公开(公告)号：US11892012B2

公开(公告)日：2024-02-06

申请号：US18052924

申请日：2022-11-06

申请人： MTU Aero Engines AG

发明人： Andreas Hoelzel ,  Christian Roth ,  Franz Prieschl ,  Josef Eichner ,  Mike Mosbacher ,  Vitalis Mairhanser

IPC分类号： F04D29/56 ,  F01D17/16 ,  F04D19/02 ,  F02C3/06

CPC分类号： F04D29/563 ,  F01D17/162 ,  F04D19/022 ,  F02C3/064

摘要： An adjustable guide vane for a compressor, in particular a high-pressure compressor, of a gas turbine, in particular an aircraft gas turbine is described, the vane comprising a radially outer bearing section, a radially inner bearing section, and a vane section, which extends in the radial direction between the outer bearing section and the inner bearing section, wherein the outer and the inner bearing sections are designed in such a way that the adjustable guide vane can be taken up rotatably about a vane axis in the compressor, and wherein the radially inner bearing section is configured like a journal (cone-shaped) and has a lateral surface that is formed circumferentially about the vane axis, the lateral surface being of convex shape. In this way, it is provided that the radius of curvature of the convex lateral surface is at least double the maximum diameter of the bearing section.

公开(公告)号：US20230235740A1

公开(公告)日：2023-07-27

申请号：US18125637

申请日：2023-03-23

申请人： Vetco Gray Scandinavia AS

发明人： Giacomo Landi ,  Vittorio Michelassi ,  Matteo Dozzini ,  Francesco Cangioli ,  Massimiliano Borghetti

IPC分类号： F04D19/02 ,  F04D25/02 ,  F04D13/06 ,  H02K3/46 ,  H02K7/14 ,  F04D29/58 ,  F04D25/06 ,  H02K21/22 ,  H02K21/14 ,  H02K1/12 ,  H02K1/22 ,  H02K16/00 ,  H02K1/16

CPC分类号： F04D19/022 ,  F04D13/06 ,  F04D19/024 ,  F04D19/026 ,  F04D25/02 ,  F04D25/0606 ,  F04D29/588 ,  H02K1/12 ,  H02K1/16 ,  H02K1/22 ,  H02K3/46 ,  H02K7/14 ,  H02K16/00 ,  H02K21/14 ,  H02K21/22

摘要： A compressor or pump stage is provided. The compressor or pump stage at least comprising a central shaft (8) and one rotor (3), where the axis of rotation of the rotor (3) is the central shaft (8) and where the rotor comprises a number, n, of rows of impellers (5) arranged at an outer perimeter of the rotor with an axial distance between neighbouring rows of impellers (5), where n={2, 3, 4...}.

公开(公告)号：US20180112675A1

公开(公告)日：2018-04-26

申请号：US15793070

申请日：2017-10-25

申请人： MAN Truck & Bus AG

发明人： Andreas Neff ,  Christian Gell

IPC分类号： F04D29/32 ,  F04D29/58 ,  B60H1/00 ,  B60H1/32

CPC分类号： F04D29/329 ,  B60H1/00035 ,  B60H1/3229 ,  F04D19/022 ,  F04D25/082 ,  F04D29/281 ,  F04D29/34 ,  F04D29/5833

摘要： An axial fan wheel, in particular for the radiator of a motor vehicle engine, is described. The axial fan wheel includes a crown ring having a multiplicity of rotor blades, a hub having an inner ring which is connected or connectable to a drive shaft, and having, for the purpose of torque transmission, connection surfaces along an outer periphery of the hub which are connected to the inner ring and to the crown ring. The hub has through-passages between the inner ring and the outer periphery. At least one element, arranged rotationally fixedly on the axial fan wheel inside the crown ring, is designed to maintain a pressure difference in the axial direction when the axial fan wheel rotates.

