公开(公告)号：US06426968B1

公开(公告)日：2002-07-30

申请号：US06374679

申请日：1982-05-04

Applicant: James R. Strife ,  John A. Dye ,  Warren R. Sigman

Inventor： James R. Strife ,  John A. Dye ,  Warren R. Sigman

IPC: H01S3081

CPC classification number: G02B7/1815 ,  H01S3/042 ,  H01S3/08059

Abstract: A hybrid mirror for reflecting high power optical beams comprises a reaction sintered silicon carbide substrate to which is bonded a plurality of silicon faceplates containing a plurality of coolant passages.

Abstract translation: 用于反射高功率光束的混合反射镜包括反应烧结的碳化硅基体，多个硅面板包含多个冷却剂通道。

公开(公告)号：US4885212A

公开(公告)日：1989-12-05

申请号：US152781

申请日：1988-02-05

Applicant: Karl M. Prewo ,  Vincent C. Nardone ,  James R. Strife

Inventor： Karl M. Prewo ,  Vincent C. Nardone ,  James R. Strife

IPC: C22C47/14

CPC classification number: C22C47/14 ,  Y10T428/12056

Abstract: A microstructurally toughened ceramic-particle-reinforced metal-matrix composite article is disclosed. The article exhibits a complex microstructure. The article exhibits high tensile strength, high elastic modulus and high impact resistance. A process for making the article is also disclosed. The process includes positioning structural elements within a metallic container to define one or more void spaces within the container, introducing a quantity of metallic particles or of a particular mixture of metallic particles and ceramic particles into the void spaces, and consolidating the container, structural elements and particles to form the microstructurally toughened composite article.

Abstract translation: 公开了一种微结构增韧的陶瓷颗粒增强金属基复合材料制品。 该文章显示出复杂的微观结构。 该制品具有高拉伸强度，高弹性模量和高抗冲击性。 还公开了制造该制品的方法。 该方法包括将结构元件定位在金属容器内以限定容器内的一个或多个空隙空间，将一定数量的金属颗粒或金属颗粒和陶瓷颗粒的特定混合物引入到空隙空间中，以及将容器，结构元件 和颗粒以形成微结构增韧的复合制品。

公开(公告)号：US08585368B2

公开(公告)日：2013-11-19

申请号：US13331957

申请日：2011-12-20

Applicant: Daniel V. Viens ,  Vincent C. Nardone ,  Peter G. Smith ,  James R. Strife ,  Foster P. Lamm

Inventor： Daniel V. Viens ,  Vincent C. Nardone ,  Peter G. Smith ,  James R. Strife ,  Foster P. Lamm

IPC: B23K5/18

CPC classification number: F01D5/147 ,  F01D5/16 ,  F01D5/282 ,  F04D29/023 ,  F04D29/324 ,  F04D29/388 ,  F05D2260/96 ,  F05D2300/603 ,  F05D2300/612 ,  F05D2300/615 ,  Y02T50/672 ,  Y02T50/673

Abstract: A hybrid airfoil for a gas turbine engine is provided that includes a body and a panel. The body has a first side and a second side orientated opposite the first side. The first and second sides extend between a tip, a base, a leading edge and a trailing edge. The body includes a plurality of cavities disposed in the first side of the body, which cavities extend inwardly toward the second side. The cavities collectively form an opening. At least one rib is disposed between the cavities. A shelf is disposed around the opening. The panel is attached to the shelf first mounting surface and to the rib, and is sized to enclose the opening. The panel is a load bearing structure operable to transfer loads to the body and receive loads from the body.

