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公开(公告)号：US06170308B2
公开(公告)日：2001-01-09
申请号：US09357260
申请日：1999-07-20
申请人： William A. Veronesi , Pedro Sainz de Baranda , Vincent C. Nardone , Stephen E. Tolman , Paul H. Wawrzonek
发明人： William A. Veronesi , Pedro Sainz de Baranda , Vincent C. Nardone , Stephen E. Tolman , Paul H. Wawrzonek
IPC分类号： B21D2614
CPC分类号： B24B31/006 , B24B39/006 , Y10S72/707 , Y10T29/479
摘要： The rate of impact between the peening elements and an internal surface of a hollow part is a function of the vibration frequency, and there is a cut-off frequency at which a hollow part can vibrate and induce repeated impact between its internal surface and the peening elements because the rate of impact becomes erratic and loses its cyclical nature as the vibration frequency deviates from the cut-off frequency. The present invention provides a method for determining the cut-off frequency at which a hollow part can vibrate and maintain the repetitive nature of the impact between its internal surface and the peening elements. Such a method requires a peening element speed limit ratio, which is the ratio of the velocity of the hollow part compared to the velocity of the peening element above which the rate of impact begins to become erratic and lose its cyclical nature. The present invention utilizes the peening element speed limit ratio to determine the frequency at which to vibrate the hollow part when peening its internal surface so as to and maintain repeated impact between it and the peening elements.
摘要翻译： 喷丸元件与中空部件的内表面之间的冲击速率是振动频率的函数，并且中空部件可以在其内表面和喷丸之间振动并引起反复冲击的截止频率 因为当振动频率偏离截止频率时，冲击速率变得不稳定并且失去周期性质。 本发明提供了一种用于确定中空部件能够振动并且保持其内表面和喷丸元件之间的冲击的重复性质的截止频率的方法。 这种方法需要喷丸元件速度限制比，其是中空部分的速度与喷丸元件的速度之比，其中冲击速率开始变得不稳定并且失去其周期性质。 本发明利用喷丸元件限速比来确定当其内表面硬化时使中空部分振动的频率，从而在其与喷丸元件之间保持重复的冲击。
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2.发明授权Method and apparatus for peening the internal surface of a non-ferromagnetic hollow part 失效非铁磁中空部件内表面喷丸处理方法及装置
公开(公告)号：US5950470A
公开(公告)日：1999-09-14
申请号：US149972
申请日：1998-09-09
CPC分类号： B24B39/006 , B24B31/006 , B24B31/102 , Y10S72/707
摘要： The present invention is a method and apparatus for peening the internal surface of non-ferromagnetic hollow parts. Ferromagnetic peening elements are inserted into the non-ferromagnetic hollow part, and a magnetic dipole creates a magnetic field through the non-ferromagnetic hollow part attracting the peening elements which contact a portion of the internal surface of the non-ferromagnetic hollow part. The magnetic field is disengaged and a second magnetic dipole creates a second magnetic field, thereby causing the peening elements to contact a second portion of the internal surface. The magnetic dipoles are repeatedly turned on and off, thereby causing repeated impact within the interior of the hollow part until the internal surface attains a predetermined stress level.
摘要翻译： 本发明是一种用于硬化非铁磁中空部件内表面的方法和装置。 铁磁喷丸元件被插入到非铁磁中空部分中，并且磁偶极通过非铁磁中空部分产生磁场，吸引与非铁磁中空部分的内表面的一部分接触的喷丸元件。 磁场被分离并且第二磁偶极子产生第二磁场，从而使喷丸元件接触内表面的第二部分。 磁偶极子反复打开和关闭，从而在中空部分的内部引起重复的冲击，直到内表面达到预定的应力水平。
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公开(公告)号：US20130039774A1
公开(公告)日：2013-02-14
申请号：US13331957
申请日：2011-12-20
CPC分类号： F01D5/147 , F01D5/16 , F01D5/282 , F04D29/023 , F04D29/324 , F04D29/388 , F05D2260/96 , F05D2300/603 , F05D2300/612 , F05D2300/615 , Y02T50/672 , Y02T50/673
摘要： 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.
