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353 results about "Small droplet" patented technology

Apparatus and method for testing solid-liquid dynamic and static contact angles by actual liquid droplet method

The invention discloses an apparatus and a method for testing solid-liquid dynamic and static contact angles by an actual liquid droplet method. The method comprises the following steps of: during the testing, placing a solid phase sample on a sample table; controlling X, Y and Z of the sample table to move to a focusing position of a lens; sucking the liquid phase sample into a micro sample injector, injection pump or peristaltic pump; controlling the X, Y and Z of the sample injector to move to the focusing position; dripping a small droplet of the liquid and adsorbing the droplet to a needle head; moving the needle head to the surface of the solid phase sample until the liquid phase sample is adsorbed to the surface of the solid; making a software system control an optical imaging system (CCD) to capture a real-time picture and analyzing the picture by using the actual liquid droplet method; and displaying calculated solid-liquid contact angle value, solid surface free energy value and adhesion work value and managing the values by a database. The apparatus and the method can completely improve the accuracy of the analysis of the solid-liquid interfacial tension, are simple to operate, can be widely applied and have high popularization value.
Owner:上海梭伦信息科技有限公司

Mixed hydrophilic/hydrophobic fiber media for liquid-liquid coalescence

An immiscible lipophilic or hydrophilic liquid phase separated respectively from a continuous hydrophilic phase or a lipophilic phase liquid. Fibers having hydrophilic and hydrophobic properties are mixed, layered, etc., and formed into a filter. The separation mechanism involves capture of small droplets of the immiscible phase, coalescence of the small droplets into larger droplets as the immiscible liquid flows through the fiber filter, and release of the large immiscible droplets from the filter. With respect to separation of a hydrophilic immiscible fluid such as water in a lipophilic continuous fluid such as oil, the hydrophobic fibers will cause small water droplets to migrate towards the hydrophilic fibers whereby large droplets are formed on hydrophilic surface. The large droplets stay on hydrophilic fiber surface for extended periods of time and continue to coalescence until they are so large that they can no longer be maintained by the hydrophilic fibers and are released and drained off of the filter. In designing such filter, wettability of the filter media is an important parameter. The filter media can be designed by mixing hydrophilic and hydrophobic fibers in various proportions to achieve an optimum wettability range for separation of the immiscible liquid from the continuous phase liquid. The wettability of filter media can be characterized by a modified Washburn Equation.
Owner:THE UNIVERSITY OF AKRON

Computing method of model parameters in icing wind tunnel experiment under supercooled large droplet condition

InactiveCN104268399AMeet the similarity requirementsSpecial data processing applicationsJet aeroplaneScale model
The invention discloses a computing method of model parameters in an icing wind tunnel experiment under a supercooled large droplet condition and aims at solving the problems that an existing parameter selecting method for a supercooled small droplet icing experiment does not function well if being applied to a supercooled large droplet icing experiment and that the real icing condition cannot be reflected by icing on a scale model of the airplane. The computing method of the model parameters in the icing wind tunnel experiment under the supercooled large droplet condition is capable of orderly giving the experimental parameters of a wind tunnel test section such as air velocity, average droplet grain diameter, air pressure, liquid water content, icing time and low supercooled water temperature corresponding to real icing flying conditions by use of a theoretical derivation and numerical computation method after determining the scale relation of the model and the real airplane. An aircraft icing wind tunnel experiment is performed according to the converted test parameters, and the experimental result and the real result are capable of meeting the similarity requirement on the major characteristics of the icing process. As a result, the computing method of the model parameters in the icing wind tunnel experiment under the supercooled large droplet condition is capable of obtaining the model parameters for the icing wind tunnel experiment; the corresponding parameters are capable of reflecting the real icing condition in the icing wind tunnel experiment.
Owner:AERODYNAMICS NAT KEY LAB

Fuel conditioning assembly

A fuel conditioning assembly having an elongated housing with an inlet, an outlet, and a flow through passage there between. The inlet is coupled with a fuel supply so as to receive fuel flow there through into the flow through passage, wherein a turbulent flow of the fuel is initiated and the fuel is influenced by a combination of elements, in compound or elemental form, some of which are maintained in a select location within the flow through passage by a binding element. These elements may include copper, aluminum, stainless steel, titanium, magnesium, barium, calcium, iron, zirconium, cerium, platinum, and/or palladium which chemically condition the fuel flowing through the flow through passage by rearranging the molecular bonds of the fuel with a catalytic effect. The fuel, regardless of its type is dispersed into very small droplets having high surface areas thereby lowering the vapor density of the fuel and substantially increasing a fuel burn efficiency. Further, the reaction of a variety of these elements, at least with one another, serves to create an electrostatic charge that is conveyed through the flow through passage by an elongate segment and causes fuel molecules to repel one another resulting in the aforementioned catalytic effect a conditioning of the fuel as it passes through the outlet into to any of a variety of fuel combustion assemblies.
Owner:ROYCE WALKER
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