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1.发明授权公开(公告)号：US07946806B2
公开(公告)日：2011-05-24
申请号：US11870061
申请日：2007-10-10
IPC分类号： F01D25/08
CPC分类号： F02K3/115 , F02C7/14 , F02C7/224 , Y02T50/675
摘要： Gas turbine engine systems and related methods involving heat exchange are provided. In this regard, a representative heat exchange system for a gas turbine engine includes: a heat exchanger; and a flow restrictor operative to selectively restrict a flow of gas flowing along an annular gas flow path; in an open position, the flow restrictor enabling gas to flow along the gas flow path and, in a closed position, the flow restrictor restricting the flow of gas such that at least a portion of the gas is provided to the heat exchanger, the heat exchanger being located radially outboard of the flow restrictor.
摘要翻译： 提供燃气涡轮发动机系统和涉及热交换的相关方法。 在这方面，用于燃气涡轮发动机的代表性的热交换系统包括：热交换器; 以及限流器，其可操作以选择性地限制沿着环形气体流动路径流动的气体流; 在打开位置，流量限制器使得气体能够沿着气体流动路径流动，并且在关闭位置，限流器限制气体的流动，使得至少一部分气体被提供给热交换器，热量 交换器位于流量限制器的径向外侧。
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2.发明申请公开(公告)号：US20090255269A1
公开(公告)日：2009-10-15
申请号：US12100470
申请日：2008-04-10
申请人： Dale William Petty , Shawn M. McMahon , Michael Joseph Murphy , Sean P. Zamora , Timothy A. Swanson
发明人： Dale William Petty , Shawn M. McMahon , Michael Joseph Murphy , Sean P. Zamora , Timothy A. Swanson
IPC分类号： F02K1/06
摘要： Gas turbine engine systems involving variable nozzles with sliding doors are provided. In this regard, a representative door assembly for a gas turbine engine includes: a door configured for alignment with an exit area of a nozzle and operative to variably open and close the nozzle exit area such that gas directed along a gas path defined, at least in part, by the nozzle exit area is regulated
摘要翻译： 提供了包括具有滑动门的可变喷嘴的燃气涡轮发动机系统。 在这方面，用于燃气涡轮发动机的代表性门组件包括：门，其被配置为与喷嘴的出口区域对准并且可操作地可变地打开和关闭喷嘴出口区域，使得沿着气体路径定向的气体至少 部分由喷嘴出口区域进行调节
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公开(公告)号：US20140037437A1
公开(公告)日：2014-02-06
申请号：US13562366
申请日：2012-07-31
CPC分类号： F02K3/075 , F05D2230/80 , Y10T29/49245
摘要： A gas turbine engine includes a fan nacelle and a core nacelle spaced radially inwardly of the fan nacelle to define a bypass flowpath. The engine includes a scoop to direct air from the bypass flowpath into an engine core. The scoop is comprised of a first piece extending outwardly of an outer surface the core nacelle to define an air inlet and a second piece extending inwardly of the core nacelle to define an air outlet.
摘要翻译： 燃气涡轮发动机包括风扇机舱和与风扇机舱径向向内隔开的芯机舱，以限定旁路流路。 发动机包括将空气从旁路流路引导到发动机芯中的勺子。 铲斗包括从外表面向外延伸的核心机舱以限定空气入口的第一件和从该核心机舱向内延伸以限定空气出口的第二件。
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公开(公告)号：US20090169359A1
公开(公告)日：2009-07-02
申请号：US11964058
申请日：2007-12-26
IPC分类号： F01D1/02
CPC分类号： F02C7/18 , F01D25/12 , F01D25/145 , F02K1/46 , F02K1/822 , F04D29/5826 , F05D2220/34 , F05D2220/50 , F05D2260/208 , Y02T50/672 , Y02T50/675
摘要： A turbine engine cooling arrangement includes a core passage for receiving a core flow for combustion, a first airflow source including a first passage adjacent the core passage for conveying a first airflow, and a second airflow source including a second passage adjacent the first passage for conveying a second airflow. A heat exchanger is thermally connected with the first passage and the second passage for transferring heat between the first airflow and the second airflow.
摘要翻译： 涡轮发动机冷却装置包括用于接收用于燃烧的芯流的芯通道，包括邻近核心通道的第一通道用于输送第一气流的第一气流源，以及包括与第一通道相邻的第二通道的第二气流源，用于输送 第二个气流。 热交换器与第一通道和第二通道热连接，用于在第一气流和第二气流之间传递热量。
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公开(公告)号：US09194330B2
公开(公告)日：2015-11-24
申请号：US13562366
申请日：2012-07-31
IPC分类号： F02K3/075
CPC分类号： F02K3/075 , F05D2230/80 , Y10T29/49245
摘要： A gas turbine engine includes a fan nacelle and a core nacelle spaced radially inwardly of the fan nacelle to define a bypass flowpath. The engine includes a scoop to direct air from the bypass flowpath into an engine core. The scoop is comprised of a first piece extending outwardly of an outer surface the core nacelle to define an air inlet and a second piece extending inwardly of the core nacelle to define an air outlet.
摘要翻译： 燃气涡轮发动机包括风扇机舱和与风扇机舱径向向内隔开的芯机舱，以限定旁路流路。 发动机包括将空气从旁路流路引导到发动机芯中的勺子。 铲斗包括从外表面向外延伸的核心机舱以限定空气入口的第一件和从该核心机舱向内延伸以限定空气出口的第二件。
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公开(公告)号：US20110243719A1
公开(公告)日：2011-10-06
申请号：US12851251
申请日：2010-08-05
IPC分类号： F01D25/24
摘要： A nacelle for a turbofan propulsion system that extends along a centerline includes a forward cowling and an aft cowling. To improve the fit of a turbofan propulsion system in the space between the wing and ground of a fixed-wing aircraft, the aft cowling of the nacelle is modified. The aft cowling has a non-circular cross-sectional geometry disposed in a plane substantially perpendicular to the centerline. The non-circular cross-sectional geometry includes a radially recessed section disposed between first and second curved sections. The first and the second curved sections each have a radius that is greater than a radial distance between the centerline and a center point of the radially recessed section.
