Abstract: A surface-mounted light-emitting device includes: a LED epitaxial structure having two opposite surfaces, wherein the first surface is a light-emitting surface; P and N electrode pads over the second surface of the epitaxial structure, which have sufficient thickness to support the LED epitaxial structure, and the P and N electrode pads have two opposite surfaces respectively, in which, the first surface is approximate to the LED epitaxial structure; an insulator between the P and N pads to prevent the P and N electrode pads from short circuit; and the P and N electrode pads are directly applied in the SMT package. Some embodiments allow structural changes compared with conventional SMT package type by directly mounting the chip over the supporting substrate through an electrode pad. In addition, soldering is followed after the chip process without package step, which is mainly applicable to flip-chip LED device.

Abstract: A vertical high-voltage light emitting device and a manufacturing method thereof. Polarities of two adjacent light emitting diodes (LEDs) are reversed by means of area laser stripping and die bonding, and the two diodes whose polarities are reversed are disposed on an insulating substrate comprising a bonding metal layer (320). A conductive wire (140) is distributed on a surface of the light emitting device, so that a single LED unit (330) has a vertical structure, and multiple LEDs are connected in series to form a high-voltage LED, thereby solving the problems of low light emitting efficiency and large thermal resistance of a horizontal structure.

Abstract: The present invention discloses a vertical AC LED element and fabrication method thereof, wherein the vertical AC LED element comprises a conductive substrate (102); a light-emitting module on the conductive substrate (102), including two horizontally arranged in parallel and mutually-isolated LEDs; wherein the first and second LEDs include a first semiconductor layer (111), a light-emitting layer (112) and a second semiconductor layer (113) from top down; a first insulating layer (131) is arranged between the second semiconductor layer (113) of the first LED and the conductive substrate (102) for mutual isolation; an ohmic contact is formed between the second semiconductor layer (113) of the second LED and the conductive substrate (102); a first conductive structure that connects the first semiconductor layer (111) of the first LED, the second semiconductor layer (113) of the second LED and the conductive substrate (102); and a second conductive structure that connects the second semiconductor layer (113) of

Abstract: A flip-chip light emitting diode (LED) includes: a substrate having a P-type pad electrode and an N-type pad electrode; a light-emitting epitaxial layer flip-chip mounted over the substrate, including, from top down, an n-type semiconductor layer, an active layer, and a p-type semiconductor layer. The n-type semiconductor layer is divided into a light-emitting region, an isolation region, and an electrode region. The light-emitting region and the electrode region are electrically isolated by the isolation region. The active layer and the p-type semiconductor layer are below the light-emitting region. The p-type semiconductor layer connects with the P-type pad electrode. The electrode region of the n-type semiconductor layer connects with the N-type pad electrode.

Abstract: A vertical LED with current blocking structure and its associated fabrication method involve an anisotropic conductive material and a conductive substrate with concave-convex structure. The anisotropic conductive material forms a bonding layer with vertical conduction and horizontal insulation between the concave-convex substrate and the light-emitting epitaxial layer, thereby forming a vertical LED with current blocking function.

Abstract: A system includes a turbine casing assembly that includes an outer shell and an inner shell positioned substantially concentrically within the outer shell. The inner shell includes an inner surface facing away from the outer shell and an outer surface facing toward the outer shell, and the outer surface has one or more false flanges. At least one of the one or more false flanges includes a first surface protruding from the outer surface and facing the outer shell, and a flow diverting portion extending between the first surface and the outer surface of the inner shell. The flow diverting portion includes a first portion that diverges in a first circumferential direction between the first surface and the outer surface.

Abstract: This invention discloses an AC-type vertical light emitting element and fabrication method thereof, which achieves polarity reversal of two LEDs via regional laser stripping and die bonding. The two LEDs are placed on a conductive substrate (e.g. Si substrate); therefore, the bonding pads of the two LEDs are on the back of the conductive substrate and the light emitting surfaces of the two LEDs, thus overcoming such problems of low light emitting efficiency and high thermal resistance of the traditional lateral structure.

