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3574 results about "Aerospace" patented technology

Aerospace is the human effort in science, engineering, and business to fly in the atmosphere of Earth (aeronautics) and surrounding space (astronautics). Aerospace organizations research, design, manufacture, operate, or maintain aircraft or spacecraft. Aerospace activity is very diverse, with a multitude of commercial, industrial and military applications.

Nanometer multiple-layer composite thermal insulation material and preparation method thereof

ActiveCN101799099AEasy to useInhibition of high temperature radiative heat transferThermal insulationPipe protection by thermal insulationAdhesiveMetal foil
The invention discloses a nanometer multiple-layer composite thermal insulation material and a preparation method thereof. The nanometer multiple-layer thermal insulation composite material is formed by alternatively overlapping an infrared reflecting screen and a spacer; the ratio of total layer amounts n of the infrared reflecting screens and the spacers to the total thickness of the nanometer multiple-layer composite thermal insulation material is 0.5-4; the infrared reflecting screen is a metal foil or a metal plated foil; the spacer is a thermostability nanometer porous aerogel composite thermal insulation material; the infrared reflecting screen and the spacer are combined by being adhered with thermostability adhesives or in puncturing connection by thermostability sewing threads. The invention also comprises the preparation method of the nanometer multiple-layer composite thermal insulation material. The nanometer multiple-layer composite thermal insulation material of the invention has low density, favorable mechanical property and favorable high-temperature thermal insulation property, lowers requirements on the vacuum degree by a VIP plate when being used as vacuum thermal insulation plate core materials, does not need getter and can satisfy harsh high-efficiency thermal insulation using requirements on materials by aviation, aerospace and civil fields. The method of the invention can prepare thermal insulation material members with large size and complex shape.
Owner:NAT UNIV OF DEFENSE TECH

Nanometer cellulose/polyvinyl alcohol gel composite material

The invention relates to a nanometer cellulose/polyvinyl alcohol gel composite material, which is characterized by comprising hydrogel and aerogel. A preparation method of the nanometer cellulose/polyvinyl alcohol gel composite material comprises the following process steps of 1, nanometer cellulose preparation by a chemical combination mechanical treatment method; 2, composite hydrogel preparation; and 3, composite aerogel preparation. The nanometer cellulose/polyvinyl alcohol gel composite material has the advantages that the composite aerogel belongs to a porous amorphous solid material consisting of nanometer level colloid particles or high-polymer molecules, and a unique open nanometer level porous structure and a continuous three-dimensional reticular structure are adopted, so the density is extremely low, the specific surface area is high, and the porosity is high, wherein the solid phase of the aerogel accounts for 0.2 percent to 20 percent of the total volume percentage, the characteristics of high adsorption catalytic capability, low thermal conductivity, low sound resistance, low refractive index and the like are shown, and wide application prospects are realized in the fields of aviation, spaceflight, chemical industry, metallurgy, energy-saving building and the like.
Owner:SHANDONG LVSEN WOOD PLASTIC COMPOSITE

Three-dimensional assembly process generation method and system for aerospace product

InactiveCN103413004AAddressing the information gapAccurate visualizationAnimationSpecial data processing applicationsAnimationInformation gap
The invention provides a three-dimensional assembly process generation method and system for an aerospace product. The system comprises a three-dimensional manufacturing resource library building module, a three-dimensional assembly process design module, a three-dimensional assembly process simulation module and a three-dimensional assembly process release module, the three-dimensional manufacturing resource library building module is used for building a three-dimensional manufacturing resource library containing product, fixture, tool and auxiliary material information, the three-dimensional assembly process design module is used for decomposing process tasks and planning a process according to the built three-dimensional manufacturing resource library to form a process structure tree, the three-dimensional assembly process simulation module is used for building a virtual assembly environment and simulating and analyzing the assembly process according to a three-dimensional model, the assembly process and the process structure tree to form a three-dimensional assembly animation meeting actual assembly requirements, and the three-dimensional assembly process release module is used for integrating process design information and simulation information, forming a three-dimensional assembly process file and releasing the three-dimensional assembly process file to an assembly site. Accurate and visual three-dimensional visual means are provided for aerospace product assembly, so that the problem of information gaps among three-dimensional product design, three-dimensional process design and three-dimensional assembly site implementation in the prior art can be solved.
Owner:SHANGHAI JIAO TONG UNIV