摘要翻译： 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。
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公开(公告)号：US5590569A
公开(公告)日：1997-01-07
申请号：US487879
申请日：1995-06-07
IPC分类号： F16F15/30 , F16F15/305
CPC分类号： F16F15/305 , F16C15/00 , Y02E60/16 , Y10T156/10 , Y10T74/19916 , Y10T74/2117 , Y10T74/212
摘要： The energy storage flywheel device (6) includes a plurality of annular shaped composite sections (8) and an annular shaped insert (10). The insert (10) has a specific radial strength substantially greater than the composite sections' specific radial strength. The composite sections (8) and the insert (10) are alternately stacked such that they have a common axis of rotation. They are bonded to each other such that shear stress is transferred between the composite sections (8) and insert (10). In some applications, the flywheel (6) may comprise at least one annular shaped metal matrix composite section (8).
摘要翻译： 能量存储飞轮装置（6）包括多个环形复合部分（8）和环形插入件（10）。 刀片（10）的特定径向强度基本上大于复合截面的特定径向强度。 复合部分（8）和插入件（10）交替堆叠使得它们具有共同的旋转轴线。 它们彼此结合，使得剪切应力在复合部分（8）和插入件（10）之间传递。 在一些应用中，飞轮（6）可以包括至少一个环形金属基复合部分（8）。
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公开(公告)号：US5015116A
公开(公告)日：1991-05-14
申请号：US485184
申请日：1990-02-26
CPC分类号： B64G9/00 , F16B7/0486 , F16B2/08 , Y10T403/21 , Y10T403/345 , Y10T403/42 , Y10T403/5766
摘要： 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.
摘要翻译： 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。
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公开(公告)号：US20110204162A1
公开(公告)日：2011-08-25
申请号：US13094881
申请日：2011-04-27
申请人： Fabio R. Bertolotti , David S. Liscinsky , Vincent C. Nardone , Michael K. Sahm , Bernd R. Noack , Daniel R. Sabatino
发明人： Fabio R. Bertolotti , David S. Liscinsky , Vincent C. Nardone , Michael K. Sahm , Bernd R. Noack , Daniel R. Sabatino
IPC分类号： B05B1/34
CPC分类号： F02K1/28 , F01D5/145 , F02C6/08 , F02K1/38 , F02K1/46 , F23D14/583 , Y02T50/673 , Y10T137/0329
摘要： In an air mixing arrangement wherein a primary fluid is introduced through an opening in a wall to be mixed with a secondary fluid flowing along the wall surface, the opening is airfoil shaped with its leading edge being orientated at an attack angle with respect to the secondary fluid flow stream so as to thereby enhance the penetration and dispersion of the primary fluid stream into the secondary fluid stream. The airfoil shaped opening is selectively positioned such that its angle of attack provides the desired lift to optimize the mixing of the two streams for the particular application. In one embodiment, a collar is provided around the opening to prevent the secondary fluid from contacting the surface of the wall during certain conditions of operation. Multiple openings maybe used such as the combination of a larger airfoil shaped opening with a smaller airfoil shaped opened positioned downstream thereof, or a round shaped opening placed upstream of an airfoil shaped opening. Pairs of openings and associated collars maybe placed in symmetric relationship so as to promote mixing in particular applications, and nozzles maybe placed on the inner side of wall to enhance the flow characteristics of the primary fluid.
