公开(公告)号：US07534087B2

公开(公告)日：2009-05-19

申请号：US10561278

申请日：2004-05-27

Applicant: Dieter Minninger

Inventor： Dieter Minninger

IPC: F01D5/08 ,  F01D5/18

CPC classification number: F01D5/08 ,  F01D5/084 ,  F01D5/085 ,  F01D25/10 ,  Y02T50/676

Abstract: The invention relates to a turbo-machine, in particular to a gas turbine and to a method for accelerating a temperature modification of a rotor shaft rotationally mounted in said turbo-machine. The aim of said invention is to develop a device and a method for the turbo-machine making it possible to reduce the size of a radial split of the turbo-machine in order to obtain greater degree of efficiency. The inventive turbo-machine comprises a rotor rotationally mounted in the case of the turbo-machine, a feeding channel embodied in the rotor for introducing a fluid and an outlet channel embodied in the rotor for removing said fluid. An inlet orifice of the feeding channel is disposed further inside than the outlet orifice of the outlet channel, and an actuating device dependent on centrifugal force is provided.

Abstract translation: 涡轮机技术领域本发明涉及一种涡轮机，特别涉及一种燃气轮机，以及用于加速旋转安装在所述涡轮机中的转子轴的温度变化的方法。 本发明的目的在于开发一种用于涡轮机的装置和方法，使得可以减小涡轮机径向分段的尺寸，以获得更高的效率。 本发明的涡轮机包括旋转地安装在涡轮机的壳体中的转子，在转子中实现的用于引入流体的进料通道和实施在转子中的用于去除所述流体的出口通道。 进料通道的入口孔设置在出口通道的出口孔的内侧，并且提供依赖于离心力的致动装置。

公开(公告)号：US20070119176A1

公开(公告)日：2007-05-31

申请号：US11557863

申请日：2006-11-08

Applicant: Bradley Ingham ,  Steven Barber

Inventor： Bradley Ingham ,  Steven Barber

IPC: F01K23/06

CPC classification number: F01D25/10 ,  F01D19/02 ,  F01K13/02 ,  F01K21/04

Abstract: A system and a method of augmenting the heat up of a unit using a compressed, heated gas that contains moisture such as steam or vaporized water such that the specific heat of the gas is increased. In a preferred embodiment, steam in compressed inert gas such as nitrogen is capable of augmenting the heat up cycle for units such as process reactor vessels, furnaces, process steam and power production boilers, turbines, and other production vessels.

Abstract translation: 使用包含诸如蒸汽或蒸发水的水分的压缩的加热气体来增加单元的加热的系统和方法，使得气体的比热增加。 在优选的实施方案中，压缩惰性气体如氮气中的蒸汽能够增加诸如过程反应器容器，熔炉，工艺蒸汽和发电生产锅炉，涡轮机和其它生产容器的单元的加热循环。

公开(公告)号：US20060162339A1

公开(公告)日：2006-07-27

申请号：US11278701

申请日：2006-04-05

Applicant: Andre Urso ,  George Durgin ,  Christopher Housley ,  George Moore ,  Harris Abramson ,  Robert Czachor

Inventor： Andre Urso ,  George Durgin ,  Christopher Housley ,  George Moore ,  Harris Abramson ,  Robert Czachor

IPC: F02C7/00

CPC classification number: F01D11/001 ,  F01D11/02 ,  F01D11/122 ,  F01D25/10 ,  F01D25/12 ,  Y02T50/672 ,  Y02T50/675

Abstract: A gas turbine engine component has an annular flange arm, a backing plate mounted to the flange arm and a bypass circuit formed between the flange arm and the backing plate. The bypass circuit includes one or more channels formed in one of the flange arm or the backing plate. When more than one channels are used, at least one connecting slot is provided between the channels. At least one inlet passage extends through the flange arm in fluid communication with the forward-most channel, and at least one outlet slot is formed between the flange arm and the backing plate in fluid communication with the aft-most channel.