Autonomous integrated navigation system

The invention relates to an autonomous integrated navigation system which belongs to the technical field of navigation systems. The SINS (Strapdown Inertial Navigation System)/SAR (Synthetic Aperture Radar)/CNS (Celestial Navigation System) integrated navigation system takes SINS as a main navigation system and SAR and CNS as aided navigation systems and is established by the following steps: firstly, designing SINS/SAR and SINS/CNS navigation sub-filters, calculating to obtain two groups of local optimal estimation values and local optimal error covariance matrixes of the integrated navigation system state, then transmitting the two groups of local optimal estimation values into a main filter by a federal filter technology for fusion to obtain an overall optimal estimation value and an overall optimal error covariance matrix, and finally, performing real-time correction on the error according to the overall optimal estimation value so as to obtain an optimal estimation fusion algorithm of the SINS/SAR/CNS integrated navigation system. The autonomous integrated navigation system, disclosed by the invention, is less in calculation amount and high in reliability, is applicable to aircrafts in near space, aircrafts flying back and forth in the aerospace, aircrafts for carrying ballistic missiles, orbit spacecrafts and the like, and has wide application prospect.
Owner:NORTHWESTERN POLYTECHNICAL UNIV

High-toughness aluminum lithium alloy and preparation method thereof

ActiveCN102021457AImpurityHeat treated
The invention discloses a high-toughness aluminum lithium alloy and a preparation method thereof. The alloy comprises the following chemical components in percentage by weight: 3.2 to 4.2 percent of Cu, 0.7 to 1.8 percent of Li, 0.20 to 0.60 percent of Mn, 0.20 to 0.60 percent of Zn, 0.06 to 0.20 percent of Zr, 0.20 to 0.80 percent of Mg, 0.2 to 0.7 percent of Ag, less than or equal to 0.10 percent of Si, less than or equal to 0.10 percent of Fe, less than or equal to 0.12 percent of Ti, less than or equal to 0.15 percent of other impurities (single impurity is less than or equal to 0.05 percent) and the balance of Al. One or five of alloy elements Mn, Zn, Mg, Ag and Zr can be selectively added. Proportioning is performed according to the alloy components, the raw materials are melted, then furnace refining and standing are performed, and alloy ingots with required specifications are cast. The alloy ingots are preferably homogenized and then molded by any process of hot extruding, hot rolling and the like, and the alloy ingots thermally treated by the preferable process can be used for processing parts. The high-toughness aluminum lithium alloy material has uniform microscopic structure and stable performance, and is suitable for manufacturing thick plates and extruded materials. The ultimate tensile strength can reach over 510MPa, and meanwhile, the elongation rate is more than 8 percent and the KIc can reach over 30MPam1/2. The material product can be used for structural elements of the fields of aerospace, nuclear industry, traffic and transportation, sports goods, weapons and the like.
Owner:AVIC BEIJING INST OF AERONAUTICAL MATERIALS

TC4 titanium alloy laser selective melting material additive manufacturing and heat treatment method

Disclosed is a TC4 titanium alloy laser selective melting material additive manufacturing and heat treatment method. According to parameters of a TC4 titanium alloy laser selective melting process, laser power ranges from 300 W to 325 W, the spot diameter ranges from 0.12 mm to 0.14 mm, scanning speed ranges from 500 mm/s to 1,200 m/s, and the thickness of a powder laying layer ranges from 0.03 mm to 0.04 mm. A dual annealing process is adopted in heat treatment of a forming component, a TC4 titanium alloy component is firstly put in a vacuum heat treatment furnace with the temperature of 780 DEG C to 820 DEG C, and temperature is reduced to room temperature in an air cooled manner after heat preservation is carried out for 1.5-2 h; and then the TC4 titanium alloy component is put in the vacuum heat treatment furnace with the temperature of 530 DEG C to 550 DEG C again, and temperature is reduced to room temperature in an air cooled manner again after heat preservation is carried out for 2-3 h. The strength of the TC4 titanium alloy component treated through the process exceeds 1,000 MPa, meanwhile, ductility is not smaller than 10%, and the TC4 titanium alloy component can meet the requirements of aerospace products for the strength and plasticity of TC4 titanium alloy key bearing structural components.
Owner:SHANGHAI SPACE PRECISION MACHINERY RES INST

