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81. 发明申请

WO2013122857A1 MULTI-SEGMENT TURBOCHARGER BEARING HOUSING AND METHODS THEREFOR 审中-公开
标题翻译：多部分涡轮增压器轴承座及其方法
公开(公告)号：WO2013122857A1
公开(公告)日：2013-08-22
申请号：PCT/US2013/025518
申请日：2013-02-11
申请人： BORGWARNER INC.
发明人： DATE, Aaron , CAVAGNARO, Augustine , BUCKING, Michael
IPC分类号： F02B39/00 , F01D25/16 , F01D25/18
CPC分类号： F04D29/056 , F01D25/16 , F01D25/162 , F01D25/18 , F01D25/243 , F04D25/045 , F04D29/063 , F04D29/403 , F05D2220/40 , F05D2220/76 , Y10T29/49325
摘要： A turbocharger (102, 202, 302) including a rotating assembly (114, 214, 314) having a compressor wheel (120, 220, 320) and a turbine wheel (110, 210, 310) mounted on opposite ends of a shaft (112, 212, 312). A bearing housing (160, 260, 360) supports the rotating assembly (114, 214, 314) and comprises at least two segments (189, 190; 289, 290; 389, 390). Each segment (189, 190; 289, 290; 389, 390) has an opening large enough to radially receive the rotating assembly (114, 214, 314). The bearing housing segments (189, 190; 289, 290; 389, 390) are fastened (193) together and a flexible seal may be provided between the segments. The bearing housing (160, 260, 360) may house rolling element bearings (325) or journal bearings (149), for example. The bearing housing (160, 260, 360) is split axially (101, 201, 301) into an upper segment (189, 289, 389) and a lower segment (190, 290, 390). Alternatively, the bearing housing (160, 260, 360) is split axially (101, 201, 301) into a left segment and a right segment. The turbocharger (102) may further comprise an electric motor stator (148) disposed in the bearing housing (160). The bearing housing (160) may also include a defined passageway (143) extending around the stator (148) and configured to receive a cooling liquid.
摘要翻译：包括具有压缩机叶轮（120,220,320）和安装在轴的相对两端的涡轮机叶轮（110,210,310）的旋转组件（114,214,314）的涡轮增压器（102,202,302） 112,212,312）。轴承座（160,260,360）支撑旋转组件（114,214,314）并且包括至少两个段（189,190; 289,290; 389,390）。每个段（189,190; 289,290; 389,390）具有足够大的径向径向接收旋转组件（114,214,314）的开口。轴承壳体段（189,190; 289,290; 389,390）被紧固（193）在一起，并且可以在段之间提供柔性密封。例如，轴承壳体（160,260,360）可容纳滚动元件轴承（325）或轴颈轴承（149）。轴承座（160,260,360）沿轴向（101,201,301）分裂成上段（189,289,389）和下段（190,290,390）。或者，轴承壳体（160,260,360）被轴向地分开（101,201,301）成左段和右段。涡轮增压器（102）还可以包括设置在轴承壳体（160）中的电动机定子（148）。轴承座（160）还可以包括围绕定子（148）延伸并且构造成接纳冷却液体的限定通道（143）。

82. 发明申请

WO2007073447A1 COMPRESSOR HAVING INTEGRAL EGR VALVE AND MIXER 审中-公开
标题翻译：具有整体式EGR阀和混合器的压缩机
公开(公告)号：WO2007073447A1
公开(公告)日：2007-06-28
申请号：PCT/US2006/042033
申请日：2006-10-27
申请人： CATERPILLAR INC. , GRIFFITH, Robert, C.
发明人： GRIFFITH, Robert, C.
IPC分类号： F02M37/00 , F02M25/07
CPC分类号： F01D5/141 , F01D5/048 , F01D9/026 , F01D17/146 , F02B29/0406 , F02B37/00 , F02B37/025 , F02C3/13 , F02M26/06 , F02M26/07 , F02M26/21 , F02M26/23 , F02M26/35 , F02M26/51 , F02M26/70 , F04D25/024 , F04D25/045 , F05D2220/40 , F05D2270/082 , Y02T10/144
摘要： A compressor (24) for a power system (5) is disclosed. The compressor has a compressor (24) wheel (55) rotatable to compress a fluid, and a compressor housing (56) at least partially enclosing the compressor wheel (55). The compressor housing (56) has a first volute (60) and a second volute (62). The first volute (60) is configured to direct an exhaust gas radially inward to the compressor wheel (55). The second volute (62) is configured to direct a mixture of the exhaust gas and air radially outward from the compressor wheel (55).
摘要翻译：公开了一种用于电力系统（5）的压缩机（24）。压缩机具有可旋转以压缩流体的压缩机（24）轮（55）和至少部分地包围压缩机叶轮（55）的压缩机壳体（56）。压缩机壳体（56）具有第一蜗壳（60）和第二蜗壳（62）。第一蜗壳（60）构造成将废气径向向内引导到压缩机叶轮（55）。第二蜗壳62构造成引导废气和空气的混合物从压缩机叶轮55径向向外引导。