公开(公告)号：US20160298633A1

公开(公告)日：2016-10-13

申请号：US15038594

申请日：2014-11-07

申请人： UNITED TECHNOLOGIES CORPORATION

发明人： Crystal LaBoudy ,  Mark R. Wood ,  Brittany Travis

IPC分类号： F04D19/02 ,  F04D27/00

CPC分类号： F04D19/022 ,  F01D17/162 ,  F04D27/002 ,  F04D29/563 ,  Y02T50/671

摘要： A variable vane assembly comprises an upstream vane stage including an airfoil coupled with an upstream vane stem and an upstream vane arm, configured to drive the upstream vane stem to rotate. The upstream vane stem is supported in an upstream housing boss. A downstream vane stage includes an airfoil coupled with a downstream vane stem and a downstream vane arm, and configured to drive the downstream vane stem to rotate. The downstream vane stem is supported in a downstream housing boss. A first clearance is defined between a radially inner end of the upstream vane arm and a radially outer end of the upstream housing boss. A second clearance is defined between a radially inner end of the downstream vane arm and a radially outer end of the downstream housing boss. A clearance ratio of the second clearance to the first clearance is greater than or equal to 10.

摘要翻译： 可变叶片组件包括上游叶片台，其包括与上游叶片杆和上游叶片臂联接的翼型件，构造成驱动上游叶片杆旋转。 上游叶片杆支撑在上游壳体凸台中。 下游叶片级包括与下游叶片杆和下游叶片臂联接的翼型件，并且构造成驱动下游叶片杆旋转。 下游叶片杆支撑在下游壳体凸台中。 在上游叶片臂的径向内端和上游壳体凸起的径向外端之间限定第一间隙。 第二间隙限定在下游叶片臂的径向内端和下游壳体凸起的径向外端之间。 第二间隙与第一间隙的间隙比大于或等于10。

公开(公告)号：US20160025108A1

公开(公告)日：2016-01-28

申请号：US14808256

申请日：2015-07-24

申请人： Techspace Aero S.A.

发明人： Eric Englebert

IPC分类号： F04D29/64 ,  F04D19/02

CPC分类号： F04D29/644 ,  F01D9/042 ,  F01D11/001 ,  F04D19/022 ,  F04D29/083 ,  F04D29/102 ,  F04D29/542

摘要： The present application relates to a stator of an axial turbomachine compressor. The stator includes a circular wall, such as an internal shroud, with a guiding surface in order to guide the primary flow of the turbomachine. The stator further includes a circular row of stator vanes, each of them including an airfoil which extends radially in the primary flow of the turbomachine, and a securing portion. The securing portion of the vane includes a lattice which has rods and which is secured and/or sealed in the shroud in order to fix the vanes to the shroud via the lattices. The stator includes a joint of abradable material which is arranged inside the internal shroud, and in which the lattice is secured in order to ensure retention, a fixing between the vane and the internal shroud. The vane is produced by means of additive production.

摘要翻译： 本申请涉及一种轴向涡轮机压缩机的定子。 定子包括诸如内部护罩的圆形壁，其具有引导表面，以便引导涡轮机的初级流动。 定子还包括一排定子叶片，它们中的每一个包括在涡轮机主流中径向延伸的翼型件和固定部分。 叶片的固定部分包括具有杆并且固定和/或密封在护罩中的格子，以便经由晶格将叶片固定到护罩上。 定子包括可磨损材料的接合部，该接头布置在内部护罩的内部，并且格子被固定在其中以确保保持力，在叶片和内部护罩之间固定。 叶片通过添加剂生产生产。

公开(公告)号：US20150063982A1

公开(公告)日：2015-03-05

申请号：US14475347

申请日：2014-09-02

申请人： Particles Plus, Inc.

发明人： David PARISEAU ,  Craig D. Adams

IPC分类号： F04D19/02 ,  G01N21/49 ,  G01N15/14

CPC分类号： F04D19/022 ,  G01N15/1404 ,  G01N2015/1486

摘要： An airborne, gas particle counter, includes an inflow multiple stage turbine pump inducing flow through a particle counter. The turbine pump includes a rotor and stator assemblies and establishes gas flow through a second housing, which defines a view volume where particles are counted by light scattering or obscuration of a beam intersecting the light flow path. Intersecting rotor and stator assemblies limit particles to those suspended in the gas flow. The pump assembly includes integral flow paths limiting the need for external tubing.

