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41.发明公开CYLINDRICAL STRUCTURE AND METHOD FOR MANUFACTURING SAME 有权ZYLINDRISCHE STRUKTUR UND HERSTELLUNGSVERFAHRENDAFÜR
公开(公告)号：EP2497626A1
公开(公告)日：2012-09-12
申请号：EP10828338.3
申请日：2010-11-05
IPC分类号： B29C70/16 , C08J5/06 , F01D25/00 , F02C7/00 , F04D29/52 , B29K105/08 , B29L23/00 , B29L31/30
CPC分类号： F04D29/522 , B29C53/562 , B29C53/58 , B29C70/32 , F02K9/00
摘要： A method for manufacturing a cylindrical structure having an axial direction includes: winding a fabric around a mandrel in a circumferential direction that is perpendicular to the axial direction, the fabric containing first fibers oriented in a first direction intersecting the circumferential direction; winding a roving into a helical shape around the mandrel, the roving containing second fibers oriented in a longitudinal direction of the roving; and joining the fabric and the roving together by using a resin.
摘要翻译： 一种制造具有轴向方向的圆柱形结构的方法包括：在与心轴垂直的圆周方向上围绕心轴缠绕织物，所述织物包含沿与圆周方向交叉的第一方向取向的第一纤维; 将纱线绕心轴缠绕成螺旋形状，粗纱包含沿着粗纱的纵向取向的第二纤维; 并通过使用树脂将织物和粗纱接合在一起。
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42.发明公开BLADE OF A GAS TURBINE ENGINE FOR AN AIRPLANE, AND A METHOD FOR MANUFACTURING THE SAME 有权移动燃气涡轮发动机的叶片中平面及其制造方法
公开(公告)号：EP2270337A4
公开(公告)日：2012-08-29
申请号：EP09725734
申请日：2009-03-27
申请人： IHI CORP , IHI AEROSPACE CO LTD
IPC分类号： F01D5/28 , B29C70/46 , B29K101/12 , B29K105/08 , B29L31/08
CPC分类号： F01D5/282 , B29C70/30 , B29C70/46 , B29D99/0025 , B29K2105/0872 , B29L2031/082 , B29L2031/087 , F01D5/141 , F04D29/023 , F04D29/324 , F04D29/388 , F05D2230/26 , F05D2300/43 , F05D2300/603 , Y02T50/672 , Y02T50/673 , Y10T29/49336
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公开(公告)号：EP2343241A1
公开(公告)日：2011-07-13
申请号：EP09823420.6
申请日：2009-09-11
发明人： ADACHI, Tadashi
摘要： A space probing apparatus is provided that can further enhance its thermal protective function for electronic apparatuses and batteries that are apparatuses each having a narrow range of permissible temperature.
The space probing apparatus includes, as a vehicle body 1 that is an apparatus body, an inner housing 13 that accommodates an electronic apparatus 11 and a battery 12, and an outer housing 15 that accommodates the inner housing 13 supporting the inner housing 13 afloat therein. A thermal insulating layer 16 is formed between the inner housing 13 and the outer housing 15 using a space therebetween. A heat dissipating body 17 is included in an upper portion of the inner housing 13. A lid 18 is included in an upper portion of the outer housing 15. The whole outer faces of the inner and the outer housings 13 and 15 are each covered with a thermal insulating material 20. Thereby, in the nighttime, the temperature of the battery 12 is maintained using the least necessary amount of heat generated and, thereby, the electronic apparatus 11 and the battery 12 are protected from an ultralow temperature. In the daytime, the lid 18 is opened and heat is discharged using the heat dissipating body 17 and, thereby, the electronic apparatus 11 and the battery 12 are protected from a high temperature.摘要翻译： 提供一种空间探测装置，其可以进一步增强其作为各自具有窄允许温度范围的装置的电子设备和电池的热保护功能。 空间探测装置包括作为装置主体的车体1，容纳电子设备11和电池12的内壳体13和容纳内壳体13的外壳体15，内壳体13支撑内壳体13浮动在其中 。 使用它们之间的空间在内壳体13和外壳体15之间形成隔热层16。 散热体17包括在内壳13的上部。盖18包括在外壳15的上部。内外壳13和15的整个外表面各自被覆盖 绝热材料20.因此，在夜间，使用产生的最少量的热量来保持电池12的温度，从而保护电子设备11和电池12免受超低温度的影响。 白天，打开盖18，利用散热体17排出热量，从而保护电子设备11和电池12免受高温的影响。
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44.发明公开BLADE OF A GAS TURBINE ENGINE FOR AN AIRPLANE, AND A METHOD FOR MANUFACTURING THE SAME 有权HERSTELLUNGSVERFAHRENFÜREINE LAUFSCHAUFEL EINER GASTURBINENMOTORSFÜREIN FLUGZEUG
