology efficiency is high, the preparation technology is simple, and the obtained coating has high oxidation resistance.
Owner:NANJING UNIV OF AERONAUTICS & ASTRONAUTICS

Three dimensional measurement method of irregular curved surface

The present invention relates to a three dimensional measurement method of an irregular curved surface. The measurement method comprises the steps of firstly planning a measurement track of a measurement needle sphere center according to an appointed cross-section position required by a drawing on a parts MBD model, generating a measurement path, then compensating the measurement data according tothe model vectors, enabling the compensated data points at an appointed cross-section height, and finally connecting the cross-section points into a curve to evaluate the blade parameters; measuringaccording to the track of the measurement needle sphere center, and then compensating the radius of a measuring head according to the model vectors, and calculating the radius compensation according to the model vectors, wherein the vectors of each measurement point on a three dimensional curved surface are different, so that the compensation directions are different; connecting the compensated cross-section actual measurement points into a blade type curve to evaluate the blade parameters. The advantages of the present invention are that a three dimensional model measurement technology of theirregular curved surface is realized, at the same time, by adopting a model-based measurement mode, the digital design, manufacturing and detection integrated flow of an engine is promoted, and a keydetection technology and the detection efficiency are also improved.
Owner:SHENYANG LIMING AERO-ENGINE GROUP CORPORATION

Aviation-engine-blade-surface data evaluation method based on model

ActiveCN109470196AGood measurement reproducibilityImprove detection technology and detection efficiencyMeasurement devicesEngineeringAviation
The invention discloses an aviation-engine-blade-surface data evaluation method based on a model. The method includes the steps that the profile degree of an evaluated blade surface is a linear profile degree, and the linear profile degree and a theory molded line fit before evaluation; an existing blade-surface design model is thickened, a new blade surface is generated through a curve set of a blade to serve as a theory model of profile degree evaluation; under the condition that it is guaranteed that the position of a blade-surface tolerance band is invariable, an upper limiting value and alower limiting value of the tolerance band are changed, original tolerance is changed to be +0.05 mm to -0.01 mm, new tolerance is changed to be +0.03 mm to -0.03 mm, and the profile tolerance band is a symmetry tolerance band; theory data of the thickened theory model is used as a theory molded line that the profile degree evaluates the blade-surface profile degree. According to the aviation-engine-blade-surface data evaluation method based on the model, reality of a part is reflected, the measuring reproducibility is good, integrated development from the engine detection technology capacityto digitization designing, manufacturing and detecting is promoted, and the key detection technology and detection efficiency are improved.
Owner:SHENYANG LIMING AERO-ENGINE GROUP CORPORATION

Decimal carrier synchronization algorithm based on cyclic prefix

The invention discloses a decimal carrier synchronization algorithm based on cyclic prefix. The decimal carrier synchronization algorithm solves the problem in the prior art that the carrier synchronization technical precision is not high enough to meet modulation order development requirements. The decimal carrier synchronization algorithm based on the cyclic prefix includes the following steps: dividing received signals into a carrier frequency offset portion and a remaining portion, dividing the carrier frequency offset portion into decimal frequency offset and integral multiple frequency offset, calculating to obtain a single estimation value of the decimal frequency offset, and obtaining the ith estimation value according to the single estimation value of the decimal frequency offset; repeating the step (b), calculating variance of the obtained decimal frequency offset, and calculating a variance average value; arranging a threshold V, if Vf>V, executing the step (a), if Vf<V, locking a current decimal frequency offset estimation value, and conducting frequency offset compensation according to the estimation value. By means of the scheme, purposes of reducing decimal frequency estimation residual, improving system stability, and enabling a system to work in a smaller residual environment are achieved, and the algorithm has high practical value and popularization value.
Owner:UNIV OF ELECTRONICS SCI & TECH OF CHINA

Primary care doctor intelligent practice cloud platform supporting health service communities

The invention discloses a primary care doctor intelligent practice cloud platform supporting health service communities. The platform comprises at least one AI cloud computing center which comprises aplurality of auxiliary diagnosis models; at least one cloud service platform which carries a plurality of different service modules, wherein the cloud service platform interacts with the auxiliary diagnosis models in the AI cloud computing center through a network to complete uploading of medical data and fusion judgment and processing of diagnosis results and corresponding services; and an integrated front end which comprises detection equipment used for acquiring physical sign data of a patient, wherein the integrated front end and the cloud service platform carry out data, service and pageinteraction, the service module is displayed on the integrated front end, and the physical sign detection data is transmitted to the service module through the integrated front end. The system has the advantages of wide coverage range of practice content, high intelligent auxiliary degree, support of a city-county-village integrated hierarchical diagnosis and treatment mode in a medical team or health service community mode, and the like.
Owner:挂号网(杭州)科技有限公司

