General Electric Company

International Business Machines Corporation

Microsoft Technology Licensing, LLC

Beijing Xiaomi Mobile Software Co., Ltd.

Southeast University

Nec (china) Co., Ltd.

Samsung Electronics Co., Ltd.

Telefonaktiebolaget Lm Ericsson (publ)

Vmware, Inc.

Lenovo (beijing) Limited

Beijing Lenovo Software Ltd.

China National Petroleum Corporation

Cnpc Engineering Technology R&d Company Limited

Hua Zhang

Valery Ivanovich Ponyavin

Bradly Aaron Kippel

Dean Matthew Erickson

Laxmikant Merchant

Douglas Scott Byrd

Naveen Ghattadhahalli Parmeshwar

David Wesley Ball, Jr

Douglas Frank Beadie

Gilbert Otto Kraemer

Jatila Ranasinghe

Jianmin Zhang

Kenneth Neil Whaling

Dinesh Venugopal Setty

Geoffrey David Myers

Jason Allen Seale

David Terry Trayhan, Jr

Christopher Conrad Frese

Fabien Thibault Codron

Iris Ziqin Hu

Gregory Allen Boardman

Kenneth Eugene Selfridge

Thomas Francis Taylor

Javeed Iqbaluddin Mohammed

Wei Xu

Ming Lei

Parag Prakash Kulkarni

Jianhua Wang

Dale Joel Davis

Zhong Tian

Chaofeng Li

Tailai Hu

Xin Liu

Sal Albert Leone

Richard Lynn Loud

William Thomas Ross

Sudhakar Todeti

Christina Renee Pompey

Biao Han

James Frederik Den Outer

Yongjiang Hao

Michael Savale

Jae-Won Lee

Ming Xu

Lewis Berkley Davis, Jr

Jing Liu

Canan Uslu Hardwicke

Joseph James Lacey

Chi Zhang

Kun Shi

Peng Han

Dong Wang

Timothy Andrew Healy

Gunnar Leif Siden

Mei-Yuh Hwang

Jeffrey Clarence Jones

Cong Peng

Gregory Allan Crum

Larry Swanson

Diego Fernando Rancruel

Neil Colin Widmer

Paul Burchell Glaser

Yue Yu

Xuan Zhu

Adam John Fredmonski

Jason Anton Byers

Hong Jun Tu

Joseph Anthony Cotroneo

Shui Liu

Thomas James Brunt

Jun Jie Nan

Yanyan Liu

Doug Scott Byrd

William James Lawson

Barrett David Gardiner

David William Smith

Jianzhou Jin

Yongjin Yu

Liping Wang

Jiaheng Wang

Wenjie Wu

Seth Harmon Chapman

Venugopala Durwasula Raju

Leslie Yung-Min Tong

Francesco Soranna

Songli Li

Priscilla Childers

Ravi Praveen S Eluripati

Yaqi Liu

Zishuai Liu

Yuchao Guo

Shuoqiong Liu

Yang Liu

Fengzhong Qi

Zhiwei Ding

Ravi Praveen Eluripati

Jitendra Harish Bijlani

Bomin Nie

Chongfeng Zhou

A method and an apparatus for adjusting antenna radiation power includes adjusting antenna radiation power includes: acquiring a power index identification of a triggered SAR sensor group; acquiring target radiation power corresponding to the power index identification according to a first mapping relationship; and determining a corresponding radiator according to a second mapping relationship and the SAR sensor group and adjusting radiation power of the radiator into the target radiation power. The method and apparatus may be incorporated in an electronic device.

Method and apparatus for adjusting antenna radiation power and electronic device

A method for detecting the state of the proximity sensor, applied to a terminal including the proximity sensor and an antenna, includes: sending a predetermined instruction to the proximity sensor; determining whether the proximity sensor is abnormal based on a feedback result of the proximity sensor to the predetermined instruction; and maintaining the antenna transmitting power at a low power if the proximity sensor is abnormal. Through the feedback of the proximity sensor to the request to obtain the capacitance value, it is determined whether the proximity sensor can work normally, and in a case that the proximity sensor cannot work normally, the antenna transmitting power is reduced to avoid the continuous high antenna transmitting power due to the inability of the proximity sensor to work normally, which reduces the radiation to the human body.

Method and apparatus for detecting state of proximity sensor, terminal and non-transitory computer-readable storage medium

The invention provides a high temperature resistant Portland cement slurry and a production method thereof. The high temperature resistant Portland cement slurry comprises the following components by weight: 100 parts of an oil well Portland cement, 60-85 parts of a high temperature reinforcing material, 68-80 parts of fresh water, 1-200 parts of a density adjuster, 0.1-1.5 parts of a suspension stabilizer, 0.8-1.5 parts of a dispersant, 3-4 parts of a fluid loss agent, 0-3 parts of a retarder and 0.2-0.8 part of a defoamer. The high temperature resistant Portland cement slurry has a good sedimentation stability at normal temperature, and develops strength rapidly at a low temperature. The compressive strength is up to 40 MPa or more at a high temperature of 350&#xb0; C., and the long-term high-temperature compressive strength develops stably without degradation. Therefore, it can meet the requirements for field application in heavy oil thermal recovery wells, reaching the level of Grade G Portland cement for cementing oil and gas wells.

High temperature resistant Portland cement slurry and production method thereof

An inlet bleed heat (IBH) system for use in a turbine engine including a silencer assembly. The inlet bleed heat (IBH) system includes a feed pipe for delivering compressor discharge air. The feed pipe includes a plurality of orifices along at least a portion of a length of the feed pipe, and each orifice of the plurality of orifices extends through a wall of the feed pipe for allowing the compressor discharge air to exit the feed pipe. The system also includes a heat shielding component that extends across the feed pipe, wherein the heat shielding component is configured to reduce heat transfer between the feed pipe and the silencer assembly of the turbine engine.

