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Aung
Hnin Thanda Aung, Indooroopilly AU
| Patent application number | Description | Published |
|---|---|---|
| 20080199961 | ANTISENSE COMPOSITION AND METHOD FOR INHIBITION OF miRNA BIOGENESIS - The present disclosure relates to compounds and methods for inhibiting the formation of miRNAs that inhibit translation of one or more identified proteins. The compounds comprise antisense oligonucleotides targeting the pri-miRNA precursor of miRNAs. | 08-21-2008 |
Joe Kyaw Soe Aung, Sunnyvale, CA US
| Patent application number | Description | Published |
|---|---|---|
| 20100121643 | MELODIS CRYSTAL DECODER METHOD AND DEVICE - The technology disclosed relates to a system and method for fast, accurate and parallelizable speech search, called Crystal Decoder. It is particularly useful for search applications, as opposed to dictation. It can achieve both speed and accuracy, without sacrificing one for the other. It can search different variations of records in the reference database without a significant increase in elapsed processing time. Even the main decoding part can be parallelized as the number of words increase to maintain a fast response time. | 05-13-2010 |
Nay Lin Htun Aung, Singapore SG
| Patent application number | Description | Published |
|---|---|---|
| 20100253170 | LOW PROFILE SPINDLE MOTOR - A low profile spindle motor for supporting and rotating media disk or disks of a hard disk drive includes a plurality of stator teeth, a winding layer which may be formed by printed circuit board or the like, and a rotor. The plurality of stator teeth are disposed in an annular region surrounding an axis of rotation of the motor, and have projected ends for increasing the tooth area facing a magnet ring of the rotor. The winding layer has a plurality of windings disposed surrounding the axis of rotation. Each winding is coupled to one of the plurality of stator teeth. The magnet ring is positioned radially spaced apart and coplanar with the annular region. The magnet ring has magnetic poles annularly distributed to generate magnetic fluxes along radial direction. Spindle motor formed according to the invention has a low profile, improved performance and manufacturability. | 10-07-2010 |
| 20110133589 | LOW PROFILE PERMANENT MAGNET SYNCHRONOUS MOTOR WITH SEGMENT STRUCTURE - A low profile permanent magnet synchronous motor with segment structure. In accordance with this invention, a stator assembly for an electromagnetic motor is provided. The stator assembly has a first stator core and a second stator core that couple windings. Teeth extend outward from each stator core and through the windings to contact the other stator core. | 06-09-2011 |
Sandra Aung, San Francisco, CA US
| Patent application number | Description | Published |
|---|---|---|
| 20120034242 | CYTOKINE-EXPRESSING CELLULAR VACCINE COMBINATIONS - The present invention in all of its associated aspects provides improved methods and compositions for treating cancer in a mammal based on the administration of the combination of a cytokine-expressing cellular vaccine and at least one additional cancer therapeutic agent or treatment to a patient with cancer, wherein administration of the combination results in enhanced therapeutic efficacy relative to administration of the cytokine-expressing cellular vaccine or cancer therapeutic agent or treatment as a monotherapy. | 02-09-2012 |
Thuya Aung, Okazaki-City JP
| Patent application number | Description | Published |
|---|---|---|
| 20090090130 | Evaporator Unit - An evaporator unit includes a first heat exchanger configured to perform heat exchange between refrigerant flowing thereinto from a refrigerant inlet and air, a bypass passage through which the refrigerant flowing from the refrigerant inlet flows while bypassing the first heat exchanger, a second heat exchanger configured to perform heat exchange between air and mixed refrigerant in which the refrigerant after passing through the first heat exchanger and the refrigerant having passed through the bypass passage are mixed, and a flow amount adjustment portion configured to adjust a flow amount of the refrigerant flowing through the first heat exchanger and a flow amount of the refrigerant flowing through the bypass passage. Accordingly, the first heat exchanger and the second heat exchanger can be configured to have respectively portions in which a dryness of the refrigerant is in a range between 0.6 and 0.9. | 04-09-2009 |
Thuya Aung, Kariya-City JP
| Patent application number | Description | Published |
|---|---|---|
| 20080196446 | Integrated unit for refrigerant cycle device - In an integrated unit for a refrigerant cycle device, at least one evaporator is integrated with an ejector having a nozzle portion for decompressing refrigerant and a refrigerant suction port from which refrigerant is drawn. In the integrated unit, an insertion hole is provided in a longitudinal end surface of a tank of the evaporator such that the ejector is inserted from the insertion hole into the tank, and a plug for sealing the insertion hole is provided. Furthermore, a spacer is configured to have a gap between the plug and the ejector, and a fixing member is disposed between the longitudinal end surface of the tank and an expansion valve, for fixing the expansion valve to the longitudinal end surface of the tank. In the integrated unit, at least one of the fixing member, the plug, and the spacer is made of a resin material. | 08-21-2008 |
| 20080314074 | Integrated unit for refrigeration cycle device - In an integrated unit including an evaporator and an ejector located inside a tank of the evaporator, a first vibration-isolating seal member and a second vibration-isolating seal member are disposed in a gap between an outer surface of the ejector and an inner surface of the tank. The first vibration-isolating seal member is located between a refrigerant discharge port and a refrigerant suction port of the ejector in a longitudinal direction, and the second vibration-isolating seal member is located between a refrigerant flow inlet of the ejector and the refrigerant suction port in the longitudinal direction. Furthermore, the first vibration-isolating seal member has a seal capability lower than that of the second vibration-isolating seal member, and a vibration isolation capability higher than that of the second vibration-isolating seal member. | 12-25-2008 |
| 20090283247 | Evaporator unit - An evaporator unit includes an evaporator configured to evaporate a refrigerant, and a capillary tube configured to decompress the refrigerant. The capillary tube has two longitudinal ends bonded to the evaporator. At least one position of a middle portion between the two longitudinal ends of the capillary tube is fixed to the evaporator by press-contacting the evaporator. Therefore, it can prevent a crack from being caused at the bonding portions of the two longitudinal ends of the capillary tube. | 11-19-2009 |
| 20090293535 | Heat exchanger - A heat exchanger includes a heat exchanging section for performing heat exchange between a refrigerant and a cooling medium and a passage section. The passage section includes a first passage and a second passage for supplying the refrigerant to the heat exchanging section and a supply passage for supplying the refrigerant to the first passage and the second passage. The first passage and the second passage define a first opening portion and a second opening portion opening at an end of the supply passage. A minimum distance between an opening edge of the first opening portion and an inner surface of the supply passage is equal to a minimum distance between an opening edge of the second opening portion and the inner surface of the supply passage. | 12-03-2009 |
Yan L. Aung, Peoria, AZ US
| Patent application number | Description | Published |
|---|---|---|
| 20080309518 | SYSTEM AND METHOD FOR DISPLAYING REQUIRED NAVIGATIONAL PERFORMANCE CORRIDOR ON AIRCRAFT MAP DISPLAY - A method is provided for indicating the boundaries of a required navigational performance (RNP) corridor on an aircraft's map display. The method includes the steps of producing an aircraft leg segment symbol on the map display, establishing an RNP value, and scaling the RNP value to the map display field of view. The method further includes the step of generating an RNP corridor boundary graphic on the map display offset from the aircraft leg segment symbol by the scaled RNP value. | 12-18-2008 |
Yan Lin Aung, Peoria, AZ US
| Patent application number | Description | Published |
|---|---|---|
| 20090327273 | METHOD FOR PROVIDING SEARCH AREA COVERAGE INFORMATION - A method for displaying search area coverage is provided. A searched area ( | 12-31-2009 |