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1. 发明公开

EP1977082A2 ELECTRIC TURBINE BYPASS FAN AND COMPRESSOR FOR HYBRID PROPULSION 审中-公开
标题翻译：旁通送风扇，电力厂进行混合动力驱动压缩机
公开(公告)号：EP1977082A2
公开(公告)日：2008-10-08
申请号：EP07716374.9
申请日：2007-01-09
申请人： Sonic Blue Aerospace , Lugg, Richard H.
发明人： LUGG, Richard, H.
IPC分类号： F01D5/02 , F01D7/00 , F01D17/12
CPC分类号： F01D5/142 , F01D15/10 , F02K3/02 , F04D19/026 , F04D25/0613 , Y02T50/673
摘要： An electric turbine compressor fan for hybrid propulsion wherein the compressor contains one or more rotor stages (compressor and diffuser), each being driven by one or more electric ring motors, such that the compressor rotor stages are designed and tuned more precisely to the compression ratio to be attained within the turbine design operating characeristics, thrust requirements and flight envelope.

2. 发明申请

WO2010096087A1 MAGNETIC ADVANCED GENERATION JET ELECTRIC TURBINE 审中-公开
标题翻译：磁力发电喷气式电动涡轮机
公开(公告)号：WO2010096087A1
公开(公告)日：2010-08-26
申请号：PCT/US2009/054317
申请日：2009-08-19
申请人： SONIC BLUE AEROSPACE, INC. , LUGG, Richard, H.
发明人： LUGG, Richard, H.
IPC分类号： F02K1/00 , F02K99/00 , F02C6/20 , F02C7/00 , F02B61/04
CPC分类号： F02C3/04 , F01D15/10 , F02C7/32 , F02K1/08 , F02K3/025 , F02K3/06 , F02K5/00 , F05D2270/172 , F05D2300/507 , H05H1/50
摘要： 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.
摘要翻译：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。

3. 发明申请

WO2007081817A2 ELECTRIC TURBINE BYPASS FAN AND COMPRESSOR FOR HYBRID PROPULSION 审中-公开
标题翻译：电动涡轮风扇和压缩机混合推进
公开(公告)号：WO2007081817A2
公开(公告)日：2007-07-19
申请号：PCT/US2007/000307
申请日：2007-01-09
申请人： SONIC BLUE AEROSPACE , LUGG, Richard, H.
发明人： LUGG, Richard, H.
IPC分类号： F01B25/00
CPC分类号： F01D5/142 , F01D15/10 , F02K3/02 , F04D19/026 , F04D25/0613 , Y02T50/673
摘要： An electric turbine compressor fan for hybrid propulsion wherein the compressor contains one or more rotor stages (compressor and diffuser), each being driven by one or more electric ring motors, such that the compressor rotor stages are designed and tuned more precisely to the compression ratio to be attained within the turbine design operating characeristics, thrust requirements and flight envelope.
摘要翻译：一种用于混合推进的电动涡轮压缩机风扇，其中压缩机包含一个或多个转子级（压缩机和扩散器），每个转子级由压缩机和扩散器驱动，每个转子级由一个或多个电动环电机驱动，使得压缩机转子级被更精确地设计和调整为压缩比在涡轮机设计操作特性，推力要求和飞行范围内达到。

4. 发明申请

WO2006113877A2 HYBRID JET/ELECTRIC VTOL AIRCRAFT 审中-公开
标题翻译：混合喷气/电动垂直起降飞机
公开(公告)号：WO2006113877A2
公开(公告)日：2006-10-26
申请号：PCT/US2006/014902
申请日：2006-04-20
申请人： LUGG, Richard, H. , YOUNGREN, Harold
发明人： LUGG, Richard, H. , YOUNGREN, Harold
IPC分类号： B64C29/04
CPC分类号： B64C39/12 , B64C29/0025 , B64D27/24 , Y02T50/44 , Y02T50/64
摘要： A fixed-wing VTOL aircraft features an array of electric lift fans distributed over the surface of the aircraft. A generator is (selectively) coupled to the gas turbine engine of the aircraft. During VTOL operation of the aircraft, the engine drives the generator to generate electricity to power the lifting fans. Power to the lifting fans is reduced as the aircraft gains forward speed and is increasingly supported by the wings.
摘要翻译：固定翼型垂直起降飞机具有分布在飞机表面上的一系列电动升降风扇。发电机（选择性地）联接到飞行器的燃气涡轮发动机。在飞机的垂直起落架操作期间，发动机驱动发电机发电以对升降风扇供电。升降风扇的功率随着飞机获得前进速度而减少，并且越来越受到机翼的支持。