Inlet bleed heat system for use in a turbine engine

A system includes an inlet duct disposed about an inlet axis, wherein the inlet duct is configured to direct an airflow along the inlet axis to a compressor inlet. The inlet includes an inlet heating system and a heating portion having a longitudinal axis that is substantially perpendicular to the inlet axis. The inlet heating system includes a first conduit substantially parallel to the longitudinal axis that is configured to distribute a heated fluid directly to the airflow via a first set of openings of a first end zone of the first conduit and a second set of openings of a second zone of the first conduit. The first end zone is configured to receive the heated fluid from a heating source, the second zone is coupled to the first end zone, and the second zone is configured to receive the heated fluid from the first end zone.

Compact compressor intake system and method

A system includes a gas turbine system having a first compressor, a combustor, and a turbine, where the first compressor provides a first portion of a discharge air directly to the combustor. The system includes a fluid circuit which receives a fluid comprising a second portion of the discharge air from the first compressor or a combustible fluid and provides the second portion of the discharge air to fuel at a location upstream of the combustor to alter a chemical and physical characteristic of the fuel in an air-fuel mixture that is provided to the combustor.

System and method for flexible fuel usage for gas turbines

A system includes a fluid distribution system. The fluid distribution system includes multiple spray rings disposed upstream of an inlet of a compressor. The multiple spray rings include a first spray ring disposed about an axis of the compressor in a first plane substantially perpendicular to the axis. The first spray ring includes a first set of nozzles disposed about the axis and configured to spray a first fluid flow toward the compressor inlet. The multiple spray rings further include a second spray ring disposed about the axis of the compressor in a second plane substantially perpendicular to the axis. The second spray ring includes a second set of nozzles disposed about the axis and configured to spray a second fluid flow toward the compressor inlet. The first plane is different than the second plane.

Compressor circumferential fluid distribution system

A gas turbine system includes an exhaust processing system that may process exhaust gas generated by a gas turbine engine, the exhaust processing system includes an exhaust diffuser that may receive the exhaust gas from a turbine of the gas turbine engine and having an annular passage disposed between an inner annular wall and an outer annular wall, and an air injection assembly disposed within the exhaust diffuser. The air injection assembly includes one or more air injection conduits disposed within the annular passage of the exhaust diffuser and including fluid injection holes that may direct a cooling fluid into a first mixing region of the exhaust diffuser.

Gas turbine exhaust diffuser with air injection

A turbine engine comprising includes at least one combustor, a liquid fuel supply system, and a fuel additive injection system. The combustor is configured to combust liquid fuel. The liquid fuel supply system is configured to channel liquid fuel through at least one fuel line to the at least one combustor. The fuel additive injection system is coupled in fluid communication with the liquid fuel supply system. The fuel additive injection system includes a recirculation circuit configured to recirculate at least a portion of liquid fuel to the liquid fuel supply system. The fuel additive injection system is configured to channel chemical additive through the recirculation circuit for mixing with the at least a portion of liquid fuel to generate an additive fuel mixture configured to inhibit coke formation in the liquid fuel supply system.

Fuel additive injection system and methods for inhibiting coke formation

An exhaust processing system that includes: an exhaust passageway for directing exhaust gases, the exhaust passageway having passageway walls that define and enclose the exhaust passageway between an upstream position and a downstream position; and an acoustic liner formed against and covering at least one of the passageway walls of the exhaust passageway. The acoustic liner may include uniformly configured modular acoustic blocks fitted against each other. The modular acoustic blocks each may include interior cavities having different lengths configured to dampen targeted sound frequencies.

Modular acoustic blocks and acoustic liners constructed therefrom

A method includes assembling a silencer baffle configured to mount in a fluid conduit along a fluid flow path, where assembling the silencer baffle includes coupling together a plurality of baffle sections via mating interlock structures.

Method for installing and removing modularized silencer baffles

In one embodiment, a turbine system includes a compressor, an intake section including a filter house and an inlet duct. The intake section is coupled to the compressor, and the filter house is upstream from the inlet duct. The turbine system also includes one or more sensors disposed in the intake section, and a processor configured to receive sensor data from the one or more sensors, one or more filter degradation rates for one or more filtration stages of the filter house, or some combination thereof, predict a compressor degradation rate for the compressor using a compressor degradation prediction model that provides a function of performance of the compressor based on the sensor data, the one or more filter degradation rates, or some combination thereof, and perform one or more preventative actions based on the compressor degradation rate prediction.

System and method for condition-based monitoring of a compressor

This disclosure provides methods and systems for using coatings to control component dimensions during operations of a mechanical system, such as gas turbine combustion air cooling system. The mechanical system may have a component with a critical dimension defined by at least one surface. Upon detecting a change in the critical dimension, such as from surface erosion, a coating additive is deployed into the mechanical system. The surface is coated with the coating additive to offset at least a portion of the change in the critical dimension.

Systems and methods for coating to control component dimensions

A system and a method for predicting and optimizing remaining hardware life of gas turbine components. Operating parameters of the gas turbine which may impact remaining hardware life are sensed and tracked using a plurality of sensors in communication with a control system including a computing device. Remaining hardware life is predicted using a physics-based hardware lifing model. The hardware lifing model may include an output of a filtration model configured to monitor contaminants based on a pressure drop across a filter. Optimizing the remaining hardware life is achieved by the control system adjusting one or more operation settings of the gas turbine.

System and method for monitoring hot gas path hardware life

Growing community of inventors

Greer, SC, United States of America

Hua Zhang