Blading system for axial compressors with axially opposing base merged double triangular prism device blades.
OA22339AActive Publication Date: 2026-10-20SPACEROLLS AEROSPACE TECHNOLOGIES PRIVATE LIMITED
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Patent Information
- Application Number
- OA1202500221
- Authority / Receiving Office
- OA · OA
- Patent Type
- Patents
- Current Assignee / Owner
- Filing Date
- 2024-01-27
- Publication Date
- 2026-10-20
- Estimated Expiration
- 2044-01-27
Abstract
Introducing the ABMP Compressor, a cuttingedge axial flow compressor technology set to transform gas turbine jet engines and find applications across various domains. Our innovation focuses on optimizing compression ratios and maximizing energy extraction, ensuring efficient operation in diverse conditions. The ABMP Compressor offers adaptability, allowing strategic adjustments for peak performance. Embracing environmentaI responsibility, it supports sustainable fuels and cleaner energy initiatives. lts seamless integration with turbofans enhances performance and reduces vibrations in gas turbine jet engines and other applications. Engineered to prevent operationaI disruptions, the compressor mitigates compression stall and surge, promoting stable combustion efficiency with uniform fuel distribution and stable flame fronts. With extended operationaI limits, reduced wear and tear, and overall system-wide performance enhancement, the ABMP Compressor signifies a transformative solution in the evolving landscape of propulsion systems. Figure 7
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