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1.发明申请DEVICE WITH SECONDARY JETS REDUCING THE NOISE GENERATED BY AN AIRCRAFT JET ENGINE 有权具有次级喷气机的设备减少飞机喷气发动机产生的噪音公开(公告)号：US20110030341A1
公开(公告)日：2011-02-10
申请号：US12935445
申请日：2009-03-31
IPC分类号： F02K1/34
CPC分类号： F02K1/34 , F02K1/46 , F05D2240/40 , F05D2250/11
摘要： An aircraft jet engine including a wall centered about a longitudinal axis and surrounding a stream of gas ejected at a downstream end of the wall in the direction of the axis, primary ducts distributed at the periphery of the downstream end of the wall configured on command each to eject a jet of primary fluid to interact with the ejected stream of gas, the primary ducts of each pair converging towards one another near the downstream end of the wall so that the primary jets ejected form two sides of a triangle that meet at the vertex thereof in a view projected onto a plane perpendicular to a transverse plane, and secondary ducts each associated with each pair of primary ducts and configured on command to eject a jet of secondary fluid directed into the triangle formed by the primary jets.
摘要翻译： 一种飞机喷气式发动机，其包括围绕纵向轴线居中并围绕沿着轴线方向在壁的下游端喷射的气体流的壁，分配在壁的下游端的周边的主要管道，其分配在每个 喷射主流体的喷射流与喷射的气流相互作用，每对的主要管道在壁的下游端彼此会聚，使得主喷嘴从三角形的两侧喷射，该三角形在顶点处相遇 它们在投影到垂直于横向平面的平面上的视图中，以及每个与每对主要管道相关联的辅助管道，并且根据命令配置以喷射引导到由主喷嘴形成的三角形形成的三角形的二次流体的射流。
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公开(公告)号：US07117619B1
公开(公告)日：2006-10-10
申请号：US10717527
申请日：2003-11-21
申请人： John Jerome Huber
发明人： John Jerome Huber
IPC分类号： G09F11/04
CPC分类号： G09F11/04 , A63B71/0672 , Y10S273/26
摘要： A two-sided, multi-sport scoring banner 30 consisting of a plurality of flexible scoring elements 44A, 44B, 44C, 44D sandwiched between a front face 32 and a back face 34. A set of scoring symbols 44A, 44B, 44C, 44D selectively positioned and uniformly spaced upon the scoring element to allow the score of a competitive event to be displayed through a plurality of windows 48, 50, 52, 54 formed into the front and back faces of the scoring banner. A plurality of utility storage pockets 90, a plurality of equipment storage loops 110 and a plurality of hooks 120 attached to the scoring banner to facilitate the organization of a variety of sport equipment items. A team insignia 74, a home and visitor title 76, 78 and a plurality of advertisement signs 130 printed on or attached to the scoring banner's two faces. In one embodiment a plurality of linear pockets 60, 62, 64, 66 are included within the scoring banner to facilitate the use and storage of a plurality of ground stakes or rods 58. The scoring banner, in all of its embodiments, having the means to be attached to a variety of structures, display a team's insignia, easily maintain the score of the sporting event as well as be rolled up and secured into a compact cylindrical configuration for storage and transport.