Abstract translation: 燃气涡轮发动机部件具有环形凸缘臂，安装到凸缘臂的背板和形成在凸缘臂和背板之间的旁路电路。 旁路回路包括形成在凸缘臂或背板之一中的一个或多个通道。 当使用多个通道时，在通道之间提供至少一个连接槽。 至少一个入口通道延伸穿过法兰臂与最前面的通道流体连通，并且至少一个出口狭槽形成在法兰臂和背板之间，与最后一个通道流体连通。

公开(公告)号：US20020146317A1

公开(公告)日：2002-10-10

申请号：US10117079

申请日：2002-04-08

Applicant: MITSUBISHI HEAVY INDUSTRIES LTD.

Inventor： Tadateru Tanioka

IPC: F01D011/00

CPC classification number: F01D9/023 ,  F01D5/085 ,  F01D19/02 ,  F01D25/10 ,  F01D25/12 ,  F02C7/16 ,  F05D2240/10 ,  F05D2260/205 ,  F05D2260/2322 ,  F05D2260/85

Abstract: A vapor tube structure in a gas turbine comprises first connecting tubes fixed to a casing, second connecting tubes fixed to a blade ring, a recovery ring and a cooling recovery ring, a bellows tube of the flexible structure, springs, a tube and a piston rings provided between the first connecting tubes and the second connecting tubes. As a result, it is possible to absorb and follow the thermal expansion/contraction difference and prevent leaking of vapor.

Abstract translation: 燃气涡轮机中的蒸汽管结构包括固定在壳体上的第一连接管，固定在叶片环上的第二连接管，回收环和冷却回收环，柔性结构的波纹管，弹簧，管和活塞 环设置在第一连接管和第二连接管之间。 结果，可以吸收和跟随热膨胀/收缩差异并防止蒸汽泄漏。

公开(公告)号：US06382903B1

公开(公告)日：2002-05-07

申请号：US09741906

申请日：2000-12-22

Applicant: Philip M. Caruso ,  Sacheverel Quentin Eldrid ,  Azad A. Ladhani ,  Alan Richard DeMania ,  Gene David Palmer ,  Ian David Wilson ,  Lisa Shirley Rathbun ,  Robert Craig Akin

Inventor： Philip M. Caruso ,  Sacheverel Quentin Eldrid ,  Azad A. Ladhani ,  Alan Richard DeMania ,  Gene David Palmer ,  Ian David Wilson ,  Lisa Shirley Rathbun ,  Robert Craig Akin

IPC: F01D508

CPC classification number: F01D25/10 ,  F01D5/081 ,  F01D5/084 ,  F05D2260/205 ,  F05D2260/232 ,  F05D2260/2322 ,  Y02T50/676

Abstract: In a turbine having closed-circuit steam-cooling passages about the rim of the rotor during steady-state operation, compressor discharge air is supplied to the rotor bore for passage radially outwardly into the wheel space cavities between the wheels and spacers. Communicating slots and channels in the spacers and wheels at circumferentially spaced positions enable egress of the compressor discharge air into the hot gas flow path. At turbine startup, cooling air flows through the closed-circuit steam passages to cool the outer rim of the rotor while compressor discharge air pre-warms the wheels and spacers. At steady-state, cooling steam is supplied in the closed-circuit steam-cooling passages and compressor discharge air is supplied through the bore and into the wheel space cavities to cool the rotor.

Abstract translation: 在稳态运行期间，具有围绕转子边缘的闭路蒸汽冷却通道的涡轮机将压缩机排出空气供应到转子孔，以便径向向外通过到车轮和间隔件之间的车轮间隙中。 在间隔件和车轮上沿周向间隔开的位置沟通槽和通道使得压缩机排出空气能够排出到热气流路径中。 在涡轮启动时，冷却空气流过闭路蒸汽通道，以冷却转子的外缘，同时压缩机排出的空气预热了车轮和间隔件。 在稳定状态下，在闭路蒸汽冷却通道中供应冷却蒸汽，压缩机排放空气通过孔提供到车轮空间以冷却转子。

