About 18 results
https://drivepatents.com/patents/1398392 · 8 Jan 2025
A turbocharger includes: a bearing; a casing for accommodating the bearing; and a first thermometer including a first temperature sensor for measuring temperature of lubricant oil. The casing includes a lubricant oil discharge part having a lubricant oil o...
https://drivepatents.com/patents/959769 · 24 Jun 2015
Acoustic pyrometry-based active temperature monitoring of gas turbine combustors, including industrial gas turbine (IGT) combustors is incorporated into the combustion monitoring and control system by addition of an acoustic transmitter or acoustic transce...
https://drivepatents.com/patents/959767 · 24 Jun 2015
Active acoustic pyrometry-based gas flow temperature measurement, such as for monitoring of gas turbine combustors, including industrial gas turbine (IGT) combustors is incorporated into the combustion monitoring and control system by addition of an acoust...
https://drivepatents.com/patents/980758 · 18 Dec 2013
A thermally actuated assembly (10) for a gas turbine assembly for a gas turbine system includes a heat transfer component (20) having a first portion (22) and a second portion (24), wherein the first portion (22) is disposed within a first cavity (14) havi...
https://drivepatents.com/patents/982179 · 6 Nov 2013
An apparatus for measuring the circumferential distribution of temperature in a fluid, comprising a plurality of sensor ladders, each incorporating a plurality of temperature sensors, wherein a first one of the sensor ladders partially overlaps a second on...
https://drivepatents.com/patents/984872 · 5 Jun 2013
A method of determining the actual position of a control surface (27). The method comprises receiving a signal (34) representative of a required position of the control surface (27), repositioning the control surface (27) in response to the signal (34) by ...
https://drivepatents.com/patents/993830 · 16 Jan 2013
A thermal management system (68) for a gas turbine engine (20) includes a first heat exchanger (HX1) and a second heat exchanger (HX2) in communication with a bypass flow through an inlet (70). A valve (72) is operable to selectively communicate the bypass...
https://drivepatents.com/patents/1000941 · 27 Jun 2012
The present invention relates to a method of detecting a predetermined condition in a gas turbine (10) and to a failure detection system for a gas turbine (10). The invention analyses instantaneous temperature readings from different locations (42, 32) in ...
https://drivepatents.com/patents/1005351 · 8 Feb 2012
A system (10) includes a radiation detector array (52) configured to direct a field of view (74) toward multiple conduits (60) within a fluid flow path from a turbine (16, 34) into a heat exchanger (26, 40). The radiation detector array (52) is configured ...
https://drivepatents.com/patents/1005335 · 8 Feb 2012
A system (10) includes a radiation sensor (66) configured to direct a field of view (90) toward at least one conduit (74) along a fluid flow path into a heat exchanger (34, 54). The radiation sensor (66) is configured to output a signal indicative of a tem...