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51. 发明授权

US6122917A High efficiency heat transfer structure 失效
标题翻译：高效传热结构
公开(公告)号：US6122917A
公开(公告)日：2000-09-26
申请号：US103605
申请日：1998-06-24
申请人： Peter Senior
发明人： Peter Senior
IPC分类号： F23R3/00 , F23R3/08 , F23R3/44 , F28F13/02 , F02C7/12
CPC分类号： F23R3/08 , F23R3/002 , F23R3/44 , F28F13/02 , F23R2900/03044 , F28D2021/0078 , Y10S165/908 , Y10S415/914
摘要： A heat transfer structure for the efficient cooling of a heated surface such as the combustor wall of a gas turbine has a high heat transfer coefficient and can therefore operate at a relatively low pressure loss. A cooling jacket is formed around the heated surface by means of an apertured wall parallel to and spaced from the heated surface. Cooling fluid such as air flows into the cooling jacket through the apertures and impinges as air jets on the heated surface. The heat transfer coefficient is greatly increased by flow diversion features associated with the apertures which act as Coanda surfaces to divert the air jets so that they impinge obliquely and turbulently on the heated surface and establish subsequent turbulent sinuous cross-flows of the cooling air on the heated surface.
摘要翻译：用于有效地冷却诸如燃气轮机的燃烧器壁的加热表面的传热结构具有高的传热系数，并且因此可以在相对低的压力损失下操作。通过平行于加热表面并与加热表面间隔开的有孔壁，在加热表面周围形成冷却套。诸如空气的冷却流体通过孔流入冷却套，并作为空气射流冲击在被加热的表面上。传导系数大大地增加了与作为柯恩达表面的孔相关联的流动分流特征，以转移空气射流，使得它们倾斜和湍动地撞击在被加热的表面上，并建立冷却空气的随后的湍流弯曲交叉流动加热面。

52. 发明授权

US5501011A Method of manufacture of an enclosure containing hot gases cooled by transportation, in particular the thrust chamber of a rocket engine 失效
标题翻译：制造包含由运输冷却的热气体的外壳的方法，特别是火箭发动机的推力室
公开(公告)号：US5501011A
公开(公告)日：1996-03-26
申请号：US279973
申请日：1994-07-25
申请人： Marc Pellet
发明人： Marc Pellet
IPC分类号： F02K9/64 , B23P15/00
CPC分类号： F02K9/64 , F05D2260/203 , F28D2021/0078 , Y10T29/49346
摘要： A method of manufacturing an enclosure containing hot gases cooled by transpiration comprises:forming a shaped rigid shell comprised of a microperforated sheet metal, hydraulic calibration sheath,welding spacers to an outside face of the hydraulic calibration sheath;welding an outer sealing envelope on an outside surface of the spacers and the partitions; andforming a porous wall by applying a deposit onto an inside face of the hydraulic calibration sheath.
摘要翻译：一种制造包含通过蒸腾冷却的热气体的外壳的方法包括：形成由微穿孔金属板，液压校准护套，焊接间隔件到液压校准护套的外表面的成形刚性壳; 在隔离物和隔板的外表面上焊接外部密封外壳; 以及通过在液压校准护套的内表面上施加沉积物而形成多孔壁。

53. 发明授权

US4752186A Coolable wall configuration 失效
标题翻译：可冷却墙体配置
公开(公告)号：US4752186A
公开(公告)日：1988-06-21
申请号：US277481
申请日：1981-06-26
申请人： George P. Liang
发明人： George P. Liang
IPC分类号： F01D5/18 , F01D5/08
CPC分类号： F01D5/187 , F28D2021/0078
摘要： A coolable wall configuration includes a slot formed between two wall portions for carrying coolant fluid in a downstream direction wherein the slot is divided into a plurality of parallel channels by as plurality of parallel barrier walls extending in a direction perpendicular to the downstream direction, the barrier walls having openings therethrough at regular intervals to interconnect the channels, wherein the openings in adjacent barrier walls are staggered so that cooling fluid flowing through each opening impinges upon a wall portion of the next barrier wall and ultimately traverses a square wave-like flow path as it moves downstream from channel to channel. This configuration is particularly suitable for use in the trailing edge region of an airfoil.
摘要翻译：可冷却壁构造包括形成在两个壁部分之间的槽，用于沿下游方向承载冷却剂流体，其中该槽由垂直于下游方向的方向延伸的多个平行阻挡壁分成多个平行通道，壁以规则的间隔穿过其中以互连通道，其中相邻阻挡壁中的开口交错，使得流过每个开口的冷却流体撞击下一个阻挡壁的壁部分，并且最终穿过方波状的流动路径，如它从通道向下游移动。该构造特别适用于翼型件的后缘区域。