Abstract translation: 提供了一种用于燃气涡轮发动机的混合翼型件，其包括主体和面板。 主体具有与第一侧相对定向的第一侧和第二侧。 第一和第二面在尖端，底座，前缘和后缘之间延伸。 主体包括设置在主体的第一侧中的多个空腔，空腔向内朝向第二侧延伸。 空腔共同形成开口。 至少一个肋设置在空腔之间。 一个搁板设置在开口周围。 面板连接到搁架第一安装表面和肋上，并且其尺寸被设计成封闭开口。 面板是承载结构，可操作以将负载传递到主体并从身体接收负载。

公开(公告)号：US5079099A

公开(公告)日：1992-01-07

申请号：US311790

申请日：1989-02-16

Applicant: Karl M. Prewo ,  Vincent C. Nardone ,  James R. Strife

Inventor： Karl M. Prewo ,  Vincent C. Nardone ,  James R. Strife

IPC: C22C47/14

CPC classification number: C22C47/14 ,  Y10T428/12056 ,  Y10T428/12083 ,  Y10T428/1209 ,  Y10T428/12097 ,  Y10T428/12486

Abstract: A microstructurally toughened ceramic-particle-reinforced metal-matrix composite article is disclosed. The article exhibits a complex microstructure. The article exhibits high tensile strength, high elastic modulus and high impact resistance. A process for making the article is also disclosed. The process includes positioning structural elments within a metallic container to define one or more void spaces within the container, introducing a quantity of metallic particles or of a particulate mixture of metallic particles and ceramic particles into the void spaces, and consolidating the container, structural elements and particles to form the microstructurally toughened composite article.

Abstract translation: 公开了一种微结构增韧的陶瓷颗粒增强金属基复合材料制品。 该文章显示出复杂的微观结构。 该制品具有高拉伸强度，高弹性模量和高抗冲击性。 还公开了制造该制品的方法。 该方法包括在金属容器内定位结构弹性体以限定容器内的一个或多个空隙空间，将一定数量的金属颗粒或金属颗粒和陶瓷颗粒的颗粒混合物引入到空隙空间中，并将容器，结构元件 和颗粒以形成微结构增韧的复合制品。

公开(公告)号：US4911990A

公开(公告)日：1990-03-27

申请号：US152773

申请日：1988-02-05

Applicant: Karl M. Prewo ,  Vincent C. Nardone ,  James R. Strife

Inventor： Karl M. Prewo ,  Vincent C. Nardone ,  James R. Strife

IPC: C22C47/14

CPC classification number: C22C47/14 ,  Y10T428/12069 ,  Y10T428/1209 ,  Y10T428/12097 ,  Y10T428/12486

Abstract: A microstructurally toughened metallic article is disclosed. The article includes discrete metal regions which are enclosed within and separated from each other by a network of metal. The regions are bonded to the network to form stable interfacial boundaries. The article exhibits high impact resistance. The process for making the article is also disclosed. The process includes positioning a plurality of structural elements within a container to define one or more void spaces within the container, introducing a quantity of metallic particles into the void spaces, and then consolidating the container, structural elements, and particles to form the microstructurally toughened article.

Abstract translation: 公开了一种微结构增韧的金属制品。 该物品包括通过金属网络封闭在彼此中并且彼此分离的离散金属区域。 这些区域结合到网络上以形成稳定的界面边界。 该物品具有高抗冲击性。 还披露了制造该物品的过程。 该方法包括将多个结构元件定位在容器内以限定容器内的一个或多个空隙空间，将一定数量的金属颗粒引入空隙空间中，然后将容器，结构元件和颗粒固结以形成微结构强化 文章。

公开(公告)号：US20130039774A1

公开(公告)日：2013-02-14

申请号：US13331957

申请日：2011-12-20

Applicant: Daniel V. Viens ,  Vincent C. Nardone ,  Peter G. Smith ,  James R. Strife ,  Foster P. Lamm

Inventor： Daniel V. Viens ,  Vincent C. Nardone ,  Peter G. Smith ,  James R. Strife ,  Foster P. Lamm

IPC: F01D5/12 ,  F01D5/28 ,  F01D5/14 ,  F01D5/18

CPC classification number: F01D5/147 ,  F01D5/16 ,  F01D5/282 ,  F04D29/023 ,  F04D29/324 ,  F04D29/388 ,  F05D2260/96 ,  F05D2300/603 ,  F05D2300/612 ,  F05D2300/615 ,  Y02T50/672 ,  Y02T50/673

Abstract: A hybrid airfoil for a gas turbine engine is provided that includes a body and a panel. The body has a first side and a second side orientated opposite the first side. The first and second sides extend between a tip, a base, a leading edge and a trailing edge. The body includes a plurality of cavities disposed in the first side of the body, which cavities extend inwardly toward the second side. The cavities collectively form an opening. At least one rib is disposed between the cavities. A shelf is disposed around the opening. The panel is attached to the shelf first mounting surface and to the rib, and is sized to enclose the opening. The panel is a load bearing structure operable to transfer loads to the body and receive loads from the body.

