公开(公告)号：US20040175269A1

公开(公告)日：2004-09-09

申请号：US10791738

申请日：2004-03-04

申请人： Halla Climate Control Corporation

发明人： Kyungseok Cho ,  Seyoung Park ,  Changho Park

IPC分类号： F03B001/00

CPC分类号： F04D29/384

摘要： This present invention relates to an axial-flow fan including a central hub connected with a driving shaft of a motor, and a plurality of blades extending radially along the circumference of the hub for blowing air toward an axial direction, the plurality of blades integrated with the hub into a single body, wherein assuming that a camber ratio at a blade root(cr1) of each blade is the value obtained by dividing a maximum camber value at the blade root into a chord length, a camber ratio at a blade tip(cr2) of each blade is the value obtained by dividing a maximum camber value at the blade tip into the chord length, and a percentage of decrease of the camber ratio is the value obtained by dividing a difference value between the camber ratio at the blade root(cr1) and the camber ratio at the blade tip(cr2) into the camber ratio at the blade root(cr1), the percentage of decrease of the camber ratio is in a range between 33% and 85%.

摘要翻译： 本发明涉及一种轴流风扇，其包括与电动机的驱动轴连接的中心轮毂，以及沿着毂的圆周径向延伸的多个叶片，用于朝向轴向吹送空气，所述多个叶片与 所述轮毂形成单个主体，其中假设每个叶片的叶根（cr1）处的外倾比是通过将叶根处的最大外倾值除以弦长而获得的值，叶尖处的外倾比 每个叶片的cr2）是通过将叶尖处的最大外倾值除以弦长而获得的值，并且外倾比的减小百分比是通过将叶片根的外倾比除以差值而获得的值 （cr1）和叶尖处的外倾比（cr2）变成叶根（cr1）的外倾比，外倾比的下降百分比在33％〜85％的范围内。

公开(公告)号：US20040141840A1

公开(公告)日：2004-07-22

申请号：US10651825

申请日：2003-08-29

发明人： Kuo-Cheng Lin ,  Wen-Shi Huang

IPC分类号： F03B001/00

CPC分类号： F04D29/646 ,  F04D29/023 ,  F05D2300/121 ,  F05D2300/16 ,  F05D2300/43

摘要： A fan housing assembly includes a mounting base formed with a through hole thereon and a bushing. The bushing has a sleeve and is coupled to the mounting base by connecting the sleeve to the through hole. The mounting base and the bushing can be separately formed with predetermined materials in view of the different quality requirements before being assembled, thus resulting in lower manufacturing cost and enhanced flexibility in the fan design.

摘要翻译： 风扇壳体组件包括在其上形成有通孔的安装基座和衬套。 衬套具有套筒并且通过将套筒连接到通孔而联接到安装基座。 考虑到组装之前的不同质量要求，安装基座和衬套可以分开形成预定材料，从而降低制造成本并提高风扇设计的灵活性。

公开(公告)号：US20040126232A1

公开(公告)日：2004-07-01

申请号：US10646025

申请日：2003-08-22

发明人： Kuo-cheng Lin ,  Wen-shi Huang ,  Hsiou-chen Chang

IPC分类号： F03B001/00

CPC分类号： H02K1/30 ,  F04D25/0613 ,  F04D29/329 ,  H02K7/14

摘要： A rotor assembly includes a housing and a hub. The housing has an open end and an opposed closed end, and is formed with a raised portion in the central location of the closed end. The hub is mounted on the closed end of the housing and covers the housing except for the raised portion to construct a thin motor.

摘要翻译： 转子组件包括壳体和轮毂。 壳体具有开口端和相对的封闭端，并且在封闭端的中心位置形成有凸起部分。 轮毂安装在壳体的封闭端，并且除了凸起部分之外还覆盖壳体以构成薄的马达。

公开(公告)号：US20040076517A1

公开(公告)日：2004-04-22

申请号：US10612116

申请日：2003-07-02

申请人： Minebea Co., Ltd.

发明人： Kaoru Matsumoto ,  Shuichi Otsuka

IPC分类号： F03B001/00

CPC分类号： H05K7/20172 ,  H05K7/2019

摘要： An apparatus for a serial ventilation device that increases airflow compared to conventional devices without increasing the size is presented. The first ventilator is mounted on the intake opening side of the serial ventilation device, with the front surface of its blades facing the air intake side. The second ventilator is mounted on the exhaust opening side of the serial ventilation device, with the front surface of its blades facing the air exhaust side. Thus a first ventilator, which ventilates from the rear side of the blades, and a second ventilator, which ventilates from the front side of the blades, operate when the ventilation side of the blades are facing the same direction and rotating in the same direction. Both ventilators are connected serially such that their rotation shafts are positioned in the same straight line, while the number of blades of the two ventilators are different.