5. 发明申请

WO2016164649A1 HYPERJET SUPERCONDUCTING TURBINE BLISK PROPULSION AND POWER GENERATION 审中-公开
标题翻译：超高压涡轮增压推进和发电
公开(公告)号：WO2016164649A1
公开(公告)日：2016-10-13
申请号：PCT/US2016/026535
申请日：2016-04-07
申请人： LUGG, Richard, H.
发明人： LUGG, Richard, H.
IPC分类号： H02K21/02 , B64D27/24 , F01D5/03 , H02K21/04
CPC分类号： F01D15/10 , F01D5/34 , F02C3/113 , F02K3/06 , F02K7/10 , F05D2220/76 , F05D2220/764 , F05D2260/20 , F05D2300/507 , H01F6/04 , H02K7/1823 , H02K55/04 , Y02T50/673 , Y02T50/676
摘要： A. turbine assembly system and apparatus for a Hyper) et™ and method for making same is provided. Specifically, the turbine assembly provides a power generation system for a turbine engine and includes a plurality of stages. Each stage of the turbine assembly includes a stator having a wire distributed winding; and a rotatable blisk that encircle the stator with an air gap disposed therebetween. The rotatable blisk includes a rotor disk and a plurality of blades that extend radially outward from the rotor disk. The rotor disk includes six superconducting magnets positioned in a circular arrangement within the rotor disk to encircle the stator. An electromagnetic Held providing high power and power density is generated between the superconducting magnets and the stator with the blisk rotates about the stator during engine operation.
摘要翻译：提供了一种用于Hyper（TM）的涡轮组件系统和装置及其制造方法。具体地，涡轮机组件提供用于涡轮发动机的发电系统并且包括多个级。涡轮组件的每个阶段包括具有线分布绕组的定子; 以及围绕定子的可旋转的叶片，其间设置有气隙。可旋转叶片包括转子盘和从转子盘径向向外延伸的多个叶片。转子盘包括六个超导磁体，其位于转子盘内的环形布置中以环绕定子。在超导磁体和定子之间产生提供高功率和功率密度的电磁场，在发动机运转期间叶片绕定子旋转。

6. 发明申请

WO2007035298A2 ADVANCED HYPERSONIC MAGNETIC JET/ELECTRIC TURBINE ENGINE 审中-公开
标题翻译：先进的超声波喷射/电动涡轮发动机
公开(公告)号：WO2007035298A2
公开(公告)日：2007-03-29
申请号：PCT/US2006/035253
申请日：2006-09-11
申请人： LUGG, Richard, H.
发明人： LUGG, Richard, H.
IPC分类号： F02C9/16
CPC分类号： F02K7/10 , F01D5/03 , F02K3/00 , F02K3/08 , F02K5/00 , F03H1/0081 , F03H99/00 , F05D2220/34 , F05D2240/515 , Y02T50/67 , Y02T50/672 , Y02T50/673
摘要： With turbine segments controlled electrically in a shaftless design, the turbine of the present invention creates high propulsion efficiencies over a broader range of operating conditions through the integration of gas turbine, electric and magnetic power systems, advanced materials and alternative petroleum-based combustion c cles,
摘要翻译：涡轮机段在无轴设计中被电气控制，本发明的涡轮通过燃气轮机，电力和磁力系统，先进材料和替代的石油基燃烧气体的集成，在更宽的操作条件范围内产生高推进效率，

7. 发明申请

WO2016164932A1 HYPERSONIC ADVANCED GENERATION JET ELECTRIC TURBINE 审中-公开
标题翻译： HYPERSONIC ADVANCED GENERATION喷气式电动涡轮机
公开(公告)号：WO2016164932A1
公开(公告)日：2016-10-13
申请号：PCT/US2016/027001
申请日：2016-04-11
申请人： LUGG, Richard, H.
发明人： LUGG, Richard, H.
IPC分类号： F02C3/04 , F02C3/02 , F02C3/073
CPC分类号： F02K5/00 , B64D27/24 , Y02T50/44 , Y02T50/64 , Y02T50/672
摘要： The examples provided herein, including any summary of above summary of example aspects, serves to provide a basic understanding of the present disclosure. Such summary is not an extensive overview of all contemplated aspects, and is intended to neither identify key or critical elements of all aspects nor delineate the scope of any or all aspects of the present disclosure. Its sole purpose is to present one or more aspects in a simplified form as a prelude to the more detailed description of the disclosure that follows. To the accomplishment of the foregoing the one or more aspects of the present disclosure include the features described and example pointed out in the claims. A system, method, and methods of assembly and manufacturing a hypersonic jet electric turbine is provided.
摘要翻译：本文提供的实例包括上述范例方面的总结的任何概述，用于提供对本发明的基本理解。这种总结不是对所有预期方面的广泛概述，并且既不旨在标识所有方面的关键或关键要素，也不描述本公开的任何或所有方面的范围。其唯一目的是以简化的形式呈现一个或多个方面作为以下公开内容的更详细描述的前奏。为了实现上述内容，本公开的一个或多个方面包括在权利要求中指出的特征和示例。提供了组装和制造超音速喷气式电动涡轮机的系统，方法和方法。

8. 发明申请

WO2009129309A3 SUPERCONDUCTING TURBINE WIND RING GENERATOR 审中-公开
公开(公告)号：WO2009129309A3
公开(公告)日：2009-10-22
申请号：PCT/US2009/040667
申请日：2009-04-15
申请人： SONIC BLUE AEROSPACE, INC. , LUGG, Richard, H.
发明人： LUGG, Richard, H.
IPC分类号： F03D11/02 , F03D1/00
摘要： A wind generator is disclosed in which superconducting ring generators are utilized without the need for a load bearing drive shaft and other mechanical components allowing. for the use of variable geometry blades, a decrease in the overall weight, and an increase in the overall efficiency of the wind generator system.

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