摘要翻译： 空气中的气体颗粒计数器包括引入流过颗粒计数器的流入多级涡轮泵。 涡轮泵包括转子和定子组件，并且建立通过第二壳体的气流，其限定了通过与光流动路径相交的光束的光散射或遮蔽而对颗粒进行计数的视图体积。 相交的转子和定子组件将颗粒限制在悬浮在气体流中的颗粒。 泵组件包括限制对外部管道的需要的整体流动路径。

公开(公告)号：US08807969B2

公开(公告)日：2014-08-19

申请号：US13282981

申请日：2011-10-27

申请人： Shun-Chen Chang ,  Chia-Ming Hsu ,  Bo-Chun Chen

发明人： Shun-Chen Chang ,  Chia-Ming Hsu ,  Bo-Chun Chen

IPC分类号： F04D25/06 ,  F04D25/16 ,  F04D19/02 ,  F04D25/12

CPC分类号： F04D19/022 ,  F04D19/026 ,  F04D25/0613 ,  F04D25/12

摘要： A fan assembly includes a housing, a first frame, a second frame, at least one driving device, a supporting device, an active impeller and a passive impeller. The housing has an air-flowing channel, and the first frame and second frame are disposed at opposite sites of the air-flowing channel. The driving device is disposed on the first frame and actuates the active impeller to rotate. The supporting device is disposed on the second frame and has the passive impeller thereon. The passive impeller is propelled by the airflow generated by the active impeller.

摘要翻译： 风扇组件包括壳体，第一框架，第二框架，至少一个驱动装置，支撑装置，主动叶轮和被动叶轮。 壳体具有空气流动通道，第一框架和第二框架设置在空气流动通道的相对位置处。 驱动装置设置在第一框架上并致动主动叶轮旋转。 支撑装置设置在第二框架上并且在其上具有被动叶轮。 被动叶轮由主动叶轮产生的气流推动。

公开(公告)号：US20060204371A1

公开(公告)日：2006-09-14

申请号：US11374179

申请日：2006-03-14

申请人： Stefan Rexhauser ,  Andreas Foerster

发明人： Stefan Rexhauser ,  Andreas Foerster

IPC分类号： F04B25/00

CPC分类号： H02K9/06 ,  F04D19/022 ,  F04D29/281

摘要： An air-cooled electric motor is provided, which may be used in a compressor assembly, including a motor unit with a motor housing out of which a drive shaft extends, such that the drive shaft drives a ventilator, the ventilator includes at least two radially and/or axially separated ventilator sections to propel a first airstream as well as at least one other, second airstream that is separate from the first airstream, such that the airstreams are conducted separately on both the inflow side of the ventilator and the outflow side of the ventilator.

摘要翻译： 提供了一种风冷电动机，其可以用在压缩机组件中，包括具有马达壳体的马达单元，驱动轴延伸穿过该马达壳体，使得驱动轴驱动呼吸机，通气机包括至少两个径向 和/或轴向分离的呼吸机部分以推进第一气流以及与第一气流分离的至少一个其它第二气流，使得气流在通气机的流入侧和流出侧的两侧分别导入 呼吸机。

公开(公告)号：US4012165A

公开(公告)日：1977-03-15

申请号：US638883

申请日：1975-12-08

申请人： Alfred Henry Kraig

发明人： Alfred Henry Kraig

IPC分类号： F04D19/02 ,  F04D21/00 ,  F01D17/00

CPC分类号： F04D19/022 ,  F04D21/00 ,  F05D2240/302 ,  Y02T50/673 ,  Y10T137/0536

摘要： A fan structure which is particularly well suited for use in a high tip speed turbofan, gas turbine engine is disclosed. Various construction details accommodate both subsonic and supersonic flow across the fan blades. The system is built around compression shock wave phenomenon which are utilized to stably convert a portion of the dynamic energy of a supersonic stream to pressure energy within a subsonic stream.

摘要翻译： 公开了一种特别适用于高速涡轮风扇燃气轮机的风扇结构。 各种构造细节适应风扇叶片上的亚音速和超音速流动。 该系统围绕压缩冲击波现象建立，用于将超音速流的一部分动态能量稳定地转换成亚音速流内的压力能量。

公开(公告)号：US1259430A

公开(公告)日：1918-03-12

申请号：US13333016

申请日：1916-11-25

申请人： MONSON JOENS

发明人： MONSON JOENS

CPC分类号： F04D19/022