Blade arrangement system for an axial compressor having double triangular prism blades with axially opposed and united bases

JP2026505049APending Publication Date: 2026-02-10スペースロールズ エアロスペース テクノロジーズ プライベート リミテッド
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Patent Information

Application Number
JP2025543794
Authority / Receiving Office
JP · JP
Patent Type
Applications
Current Assignee / Owner
Priority Date
2023-01-27
Filing Date
2024-01-27
Publication Date
2026-02-10

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Abstract

The introduction of the ABMP compressor marks a revolution in gas turbine jet engines with cutting-edge axial compressor technology, finding applications across diverse sectors. Our innovation focuses on optimizing the compression ratio and maximizing energy extraction, ensuring efficient operation in diverse conditions. The ABMP compressor offers adaptability, enabling strategic adjustments toward peak performance. This supports initiatives toward sustainable fuels and cleaner energy, embracing environmental responsibility. Seamless integration with the turbofan enhances performance and reduces vibration in gas turbine jet engines and other applications. The compressor is designed to prevent operational interruptions, mitigating compression stall and surge, and promoting consistent combustion efficiency with uniform fuel distribution and a stable flame front. With extended operating limits, reduced wear and tear, and system-wide performance enhancements, the ABMP compressor represents a breakthrough solution in the evolving landscape of propulsion systems.
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