公开(公告)号：EP2270337A1
公开(公告)日：2011-01-05
申请号：EP09725734.9
申请日：2009-03-27
IPC分类号： F04D29/38 , B29C43/20 , B29K101/12 , B29K105/08 , B29L31/30
CPC分类号： F01D5/282 , B29C70/30 , B29C70/46 , B29D99/0025 , B29K2105/0872 , B29L2031/082 , B29L2031/087 , F01D5/141 , F04D29/023 , F04D29/324 , F04D29/388 , F05D2230/26 , F05D2300/43 , F05D2300/603 , Y02T50/672 , Y02T50/673 , Y10T29/49336
摘要： A gas turbine engine blade for aircraft which has a 3-dimensional blade surface shape twisted around a center line at an angle of 45 degrees or more and 70 degrees or less, wherein the aforementioned blade is provided with multiple composite material prepregs which contain reinforced fiber and which are integrally molded after being laminated in the thickness direction, and the aforementioned reinforced fiber runs continuously without interruption within each layer of the aforementioned composite material prepregs.
摘要翻译： 一种用于飞机的燃气涡轮发动机叶片，其具有以45度以上且70度以下的角度绕中心线扭转的3维叶片表面形状，其中，所述叶片设置有多个复合材料预浸料，其包含增强纤维 并且在厚度方向层叠后一体成型，上述增强纤维在上述复合材料预浸料的各层内连续不间断地延伸。
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公开(公告)号：EP1434021A4
公开(公告)日：2009-05-27
申请号：EP02775251
申请日：2002-09-27
申请人： IHI AEROSPACE CO LTD
CPC分类号： F27D21/02 , F27B17/00 , F27B17/0016 , F27B17/02 , F27D7/06 , F27D11/00 , F27D19/00 , H05B6/32
摘要： An electrostatic levitation furnace, wherein three sets of electrodes opposed to each other on three axes orthogonal to each other around the levitated position of a specimen are installed in a vacuum chamber, and an access port directed to the levitated position of the specimen is three-dimensionally disposed in the vacuum chamber, whereby the freedom degree of arrangement of various types of equipment can be increased by increasing the number of the directions for access to the specimen and equipment can also be easily added.
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46.发明公开
公开(公告)号：EP1462782A1
公开(公告)日：2004-09-29
申请号：EP03006710.2
申请日：2003-03-24
IPC分类号： G01J5/10
CPC分类号： G01J5/10
摘要： A thermal type-infrared detection device improved in the sensitivity and the power of output signal without deterioration of strength of the diaphragm, which is provided with a silicon substrate with a concave, a diaphragm made of an insulation material substantially covering the concave of the silicon substrate, an infrared detecting section positioned on the diaphragm, and the silicon substrate is formed with a projection made of a thermal conductor for supporting the diaphragm away from the silicon substrate.
摘要翻译： 的热式红外线检测装置的灵敏度和输出信号的无隔膜的强度的劣化的功率提高，所有这些都被提供有一个硅衬底具有凹入，由绝缘材料构成的隔膜基本上覆盖硅氧烷的凹 其中红外线检测部在隔膜上定位衬底，以及硅衬底上形成有用于支撑所述隔膜从所述硅衬底远离由热导体的投影。
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公开(公告)号：EP1434021A1
公开(公告)日：2004-06-30
申请号：EP02775251.8
申请日：2002-09-27
发明人： KAWASAKI, Kazunori, IHI AEROSPACE CO., LTD. , ASAHI, Hiroaki, IHI AEROSPACE ENGINEERING CO., LTD , MURAMATSU, Shoji, IHI AEROSPACE CO., LTD. , TAKADA, Tetsuya, IHI AEROSPACE ENGINEERING CO.LTD
IPC分类号： F27B17/00
CPC分类号： F27D21/02 , F27B17/00 , F27B17/0016 , F27B17/02 , F27D7/06 , F27D11/00 , F27D19/00 , H05B6/32
摘要： An electrostatic levitation furnace is improved by providing three pairs of electrodes opposed to each other respectively on three axes perpendicularly intercepting each other at a position where the sample is to be levitated in the vacuum chamber, and disposing a plurality of access ports, which are directed to the position of the sample, to the vacuum chamber tree-dimensionally, whereby the accessible direction against the sample is diversified, it becomes possible to improve the degree of freedom in distribution of various apparatuses and easily cope with increase of apparatuses.