摘要翻译： 一个沿着中心线延伸的涡轮风扇推进系统的机舱包括一个正向整流罩和一个后罩。 为了提高涡轮风扇推进系统在固定翼飞机机翼与地面之间的空间配合，改装了机舱的后罩。 后罩具有设置在基本上垂直于中心线的平面中的非圆形横截面几何形状。 非圆形横截面几何形状包括设置在第一和第二弯曲部分之间的径向凹陷部分。 第一和第二弯曲部分各自具有大于中心线和径向凹陷部分的中心点之间的径向距离的半径。
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公开(公告)号：US07866158B2
公开(公告)日：2011-01-11
申请号：US11950956
申请日：2007-12-05
IPC分类号： F02K1/00
CPC分类号： F02K1/82 , Y10T29/49323
摘要： A turbine engine exhaust nozzle is disclosed that includes an exhaust liner having a first attachment structure. A liner support member includes a second attachment structure. A pin cooperates with the first and second attachment structures and is configured to secure the exhaust liner relative to the liner support member. The pin includes first and second dimensions that are different than one another. The pin is inserted into apertures provided by the attachment structures, in one example. The pin is oriented to position the first and second dimensions in a manner providing increased clearance within the apertures. The pin is rotated to load the components and firmly secure the liner to the liner support member.
摘要翻译： 公开了一种涡轮发动机排气喷嘴，其包括具有第一附接结构的排气衬套。 衬套支撑构件包括第二附接结构。 销与第一和第二附接结构配合并且构造成相对于衬套支撑构件固定排气衬套。 销包括彼此不同的第一和第二尺寸。 在一个示例中，销被插入由附接结构提供的孔中。 销被定向成以在孔内提供增加的间隙的方式定位第一和第二尺寸。 旋转销以加载部件并将衬套牢固地固定到衬垫支撑构件上。
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公开(公告)号：US20090178383A1
公开(公告)日：2009-07-16
申请号：US12015033
申请日：2008-01-16
IPC分类号： F02C7/08
CPC分类号： F02K1/822 , Y02T50/675
摘要： A gas turbine engine includes an exhaust liner having cold and hot sheets radially spaced from one another and interconnected by a band arranged in a cavity between the hot and cold sheets. In one example, the band is Z-shaped to permit thermal growth of the hot sheets relative to the cold sheets in the axial and radial directions. The hot sheets include axially adjacent portions that provide slots that are in fluid communication with the space. Cooling fluid is provided to the cavity through impingement jets in the cold sheet. The slots are arranged radially between the hot sheet portions.
摘要翻译： 燃气涡轮发动机包括具有彼此径向间隔开的冷热片的排气衬套，并且通过布置在热片和冷片之间的空腔中的带相互连接。 在一个示例中，带是Z形的，以允许热片相对于冷片在轴向和径向上的热生长。 热片包括提供与空间流体连通的槽的轴向相邻部分。 通过冷板中的冲击射流将冷却流体提供到空腔。 狭槽在热片部分之间径向布置。
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公开(公告)号：US20090145133A1
公开(公告)日：2009-06-11
申请号：US11950956
申请日：2007-12-05
CPC分类号： F02K1/82 , Y10T29/49323
摘要： A turbine engine exhaust nozzle is disclosed that includes an exhaust liner having a first attachment structure. A liner support member includes a second attachment structure. A pin cooperates with the first and second attachment structures and is configured to secure the exhaust liner relative to the liner support member. The pin includes first and second dimensions that are different than one another. The pin is inserted into apertures provided by the attachment structures, in one example. The pin is oriented to position the first and second dimensions in a manner providing increased clearance within the apertures. The pin is rotated to load the components and firmly secure the liner to the liner support member.
摘要翻译： 公开了一种涡轮发动机排气喷嘴，其包括具有第一附接结构的排气衬套。 衬套支撑构件包括第二附接结构。 销与第一和第二附接结构配合并且构造成相对于衬套支撑构件固定排气衬套。 销包括彼此不同的第一和第二尺寸。 在一个示例中，销被插入由附接结构提供的孔中。 销被定向成以在孔内提供增加的间隙的方式定位第一和第二尺寸。 旋转销以加载部件并将衬套牢固地固定到衬垫支撑构件上。
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公开(公告)号：US06171324B2
公开(公告)日：2001-01-09
申请号：US09163961
申请日：1998-09-30
IPC分类号： A61F900
CPC分类号： A61F9/0136
摘要： A corneal marker and a method of using a corneal marker are disclosed. The corneal marker includes a handle having a head coupled thereto. The inferior surface of the head includes a set of protuberances which form marking surfaces adapted to simultaneously engage corneal tissue. The marking surfaces form opposing sets of marks which allow a surgeon to form an incision of precise length and width. An alignment line on the superior and/or front surface of the marker facilitates the positioning thereof. A method of performing clear corneal surgery following the application of markings to the cornea is also provided.
摘要翻译： 公开了角膜标记物和使用角膜标记物的方法。 角膜标记器包括具有联接到其上的头部的手柄。 头部的下表面包括一组突起，其形成适于同时接合角膜组织的标记表面。 标记表面形成相对的标记组，允许外科医生形成精确的长度和宽度的切口。 在标记的上表面和/或前表面上的对准线有利于其定位。 还提供了在将标记应用于角膜之后执行透明角膜手术的方法。
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