General Electric Company

Bha Altair. LLC

Steve David Hiner

Paul Sherwood Bryant

Rahul Jaikaran Chillar

Rebecca Evelyn Hefner

Etienne Rene Jarrier

William Keith Eyers

Stephen Francis Banks

Simon Charles Larcombe

Jeff P Czapiewski

Paul Richardson

Certain embodiments herein relate to systems and methods for managing turbine intake filters. In one embodiment, a system can include at least one memory configured to store computer-executable instructions and at least one controller configured to access the at least one memory and execute the computer-executable instructions. The instructions may be configured to monitor an indication associated with air flow through at least one filter of a turbine intake system. The instructions may be further configured to facilitate in the execution of at least management task of the turbine intake system, based at least in part on the indication of air flow through the filter.

Systems and methods for managing turbine intake filters

A filtration system comprising at least one filter element, at least a first and a second filter media that are different to one another and are arranged in a parallel relationship, wherein fluid flow through the filtration system comprises a first fluid flow portion that flows through the first media and a second fluid flow portion that flows through the second media.

Filtration system and method of design

A monitoring system for monitoring the integrity of a member disposed within a machine includes an image analyzer configured to receive image data from an imaging device and to determine an amount of radiation incident on one or more of one or more pixels of the imaging device. The monitoring system also includes a monitor coupled to the image analyzer and configured to generate an alarm in the event an amount of radiation on one or more of the one or more pixels exceeds a limit.

Member integrity monitoring system and method

An embodiment of the present invention provides an air sampling system for measuring corrosives within an airstream flowing within an inlet system. This air sampling system may include an air sampling unit with a plurality of sampling coupons secured within. Parts of the air sampling system may be externally mounted to the inlet system, allowing for an operator to access the sampling coupons, while the inlet system operates. In operation, an embodiment of the present invention has a sampling line connected to the air sampling system; the airstream flowing within the sampling line passes over the sampling coupons and then returns to the inlet system.

System for sampling the airflow entering the compressor of a turbomachine

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Salisbury, United Kingdom

Steve David Hiner