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124results about How to "Performance tuning" patented technology

Shape memory polymer pipeline and use of shape memory polymer pipeline as aircraft engine intake

The invention relates to a shape memory polymer pipeline and use of the shape memory polymer pipeline as an aircraft engine intake, in particular to a shape memory polymer pipeline and use thereof, which solve the problem that a structure of the conventional aircraft engine intake cannot be deformed according to requirements, so air inflow cannot be regulated and the shape of the air intake cannot be changed to cause that the through capacity of the aircraft engine intake is discordant with the requirement of an engine to influence the aerodynamics performance of an air engine. The shape memory polymer pipeline is made of a shape memory composition material, and the shape memory composition material consists of 5 to 98 volume parts of shape memory polymer materials, 2 to 95 volume parts of reinforcement phase materials and 0 to 100 volume parts of resistance heating materials; and the shape memory polymer pipeline serving as the aircraft engine intake overcomes the defect that the structure of the conventional air intake cannot be deformed according to the requirements, and regulates the air inflow and changes the shape of the air intake, so that the through capacity of the air intake is in accordance with the requirement of the engine to improve the aerodynamics performance of aircrafts.
Owner:HARBIN INST OF TECH

Acrylic acid non-aqueous dispersoid containing amino ester bonds and siloxy groups and preparation method thereof

The invention relates to an acrylic acid non-aqueous dispersoid containing amino ester bonds and siloxy groups and a preparation method thereof. The non-aqueous dispersoid consists of a dispersion stabilizer, a dispersion phase and a dispersion medium; based on solids, the dispersion stabilizer and the dispersion phase accounts for 50 to 80 weight percent of the non-aqueous dispersoid, wherein the weight ratio of the dispersion stabilizer and the dispersion phase is 1:3-10; the weight-average molecular weight of the non-aqueous dispersoid is 20,000 to 30,000; the dispersion stabilizer is polyurethane modified acrylic polymer, and has the weight-average molecular weight of 10,000 to 15,000; the dispersion phase is gelled grafted siloxane acrylic polymer, and the siloxane monomer accounts for 0.5 to 5 weight percent; and aliphatic hydrocarbon solvents at least accounts for 80 weight percent of the dispersion medium. After the non-aqueous dispersoid is used as a hydroxyl component to be prepared into a double-component polyurethane coating, the double-component polyurethane coating has the tolerance for solvents, chemicals, water, acids and alkalis superior to that of a coating prepared from a common polyhydroxy acrylic acid non-aqueous dispersoid.
Owner:CNOOC CHANGZHOU PAINT & COATINGS IND RES INST +1

A supercomputer-based overlap optimization method for parallel CFD computation and communication is proposed

The invention discloses a parallel CFD calculation and communication overlap optimization method based on a supercomputer, which comprises the following steps: firstly, dividing the discrete flow field grid into a plurality of flow field regions with balanced computational load by domain decomposition; and secondly, dividing the discrete flow field grid into a plurality of flow field regions withbalanced computational load. Using the data parallelism strategy of single program and multiple data, each node in the cluster computes an approximate numerical solution of one of the flow fields. Inthe calculation process, according to the different positions of the flow field grids in the flow field region, the flow field grids are divided into two types: pure internal grids and boundary grids.The neighboring flow field regions located at different nodes need to exchange the flow field values of the boundary grids through the interconnected network. Secondly, the parallelism of computationand communication process is recognized by analyzing the read-write dependence of the flow field values in parallel CFD algorithm. Finally, the computation and communication flow of the parallel CFDprogram is adjusted, the parallel CFD program is overlapped with the communication program, and the performance of the parallel CFD program is tuned by the performance analysis tool TAU (Tuning and Analysis Utilities).
Owner:XI AN JIAOTONG UNIV
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