Axial compressor
A technology for axial flow compressors and rotating shafts, which is applied in the direction of axial flow pumps, mechanical equipment, engine components, etc., and can solve problems such as rusting and leakage of sliding parts, regardless of the sealability of variable stator blades and casings, and achieve suppression Leakage, the effect of improving reliability
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment Construction
[0020] Embodiments of the present invention will be described below using the drawings. First, use figure 1 A configuration example of a gas turbine system including an air suction spray mechanism will be described. figure 1 This is a simplified overall configuration diagram of a gas turbine system equipped with a suction spray mechanism.
[0021] The gas turbine system shown in this figure includes a compressor 1 that compresses air to generate high-pressure air, a combustor 2 that mixes the compressed air with fuel and burns them, and a turbine 3 that is rotationally driven by high-temperature combustion gas . The compressor 1 and the turbine 3 are mechanically connected to a generator 4 via a rotating shaft.
[0022] next, yes figure 1 The flow of working fluid in a gas turbine system is described. Air 11 as a working fluid flows into the compressor 1 , is compressed by the compressor 1 and flows into the combustor 2 as high-pressure air 12 . In the combustor 2 , high...
PUM
Login to View More Abstract
Description
Claims
Application Information
Login to View More - R&D
- Intellectual Property
- Life Sciences
- Materials
- Tech Scout
- Unparalleled Data Quality
- Higher Quality Content
- 60% Fewer Hallucinations
Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic, Popular Technical Reports.
© 2025 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap|About US| Contact US: help@patsnap.com