Method for eliminating three-dimensional genomics technology noise by utilizing exonuclease combination

The invention discloses a method for eliminating three-dimensional genomics technology noise by utilizing exonuclease combination. The method comprises the step of adding exonuclease combination to eliminate adjacently connected linear DNA when performing the adjacent connection at the key step of the three-dimensional genomics technology, thereby improving the cyclic effective interaction proportion. The excellent performance of the exonuclease combination for eliminating the linear DNA provides an effective measure for eliminating the noise through the enzyme digestion of the exonuclease combination after the C-technology connection; the method for eliminating the three-dimensional genomics technology noise by utilizing exonuclease combination has the advantages of being convenient, fastand efficient, the possibility of producing the false-positive product or signal can be reduced, the effective interaction cyclic DNA proportion is enhanced, the terminal effective interaction data output ratio is greatly improved, the sequencing space is saved, the sequencing cost is reduced, and the operation for eliminating the resource consumed by ineffective information in the big data by using the complex biological information at later is simplified.
Owner:AGRI GENOMICS INST CHINESE ACADEMY OF AGRI SCI

Coordinate system measurement method for blade parts without positioning datum plane

Disclosed is a coordinate system measurement method for blade parts without a positioning datum plane. A measurement method for blades without direct positioning datum comprises the following steps: (1) generating an MBD model of a part based on spline surface characteristics according to blade profile coordinate data; (2) importing the MBD model into offline measurement software, and adjusting the coordinate system direction of the model to make the coordinate system direction of the model consistent with that of a measuring machine to avoid interference between a virtual probe and the model; and (3) designing measurement point distribution (please see attached figure 3) to ensure that the measurement points cover a measured surface or the part length. The method not only satisfies the requirements of parts, but also conforms to the principle of economical measurement. Through the measurement method for blades without direct positioning datum, measurement of special-form characteristics is realized. The method plays an important role in keeping the quality of engine running stable, improves the product quality and the detection efficiency, and is of great economic and social values.
Owner:SHENYANG LIMING AERO-ENGINE GROUP CORPORATION

Method and device for acquiring electric anisotropy of underground media based on direct current method

The invention relates to a method and device for acquiring electrical anisotropy of underground media based on a direct current method. The method comprises the following steps: after arranging an emission field source at any position of a measurement area, carrying out whole-area observation in the measurement area by adopting mutually orthogonal electrodes to obtain mutually orthogonal potential differences in two directions between different measurement points, calculating apparent resistivity according to the potential differences, calculating normalized apparent resistivity, calculating background apparent resistivity according to a selected background resistivity model, calculating normalized background apparent resistivity, and calculating the resistivity anisotropy coefficient according to actual normalized resistivity and the normalized background apparent resistivity. According to the invention, field source arrangement is flexible and simple; by adopting the resistivity anisotropy coefficient, the influence of an apparent resistivity null line can be effectively suppressed, the projection and the shape of an underground anisotropic structure on the ground can be well reflected, tensor resistivity can be prevented from being solved, and high efficiency is obtained; and the normalized apparent resistivity is adopted, so the error of the apparent resistivity near the field source can be effectively counteracted, and precision is improved.
Owner:HUNAN UNIV OF SCI & TECH

Titanium alloy surface high temperature oxidation resistance and wear resistance oxide gradient coat, and preparation method thereof

ActiveCN102732832BDense tissueSolve the problem of poor high temperature oxidation resistanceVacuum evaporation coatingSputtering coatingGlow plasmaOxidation resistant
The invention relates to a titanium alloy surface high temperature oxidation resistance and wear resistance oxide gradient coat. According to the coat, the surface of the coat is an oxide film layer comprising Al2O3, Cr2O3 and NiO2, wherein the thickness is 4-6 mum; the middle of the coat is an Al-Cr-Ni alloy layer, wherein the thickness is 2-4 mum; and an Al-Cr-Ni-Ti interdiffusion layer is arranged between the coat and a substrate to achieve metallurgical collection, wherein the thickness of the Al-Cr-Ni-Ti interdiffusion layer is 4-6 mum. According to the present invention, the oxide film layer on the surface of the coat has characteristics of compactness, flatness and strong antioxidant capacity; the Al-Cr-Ni alloy layer in the middle of the coat has characteristics of compact structure and high hardness so as to greatly improve wear resistance of the titanium alloy; the metallurgical collection of the coat and the substrate is achieved through the Al-Cr-Ni-Ti interdiffusion layer, and the combination strength is high; and a double glow plasma surface metallurgy technology is adopted to prepare the Al-Cr-Ni alloy layer on the surface of the titanium alloy, and then a plasma oxygen permeation treatment is performed on the Al-Cr-Ni alloy layer to prepare the high temperature oxidation resistance and wear resistance coat, such that the efficiency is high, and the process is simple.
Owner:NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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