83. 发明申请

WO2006059996A1 BALANCED TURBINE ROTOR FAN BLADE FOR A TIP TURBINE ENGINE 审中-公开
标题翻译：平衡式涡轮转子风扇叶片涡轮发动机
公开(公告)号：WO2006059996A1
公开(公告)日：2006-06-08
申请号：PCT/US2004/040124
申请日：2004-12-01
申请人： UNITED TECHNOLOGIES CORPORATION , NORDEEN, Craig A. , SUCIU, Gabriel L.
发明人： NORDEEN, Craig A. , SUCIU, Gabriel L.
IPC分类号： F02C3/073 , F04D25/04 , F01D5/18 , F02K3/068
CPC分类号： F02C3/073 , F01D5/18 , F02K3/068 , F04D25/045 , F04D29/321 , Y02T50/673 , Y02T50/676
摘要： A fan-turbine rotor assembly for a tip turbine engine includes a multiple of fan blades, which include an inducer section (66), a hollow fan blade section (72) and a diffuser section (74). The hollow fan blade section defines a airflow passage (80). The core airflow is turned, spread and split toward opposite ends of the diffuser section by a multiple of internal turning vanes (122). The airflow streams are then further turned by discharge turning vanes (124) before discharge from a diffuser discharge outlet. Along with turning and splitting the core airflow, the fan blade profile balances the mass of the diffuser section such that the center of mass thereof is over the hollow airfoil section structure.
摘要翻译：用于尖端涡轮发动机的风扇涡轮转子组件包括多个风扇叶片，其包括导流部分（66），中空风扇叶片部分（72）和扩散器部分（74）。中空风扇叶片部分限定了气流通道（80）。核心气流通过多个内部转向叶片（122）转动，展开并且分散到扩散器部分的相对端部。然后在从扩散器排出口排放之前，排气转向叶片（124）进一步转动气流。随着转动和分离核心气流，风扇叶片轮廓使扩散器部分的质量平衡，使得其中心在中空翼型部分结构之上。

84. 发明申请

WO2004029418A1 SUPERCHARGER COUPLED TO A MOTOR/GENERATOR UNIT 审中-公开
标题翻译：超级电机耦合到电机/发电机组
公开(公告)号：WO2004029418A1
公开(公告)日：2004-04-08
申请号：PCT/IB2003/004311
申请日：2003-09-30
申请人： FERRARO, Giuseppe
发明人： FERRARO, Giuseppe
IPC分类号： F01D15/10
CPC分类号： F01D15/10 , F02B37/04 , F02B37/18 , F02B39/10 , F02C6/12 , F04D25/045 , F04D25/06 , Y02T10/144 , Y02T50/672
摘要： A device for handling and recovering of kinetic energy in a fluid is presented which basically features a bladed impeller (11). The impeller is operated by an electric engine (12) and acts as a centrifugal blower yielding energy to the air when the main engine is in a low boost phase; otherwise in case of excessive boost pressure, the impeller receives the moving fluid which will drive its rotation, reducing pressure and absorbing the energy to operate the electric engine (12) which will act as a reversible electric machine, thus generating electric power.
摘要翻译：提出了一种用于处理和回收流体中的动能的装置，其基本上具有叶片叶轮（11）。叶轮由电动发动机（12）操作，当主发动机处于低增压阶段时，作为离心鼓风机向空气产生能量; 否则在过大的增压压力的情况下，叶轮接收将驱动其旋转的运动流体，减小压力并吸收能量以操作将用作可逆电机的电动发动机（12），从而产生电力。

85. 发明公开

EP3385170A1 TURBINE-ASSISTED CABIN AIR COMPRESSOR 审中-公开
公开(公告)号：EP3385170A1
公开(公告)日：2018-10-10
申请号：EP18165512.7
申请日：2018-04-03
申请人： Hamilton Sundstrand Corporation
发明人： DeFrancesco, Gregory L.
IPC分类号： B64D13/06
CPC分类号： B64D13/08 , B64D13/02 , B64D13/06 , B64D2013/0611 , B64D2013/0618 , B64D2013/0644 , B64D2013/0648 , F04D25/045 , F04D25/06 , F04D29/053 , F04D29/5826 , Y02T50/56
摘要： An airplane is provided. The airplane includes a motor-driven compressor assembly (120). The motor-driven compressor assembly includes a shaft (216), a motor (212), a compressor (210), and a turbine (214) coupled to the compressor via the shaft. The motor provides a first power to the compressor via the shaft. The turbine receives and expands a second medium to provide a second power to the compressor via the shaft. The compressor receives and compresses a first medium in accordance with the first power provided by the turbine and the second power provided by the motor.