摘要翻译： 提出了一种用于连续通风装置的装置，其与常规装置相比增加了气流而不增加尺寸。 第一通风机安装在串联通气装置的进气口侧，其叶片的前表面面向进气侧。 第二通风机安装在串联通风装置的排气口侧，其叶片的前表面面向排气侧。 因此，当叶片的通风侧面向相同的方向并沿相同的方向旋转时，从叶片的后侧通风的第一通风机和从叶片的前侧通风的第二通风机运行。 两个通风机串联连接，使得它们的旋转轴位于相同的直线上，而两个通气机的叶片数量不同。

公开(公告)号：US20030206799A1

公开(公告)日：2003-11-06

申请号：US10425639

申请日：2003-04-30

发明人： John M. Scott

IPC分类号： F03B001/00

CPC分类号： F04D29/164 ,  F01D9/04 ,  F01D11/122 ,  F01D25/24 ,  F04D29/542

摘要： A casing section (30) for rotary apparatus (13, 14) of a gas turbine engine (10) is described. The casing section (30) comprises a partially circumferential casing member (32) and a plurality of radially inwardly extending vanes (34) fixed on the casing member (32).

摘要翻译： 描述了一种用于燃气涡轮发动机（10）的旋转设备（13,14）的壳体部分（30）。 壳体部分（30）包括部分圆周的壳体构件（32）和固定在壳体构件（32）上的多个径向向内延伸的叶片（34）。

公开(公告)号：US20030123977A1

公开(公告)日：2003-07-03

申请号：US09878027

申请日：2001-06-08

发明人： Karl-Heinz Bertnik ,  Volker Doring ,  Hans-Dieter Hensel ,  Peter Schick

IPC分类号： F03B001/00 ,  F01D017/16

CPC分类号： F02B37/025 ,  F01D5/28 ,  F01D17/141 ,  F02B37/22 ,  F02B39/00 ,  F05D2250/15 ,  F05D2250/25 ,  Y02T10/144

摘要： An exhaust-gas turbine for a turbocharger includes a rotor mounted rotatably in a turbine casing having a spiral inlet duct which is followed by an annular space surrounding the rotor. A guide-blade cascade is capable of being pushed axially into the annular space near the outer circumference of the rotor. The guide-blade cascade includes guide blades, is guided in an annular gap between an inner part and the turbine casing and is axially displaceable via an axial slide by a sliding sleeve. The guide-blade cascade with the axial slide, the inner part and/or the sliding sleeve are produced from an austenitic cast steel material having the following components: Cnull0.2%; Si 1.5-2.5%; Mnnull2.00%; Pnull0.045%; Snull0.03%; Cr 24.0-26.0%; Ni 19-22%; and Wnull5%.

摘要翻译： 用于涡轮增压器的废气涡轮机包括可旋转地安装在具有螺旋入口管道的涡轮机壳体中的转子，其后面是围绕转子的环形空间。 引导叶片级联能够被轴向推入靠近转子外圆周的环形空间。 引导叶片级联包括导向叶片，在内部部分和涡轮机壳体之间的环形间隙中被引导，并且通过滑动套筒通过轴向滑动件可轴向移动。 具有轴向滑动件，内部部件和/或滑动套筒的导向叶片级联由具有以下部件的奥氏体铸钢材料制成：C <= 0.2％; Si 1.5-2.5％; Mn <= 2.00％; P <= 0.045％; S <= 0.03％; Cr 24.0-26.0％; 倪19-22％; W <= 5％。

公开(公告)号：US20030082051A1

公开(公告)日：2003-05-01

申请号：US10283279

申请日：2002-10-30

申请人： SNECMA MOTEURS

发明人： Jean-Louis Bertrand ,  Jean-Marc Claude Perrollaz

IPC分类号： F03B001/00

CPC分类号： F01D25/246 ,  F01D9/042 ,  F04D29/542

摘要： The invention relates to a fixed guide vane assembly comprising a circular casing composed of at least two parts (11) and supporting sectors (5), each composed of an inner segment (7) and an outer segment (6) connected by vanes (8). The parts of the casing and the sectors of the guide vane assembly are held together by a system forming a slide and a slider. Anti-rotation means (30) are provided to prevent the sectors from rotating with respect to the casing.

摘要翻译： 本发明涉及一种固定导向叶片组件，其包括由至少两个部分（11）和支撑扇区（5）组成的圆形壳体，每个部分由内部段（7）和外部段（6）组成，所述内部段（7）和叶片（8） ）。 壳体的部件和导叶组件的扇区通过形成滑块和滑块的系统保持在一起。 提供防旋转装置（30）以防止扇区相对于壳体旋转。

公开(公告)号：US20030002982A1

公开(公告)日：2003-01-02

申请号：US10180029

申请日：2002-06-27

发明人： Kouichi Irie ,  Tomoyoshi Okamura ,  Yoshio Anzai ,  Junichi Kurokawa

IPC分类号： F03B001/00

CPC分类号： F01D11/08 ,  F01D11/22 ,  F04D3/00 ,  F04D15/0027 ,  F04D27/0215 ,  F04D29/528 ,  F04D29/547 ,  F04D29/685 ,  F04D29/688

摘要： In an axial flow hydraulic machine, a plural number of grooves 5 are formed on an inner surface of a casing, directed into a pressure gradient direction, for connecting between an inlet side of an impeller 1 and an inside of blade residing region on the casing inner surface. With movement of movable members 6 provided on the casing inner surface, the grooves appear within the blade residing region in an unstable operation region, while the grooves cause no interference with the blades of the impeller in a stable operation region.