Abstract: Airfoils according to embodiments of this invention result in a hybrid controlled flow concept that reduces leakage loss by creating a different vortexing concept near endwall regions of the airfoils than at the core region of the airfoils. Specifically, a turbine static nozzle airfoil is disclosed having a variable, non-linear, throat dimension, s, divided by a pitch length, t, distribution (“s/t distribution”) across its radial length. In one embodiment, a plurality of static nozzle airfoils are provided, with each static nozzle airfoil configured such that a throat distance between adjacent static nozzle airfoils is larger proximate the hub regions of the airfoils than proximate the core regions of the airfoils, and the throat distance between adjacent static nozzle airfoils is smaller proximate the tip regions of the airfoils than proximate the core regions.

Abstract: A seal is provided for preventing axial leakage through a radial gap between a stationary structure and a rotating structure. The radial gap is defined by an inner radial surface opposing an outer radial surface across the radial gap. The seal includes at least one land disposed on one of the inner radial surface and outer radial surface. At least one first tooth and at least one second tooth project from the other of the radial surfaces. The second tooth is shorter than the first tooth. At least one of the first tooth and second tooth, is configured to extend at an angle upstream. This angle is defined between a radial surface from which the first or second tooth projects and an upstream surface of the same tooth. The angle is less than or equal to about 80 degrees.

Abstract: Airfoils according to embodiments of this invention result in a hybrid controlled flow concept that reduces leakage loss by creating a different vortexing concept near endwall regions of the airfoils than at the core region of the airfoils. Specifically, a turbine static nozzle airfoil is disclosed having a variable, non-linear, throat dimension, s, divided by a pitch length, t, distribution (“s/t distribution”) across its radial length. In one embodiment, a plurality of static nozzle airfoils are provided, with each static nozzle airfoil configured such that a throat distance between adjacent static nozzle airfoils is larger proximate the hub regions of the airfoils than proximate the core regions of the airfoils, and the throat distance between adjacent static nozzle airfoils is smaller proximate the tip regions of the airfoils than proximate the core regions.

Abstract: A turbomachine includes a housing, and a plurality of turbomachine nozzles. At least one of the plurality of turbomachine nozzles includes a body having a first surface and an opposing second surface that extend between a first end and a second end. At least one of the first and second surfaces includes a profile having an angle of between about 3° and about 8° between a first line passing through the first end and a first position located between about 28% and about 38% from the first end and a second line passing through the first position and a second position located between about 53% and about 63% from the first end, and an angle of between about 10° and about 20° between the second line and a third line passing through the second position and a third position located between about 74% and about 84% from the first end.

Abstract: A seal is provided for preventing axial leakage through a radial gap between a stationary structure and a rotating structure. The radial gap is defined by an inner radial surface opposing an outer radial surface across the radial gap. The seal includes at least one land disposed on one of the inner radial surface and outer radial surface. At least one first tooth and at least one second tooth project from the other of the radial surfaces. The second tooth is shorter than the first tooth. At least one of the first tooth and second tooth, is configured to extend at an angle upstream. This angle is defined between a radial surface from which the first or second tooth projects and an upstream surface of the same tooth. The angle is less than or equal to about 80 degrees.

Abstract: A turbomachine includes a housing, and a plurality of turbomachine nozzles. At least one of the plurality of turbomachine nozzles includes a body having a first surface and an opposing second surface that extend between a first end and a second end. At least one of the first and second surfaces includes a profile having an angle of between about 3° and about 8° between a first line passing through the first end and a first position located between about 28% and about 38% from the first end and a second line passing through the first position and a second position located between about 53% and about 63% from the first end, and an angle of between about 10° and about 20° between the second line and a third line passing through the second position and a third position located between about 74% and about 84% from the first end.

Abstract: A seal in a turbine engine for preventing axial leakage through a radial gap between a stationary structure and a rotating structure, wherein the radial gap is defined by an inner radial surface that opposes an outer radial surface across the radial gap, the seal including: a first groove disposed on one of the inner radial surface and the outer radial surface; and a first tooth that projects radially from the other of the inner radial surface and the outer radial surface; wherein the first groove, at an upstream end, comprises a gradual slope that slopes away from the surface on which the first tooth is located and, at a downstream end, comprises a steep slope; and wherein the first tooth comprises an axial position that is approximately just upstream of the axial position of the upstream end of the groove.