54. 发明授权

US4214884A Air fin coolers for glass fiber forming apparatus 失效
标题翻译：用于玻璃纤维成型设备的空气翅片冷却器
公开(公告)号：US4214884A
公开(公告)日：1980-07-29
申请号：US969529
申请日：1978-12-14
申请人： Walter L. Martin, Jr.
发明人： Walter L. Martin, Jr.
IPC分类号： C03B37/02
CPC分类号： C03B37/0213 , C03B37/0209 , F28D2021/0029 , F28D2021/0078
摘要： A thin nickel fin cooler is described which has a plurality of precision holes of equal size formed thereon, the fin being tubular in shape so that air can pass from the interior of the fin outwardly to provide uniform gas flow in all directions from the surface of the fin.
摘要翻译：描述了一种薄镍翅片冷却器，其具有形成在其上的多个具有相同尺寸的精密孔，翅片呈管状形状，使得空气可以从翅片的内部向外通过，以从所有方向从翅膀

55. 发明授权

US4078604A Cooling channel surface arrangement for a heat exchanger wall construction 失效
标题翻译：用于热交换器壁结构的冷却通道表面布置
公开(公告)号：US4078604A
公开(公告)日：1978-03-14
申请号：US568832
申请日：1975-04-17
申请人： Manfred Christl , Karl Butter , Helmut Dederra , Michael Kaufmann , Willibald Wittich, deceased , by Renate Wittich nee Padberg, legal guardian , Manfred Lechner
发明人： Manfred Christl , Karl Butter , Helmut Dederra , Michael Kaufmann , Willibald Wittich, deceased , by Renate Wittich nee Padberg, legal guardian , Manfred Lechner
IPC分类号： F28F19/00 , F02K9/64 , F28F19/06 , F02K11/02
CPC分类号： F02K9/64 , F28D2021/0078 , F28F2220/00
摘要： In a heat exchanger wall construction, such as used in regeneratively cooled combustion chambers for liquid fueled rocket engines, the wall construction consists of an inner wall with cooling channels spaced apart by webs. The cooling channels are open on one surface of the inner wall. An outer wall contacts the webs of the inner wall and forms a closure over the openings from the cooling channels. The outer wall consists of an intermediate layer electro-deposited on the surface of the inner wall in which the cooling channels are formed so that it provides a closure surface for the channels. The surfaces of the channels within the inner wall are coated by electro-depositing a layer of gold on them. After forming the gold layer on the surfaces of the cooling channels, the outer surfaces of the webs are etched so that the gold layer extends outwardly from the outer surface of the webs. Next the intermediate layer is deposited and it can be either a single layer or multi-layered. The inner surface of the intermediate layer, whether it is of a single or multi-layered construction, is formed of gold. When the intermediate layer is formed of multiple layers, alternating layers of gold and copper are used.
摘要翻译：在用于液体燃料火箭发动机的再生冷却燃烧室中的热交换器壁结构中，壁结构包括具有通过腹板隔开的冷却通道的内壁。冷却通道在内壁的一个表面上敞开。外壁与内壁的腹板接触，并在冷却通道的开口上形成一个闭合件。外壁由电沉积在内壁的表面上的中间层组成，其中形成冷却通道，使得其提供通道的封闭表面。内壁上的通道的表面通过在其上电沉积一层金而被涂覆。在冷却通道的表面上形成金层之后，对网的外表面进行蚀刻，使得金层从腹板的外表面向外延伸。接下来，沉积中间层，并且其可以是单层或多层。中间层的内表面，无论是单层还是多层结构，均由金形成。当中间层由多层形成时，使用金和铜的交替层。

56. 发明授权

US3652070A Cooling assembly for blast furnace shells 失效
标题翻译：用于吹制炉的冷却总成
公开(公告)号：US3652070A
公开(公告)日：1972-03-28
申请号：US3652070D
申请日：1969-10-16
申请人： MITSUBISHI HEAVY IND LTD
发明人： SAGARA HIDEO
IPC分类号： C21B7/10 , F27D9/00 , F28F13/00 , F27B1/24
CPC分类号： F28F13/00 , C21B7/10 , F27D2009/0021 , F28D2021/0078
摘要： On the inside of a steel shell of a blast furnace there is provided a wall made of a refractory material having a high heat transfer characteristic, such as silicon carbide. Steel pipe loops for circulating a cooling medium are embedded in the wall and temperature sensing means within the refractory material check the temperature adjacent the pipe loops.
摘要翻译：在高炉钢壳的内侧设置有由具有高传热特性的耐火材料制成的壁，例如碳化硅。用于使冷却介质循环的钢管回路嵌入在壁中，耐火材料内的温度检测装置检查管道周围的温度。

57. 发明专利

JP5511352B2 Multiple impingement complex for cooling the wall 有权
公开(公告)号：JP5511352B2
公开(公告)日：2014-06-04
申请号：JP2009283250
申请日：2009-12-14
申请人：シーメンスアクチエンゲゼルシヤフトSiemens Aktiengesellschaft
发明人：へーゼルハウスアンドレアス
IPC分类号： F01D5/18 , F01D9/02 , F02C7/18
CPC分类号： F28F3/02 , B22F7/064 , B22F7/08 , C21C5/4646 , F01D5/183 , F01D5/184 , F05D2250/185 , F23M5/00 , F23R3/002 , F23R2900/03044 , F28D2021/0078