摘要翻译： 在空气混合装置中，其中主要流体通过壁中的开口引入以与沿着壁表面流动的次级流体混合，所述开口是翼型，其前缘相对于次级 流体流动，从而增强初级流体流进入次级流体流的渗透和分散。 翼型开口被选择性地定位成使得其迎角提供所需的升力以优化用于特定应用的两个流的混合。 在一个实施例中，围绕开口设置套环，以防止在某些操作条件下次要流体接触壁的表面。 可以使用多个开口，例如较大的翼型形状的开口与位于其下游的较小的翼型形状的组合，或者设置在翼型形状的开口的上游的圆形开口。 一对开口和相关的套环可以放置在对称关系中，以促进特定应用中的混合，并且喷嘴可以放置在壁的内侧以增强初级流体的流动特性。
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公开(公告)号：US5873699A
公开(公告)日：1999-02-23
申请号：US670302
申请日：1996-06-27
CPC分类号： F01D5/147 , F01D5/282 , F05D2230/24 , F05D2300/173 , F05D2300/603 , Y10T29/49337 , Y10T29/49339
摘要： An airfoil is provided having a cross-sectional geometry which includes a first wall, a second wall disposed opposite the first wall, a leading edge, a trailing edge disposed opposite the leading edge, and a first cavity. The first cavity is disposed between the first and second walls, and the leading and trailing edges. The cross-sectional geometry extends between a first and a second end, and the airfoil is formed from discontinuously reinforced aluminum.
摘要翻译： 提供一种翼型件，其横截面几何形状包括第一壁，与第一壁相对设置的第二壁，前缘，与前缘相对设置的后缘和第一腔。 第一腔设置在第一和第二壁之间以及前缘和后缘之间。 横截面几何形状在第一和第二端之间延伸，翼型由不连续增强的铝形成。
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公开(公告)号：US5478219A
公开(公告)日：1995-12-26
申请号：US200088
申请日：1994-02-22
CPC分类号： F01C1/0246 , F05C2201/021 , F05C2203/08 , F05C2253/04 , Y10T29/4924
摘要： An orbiting scroll is made with a ceramic particle reinforced aluminum metal matrix composite. The resultant part has increased wear resistance, closer thermal expansion matching with cast iron, can be used without tip seals and offers the advantages associated with a reduced mass. In manufacturing the part, the part is pressure cast to a near net shape and machined to the final shape.
摘要翻译： 轨道运行的涡卷由陶瓷颗粒增强铝金属基复合材料制成。 所得到的部件具有增加的耐磨性，与铸铁更加热膨胀匹配，可以使用无尖端密封，并提供与减小质量相关的优点。 在制造零件时，该零件被压铸成近净形并加工成最终形状。
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公开(公告)号：US5452625A
公开(公告)日：1995-09-26
申请号：US128319
申请日：1993-09-29
IPC分类号： F16F15/30 , F16F15/305
CPC分类号： F16F15/305 , F16C15/00 , Y02E60/16 , Y10T156/10 , Y10T74/19916 , Y10T74/2117 , Y10T74/212
摘要： The energy storage flywheel device (6) includes a plurality of annular shaped composite sections (8) and an annular shaped insert (10). The insert (10) has a specific radial strength substantially greater than the composite sections' specific radial strength. The composite sections (8) and the insert (10) are alternately stacked such that they have a common axis of rotation. They are bonded to each other such that shear stress is transferred between the composite sections (8) and insert (10). In some applications, the flywheel (6) may comprise at least one annular shaped metal matrix composite section (8).
摘要翻译： 能量存储飞轮装置（6）包括多个环形复合部分（8）和环形插入件（10）。 刀片（10）的特定径向强度基本上大于复合截面的特定径向强度。 复合部分（8）和插入件（10）交替堆叠使得它们具有共同的旋转轴线。 它们彼此结合，使得剪切应力在复合部分（8）和插入件（10）之间传递。 在一些应用中，飞轮（6）可以包括至少一个环形金属基体复合部分（8）。
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公开(公告)号：US08585368B2
公开(公告)日：2013-11-19
申请号：US13331957
申请日：2011-12-20
IPC分类号： B23K5/18
CPC分类号： F01D5/147 , F01D5/16 , F01D5/282 , F04D29/023 , F04D29/324 , F04D29/388 , F05D2260/96 , F05D2300/603 , F05D2300/612 , F05D2300/615 , Y02T50/672 , Y02T50/673
摘要： 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.
摘要翻译： 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。
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