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Title: Connector tube for a turbine rotor cooling circuit

Abstract

A tubular connector adapted to extend between two tubular components comprising a tubular body having an internal diameter, a first free end including an annular radial flange having a tapered surface adapted to engage a complementary seating surface on a first of the two tubular components, the internal diameter remaining constant through the first free end; and a second free end having an annular bulbous shape adapted to seat within a cylindrical end of a second of the two tubular components.

Inventors:
 [1]
  1. Cincinnati, OH
Publication Date:
Research Org.:
General Electric Co., Schenectady, NY (United States)
OSTI Identifier:
874770
Patent Number(s):
US 6457934
Assignee:
General Electric Company (Schenectady, NY)
DOE Contract Number:  
FC21-95MC31176
Resource Type:
Patent
Country of Publication:
United States
Language:
English
Subject:
connector; tube; turbine; rotor; cooling; circuit; tubular; adapted; extend; components; comprising; internal; diameter; free; including; annular; radial; flange; tapered; surface; engage; complementary; seating; remaining; constant; bulbous; shape; seat; cylindrical; cooling circuit; tapered surface; /415/285/

Citation Formats

Li, Ming Cheng. Connector tube for a turbine rotor cooling circuit. United States: N. p., 2002. Web.
Li, Ming Cheng. Connector tube for a turbine rotor cooling circuit. United States.
Li, Ming Cheng. 2002. "Connector tube for a turbine rotor cooling circuit". United States. https://www.osti.gov/servlets/purl/874770.
@article{osti_874770,
title = {Connector tube for a turbine rotor cooling circuit},
author = {Li, Ming Cheng},
abstractNote = {A tubular connector adapted to extend between two tubular components comprising a tubular body having an internal diameter, a first free end including an annular radial flange having a tapered surface adapted to engage a complementary seating surface on a first of the two tubular components, the internal diameter remaining constant through the first free end; and a second free end having an annular bulbous shape adapted to seat within a cylindrical end of a second of the two tubular components.},
doi = {},
url = {https://www.osti.gov/biblio/874770}, journal = {},
number = ,
volume = ,
place = {United States},
year = {2002},
month = {1}
}

Works referenced in this record:

Development Requirements for an Advanced Gas Turbine System
journal, October 1995


Advances in Steam Path Technology
journal, April 1996