公开(公告)号：US20010005480A1

公开(公告)日：2001-06-28

申请号：US09761635

申请日：2001-01-18

Inventor： Yufeng Phillip Yu ,  Gary Michael Itzel ,  Victor H. S. Correia

IPC: F01D009/06 ,  F01D005/08 ,  F01D005/18 ,  F03D011/00 ,  F03B011/00 ,  F01D011/00 ,  F01D025/08 ,  F01D025/16 ,  F01D025/18 ,  F04D029/04

CPC classification number: F01D25/10 ,  F01D5/187 ,  F01D11/24 ,  F01D25/08 ,  F01D25/12 ,  F05D2240/81

Abstract: To control the temperature mismatch between the inner and outer bands and covers forming plenums with the inner and outer bands on sides thereof remote from the hot gas path, passages extend from the leading edge of the covers in communication with the hot gases of combustion to the trailing edge of the covers in communication with the hot gas flowpath. A mixing chamber is provided in each passage in communication with compressor discharge air for mixing the hot gases of combustion and compressor discharge air for flow through the passage, thereby heating the cover and minimizing the temperature differential between the inner and outer bands and their respective covers. The passages are particularly useful adjacent the welded or brazed joints between the covers and inner band portions.

Abstract translation: 为了控制内带和外带之间的温度失配，并且覆盖形成集气室，其侧壁上的内带和外带远离热气路径，通道从盖的前缘延伸，与燃烧的热气体连通 盖子的后缘与热气流路相通。 在每个通道中设置有与压缩机排放空气连通的混合室，用于混合燃烧的热气体和压缩机排放空气以流过通道，从而加热盖并最小化内带和外带之间的温差及其各自的盖 。 这些通道在盖和内带部分之间的焊接或钎焊接头附近特别有用。

公开(公告)号：US5172553A

公开(公告)日：1992-12-22

申请号：US823420

申请日：1992-01-21

Applicant: Serge P. Barton ,  Peter G. Smith

Inventor： Serge P. Barton ,  Peter G. Smith

IPC: F01D25/12 ,  F01D25/10 ,  F01K13/00

CPC classification number: F01D25/10 ,  F01K13/006

Abstract: A method and apparatus wherein, during time periods when a turbine is off-line and in a restart-ready condition, residual steam is circulated in the turbine between the cover and base of the turbine such that the cover and base are maintained at generally equal temperatures.

Abstract translation: 一种方法和装置，其中在涡轮机离线并且处于重新启动状态的时间段期间，残余蒸汽在涡轮机中在涡轮机的盖和基座之间循环，使得盖和基座保持在大致相等 温度。

公开(公告)号：US4688385A

公开(公告)日：1987-08-25

申请号：US694054

申请日：1985-01-23

Applicant: Naoaki Shibashita ,  Hajime Toriya ,  Kiyoshi Shimomura ,  Haruo Urushidani ,  Ryoichi Kaneko

Inventor： Naoaki Shibashita ,  Hajime Toriya ,  Kiyoshi Shimomura ,  Haruo Urushidani ,  Ryoichi Kaneko

IPC: F01D5/06 ,  F01D19/02 ,  F01D25/10 ,  F01K9/02 ,  F01K13/02

CPC classification number: F01K9/023 ,  F01D19/02 ,  F01D25/10

Abstract: A method of starting a turbine having a shrinkage-fitted rotor provided by shrinkage-fitting discs onto a shaft comprises the steps of raising the temperature of the rotor above a predetermined temperature determined from a physical value of the material constituting the rotor and, thereafter, raising the rotational speed of the turbine from the turning speed to the rated speed, whereby the centrifugal stress on raising the speed acts on the discs in a state wherein the value of fracture toughness of the discs fitted on to the shaft has increased.