58. 发明专利

JP5455962B2 Method of manufacturing a cooling structure 有权
公开(公告)号：JP5455962B2
公开(公告)日：2014-03-26
申请号：JP2011084562
申请日：2011-04-06
申请人：三菱重工業株式会社
发明人：慶明三宅
IPC分类号： F02C7/18 , F23R3/42
CPC分类号： F23R3/005 , F23R3/002 , F23R2900/03045 , F28D2021/0078 , F28F3/022 , F28F3/048 , F28F13/12 , Y02T50/675 , Y10T29/49359

59. 发明专利

JP2012219668A Cooling structure, gas turbine combustor and manufacturing method of cooling structure 有权
标题翻译：冷却结构，燃气轮机和冷却结构的制造方法
公开(公告)号：JP2012219668A
公开(公告)日：2012-11-12
申请号：JP2011084562
申请日：2011-04-06
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： MIYAKE YOSHIAKI
IPC分类号： F02C7/18 , F23R3/42
CPC分类号： F23R3/005 , F23R3/002 , F23R2900/03045 , F28D2021/0078 , F28F3/022 , F28F3/048 , F28F13/12 , Y02T50/675 , Y10T29/49359
摘要： PROBLEM TO BE SOLVED: To provide a cooling structure, a gas turbine combustor, and a method of manufacturing the cooling structure which can achieve high cooling efficiency without increasing a manufacturing cost.SOLUTION: A cooling structure includes a first member 3 as a cooling object having a first plane and a second member 4 arranged above the first plane and provided with a second plane opposite to the first plane so as to form a passage in which a cooling medium flows between the first plane and the second plane. The first member comprises a plurality of protrusions 15 extending upwardly from the first plane. Each of the plurality of protrusion extends so as to be inclined along a direction in which the cooling medium flows. A clearance between the second plane and a tip of the each protrusions set so that a heat transfer coefficient between the cooling medium and the second member becomes larger than a heat transfer coefficient when each projection extends upwardly in a vertical direction from the first plane.
摘要翻译：要解决的问题：提供一种冷却结构，燃气轮机燃烧器以及可以在不增加制造成本的情况下实现高冷却效率的制冷结构的制造方法。解决方案：冷却结构包括作为具有第一平面的冷却对象的第一构件3和布置在第一平面上方的第二构件，并且设置有与第一平面相对的第二平面，以形成通道，其中冷却介质在第一平面和第二平面之间流动。第一构件包括从第一平面向上延伸的多个突起15。多个突起中的每一个沿着冷却介质流动的方向延伸。第二平面与每个突出部的尖端之间的间隙，使得当每个突起从第一平面沿垂直方向向上延伸时，冷却介质和第二部件之间的传热系数变得大于传热系数。版权所有（C）2013，JPO＆INPIT

60. 发明专利

JP2004233043A Active cooling panel of thermostructural composite material and method for manufacturing the same 审中-公开
公开(公告)号：JP2004233043A
公开(公告)日：2004-08-19
申请号：JP2004023396
申请日：2004-01-30
申请人： Snecma Propulsion Solide , スネクマ・プロピュルシオン・ソリドSnecma Propulsion Solide
发明人： LARRIEU JEAN MICHEL , UHRIG GILLES , THEBAULT JACQUES , BOUQUET CLEMENT
IPC分类号： F01D5/28 , B23K20/00 , B23K103/16 , C04B37/00 , C04B41/88 , F02C7/00 , F02C7/18 , F02C7/28 , F02K9/34 , F02K9/64 , F02K9/97 , F23R3/00 , F23R3/42 , F28F3/12 , F28F21/08
CPC分类号： F28F21/081 , F02K9/64 , F02K9/972 , F02K9/974 , F23R3/005 , F23R3/007 , F28D2021/0078 , F28F3/12
摘要： PROBLEM TO BE SOLVED: To provide an active cooling panel of a thermostructural composite material and a method for manufacturing the same suitable for manufacturing a heat exchange wall such as the wall of a combustion chamber of an aircraft engine, a branch part of a rocket engine or an extreme plasma chamber of a nuclear fusion reactor.
SOLUTION: The active cooling panel 10 is assembled by joining the inner surfaces 21, 31 with first and second components 20, 30 of the thermostructural composite material respectively having inner surfaces 21, 31 and opposite outer surfaces, and provided with a channel 24 formed of a recess formed on the inner surface of at lease one of the first and second components. The panel 10 is provided with a seal layer joined with at least one of the first and second components 20, 30 and positioned at a specified distance from respective inner faces for assembly.
COPYRIGHT: (C)2004,JPO&NCIPI

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