Abstract translation: 提供了一种用于燃气涡轮发动机的混合翼型件，其包括主体和面板。 主体具有与第一侧相对定向的第一侧和第二侧。 第一和第二面在尖端，底座，前缘和后缘之间延伸。 主体包括设置在主体的第一侧中的多个空腔，空腔向内朝向第二侧延伸。 空腔共同形成开口。 至少一个肋设置在空腔之间。 一个搁板设置在开口周围。 面板连接到搁架第一安装表面和肋上，并且其尺寸被设计成封闭开口。 面板是承载结构，可操作以将负载传递到主体并从身体接收负载。

公开(公告)号：US5015116A

公开(公告)日：1991-05-14

申请号：US485184

申请日：1990-02-26

Applicant: Vincent C. Nardone ,  James R. Strife ,  Karl M. Prewo

Inventor： Vincent C. Nardone ,  James R. Strife ,  Karl M. Prewo

IPC: B64G99/00 ,  F16B2/08 ,  F16B7/04

CPC classification number: B64G9/00 ,  F16B7/0486 ,  F16B2/08 ,  Y10T403/21 ,  Y10T403/345 ,  Y10T403/42 ,  Y10T403/5766

Abstract: A dimensionally stable structural joint particularly suited for use in space systems. The joint comprises a connector having at least two tubular sleeves, at least two tubular members, and at least two annular clamping means for securing the tubular members inside the connector. The connector comprises at least two elements, manufactured from a fiber reinforced composite, which, when mated, form the connector. The tubular members are manufactured from a material having a coefficient of axial expansion of substantially zero. The annular clamping means are manufactured from a material having substantially the same coefficient of radial expansion as the tubular members. The combination of the connector comprises at least two elements and the annular clamping means with substantially the same coefficient of radial expansion as the tubular members allows the joint to accommodate radial expansion and contraction while maintaining axial dimensional stability.

Abstract translation: 特别适用于空间系统的尺寸稳定的结构接头。 接头包括具有至少两个管状套管，至少两个管状构件和用于将管状构件固定在连接器内的至少两个环形夹紧装置的连接器。 连接器包括由纤维增强复合材料制成的至少两个元件，当被配合时形成连接器。 管状构件由具有基本为零的轴向膨胀系数的材料制成。 环形夹紧装置由具有与管状构件基本相同的径向膨胀系数的材料制成。 连接器的组合包括至少两个元件和环形夹持装置，其具有与管状构件基本上相同的径向膨胀系数，从而允许接头适应径向膨胀和收缩，同时保持轴向尺寸稳定性。

公开(公告)号：US08083489B2

公开(公告)日：2011-12-27

申请号：US12425133

申请日：2009-04-16

Applicant: Daniel V. Viens ,  Vincent C. Nardone ,  Peter G. Smith ,  James R. Strife ,  Foster P. Lamm

Inventor： Daniel V. Viens ,  Vincent C. Nardone ,  Peter G. Smith ,  James R. Strife ,  Foster P. Lamm

IPC: F01D5/18

CPC classification number: F01D5/147 ,  F01D5/282 ,  F04D29/023 ,  F04D29/324 ,  F04D29/388 ,  F05D2300/43 ,  F05D2300/437 ,  F05D2300/603 ,  F05D2300/615

Abstract: A hybrid fan blade for a gas turbine engine is provided that includes an airfoil and a composite panel. The airfoil has a first side and a second side orientated opposite the first side. The first and second sides extend between a tip, a base, a leading edge and a trailing edge. The airfoil includes a plurality of cavities disposed in the first side of the airfoil, which cavities extend inwardly toward the second side. The cavities collectively form an opening. At least one rib is disposed between the cavities. A shelf is disposed around the opening. The composite panel is attached to the shelf first mounting surface and to the rib, and is sized to enclose the opening. The first composite panel is a load bearing structure operable to transfer loads to the airfoil and receive loads from the airfoil.

