Kurt Kramer Schleif - Greenville SC, US Philip Michael Caruso - Simpsonville SC, US Seung-Woo Choi - Greer SC, US Robert David Jones - Simpsonville SC, US Jong Youn Pak - Oakland Township MI, US
Assignee:
General Electric Company - Schenectady NY
International Classification:
G01M 15/14
US Classification:
7311201
Abstract:
A sensor is provided and includes a body disposed at a point of measurement interest on a rotor at a radial distance from a centerline thereof and having a substantially cylindrical shape and first and second opposing ends and a sensing end coupled to one of the first and second opposing ends, the other of the first and second opposing ends being coupled to a communication system, the sensing end including a sensing device configured to generate a signal reflective of a detected condition at the point of measurement interest, and at least one of the first and the second opposing ends being formed to define a shoulder portion for absorbing gravitational loading.
Kurt Kramer Schleif - Greenville SC, US Gregory Quentin Brown - Simpsonville SC, US Philip Michael Caruso - Simpsonville SC, US Fernando Jorge Casanova - Simpsonville SC, US Seung-Woo Choi - Greer SC, US Josef Scott Cummins - Simpsonville SC, US Matthew Ryan Ferslew - Johnson City TN, US Andrew Clifford Hart - Mauldin SC, US Robert David Jones - Simpsonville SC, US Jong Youn Pak - Oakland Township MI, US Francesco Soranna - Greer SC, US
Assignee:
GENERAL ELECTRIC COMPANY - Schenectady NY
International Classification:
G01D 21/00
US Classification:
7311201
Abstract:
A communication system is provided and includes a sensor to measure a condition at a point of measurement interest defined on a rotor of a turbine at a radial distance from a centerline about which the rotor is rotatable, wiring disposed on the rotor at a radial distance from the centerline, the wiring including a first wiring section coupled to the sensor, a second wiring section and a first connection by which the first and second wiring sections are connectable, a second connection by which the second wiring section transmits a signal reflective of the detected condition to a non-rotating recording element and a temperature compensation module disposed on the second wiring section to adjust the signal.
Kurt Kramer Schleif - Greenville SC, US Gregory Quentin Brown - Simpsonville SC, US Philip Michael Caruso - Simpsonville SC, US Fernando Jorge Casanova - Simpsonville SC, US Seung-Woo Choi - Greer SC, US Josef Scott Cummins - Simpsonville SC, US Matthew Ryan Ferslew - Johnson City TN, US Andrew Clifford Hart - Mauldin SC, US Robert David Jones - Simpsonville SC, US Jong Youn Pak - Oakland Township MI, US Francesco Soranna - Greer SC, US
Assignee:
GENERAL ELECTRIC COMPANY - Schenectady NY
International Classification:
G01L 7/00 G01D 21/00
US Classification:
73756, 738665
Abstract:
A turbine is provided and includes a rotor, which is rotatable about a centerline thereof, a sensor to measure a condition at a point of measurement interest defined on the rotor at a radial distance from the centerline, a communication system by which condition measurements are transmittable from the sensor to a non-rotating recording system and a probe holder to secure the sensor and a portion of the communication system on the rotor proximate to the point of measurement interest.
Kurt Kramer Schleif - Greenville SC, US Gregory Quentin Brown - Simpsonville SC, US Philip Michael Caruso - Simpsonville SC, US Fernando Jorge Casanova - Simpsonville SC, US Seung-Woo Choi - Greer SC, US Josef Scott Cummins - Simpsonville SC, US Matthew Ryan Ferslew - Johnson City TN, US Andrew Clifford Hart - Mauldin SC, US Robert David Jones - Simpsonville SC, US Jong Youn Pak - Oakland Township MI, US
Assignee:
GENERAL ELECTRIC COMPANY - Schenectady NY
International Classification:
G01D 21/00
US Classification:
738665
Abstract:
A turbine is provided and includes a component having a body, which is rotatable about a rotor centerline and which is formed to define a cavity radially proximate to a point of measurement interest defined at a radial distance from the centerline, a sensor to measure a condition at the point of measurement interest, a communication system by which condition measurements are transmittable from the sensor to a non-rotating recording system and a probe holder insertible into the cavity to secure the sensor proximate to the point of measurement interest.
Purge Systems For Rotary Machines And Methods Of Assembling Same
Creston Lewis Dempsey - Mauldin SC, US Seung-Woo Choi - Greer SC, US Raymond Joseph Lecuyer - Taylors SC, US Matthew Ryan Ferslew - Johnson City TN, US Jong Youn Pak - Oakland Township MI, US Josef Scott Cummins - Simpsonville SC, US
International Classification:
F01D 17/00 B23P 19/00
US Classification:
415145, 29700
Abstract:
A method for assembling a rotary machine includes providing a first rotatable element. The method also includes coupling a second rotatable element to the first rotatable element. The first rotatable element and the second rotatable element at least partially define a cavity therein and at least one conduit extending substantially axially therebetween. Further, the method includes coupling a purge device including at least one radial channel defined therein and extending to the first rotatable element and to the second rotatable element such that the at least one radial channel is coupled in flow communication with the cavity and with the at least one axial conduit.
Systems And Methods For Reducing Or Limiting One Or More Flows Between A Hot Gas Path And A Wheel Space Of A Turbine
- Schenectady NY, US Xiaoqing Zheng - Schenectady NY, US Jong Youn Pak - Oakland Township MI, US
Assignee:
General Electric Company - Schenectady NY
International Classification:
F01D 11/02
US Classification:
60722, 4151745, 277301
Abstract:
A turbine assembly is disclosed herein. The turbine assembly may include a rotor with at least one bucket extending radially therefrom. The turbine assembly also may include a stator assembly positioned adjacent to the at least one bucket. Moreover, the turbine assembly may include a seal assembly. The seal assembly may include a first flange extending in a substantially axial direction from the at least one bucket. The seal assembly also may include a second flange extending from the stator assembly in the substantially axial direction opposite the first flange. The second flange may include at least one protuberance projecting towards the first flange.