专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明公开

EP3119991A1 CENTRIFUGAL RADIAL TURBINE 有权
标题翻译： ZENTRIFUGALE RADIALTURBINE
公开(公告)号：EP3119991A1
公开(公告)日：2017-01-25
申请号：EP15718087.8
申请日：2015-03-17
申请人： Exergy S.p.A.
发明人： SPADACINI, Claudio , RIZZI, Dario
IPC分类号： F01D1/06 , F01D1/14 , F01K25/08
CPC分类号： F01D1/06 , F01D1/14 , F01D1/28 , F01K7/16 , F01K25/08
摘要： A centrifugal radial turbine includes at least one support disc having a first face bearing at least one radial rotor stage formed by an array of blades arranged in succession along a respective circular path. The disc has through induction channels situated in a position radially external with respect to a respective shaft and radially internal with respect to the radial rotor stage. At the respective through induction channels, the disc includes a plurality of induction rotor blades of at least one respective axial rotor stage.
摘要翻译：离心式径向涡轮机包括至少一个支撑盘，所述至少一个支撑盘具有第一面轴承，所述第一面轴承具有沿着相应的圆形路径连续布置的由一组叶片形成的至少一个径向转子级该盘通过位于相对于相应的轴径向外部的位置并且相对于径向转子级径向内部的感应通道。在相应的通过感应通道中，盘包括至少一个相应的轴向转子级的多个感应转子叶片。

2. 发明公开

EP2426313A1 Transmission comprising centrifugal impellers 有权
标题翻译： Wandler mit zentrifugalen Impellern
公开(公告)号：EP2426313A1
公开(公告)日：2012-03-07
申请号：EP11179681.9
申请日：2011-09-01
申请人： Chen, Chun-Chieh
发明人： Chen, Chun-Chieh
IPC分类号： F01D1/28 , F02C3/05
CPC分类号： F01D1/28 , F02C3/05
摘要： It is a kind of transmission that is to transform air power into torque. The key parts are two centrifugal impellers: one is an active part, it is to generate air power. Another is a passive part, it is to transform air power into torque.
摘要翻译：它是将空气动力转化为扭矩的一种变速器。关键部件是两台离心式叶轮：一种是主动部件，它是产生空气动力。另一个是被动部分，它将空气动力转化为扭矩。

3. 发明公开

EP1509688A1 HIGH EFFICIENCY GAS TURBINE POWER GENERATOR SYSTEMS 审中-公开
标题翻译：高性能燃机发电系统
公开(公告)号：EP1509688A1
公开(公告)日：2005-03-02
申请号：EP03726652.5
申请日：2003-05-07
申请人： PAUL, Marius A.
发明人： PAUL, Marius A.
IPC分类号： F02C3/067
CPC分类号： F02C3/05 , F01D1/28 , F01D3/00 , F01D13/02 , F01D15/10 , F02C3/067 , F02C3/30 , F02C5/02 , H02K7/1823
摘要： A gas turbine power generator with ultra high efficiency, the generator being an assembly of electric motor-generator machines (171, 172, 173) and turbine configurations (110, 140) used in combination with combustor systems (180) for operation of select integrated turbine configurations.

4. 发明授权

EP0811752B1 CENTRIFUGAL GAS TURBINE 失效
标题翻译：与INSIDE OUT灌注径向燃气轮机
公开(公告)号：EP0811752B1
公开(公告)日：2000-09-06
申请号：EP96912042.7
申请日：1996-04-29
申请人： Abundancia Navarro, Juan Carlos , Abundancia Navarro, Cristina , Abundancia de Santiago, Ramon
发明人： ABUNDANCIA DE SANTIAGO, Ramon
IPC分类号： F01D1/28 , F02C3/05 , F01D1/22
CPC分类号： F02C3/05 , F01D1/22 , F01D1/28 , F01D5/041 , F02C3/085
摘要： Contrarotating outward-flow gas turbine without stators and with two rotors (1 and 2) which set in motion the power shaft (3) and the compressor shaft (17), respectively. The inlet air (19) is sent through the impellers (20) of the outward-flow compressor to the manifold (22) and from there to the regenerator (24) where it is preheated; then, it reaches the combustion chamber (14) and from there it expands to the rotors, and finally passes through the exhaust manifold (27). The rotors (1 and 2) contrarotate coaxially on their bearings (11), both rotors having one or a plurality of rings of vanes (5, 6, 7, 8), and additionally flow guiding fins (9).

