Abstract: A multilayer composite materials nano-scale filter apparatus includes a vessel including an inlet and an outlet; a main line for flowing contaminants to the vessel through the inlet; a filtration assembly disposed in the vessel for separating particulates from the contaminants to obtain filtered liquids, the filtration assembly including a first magnetic layer, a second magnetic layer, an intermediate filtration layer disposed between the first magnetic layer and the second magnetic layer; and an outlet line for flowing the filtered liquids out of the vessel through the outlet. The intermediate filtration layer is a steel layer or a resin layer.

Abstract: An electronic thermometer includes an external casing unit, a circuit substrate, an electronic switch, a rotating arm unit, a probe unit and a waterproof unit. The external casing unit includes a top cover casing and a bottom cover casing, a receiving space is formed between the top and the bottom cover casings, and the bottom cover casing has a through hole communicated with the receiving space. The waterproof unit includes a first waterproof element and a second waterproof element. The first waterproof element is disposed between the top cover casing and the bottom cover casing and around the receiving space for preventing water vapor from entering the receiving space through the external casing unit, and the second waterproof element is disposed inside the through hole of the bottom cover casing for preventing water vapor from entering the receiving space through the through hole.

Abstract: An approach is provided for determining the authenticity of an available wireless network access point. The approach involves detecting one or more available wireless network access points. The approach also involves communicating one or more authentication requests to each of the available wireless network access points requesting a corresponding access point certificate. The approach further involves processing one or more of one or more received root certificates, one or more received certificate revocation lists, and one or more received access point certificates, the one or more access point certificates being received in response to the one or more authentication requests, to determine an authenticity status of each of the one or more available wireless network access points. The approach additionally involves displaying a list of the one or more available wireless network access points and the authenticity status of each of the one or more available wireless network access points.

Abstract: Systems, methods, and devices are provided for providing flight response to flight-restricted regions. The location of an unmanned aerial vehicle (UAV) may be compared with a location of a flight-restricted region. If needed a flight-response measure may be taken by the UAV to prevent the UAV from flying in a no-fly zone. Different flight-response measures may be taken based on the distance between the UAV and the flight-restricted region and the rules of a jurisdiction within which the UAV falls.

Abstract: A copolymer according to the present disclosure is provided, which includes 30 to 80 mol % of a repeating unit represented by formula (I), 5 to 25 mol % of a repeating unit represented by formula (II), and 5 to 30 mol % of a repeating unit represented by formula (III): wherein R1 is C6-C13 aryl group, C7-C13 aralkyl group, C6-C8 halogenated aryl group or C7-C8 aryloxyalkyl group; R3 is C3-C16 alkyl group or C3-C6 alkoxy substituted alkyl group; R5 is a single bond or C1-C3 alkylene group, R6 and R7 are independently C1-C3 alkoxy group, R8 is polysiloxane with methyl and phenyl groups; and R2, R4 and R9 are independently hydrogen or methyl. In addition, a resin composition, a packaging film and a package structure including the same are provided.

Abstract: Embodiments of the present invention provide a method of forming fin-type transistors. The method includes forming a finFET structure having a fin channel region underneath a gate structure, and a source region and a drain region directly adjacent to the fin channel region at two opposing sides of the gate structure; and subjecting the source region and the drain region to a compressive strain; thereby causing the source region and the drain region to exert a tensile strain to the fin channel region. A finFET transistor formed thereby is also provided, which includes a channel region of fin shape covered by a gate on top thereof; a source next to a first end of the channel region on a first side of the gate; and a drain next to a second end of the channel region on a second side of the gate, wherein the source and drain are made of epitaxially grown silicon-germanium (SiGe) having a Ge concentration level of at least 50% atomic percentage covered with silicon cap.

Abstract: The present invention provides a method for manufacturing a flexible display device and a flexible display device so manufactured. The method for manufacturing a flexible display device according to the present invention uses a connection layer to replace a release layer and a bonding layer that are commonly used in the prior art so as to enhance the bonding strength between a flexible backing plate and a rigid carrier board and to additionally function as a release layer for easily achieving separation between the flexible backing plate and the rigid carrier board; and further, a thermal isolation layer is provided on one side or two sides of the soft glass plate to isolate heat generated in a high temperature process, an ELA process, or a laser based separation process and thus reduce thermal impact caused the heat on the soft glass plate and the display device so as to prevent cracking resulting from increase of brittleness of the soft glass plate and enhance performance of a flexible display device.

Abstract: A cover for a bicycle saddle comprises a basic layer and a first auxiliary layer. The basic layer is made of a first plastic material and has a top surface with a first friction factor. The first auxiliary layer is made of a second plastic material with a second friction factor and is directly disposed on a predetermined area of the top surface of the basic layer. The second friction factor is smaller than the first friction factor. A method is provided for making a cover as above.

Abstract: A SRAM-like electron beam inspection (EBI) structure and method for determining defects in integrated circuits inline during the production process at a level that enables earlier detection during fabrication. Initial layers, such as active layer, poly gate and contact of an IC are first fabricated, and a conductive mesh with horizontal components is provided above the contact layers connecting contact nodes of the contact layers. Voltage contrast is observed during EBI to detect short-circuits, open-circuits, or leakage currents formed between the horizontal components of the conductive mesh and metallized islands placed therebetween.