Space rolling bearing comprehensive performance experiment device

ActiveCN104568443ALoad accuratelyAccurate and stable loadingMachine bearings testingAviationFriction torque
The invention discloses a space rolling bearing comprehensive performance experiment device, relates to an experiment device and provides an experiment device capable of accurately measuring axial and redial united loads of a space rolling bearing and basic data including friction moment, bearing temperature rise, vibration and the like under different rotation speed working conditions. The space rolling bearing comprehensive performance experiment device can simultaneously conduct axial force and radial force accurate load on a measured bearing through an axial loading device and a radial loading device. A three-axis acceleration sensor is used for measuring radial, axial and peripheral vibration situations of the measured bearing. A temperature sensor is used for measuring the temperature rise situation of the measured bearing. A pressure sensor is used for measuring the friction moment of the measured bearing. An annular pressure sensor is used for measuring axial force borne by the measured bearing. Weights are used for marking radial force borne by the measured bearing. The space rolling bearing comprehensive performance experiment device can evaluate the comprehensive performance of the space rolling bearing and provide key scientific technical basis and test platform support for development of high-end bearings in the aerospace field of our country.
Owner:SICHUAN UNIV

Electromagnetic shielding conformal optical window with longitude and latitude-shaped mesh structure

The invention provides an electromagnetic shielding conformal optical window with a longitude and latitude-shaped mesh structure, which belongs to the technical field of electromagnetic shielding of optical transparent pieces. The electromagnetic shielding conformal optical window comprises a conformal optical window and is characterized in that: (1) a longitude and latitude-shaped metal mesh is manufactured on the inner side surface of the conformal optical window shell; and the longitude and latitude-shaped metal mesh covers the whole inner side surface of the conformal optical window shell; or (2) a longitude and latitude-shaped metal mesh and a conformal optical window inner shell are manufactured on the inner surface of the conformal optical window shell from outside to inside in turn; the longitude and latitude-shaped metal mesh covers the whole inner surface of the conformal optical window shell and outer surface of the conformal optical window inner shell; the latitude-shaped metal mesh consists of metal longitudes and metal latitudes; the metal latitudes are uniformly arranged in an equivalent centre angle along a circumferential direction; the metal longitudes are arranged at equal intervals according to a metal mesh cycle along a generatrix direction; and the metal longitudes and the metal latitudes are electrically connected with one another. The electromagnetic shielding conformal optical window with the longitude and latitude-shaped mesh structure is suitable for electromagnetic shielding technology of military or civil conformal optical windows for remote measuring and sensing, medical diagnosis, secret communication, aerospace equipment and the like.
Owner:HARBIN INST OF TECH

Anti-icing and anti-frosting polyurethane coating and preparation method thereof

The invention belongs to the fields of aerospace, low temperature refrigeration and heat pump air-conditioning and relates to an anti-icing and anti-frosting polyurethane coating and a preparation method thereof. The anti-icing and anti-frosting polyurethane coating has good film forming properties, low temperature resistance and high hydrophobicity. The preparation method comprises that based on weight parts of a fluorosiloxane-containing polyurethane resin, 20 to 45 parts by weight of the fluorosiloxane-containing polyurethane resin, 40 to 50 parts by weight of one or more organic solvents, 0.2 to 1 part by weight of one or more defoamers, 0.2 to 1 part by weight of one or more anti-settling agents and 0.3 to 1 part by weight of one or more flatting agents are mixed into a mixed solution; 3 to 10 parts by weight of one or more silane coupling agents, 1 to 10 parts by weight of nanoscale inorganic oxide particles and 5 to 10 parts by weight of titanium dioxide are added into the mixed solution; and the mixture is subjected to ball-milling to form the anti-icing and anti-frosting polyurethane coating. Through utilization of the fluorosiloxane-containing polyurethane resin, the anti-icing and anti-frosting polyurethane coating has good adhesion with a base and has good surface hydrophobicity.
Owner:INST OF CHEM CHINESE ACAD OF SCI
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