摘要翻译： 由多个柔性刻痕元件44A，44B，44C，44D夹在前面32和背面34之间的双面多体育评分横幅30。 一组记分符号44A，44B，44C，44D选择性地定位并均匀地间隔在刻痕元件上，以允许竞争事件的得分通过多个窗口48,50,52,54形成为 得分横幅的前脸和背面。 多个公用设施储存袋90，多个设备储存环110和连接到得分横幅上的多个钩子120，以便于组织各种运动器材物品。 一个团队徽章74，一个家庭和访问者名称76,78，以及印刷在评分横幅的两个面上或附着在评分横幅的两个面上的多个广告标志130。 在一个实施例中，多个线性袋60,62,64,66包括在刻痕横幅内，以便于多个地面桩或杆58的使用和储存。 在其所有实施例中，得分横幅具有附接到各种结构的装置，显示团队的徽章，容易地保持体育赛事的得分，并且被卷起并固定成紧凑的圆柱形配置以用于存储 和运输。
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3.发明授权Aircraft jet engine comprising a system for reducing the noise generated by the ejection of the gases 有权飞机喷气发动机包括用于降低由气体喷射产生的噪音的系统公开(公告)号：US09151244B2
公开(公告)日：2015-10-06
申请号：US13357065
申请日：2012-01-24
申请人： Jerome Huber , Jean Paul Bonnet , Luis Gomes , Remy Maury
发明人： Jerome Huber , Jean Paul Bonnet , Luis Gomes , Remy Maury
CPC分类号： F02K1/34 , B64D33/06 , F02K1/46 , F04B43/025
摘要： An aircraft jet engine comprising a nozzle to eject a gas stream, and a system for reducing the noise generated by the ejection of the gas stream. This system comprises several ducts which each are connected upstream to a recess divided into several chambers and open, downstream, at the outlet of nozzle. In this way, each duct ejects a fluid jet deriving from the recess and which interacts with the gas stream of the engine. The system also comprises a pulsation means for the fluid jet which brings about its ejection at the nozzle outlet and/or modulates its speed by varying the volume contained in the recess.
摘要翻译： 一种包括用于喷射气流的喷嘴的飞机喷气发动机，以及用于降低由气流喷射产生的噪音的系统。 该系统包括几个管道，每个管道上游连接到分为几个室的凹部并且在喷嘴的出口处开放，下游。 以这种方式，每个管道喷射从凹部导出并与发动机的气流相互作用的流体射流。 该系统还包括用于流体射流的脉动装置，其使其在喷嘴出口处的喷射和/或通过改变容纳在凹部中的体积来调制其速度。
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公开(公告)号：US08770921B2
公开(公告)日：2014-07-08
申请号：US12935450
申请日：2009-03-31
IPC分类号： F01D9/02
CPC分类号： F02K1/34 , F02K1/46 , F05D2240/40
摘要： An aircraft jet engine with a longitudinal axis, including a wall enclosing a gas flow ejected from a downstream end of the wall in the longitudinal axis, plural ducts being distributed around the periphery of the downstream end of the wall each including a terminal section, including an outlet opening. Each duct can eject a fluid jet through the outlet opening thereof. The ducts are configured to eject the fluid jets essentially parallel to each other, each fluid jet ejected through the corresponding outlet opening forming a lateral angle with the longitudinal axis in a projection view in a plane with the longitudinal axis.
摘要翻译： 一种具有纵向轴线的飞机喷气发动机，包括围绕在纵向轴线上的壁的下游端喷出的气流的壁，多个管道围绕壁的下游端的周边分布，每个管道包括终端部分，包括 出口开口。 每个管道可以通过其出口开口喷射流体射流。 导管构造成喷射基本上彼此平行的流体射流，通过对应的出口开口喷射的每个流体射流在与纵向轴线的平面中的投影视图中与纵向轴线形成横向角度。
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5.发明申请AIRCRAFT JET ENGINE COMPRISING A SYSTEM FOR REDUCING THE NOISE GENERATED BY THE EJECTION OF THE GASES 有权飞机喷气式发动机，包括减少由气体喷射产生的噪音的系统公开(公告)号：US20120186224A1
公开(公告)日：2012-07-26
申请号：US13357065
申请日：2012-01-24
申请人： Jerome Huber , Jean Paul Bonnet , Luis Gomes , Remy Maury
发明人： Jerome Huber , Jean Paul Bonnet , Luis Gomes , Remy Maury
IPC分类号： F02K1/06
CPC分类号： F02K1/34 , B64D33/06 , F02K1/46 , F04B43/025
摘要： The invention relates to an aircraft jet engine comprising a nozzle (2) intended to eject a gas stream, and a system for reducing the noise (3) generated by the ejection of the gas stream.This system comprises several ducts (11a) which each, on the one hand, are connected upstream to a recess divided into several chambers and, on the other hand, open, downstream, at the outlet of nozzle (2). In this way, each duct ejects a fluid jet deriving from the recess and which interacts with the gas stream of the engine.The system also comprises a pulsation means (12) for the fluid jet which brings about its ejection at the nozzle outlet and/or modulates its speed by varying the volume contained in the recess.The system is configured in particular for balancing static pressures between the chambers.