Abstract translation: 提供了一种用于燃气涡轮发动机的混合风扇叶片，其包括翼型件和复合板。 翼型件具有与第一侧相对定向的第一侧和第二侧。 第一和第二面在尖端，底座，前缘和后缘之间延伸。 翼型件包括设置在翼型件的第一侧中的多个空腔，这些空腔朝向第二侧向内延伸。 空腔共同形成开口。 至少一个肋设置在空腔之间。 一个搁板设置在开口周围。 复合板被附接到搁架第一安装表面和肋上，并且其尺寸被设计成包围开口。 第一复合板是承载结构，可操作以将载荷传递到翼型件并从翼型接收载荷。

公开(公告)号：US20100266415A1

公开(公告)日：2010-10-21

申请号：US12425133

申请日：2009-04-16

Applicant: Daniel V. Viens ,  Vincent C. Nardone ,  Peter G. Smith ,  James R. Strife ,  Foster P. Lamm

Inventor： Daniel V. Viens ,  Vincent C. Nardone ,  Peter G. Smith ,  James R. Strife ,  Foster P. Lamm

IPC: F01D5/18

CPC classification number: F01D5/147 ,  F01D5/282 ,  F04D29/023 ,  F04D29/324 ,  F04D29/388 ,  F05D2300/43 ,  F05D2300/437 ,  F05D2300/603 ,  F05D2300/615

Abstract: A hybrid fan blade for a gas turbine engine is provided that includes an airfoil and a composite panel. The airfoil has a first side and a second side orientated opposite the first side. The first and second sides extend between a tip, a base, a leading edge and a trailing edge. The airfoil includes a plurality of cavities disposed in the first side of the airfoil, which cavities extend inwardly toward the second side. The cavities collectively form an opening. At least one rib is disposed between the cavities. A shelf is disposed around the opening. The composite panel is attached to the shelf first mounting surface and to the rib, and is sized to enclose the opening. The first composite panel is a load bearing structure operable to transfer loads to the airfoil and receive loads from the airfoil.

Abstract translation: 提供了一种用于燃气涡轮发动机的混合风扇叶片，其包括翼型件和复合板。 翼型件具有与第一侧相对定向的第一侧和第二侧。 第一和第二面在尖端，底座，前缘和后缘之间延伸。 翼型件包括设置在翼型件的第一侧中的多个空腔，空腔向内朝向第二侧延伸。 空腔共同形成开口。 至少一个肋设置在空腔之间。 一个搁板设置在开口周围。 复合板被附接到搁架第一安装表面和肋上，并且其尺寸被设计成包围开口。 第一复合板是承载结构，可操作以将载荷传递到翼型件并从翼型接收载荷。

公开(公告)号：US20090014059A1

公开(公告)日：2009-01-15

申请号：US11825740

申请日：2007-07-09

Applicant: Rakesh Radhakrishnan ,  Craig R. Walker ,  James R. Strife ,  James R. Irish

Inventor： Rakesh Radhakrishnan ,  Craig R. Walker ,  James R. Strife ,  James R. Irish

IPC: H01L31/058

CPC classification number: H02S10/30 ,  H01L31/02325

Abstract: A thermophotovoltaic electricity generating system having a heat source generating a thermal emission having a plurality of wavelengths. There is an optical filter filtering the thermal emission into a filtered emission. There is also a thermophotovoltaic device receiving the filtered emission. The thermophotovoltaic device is configured to absorb the thermal emission converting the thermal emission into electricity.

Abstract translation: 一种具有产生具有多个波长的热发射的热源的热光发电系统。 有一个滤光器将热发射过滤成滤波后的发射。 还有一个接收过滤发射的热光伏器件。 热光伏器件被配置为吸收将热发射转换成电的热发射。