摘要翻译： 通过在真空室中将待样品悬浮的位置上相互垂直截取的三个轴上分别设置三对相对的电极来提高静电悬浮炉，并且设置多个导向孔 到样品的位置，树立到真空室，由此对样品的可触及方向多样化，可以提高各种装置的分配自由度，并且容易应对装置的增加。
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公开(公告)号：EP1209455A3
公开(公告)日：2003-08-27
申请号：EP01127321.6
申请日：2001-11-19
IPC分类号： G01J5/10
CPC分类号： G01J5/02 , G01J5/0225 , G01J5/10 , G01J5/12
摘要： A large-area high-output infrared detecting device S is realized in which a heat-separation-structure diaphragm 2 made of a thermal insulating material is formed through a cavity 7 from a silicon substrate 1, a thermocouple 4 serving as an infrared detection section is formed on the diaphragm 2, a heat absorption area 5 is formed on the thermocouple 4 through insulation layers 3a and 3b so as to have an etching aperture 9 for forming a cavity in the heat absorption area 5, and the cavity 7 is formed in a short time without being influenced by the size of the heat absorption area 5 to secure a structural strength.
摘要翻译： 实现了一种大面积高输出红外检测装置S，其中由绝热材料制成的隔热结构隔膜2通过来自硅基板1的空腔7形成，用作红外检测部分的热电偶4 形成在隔膜2上，通过绝缘层3a和3b在热电偶4上形成吸热区域5，以具有用于在吸热区域5中形成空腔的蚀刻孔9，并且形成空腔7 短时间而不受吸热区域5的尺寸的影响，以确保结构强度。
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49.发明公开Electromotive actuator and method for controlling the same 有权Elektromotorischer Stellantrieb und Verfahren zum Steuern desselben
公开(公告)号：EP1262687A2
公开(公告)日：2002-12-04
申请号：EP02011609.1
申请日：2002-05-28
发明人： Oyori, Hitoshi
CPC分类号： H02K16/00 , F16H25/2018 , F16H25/2204 , F16H2025/2075 , H02K7/06 , H02K7/116
摘要： To realize structure simplification and reduction in manufacturing cost without lowering power transmission efficiency and reliability. The present invention includes a first motor 5 and a second motor 6, and a lead 2 of a ball screw 12 is disposed coaxially with a motor rotary shaft 5a on a first motor 5 side and a nut 3 of the ball screw 12 is disposed coaxially with a motor rotary shaft 6a on a second motor 6 side so that the first motor 5 and the second motor 6 are connected to each other via the ball screw 12.
摘要翻译： 实现结构简化和降低制造成本，而不降低动力传递效率和可靠性。 本发明包括第一电动机5和第二电动机6，滚珠丝杠12的引线2与第一电动机5侧的电动机旋转轴5a同轴配置，并且滚珠丝杠12的螺母3同轴地配置 在第二电动机6侧具有电机旋转轴6a，使得第一电动机5和第二电动机6经由滚珠丝杠12彼此连接。
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公开(公告)号：EP1213570A2
公开(公告)日：2002-06-12
申请号：EP01128473.4
申请日：2001-12-06
IPC分类号： G01J5/12
CPC分类号： G01J5/12
摘要： An infrared detecting device possible to improve SN ratio, which is provided with a semiconductor substrate, a diaphragm set on the semiconductor substrate, a thermopile formed on the diaphragm by arranging a plurality of thermocouples composed of p-type polysilicon and n-type polysilicon in a row and electrically connecting them each other in series, and a heat absorption film formed on the central portion through an insulation layer, and sectional areas of the p-type and n-type polysilicons between hot and cold junctions of each of the thermocouples are made different from each other.
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