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公开(公告)号：US20110286847A1
公开(公告)日：2011-11-24
申请号：US12978971
申请日：2010-12-27
申请人： Brian Paul King
发明人： Brian Paul King
IPC分类号： F01D5/22
CPC分类号： F01D9/041 , F01D9/042 , F01D9/065 , F05D2260/30 , Y02T50/672 , Y02T50/673
摘要： One embodiment of the present invention is a gas turbine engine. Another embodiment is a gas turbine engine vane system. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for gas turbine engine vanes. Further embodiments, forms, features, aspects, benefits, and advantages of the present application shall become apparent from the description and figures provided herewith.
摘要翻译： 本发明的一个实施例是燃气涡轮发动机。 另一实施例是燃气涡轮发动机叶片系统。 其他实施例包括用于燃气涡轮发动机叶片的装置，系统，装置，硬件，方法和组合。 本申请的其他实施例，形式，特征，方面，益处和优点将从本文提供的描述和图中变得显而易见。
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公开(公告)号：US09109539B2
公开(公告)日：2015-08-18
申请号：US12978876
申请日：2010-12-27
申请人： Robert T. Duge , Craig Heathco , Brian Paul King
发明人： Robert T. Duge , Craig Heathco , Brian Paul King
CPC分类号： F02K7/16 , F02K3/02 , F02K7/10 , F02K7/14 , F05D2220/74
摘要： An aircraft powerplant is disclosed that can be operated in at least three modes including as a gas turbine engine, as an engine having a ramburner, and as an engine having a forward compression combustor engine such as a ramjet and/or scramjet. An airflow valve is provided to direct air to a downstream portion of the aircraft engine and can be positioned as a function of the aircraft operating modes. The valve can be used to cocoon the gas turbine engine.
摘要翻译： 公开了一种飞行器动力装置，其可以以至少三种模式运行，包括作为燃气涡轮发动机，具有前进式飞行器的发动机，以及作为具有诸如冲压喷气发动机和/或冲压喷气发动机的正压缩燃烧器发动机的发动机。 提供一个气流阀以将空气引导到飞行器发动机的下游部分，并且可以根据飞行器操作模式来定位。 该阀可用于焚化燃气轮机。
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公开(公告)号：US09080448B2
公开(公告)日：2015-07-14
申请号：US12978971
申请日：2010-12-27
申请人： Brian Paul King
发明人： Brian Paul King
CPC分类号： F01D9/041 , F01D9/042 , F01D9/065 , F05D2260/30 , Y02T50/672 , Y02T50/673
摘要： One embodiment of the present invention is a gas turbine engine. Another embodiment is a gas turbine engine vane system. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for gas turbine engine vanes. Further embodiments, forms, features, aspects, benefits, and advantages of the present application shall become apparent from the description and figures provided herewith.
摘要翻译： 本发明的一个实施例是燃气涡轮发动机。 另一实施例是燃气涡轮发动机叶片系统。 其他实施例包括用于燃气涡轮发动机叶片的装置，系统，装置，硬件，方法和组合。 本申请的其他实施例，形式，特征，方面，益处和优点将从本文提供的描述和图中变得显而易见。
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公开(公告)号：US20120159925A1
公开(公告)日：2012-06-28
申请号：US12978876
申请日：2010-12-27
申请人： Robert T. Duge , Craig Heathco , Brian Paul King
发明人： Robert T. Duge , Craig Heathco , Brian Paul King
IPC分类号： F02K3/06
CPC分类号： F02K7/16 , F02K3/02 , F02K7/10 , F02K7/14 , F05D2220/74
摘要： An aircraft powerplant is disclosed that can be operated in at least three modes including as a gas turbine engine, as an engine having a ramburner, and as an engine having a forward compression combustor engine such as a ramjet and/or scramjet. An airflow valve is provided to direct air to a downstream portion of the aircraft engine and can be positioned as a function of the aircraft operating modes. The valve can be used to cocoon the gas turbine engine.
摘要翻译： 公开了一种飞行器动力装置，其可以以至少三种模式运行，包括作为燃气涡轮发动机，具有前进式飞行器的发动机，以及作为具有诸如冲压喷气发动机和/或冲压喷气发动机的正压缩燃烧器发动机的发动机。 提供一个气流阀以将空气引导到飞行器发动机的下游部分，并且可以根据飞行器操作模式来定位。 该阀可用于焚化燃气轮机。
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公开(公告)号：US06190133B1
公开(公告)日：2001-02-20
申请号：US09134392
申请日：1998-08-14
IPC分类号： F01D514
CPC分类号： F01D5/28 , F01D5/147 , F05D2240/80 , Y02T50/672 , Y02T50/673
摘要： A cast metallic airfoil structure having a high stiffness core positioned therein for increasing the stiffness of the airfoil. In one embodiment, the high stiffness core is preferably formed of gamma titanium aluminde or a titanium metal matrix composite and is metallurgically bonded to the cast metallic airfoil structure. In one form the airfoil structure forms a portion of an integrally bladed rotor, and in a second form the airfoil structure has a dove tail attachment portion.
摘要翻译： 一种铸造金属翼型结构，其中具有高刚性芯，其中设置有用于增加翼型的刚度。 在一个实施例中，高刚度芯优选由γ钛铝或钛金属基复合材料形成，并与铸造金属翼型结构冶金结合。 在一种形式中，翼型结构形成整体叶片转子的一部分，并且在第二形式中，翼型结构具有鸽尾配件部分。
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