Abstract: The present invention is a surface treated drug-loaded solid (e.g., non-porous) microparticle that aggregates in vivo to form a consolidated larger particle for medical therapy. In one embodiment, the particles are used for ocular therapy. Processes for producing the surface treated microparticle and injectable formulations which include the surface treated microparticle are also provided. When used in the eye, long-term consistent intraocular delivery can be achieved without disrupting vision and minimizing undesirable inflammatory responses.

Abstract: The present invention relates to a negative pressure device, comprising: a hollow needle assembly including: a hollow needle adaptor, the hollow needle adaptor has an axial through hole, a proximal connector, a distal connector and a flange between the proximal connector and the distal connector, and at least one hollow needle, each of the at least one hollow needle has a tip and an axial through hole and is in fluid communication with the proximal connector of the hollow needle adaptor; a host machine, the host machine comprises a control module and a vacuum pump; and an exhaust pipe, the exhaust pipe is in fluid communication with the host machine and the distal connector of the hollow needle adaptor.

Abstract: A load-bearing frame of a bicycle saddle comprises a base and a rim surrounding the base. The base is made of a first plastic material of predetermined rigidity and includes a relatively narrow anterior portion and a relatively wider posterior portion. The base further has a top surface, a bottom surface, and a peripheral edge. The rim is made of a second plastic material of rigidity being smaller than that of the first plastic material. The rim has an inner side coupled with the periphery edge of the base and an outer side extending upwardly from the inner side to define a first receiving space with a first upper opening.

Abstract: Systems, methods, and devices are provided for providing flight response to flight-restricted regions. The location of an unmanned aerial vehicle (UAV) may be compared with a location of a flight-restricted region. If needed a flight-response measure may be taken by the UAV to prevent the UAV from flying in a no-fly zone. Different flight-response measures may be taken based on the distance between the UAV and the flight-restricted region and the rules of a jurisdiction within which the UAV falls.

Abstract: Systems and methods are provided for aircraft attitude control. The aircraft attitude control may take physical parameters of the aircraft into account. For example, one or more aircraft configuration parameters, such as moment of inertia, motor lift curve, and/or axial distance may be calculated and/or taken into account based on the aircraft physical parameters. The aircraft configuration parameters may include non-linear parameters. The control systems may include feedback control systems, and may optionally use a feedforward and feedback control for angular acceleration.

Abstract: A method and a device for measuring flight parameters of an unmanned aerial vehicle (UAV) are provided, the method includes, capturing images and collecting an angular velocity of the UAC, extracting corner points from a current frame image, estimating an estimated area according to the angular velocity of the UAV, searching for a corresponding corner point in the estimated area, obtaining a speed of each of the corner points, obtaining a pixel velocity, and obtaining an actual speed of the UAV based on the pixel velocity and a flight altitude of the UAV.

Abstract: A main body of a bicycle saddle includes an elastomer provided on a top surface thereof with a recess, a cover layer covering the top surface and having a concave area corresponding to the recess, and an auxiliary functional piece embedded in the concave area. The main body is manufactured by attaching a contacting surface of the cover layer to a mold cavity of a forming mold by vacuum suction to make a protrusion of the inner wall or a piece material glued to the contacting surface and including the auxiliary functional piece prop up the cover layer to form the concave area, forming the elastomer in the mold cavity, and embedding the auxiliary functional piece in the concave area or exposing the auxiliary functional piece on the contacting surface.

Abstract: An inline dark field holographic method for measuring strain in a semiconductor or other crystalline material using a transmission electron microscope having an electron gun for passing an electron beam through strained and unstrained specimens. A condenser mini-lens between the magnetic tilting coil and the specimens increases defection of the beam at an angle with prior to passing through the pair of specimens. The first objective lens forms a virtual image of each of the specimens and the second objective lens focuses the virtual images of each of the specimens at an intermediate image plane to form intermediate images of each of the specimens. The biprism creates the interference pattern between the specimens is formed at the image plane, which may then be viewed to determine the degree of strain of the strained specimen and provides a coma-free strain map with minimal optical distortion.

Abstract: Embodiments of the present invention provide a method of forming fin-type transistors. The method includes forming a finFET structure having a fin channel region underneath a gate structure, and a source region and a drain region directly adjacent to the fin channel region at two opposing sides of the gate structure; and subjecting the source region and the drain region to a compressive strain; thereby causing the source region and the drain region to exert a tensile strain to the fin channel region. A finFET transistor formed thereby is also provided, which includes a channel region of fin shape covered by a gate on top thereof; a source next to a first end of the channel region on a first side of the gate; and a drain next to a second end of the channel region on a second side of the gate, wherein the source and drain are made of epitaxially grown silicon-germanium (SiGe) having a Ge concentration level of at least 50% atomic percentage covered with silicon cap.

Abstract: A method of manufacturing a main body of a bicycle saddle includes the steps of attaching a cover layer to an inner wall of a mold cavity of a forming mold by vacuum suction to make the cover layer have a main area attached to the inner wall and a circumferential area around the main area, heating a base material in the mold cavity to form it into an elastomer and make the main area of the cover layer be combined with and fit the elastomer, combining a bottom shell with the elastomer, and folding back and fixing the circumferential area of the cover layer to a bottom of the bottom shell.

Abstract: Systems, methods, and devices are provided for providing flight response to flight-restricted regions. The location of an unmanned aerial vehicle (UAV) may be compared with a location of a flight-restricted region. If needed a flight-response measure may be taken by the UAV to prevent the UAV from flying in a no-fly zone. Different flight-response measures may be taken based on the distance between the UAV and the flight-restricted region and the rules of a jurisdiction within which the UAV falls.