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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Figure 2026505049000001_ABST
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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