Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

Method and apparatus for radial exhaust gas turbine

a technology of radial exhaust, which is applied in the direction of machines/engines, stators, liquid fuel engines, etc., can solve the problems of adversely affecting engine performance and/or engine efficiency, known gas turbine engines and known radial exhaust gas turbines that include an outer casing may experience high pressure losses in their exhaust diffuser sections

Inactive Publication Date: 2011-09-29
GENERAL ELECTRIC CO
View PDF11 Cites 196 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

[0007]It will thus be understood that embodiments of involute type casings are formed by joining different straight sections of metal sheets. The arrangement when installed on the radial exhaust gas turbine will reduce the pressure loss in the casing without increasing the cost of manufacturing the casing. The casing will collect the flue gas coming out from vanes and direct the flue gas towards one side. The involute type casing can be manufactured in right handed embodiments or left handed embodiments based upon engineering and installation requirements.

Problems solved by technology

At least some known gas turbine engines may experience high pressure losses.
Such pressure losses may adversely affect engine performance and / or engine efficiency.
For example, at least some known radial exhaust gas turbines that include an outer casing may experience high pressure losses in their exhaust diffuser sections.
Although circular outer casings can be used to reduce this pressure drop, such casings may be expensive to manufacture, especially for gas turbines that require large size casings.

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Method and apparatus for radial exhaust gas turbine
  • Method and apparatus for radial exhaust gas turbine
  • Method and apparatus for radial exhaust gas turbine

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0015]Embodiments of the present disclosure include an involute type casing for use with a radial exhaust diffuser of a gas turbine generator. The radial exhaust diffuser, when installed on the radial exhaust gas turbine facilitates reducing pressure loss in the casing generally, without increasing costs of manufacturing the casing. Flue gas discharged from vanes enters the casing and is directed towards one side of the casing.

[0016]In some embodiments, and referring specifically to FIG. 1, a radial exhaust gas turbine 100 includes an inlet section 102, a compressor section 104, a combustor section 106, a turbine section 108, and an exhaust diffuser section 112. FIG. 2 and FIG. 3 illustrate respective triaxial and exploded triaxial views, respectively, of exhaust diffuser casing 110. In the illustrated embodiment, exhaust diffuser casing 110 includes a turbine engagement wall 113 that includes an entry opening 114. An exhaust diffuser engagement wall 116 is positioned opposite turbi...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

No PUM Login to View More

Abstract

A radial exhaust gas turbine apparatus has a gas turbine engine that includes a radial exhaust diffuser section and a casing apparatus consisting essentially of polygonal walls, substantially straight plates, and substantially straight sidewalls. The casing apparatus encloses the radial exhaust diffuser section and is configured to direct at least a substantial portion of the gas exiting the radial exhaust diffuser section to an exit in the casing apparatus via an approximately involute path.

Description

BACKGROUND OF THE INVENTION[0001]The field of the present invention relates generally to gas turbine generators, and more specifically to involute type casings for use with radial exhaust gas turbines.[0002]At least some known gas turbine engines may experience high pressure losses. Such pressure losses may adversely affect engine performance and / or engine efficiency. For example, at least some known radial exhaust gas turbines that include an outer casing may experience high pressure losses in their exhaust diffuser sections. Although circular outer casings can be used to reduce this pressure drop, such casings may be expensive to manufacture, especially for gas turbines that require large size casings.[0003]It would therefore be desirable to provide a more efficient and less expensive casing for use with gas turbines that include a radial exhaust. In particular, it would be desirable to provide a casing that reduces pressure losses in the outer casing section while not being relat...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
IPC IPC(8): F04D29/44
CPCF01D25/30
Inventor SHENDE, SUMEDHKUMAR VYANKATESH
Owner GENERAL ELECTRIC CO
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Patsnap Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Patsnap Eureka Blog
Learn More
PatSnap group products