摘要翻译： 本发明涉及一种包括用于喷射气流的喷嘴（2）的飞机喷气式发动机，以及用于减少由气流喷射产生的噪声（3）的系统。 该系统包括几个管道（11a），其一方面一方面连接到分成几个室的凹部的上游，另一方面在喷嘴（2）的出口处是开放的，下游的。 以这种方式，每个管道喷射从凹部导出并与发动机的气流相互作用的流体射流。 该系统还包括用于流体射流的脉动装置（12），其使其在喷嘴出口处的喷射和/或通过改变包含在凹部中的体积来调节其速度。 该系统特别用于平衡室之间的静压力。
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6.发明申请DEVICE WITH PLANE JETS FOR REDUCING THE NOISE GENERATED BY A JET AIRCRAFT 有权具有飞机喷气式飞机的装置，用于减少喷气式飞机产生的噪音公开(公告)号：US20100065680A1
公开(公告)日：2010-03-18
申请号：US12415353
申请日：2009-03-31
CPC分类号： F02K1/34 , F02K1/46 , F05D2240/40
摘要： The invention relates to an aircraft engine having a longitudinal axis (XX′), comprising a wall (30) surrounding a gas stream that is ejected at a downstream end (30a) of the wall along the longitudinal axis, characterized in that a plurality of conduits (60, 62, 64, 66, 68, 70, 72, 74) distributed at the periphery of the downstream end of the wall are each capable of ejecting, via an outlet orifice (60c), a fluid jet (76) in the form of a sheet, in such a way that the jets thus ejected each form a fluid perturbation around the ejected gas stream.
摘要翻译： 本发明涉及一种具有纵向轴线（XX'）的飞行器发动机，其包括围绕沿着纵向轴线在壁的下游端（30a）处喷射的气流的壁（30），其特征在于，多个 分布在壁的下游端的周边处的导管（60,62,64,66,68,70,72,74）各自能够经由出口孔（60c）喷射流体射流（76） 片状的形式，使得这样喷射的射流在喷出的气流周围形成流体扰动。
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公开(公告)号：US5865979A
公开(公告)日：1999-02-02
申请号：US760058
申请日：1996-12-04
申请人： Albert Lee Collins, Jr. , Rick Alan Boyd , Herbert Lester Bradshaw II , Alvin Jerome Huber , Charles Thomas Wessner , Dennis Bowman Ruch
发明人： Albert Lee Collins, Jr. , Rick Alan Boyd , Herbert Lester Bradshaw II , Alvin Jerome Huber , Charles Thomas Wessner , Dennis Bowman Ruch
摘要： The entire outer surface of a ground rod, including its pointed end portion, has a continuous and uniform electroplated coating. The rod has a blunt end portion shaped to minimize mushrooming when it is hammered for driving the rod into the ground. Jets of plating solution directed against the rod produce swirling motion of plating solution around the rod while it moves longitudinally through a plating bath. Uniformity of the plated coating may be enhanced by rotating the rod during longitudinal movement through the plating bath.
摘要翻译： 接地棒的整个外表面，包括其尖端部分，具有连续和均匀的电镀涂层。 杆具有钝端部，其成形为当锤击以将杆推入地面时最小化。 针对杆的电镀液喷射器在电镀液纵向移动通过电镀槽的同时产生电镀溶液围绕棒的旋转运动。 通过在纵向运动通过电镀槽期间旋转杆可以增强镀覆层的均匀性。
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8.发明授权Device with secondary jets reducing the noise generated by an aircraft jet engine 有权具有次级喷气机的装置降低飞机喷气发动机产生的噪音公开(公告)号：US08393139B2
公开(公告)日：2013-03-12
申请号：US12935445
申请日：2009-03-31
IPC分类号： F02K3/04
CPC分类号： F02K1/34 , F02K1/46 , F05D2240/40 , F05D2250/11
摘要： An aircraft jet engine including a wall centered about a longitudinal axis and surrounding a stream of gas ejected at a downstream end of the wall in the direction of the axis, primary ducts distributed at the periphery of the downstream end of the wall configured on command each to eject a jet of primary fluid to interact with the ejected stream of gas, the primary ducts of each pair converging towards one another near the downstream end of the wall so that the primary jets ejected form two sides of a triangle that meet at the vertex thereof in a view projected onto a plane perpendicular to a transverse plane, and secondary ducts each associated with each pair of primary ducts and configured on command to eject a jet of secondary fluid directed into the triangle formed by the primary jets.