摘要翻译： 在轴流式液压机中，在壳体的内表面上形成有多个槽5，该槽指向压力梯度方向，用于连接叶轮1的入口侧和壳体上的叶片驻留区域的内部 内表面。 随着设置在壳体内表面上的活动件6的运动，凹槽在不稳定的操作区域内出现在刀片停留区域内，而沟槽在稳定的操作区域中不会干扰叶轮的叶片。

公开(公告)号：US20010033792A1

公开(公告)日：2001-10-25

申请号：US09853569

申请日：2001-05-14

发明人： Yoshihiro Nagaoka ,  Sadashi Tanaka ,  Yukiji Iwase ,  Michiaki Ida ,  Hirotoshi Ishimaru ,  Saburo Iwasaki ,  Yoshiharu Ueyama ,  Tetuya Yoshida

IPC分类号： F03B001/00 ,  F01D001/02

CPC分类号： F04D29/669 ,  F04D1/06 ,  F04D29/2216 ,  F04D29/422 ,  F04D29/428 ,  F04D29/444 ,  F04D29/448 ,  F04D29/661 ,  F04D29/663 ,  F05B2260/96 ,  F05D2240/121 ,  F05D2240/304 ,  F05D2250/52

摘要： At a vaned diffuser or a volute casing of a centrifugal fluid machine, pressure pulsation and vibrating forces acting upon the diffuser or the volute casing are mitigated or cancelled so as to abate the noise from the centrifugal fluid machine. The fluid machine having an impeller 3 rotating about a rotating shaft 2 within a casing 1 and having a vaned diffuser 4 or volute 12 fixed to the casing 1 is constructed such that radius of the vane trailing edge of the impeller 3 and radius of the vane leading edge of the diffuser 4 or radius of the volute tongue is varied in the direction of axis of rotation and inclinations, on a meridional plane, of the vane trailing edge of the impeller 3 and the vane leading edge of the diffuser 4 or the volute tongue are set in the same orientation, thereby reduction in head and efficiency or occurrence of an axial thrust may be restrained to the extent possible to optimally abate the noise and pressure pulsation of the centrifugal fluid machine.

摘要翻译： 在离心式流体机械的叶片扩散器或蜗壳上，作用在扩散器或涡壳壳体上的压力脉动和振动力被减轻或消除，从而减轻离心流体机器的噪音。 具有围绕壳体1内的旋转轴2旋转并且具有固定到壳体1的带叶片的扩散器4或蜗壳12的叶轮3的流体机构被构造成使得叶轮3的叶片后缘的半径和叶片的半径 扩散器4的前缘或蜗壳舌的半径在叶轮3的叶片后缘和扩散器4的叶片前缘或蜗壳的经向平面上的旋转轴线和倾斜方向上变化 舌头被设置在相同的方向上，从而可以在可能的程度上限制头部和效率的降低或轴向推力的发生，以最佳地消除离心式流体机械的噪声和压力脉动。

公开(公告)号：US20040265124A1

公开(公告)日：2004-12-30

申请号：US10610130

申请日：2003-06-30

发明人： Hsin-Tuan Liu ,  William Andrew Bailey ,  John Doane Niedermeier

IPC分类号： F03B001/00

CPC分类号： F04D29/668 ,  F01D5/26 ,  F01D9/041 ,  F04D29/544 ,  F04D29/666 ,  F05D2260/961 ,  Y02T50/671 ,  Y10T29/49323

摘要： A method of assembling a gas turbine engine includes coupling an inner engine casing to an outer engine casing such that an annular flow path is defined therebetween, coupling a plurality of circumferentially-spaced support struts between the inner and outer casings, and coupling a plurality of circumferentially-spaced outlet guide vanes within the flow path upstream from the support struts, such that a first circumferential spacing is defined between a first guide vane and a second guide vane, and a second circumferential spacing is defined between the second guide vane and a third guide vane. The guide vanes are arranged such that the second guide vane is between the first and third guide vanes and the second circumferential spacing is different from the first circumferential spacing.

摘要翻译： 一种组装燃气涡轮发动机的方法包括将内部发动机壳体联接到外部发动机壳体，使得在其间限定环形流动路径，将多个周向间隔开的支撑支柱联接在内部壳体和外部壳体之间，以及将多个 在支撑支柱的上游的流动路径内的周向间隔的出口导向叶片，使得在第一导向叶片和第二导向叶片之间限定第一周向间隔，并且第二周向间隔限定在第二导叶和第三导叶之间 导叶。 引导叶片布置成使得第二导叶位于第一和第三导叶之间，第二周向间隔与第一周向间隔不同。