5. 发明公开

EP2410126A4 TURBINE WHEEL 有权
公开(公告)号：EP2410126A4
公开(公告)日：2018-02-28
申请号：EP10828136
申请日：2010-07-28
申请人： MITSUBISHI HEAVY IND LTD
发明人： YOKOYAMA TAKAO , OSAKO KATSUYUKI , YOSHIDA TOYOTAKA , EBISU MOTOKI
IPC分类号： F01D1/28 , F01D5/04 , F02B39/00 , F02C3/05
CPC分类号： F01D5/048 , F01D1/28 , F05D2220/40 , F05D2240/307 , F05D2250/70 , F05D2260/20
摘要： Providing a turbine wheel that includes, but not limited to: a plurality of blade parts and a scallop cut-out profile, the scallop cut-out profile being formed by cutting-out the back side wall part of the turbine wheel between the suction surface side of a blade part and the pressure surface side of the adjacent blade part, wherein the leakage flow on the rear side of the blade part is constrained so as to enhance the turbocharger efficiency. Providing the blade part 5 (i.e. the area between the scallop parts on the tip end side of the blade part) with the suction surface side extended part 25 in the neighborhood of the suction surface 21 of the blade part so that the thickness of the blade part on the tip end side of the scallop cut-out profile is increased; or, the pressure surface side extended part 32 in the neighborhood of the pressure surface 19 of the blade part so that the thickness of the blade part on the tip end side of the scallop cut-out profile is increased. Or, the positive/suction surface side extended parts are provided. Thereby, the extended width of the extended part is formed so that the width is an almost constant width along the camber line of the blade part from the tip end side to the root side of the blade, the projecting-out width part forming a strip area.

6. 发明授权

EP2426313B1 Transmission comprising centrifugal impellers 有权
标题翻译：包含离心叶轮的传动装置
公开(公告)号：EP2426313B1
公开(公告)日：2017-05-24
申请号：EP11179681.9
申请日：2011-09-01
申请人： Chen, Chun-Chieh
发明人： Chen, Chun-Chieh
IPC分类号： B62M19/00
CPC分类号： F01D1/28 , F02C3/05

7. 发明公开

EP2410126A1 TURBINE WHEEL 有权
标题翻译：涡轮机轮
公开(公告)号：EP2410126A1
公开(公告)日：2012-01-25
申请号：EP10828136.1
申请日：2010-07-28
申请人： Mitsubishi Heavy Industries, Ltd.
发明人： YOKOYAMA, Takao , OSAKO, Katsuyuki , YOSHIDA, Toyotaka , EBISU, Motoki
IPC分类号： F01D1/28 , F01D5/04 , F02B39/00 , F02C3/05
CPC分类号： F01D5/048 , F01D1/28 , F05D2220/40 , F05D2240/307 , F05D2250/70 , F05D2260/20
摘要： Providing a turbine wheel that includes, but not limited to: a plurality of blade parts and a scallop cut-out profile, the scallop cut-out profile being formed by cutting-out the back side wall part of the turbine wheel between the suction surface side of a blade part and the pressure surface side of the adjacent blade part, wherein the leakage flow on the rear side of the blade part is constrained so as to enhance the turbocharger efficiency. Providing the blade part 5 (i.e. the area between the scallop parts on the tip end side of the blade part) with the suction surface side extended part 25 in the neighborhood of the suction surface 21 of the blade part so that the thickness of the blade part on the tip end side of the scallop cut-out profile is increased; or, the pressure surface side extended part 32 in the neighborhood of the pressure surface 19 of the blade part so that the thickness of the blade part on the tip end side of the scallop cut-out profile is increased. Or, the positive/suction surface side extended parts are provided. Thereby, the extended width of the extended part is formed so that the width is an almost constant width along the camber line of the blade part from the tip end side to the root side of the blade, the projecting-out width part forming a strip area.
摘要翻译：提供涡轮机叶轮，该涡轮机叶轮包括但不限于：多个叶片部件和扇贝切口轮廓，扇贝切口轮廓通过将涡轮机叶轮的后侧壁部分切除在吸力表面其中叶片部分后侧的泄漏流被约束以提高涡轮增压器的效率。在叶片部的吸附面21的附近设置叶片部5（即，叶片部的前端侧的扇贝状部分之间的区域）与吸附面侧延伸部25，使得叶片的厚度扇贝切出轮廓的顶端侧的部分增加; 或者在叶片部分的压力表面19附近的压力表面侧延伸部分32，以便扇贝切口轮廓的顶端侧上的叶片部分的厚度增加。或者，设置正/负表面侧延伸部。由此，延伸部的延伸宽度形成为，从叶片的前端侧到根部侧沿着叶片部的弧线的宽度大致恒定，形成条的突出宽度部区。

8. 发明公开

EP0811752A1 CENTRIFUGAL GAS TURBINE 失效
标题翻译： GASTURBINE MIT VON INNEN NACH AUSSENDURCHSTRÖMTEMRADIALRAD
公开(公告)号：EP0811752A1
公开(公告)日：1997-12-10
申请号：EP96912042.7
申请日：1996-04-29
申请人： Abundancia Navarro, Juan Carlos , Abundancia Navarro, Cristina , Abundancia de Santiago, Ramon
发明人： ABUNDANCIA DE SANTIAGO, Ramon
IPC分类号： F01D1/28 , F02C3/05 , F01D1/22
CPC分类号： F02C3/05 , F01D1/22 , F01D1/28 , F01D5/041 , F02C3/085
摘要： Contrarotating outward-flow gas turbine without stators and with two rotors (1 and 2) which set in motion the power shaft (3) and the compressor shaft (17), respectively. The inlet air (19) is sent through the impellers (20) of the outward-flow compressor to the manifold (22) and from there to the regenerator (24) where it is preheated; then, it reaches the combustion chamber (14) and from there it expands to the rotors, and finally passes through the exhaust manifold (27). The rotors (1 and 2) contrarotate coaxially on their bearings (11), both rotors having one or a plurality of rings of vanes (5, 6, 7, 8), and additionally flow guiding fins (9).
摘要翻译：不带定子的对流向外流动燃气轮机和分别设置在动力轴（3）和压缩机轴（17）上的两个转子（1和2）。入口空气（19）通过外流式压缩机的叶轮（20）送到歧管（22），并从那里进入再生器（24），在那里进行预热; 那么它到达燃烧室（14）并且从那里膨胀到转子，并最终通过排气歧管（27）。转子（1和2）同轴地在其轴承（11）上反转，两个转子具有一个或多个叶片环（5,6,7,8）和另外的引导翅片（9）。

9. 发明授权

EP3119991B1 CENTRIFUGAL RADIAL TURBINE 有权
标题翻译：离心式径向涡轮机
公开(公告)号：EP3119991B1
公开(公告)日：2018-05-02
申请号：EP15718087.8
申请日：2015-03-17
申请人： Exergy S.p.A.
发明人： SPADACINI, Claudio , RIZZI, Dario
IPC分类号： F01D1/06 , F01D1/14 , F01K25/08
CPC分类号： F01D1/06 , F01D1/14 , F01D1/28 , F01K7/16 , F01K25/08
摘要： A centrifugal radial turbine includes at least one support disc having a first face bearing at least one radial rotor stage formed by an array of blades arranged in succession along a respective circular path. The disc has through induction channels situated in a position radially external with respect to a respective shaft and radially internal with respect to the radial rotor stage. At the respective through induction channels, the disc includes a plurality of induction rotor blades of at least one respective axial rotor stage.

10. 发明授权

EP2820280B1 COUNTER-ROTATING LOW PRESSURE TURBINE WITH GEAR SYSTEM MOUNTED TO TURBINE EXHAUST CASE 有权转让
标题翻译：带齿轮系统的反转低压涡轮机安装在涡轮机排气箱上
公开(公告)号：EP2820280B1
公开(公告)日：2017-09-27
申请号：EP13784640.8
申请日：2013-02-15
申请人： United Technologies Corporation
发明人： SUCIU, Gabriel L. , MERRY, Brian D.
IPC分类号： F02K3/072 , F02K3/04 , F02C7/04 , F02C3/107 , F02C3/067 , F01D15/12 , F02K3/068 , F02C7/06 , F01D1/26 , F02C7/36
CPC分类号： F02C7/36 , F01D1/26 , F01D1/28 , F01D15/12 , F02C3/067 , F02C3/107 , F02C7/06 , F02K3/068 , F02K3/072 , F05D2260/40311 , F05D2260/53 , Y02T50/671

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式