摘要翻译： 一种飞机喷气式发动机，其包括围绕纵向轴线居中并围绕沿着轴线方向在壁的下游端喷射的气体流的壁，分配在壁的下游端的周边的主要管道，其分配在每个 喷射主流体的喷射流与喷射的气流相互作用，每对的主要管道在壁的下游端彼此会聚，使得主喷嘴从三角形的两侧喷射，该三角形在顶点处相遇 它们在投影到垂直于横向平面的平面上的视图中，以及每个与每对主要管道相关联的辅助管道，并且根据命令配置以喷射引导到由主喷嘴形成的三角形形成的三角形的二次流体的射流。
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9.发明申请DEVICE FOR REDUCING NOISE GENERATED BY AN AIRCRAFT JET ENGINE WITH CURVE DUCTS 有权用于降低飞机喷气发动机产生的噪音的装置公开(公告)号：US20110042162A1
公开(公告)日：2011-02-24
申请号：US12935423
申请日：2009-03-31
IPC分类号： F01N1/14
CPC分类号： F02K1/46 , F02K1/34 , F05D2240/40
摘要： A jet engine, including a wall surrounding a first gas flow ejected from a downstream end of the wall along a longitudinal axis, a second flow of gas running outside the wall in a direction of ejection of the first gas flow, at least one duct arranged on the periphery of the downstream end of the wall which is desired to eject a gas flow for interacting with one and/or the other gas flow, the at least one duct including a terminal section provided at the free end thereof with an outlet opening through which the fluid is ejected. The terminal section successively includes a first section of straight duct aligned along a median axis and a second duct section forming a bend relative to the straight section, the second portion having a free end provided with the outlet opening and sufficiently close to the median axis of the first section to give the terminal section a reduced restriction in a direction of formation of the bend.
摘要翻译： 一种喷气发动机，包括围绕沿着纵向轴线从壁的下游端喷出的第一气流的壁，在第一气流的喷射方向上在壁外延伸的第二气体流，至少一个管道，其布置 在壁的下游端的周边上，其期望喷射与一个和/或另一个气流相互作用的气流，所述至少一个管道包括在其自由端设置有出口开口的端子部分 流体被喷射。 端子部分依次包括沿着中间轴对准的直管道的第一部分和相对于直线部分形成弯曲部的第二管道部分，第二部分具有设置有出口开口的自由端，并且足够接近中心轴 使端子部分在形成弯曲方向上的限制减小的第一部分。
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公开(公告)号：US20110027070A1
公开(公告)日：2011-02-03
申请号：US12935450
申请日：2009-03-31
IPC分类号： F04D29/66
CPC分类号： F02K1/34 , F02K1/46 , F05D2240/40
摘要： An aircraft jet engine with a longitudinal axis, including a wall enclosing a gas flow ejected from a downstream end of the wall in the longitudinal axis, plural ducts being distributed around the periphery of the downstream end of the wall each including a terminal section, including an outlet opening. Each duct can eject a fluid jet through the outlet opening thereof. The ducts are configured to eject the fluid jets essentially parallel to each other, each fluid jet ejected through the corresponding outlet opening forming a lateral angle with the longitudinal axis in a projection view in a plane with the longitudinal axis.
摘要翻译： 一种具有纵向轴线的飞机喷气发动机，包括围绕在纵向轴线上的壁的下游端喷出的气流的壁，多个管道围绕壁的下游端的周边分布，每个管道包括终端部分，包括 出口开口。 每个管道可以通过其出口开口喷射流体射流。 导管构造成喷射基本上彼此平行的流体射流，通过对应的出口开口喷射的每个流体射流在与纵向轴线的平面中的投影视图中与纵向轴线形成横向角度。
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