Abstract translation: 将通过收缩配合盘提供的收缩配合转子的涡轮机起动到轴上的方法包括以下步骤：将转子的温度提高到由构成转子的材料的物理值确定的预定温度以下， 将涡轮机的转速从转速提高到额定速度，由此在安装在轴上的盘的断裂韧性值增加的状态下，提高速度的离心应力作用在盘上。

公开(公告)号：US4200784A

公开(公告)日：1980-04-29

申请号：US857481

申请日：1977-12-05

Applicant: Jacques E. Albaric ,  Forrest E. Coyle ,  Thomas P. Sherlock

Inventor： Jacques E. Albaric ,  Forrest E. Coyle ,  Thomas P. Sherlock

IPC: F01D5/08 ,  F01D25/10 ,  H05B3/00

CPC classification number: H05B3/0095 ,  F01D25/10

Abstract: A hollow, rotatable shaft bore heater assembly for heating a shaft from its inside to its outside. Rapid rotatable shaft heating is provided by a plurality of electrical heaters situated in slots formed on the inner surfaces of a plurality of foundation members which are insertable in the hollow shaft and are biased thereagainst by biasing structure. When assembled, the foundation members constitute a substantially cylindrical structure which has the slots formed on its inner surface and the electrical heaters are restrained within those axially extending and circumferentially separated slots by insulation disposed on the inner surface of the foundation members across the slots open mouths. The biasing structure provides biasing force between circumferentially adjacent foundation members so as to maintain contact between the shaft and foundation members during non-rotation of the shaft.

Abstract translation: 一种用于将轴从其内部加热到其外部的中空的可旋转轴孔加热器组件。 快速旋转轴加热由多个电加热器提供，多个电加热器位于形成在可插入中空轴中的多个基础构件的内表面上的狭槽中，并通过偏置结构偏压。 当组装时，基础构件构成基本上圆柱形的结构，其中在其内表面上形成有槽，并且电加热器被限制在这些轴向延伸和周向分隔的槽内，该绝缘体设置在基础构件的内表面上，穿过狭槽开口 。 偏置结构在周向相邻的基础构件之间提供偏压力，以便在轴的不旋转期间保持轴和基础构件之间的接触。

公开(公告)号：US3997758A

公开(公告)日：1976-12-14

申请号：US451248

申请日：1974-03-14

Applicant: Neville K. Patel

Inventor： Neville K. Patel

IPC: F01D9/02 ,  F01D9/04 ,  F01D25/10 ,  H05B3/00 ,  H05B1/00 ,  F01D5/08 ,  F04D29/58

CPC classification number: F01D25/10 ,  F01D9/041 ,  H05B3/00

Abstract: An axial flow elastic fluid turbine apparatus includes a rotor having an annular array of circumferentially spaced blades. A casing encircles the rotor and an annular array of circumferentially spaced stationary nozzle blades is fastened the casing and arranged to direct the elastic fluid against the blades of the rotor. An outer covering is disposed over the radially outermost half of at least one blade of the stationary array and a thermal insulating member is disposed between the surface of the blade and the outer covering. Electric heating means are provided for raising the temperature of the outer covering to the Leidenfrost point, i.e., the point at which the temperature of the covering exceeds the vaporization temperature of the elastic fluid corresponding to the prevailing ambient pressure by more than 200.degree. C., to evaporate water droplets which collect on the stationary blade and to prevent the accumulation of relatively smaller water droplets on the stationary blade. By preventing the accumulation of water droplets on the stationary blades, erosion of the rotor blades is avoided.

Abstract translation: 轴流式弹性流体涡轮机装置包括具有周向间隔开的叶片的环形阵列的转子。 壳体围绕转子，并且周向间隔开的静止喷嘴叶片的环形阵列紧固壳体并布置成将弹性流体引导到转子的叶片上。 外部覆盖物设置在固定阵列的至少一个叶片的径向最外半部的上方，并且隔热构件设置在叶片的表面和外覆盖物之间。 提供电加热装置，用于将外覆盖层的温度升高到莱顿冰霜点，即覆盖层的温度超过对应于主要环境压力的弹性流体的蒸发温度超过200℃的点。 以蒸发聚集在固定叶片上的水滴并防止相对较小的水滴在固定叶片上积聚。 通过防止水滴积聚在固定叶片上，避免了转子叶片的腐蚀。