86. 发明公开

EP3385169A1 HYBRID THIRD AIR CONDITION PACK 有权
公开(公告)号：EP3385169A1
公开(公告)日：2018-10-10
申请号：EP18165479.9
申请日：2018-04-03
申请人： Hamilton Sundstrand Corporation
发明人： Zywiak, Thomas M. , DeFrancesco, Gregory L. , Hall, David E.
IPC分类号： B64D13/06
CPC分类号： B64D13/08 , B64D13/02 , B64D13/06 , B64D2013/0603 , B64D2013/0618 , B64D2013/0648 , B64D2013/0688 , F04D25/045 , F04D29/053 , F04D29/5826 , Y02T50/56
摘要： An airplane is provided. The airplane includes a pack. The pack includes a shaft (222), a compressor (210), a turbine (220) coupled to the compressor via the shaft; and a heat exchanger (250). The compressor receives and compresses a first medium in accordance with power provided by the turbine via the shaft. The turbine receives and expands a second medium to provide the power to the compressor via the shaft. The heat exchanger is configured to cool the first medium.

87. 发明授权

EP2928592B1 A REACTION PUMP FOR HYDROCARBON CONVERSION 有权
标题翻译：一种用于烃转化的反应泵
公开(公告)号：EP2928592B1
公开(公告)日：2018-04-04
申请号：EP13831971.0
申请日：2013-12-07
申请人： Ecofuel Technologies Ltd
发明人： GUENTHER, Thomas Andreas
IPC分类号： B01F5/10 , C10G11/16 , C10G15/08 , F04D25/04 , B01J19/00 , B01J19/18
CPC分类号： F04D25/045 , B01F5/10 , B01J19/0066 , B01J19/0073 , B01J19/1806 , B01J2219/0006 , B01J2219/00189 , C10G11/16 , C10G15/08 , C10G2300/40 , C10G2400/02 , C10G2400/04 , C10G2400/08
摘要： Reaction pumps and systems for hydrocarbon conversion are disclosed. A reaction pump for conversion of hydrocarbons has a housing, a reaction chamber enclosed by the housing, for containment of a hydrocarbon process fluid or liquid reactant, a mixing element disposed inside the reaction chamber, the mixing element coupled to a rotatable shaft, and a plurality of bearings receiving the shaft, each bearing being disposed outside the reaction chamber. At least one of the bearings is closest to the reaction chamber. A type of barrier is disposed between the reaction chamber and the closest bearing, for fluidically separating the reactant from the closest bearing. This barrier can take the form of a seal protection chamber. A system for hydrocarbon conversion includes the reaction pump and an additional circuit for cleaning and recycling process fluid or liquid.

88. 发明公开

EP3165775A4 COMPRESSOR COVER, CENTRIFUGAL COMPRESSOR, AND SUPERCHARGER, AND COMPRESSOR COVER MANUFACTURING METHOD 有权
公开(公告)号：EP3165775A4
公开(公告)日：2018-02-14
申请号：EP14896487
申请日：2014-07-03
申请人： MITSUBISHI HEAVY IND ENGINE & TURBOCHARGER LTD
发明人： OZAKI MAKOTO , SUZUKI HIROSHI , WAKASHIMA KOJI , TOMITA ISAO , KANZAKA TADASHI
IPC分类号： F04D29/42 , F02B33/40 , F04D17/10 , F04D25/04 , F04D27/02 , F04D29/44 , F04D29/62 , F04D29/68 , F04D29/70
CPC分类号： F04D29/66 , F02B33/40 , F04D17/10 , F04D25/045 , F04D27/02 , F04D27/0215 , F04D27/023 , F04D27/0238 , F04D29/4213 , F04D29/44 , F04D29/441 , F04D29/62 , F04D29/624 , F04D29/685 , F04D29/701 , F05D2220/40 , F05D2250/51
摘要： Provided is a compressor cover that covers a delivery fan which outwardly discharges in the radial direction a fluid sucked in from an axial direction by rotating around the axis, the compressor cover comprising: a cover body that includes a tubular part in which a tubular inner peripheral surface along the axis and a shroud surface that is disposed on an axially downstream side of the tubular inner peripheral surface and expands in diameter toward the downstream side are formed; and a sleeve that includes an outer tube having an outer peripheral surface that is fixed to the tubular inner peripheral surface, an inner tube that is disposed on a radially inner side of the outer tube and defines a recirculation flow path in which a portion of the fluid that is sucked in by the delivery fan circulates between the inner tube and the outer tube, and a plurality of struts that are disposed at intervals in the peripheral direction so as to connect the outer tube and the inner tube, thereby partitioning the recirculation flow path into a plurality of sections.

