Gas turbine combustion chamber
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Benefits of technology
Problems solved by technology
Method used
Image
Examples
Embodiment Construction
[0017] Identical parts are provided with the same reference characters in both figures.
[0018] The gas turbine 1 according to FIG. 1 has a compressor 2 for combustion air, a combustion chamber or a gas turbine combustion chamber 4 and a turbine 6 for driving the compressor 2 and a generator (not shown) or a machine. To this end, the turbine 6 and the compressor 2 are arranged on a common turbine shaft 8 known as a turbine rotor, to which the generator and / or the machine are also connected, and which is supported such that it can be rotated about its center axis 9.
[0019] The combustion chamber 4 is equipped with a number of burners 10 for combusting a liquid or a gaseous fuel. Furthermore liner elements 25 are provided on its interior wall or combustion chamber wall 23.
[0020] The turbine 6 comprises a number of rotatable blades 12 connected to the turbine shaft 8. The blades 12 are arranged in a ring shape on the turbine shaft 8, thus forming a number of rows of blades. The turbine...
PUM
![No PUM](https://static-eureka.patsnap.com/ssr/23.2.0/_nuxt/noPUMSmall.5c5f49c7.png)
Abstract
Description
Claims
Application Information
![application no application](https://static-eureka.patsnap.com/ssr/23.2.0/_nuxt/application.06fe782c.png)
- R&D Engineer
- R&D Manager
- IP Professional
- Industry Leading Data Capabilities
- Powerful AI technology
- Patent DNA Extraction
Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic.
© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap