会员体验
专利管家(专利管理)
工作空间(专利管理)
风险监控(情报监控)
数据分析(专利分析)
侵权分析(诉讼无效)
联系我们
交流群
官方交流:
QQ群: 891211   
微信请扫码    >>>
现在联系顾问~
热词
    • 7. 发明申请
    • MAGNETIC ADVANCED GENERATION JET ELECTRIC TURBINE
    • 磁力发电喷气式电动涡轮机
    • WO2010096087A1
    • 2010-08-26
    • PCT/US2009/054317
    • 2009-08-19
    • SONIC BLUE AEROSPACE, INC.LUGG, Richard, H.
    • LUGG, Richard, H.
    • F02K1/00F02K99/00F02C6/20F02C7/00F02B61/04
    • F02C3/04F01D15/10F02C7/32F02K1/08F02K3/025F02K3/06F02K5/00F05D2270/172F05D2300/507H05H1/50
    • Supersonic Magnetic Advanced Generation Jet Electric Turbine (S-MAGJET) described herein, and a subsonic derivative, MAGJET, integrate a gas power turbine, superconducting electric power and propulsion generation, and magnetic power flux field systems along with an ion plasma annular injection combustor which utilizes alternative petroleum-based fuel and combustion cycles to create a hybrid turbine turbomachine for aerospace propulsion. The propulsion unit is able to achieve a dramatic increase in horsepower, combustion and propulsion efficiency, and weight reduction. In addition, the turbomachinery structures may be disposed within an exo-skeleton architecture that achieves an increase in thrust to weight ratio with a concomitant increase in fuel efficiency and power generation over traditional gas turbine technology today. The engine continuously adjusts the temperature, pressure and mass airflow requirements using an electromagnetic power management system architecture. Engine performance may be controlled across the entire desired flight envelope, whether subsonic, transonic or supersonic flight conditions. With bypass fan(s), compressor stages and turbine segments controlled electrically in a shaftless turbine design, the S-MAGJET maximizes the propulsion efficiencies over a broader range of operating conditions compared to current art of turbine technology and at much higher thermodynamic and aerodynamic efficiencies.
    • 本文所述的超音速磁性高级发电喷射式电动涡轮机(S-MAGJET)以及亚音速衍生物MAGJET将气体动力涡轮机,超导电力和推进发电以及磁力通量场系统与离子等离子体环形喷射燃烧器 利用替代的石油基燃料和燃烧循环来创建用于航空航天推进的混合涡轮机涡轮机。 推进装置能够大幅提高马力,燃烧和推进效率,减轻重量。 此外,涡轮机械结构可以设置在外骨架结构中,其实现了随着传统燃气轮机技术的燃料效率和发电量的同时增加,推力与重量比的增加。 发动机使用电磁功率管理系统架构连续调节温度,压力和质量气流要求。 发动机性能可以跨越整个所需的飞行包线进行控制,无论是亚音速,跨音速还是超音速飞行条件。 随着旁通风扇,压缩机级和涡轮机段在无轴式涡轮机设计中电气控制,与现有技术的涡轮技术相比,S-MAGJET在更宽的工作条件范围内最大限度地提高了推进效率,并且在更高的热力学和空气动力学效率 。