89. 发明公开

EP3182490A1 INTEGRATED FUEL CELL AIRCRAFT PRESSURIZATION AND COOLING SYSTEM 有权转让
标题翻译：综合燃料电池飞机加压和冷却系统
公开(公告)号：EP3182490A1
公开(公告)日：2017-06-21
申请号：EP16202222.2
申请日：2016-12-05
申请人： Hamilton Sundstrand Corporation
发明人： LENTS, Charles E. , RHEAUME, Jonathan
IPC分类号： H01M8/04089 , H01M8/04111 , H01M8/04082 , B64D13/06 , F04D25/06 , F04D29/28 , B64D41/00
CPC分类号： H01M8/04111 , B64D13/02 , B64D13/06 , B64D15/04 , B64D37/32 , B64D2013/0607 , B64D2013/0618 , B64D2013/0644 , B64D2013/0648 , B64D2013/0651 , B64D2041/005 , F04D25/045 , F04D25/06 , F04D29/284 , H01M8/04097 , H01M8/04201 , H01M2250/20 , H01M2250/407 , Y02E60/563 , Y02T50/44 , Y02T50/54 , Y02T50/56 , Y02T90/32 , Y02T90/36
摘要： According to one embodiment of this disclosure an integrated fuel cell and environmental control system (30) includes a turbo-compressor (32). The turbo-compressor includes a rotatable shaft (40, a compressor (34) rotatable with the shaft (40) to generate a flow of compressed air, a motor (36) connected to the shaft (40), and a turbine (38) connected to the shaft (40). The system further includes a fuel cell (10A, 10B) connected to the compressor by a first compressed air supply line that supplies a first portion of the flow of compressed air to the fuel cell. The fuel cell (10A, 10B) is connected to the turbine (38) by a fuel cell exhaust line that supplies a flow of fuel cell exhaust to the turbine (38) and causes the turbine (38) to rotate. The system further includes an environmental control system (56) connected to the compressor by a second compressed air supply line that supplies a second portion of the flow of compressed air to the environmental control system (56).
摘要翻译：根据本公开的一个实施例，集成燃料电池和环境控制系统（30）包括涡轮压缩机（32）。涡轮压缩机包括可旋转的轴（40，与轴（40）一起旋转以产生压缩空气流的压缩机（34），连接到轴（40）的电动机（36）以及涡轮机（38）所述系统还包括通过第一压缩空气供应管线连接到所述压缩机的燃料电池（10A，10B），所述第一压缩空气供应管线将所述压缩空气流的第一部分供应到所述燃料电池，所述燃料电池（10A，10B）通过向燃气轮机（38）供给燃料电池排气流而使涡轮（38）旋转的燃料电池排气管路与涡轮（38）连接，该系统还包括环境控制通过第二压缩空气供应管线连接到所述压缩机的系统（56），所述第二压缩空气供应管线将所述压缩空气流的第二部分供应到所述环境控制系统（56）。

90. 发明公开

EP3176440A1 METHOD FOR CONTROLLING A TRIM-ADJUSTMENT MECHANISM FOR A CENTRIFUGAL COMPRESSOR 有权转让
标题翻译：用于控制离心压缩机的调整机构的方法
公开(公告)号：EP3176440A1
公开(公告)日：2017-06-07
申请号：EP16196440.8
申请日：2016-10-28
申请人： Honeywell International Inc.
发明人： HOUST, Vit , SMITH, William Joseph
IPC分类号： F04D27/02
CPC分类号： F04D29/464 , F01D17/165 , F02B37/183 , F04D25/045 , F04D27/0253 , F04D29/284 , F04D29/4206 , F05D2220/40 , Y02T10/144
摘要： A method for controlling an inlet-adjustment mechanism in an air inlet for a compressor so as to switch the mechanism in a binary fashion between two positions P1 and P2 for adjusting a flow area of the inlet. The method includes identifying a threshold line on a compressor map of pressure ratio versus corrected flow rate for the compressor. The threshold line is a line on which the pressure ratio and flow rate of the compressor are the same for the P1 and P2 positions of the inlet-adjustment mechanism at equal speeds. When the operating point of the compressor on the compressor map crosses the threshold line, the inlet-adjustment mechanism is switched from one of its binary positions to the other.
摘要翻译：一种用于控制压缩机的空气入口中的入口调整机构的方法，以在二个位置P1和P2之间以二元方式切换机构以调整入口的流动面积。该方法包括识别压缩机的压力比图上的阈值线，所述压力比针对压缩机的压力比与校正的流量比。阈值线是在相同速度下压缩机的压力比和流量对于进口调节机构的P1和P2位置相同的线。当压缩机图上的压缩机的操作点越过阈值线时，进口调节机构从其二进制位置之一切换到另一位置。

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