公开(公告)号：US20130224005A1

公开(公告)日：2013-08-29

申请号：US13406943

申请日：2012-02-28

申请人： Matthew Stephen Casavant ,  Brett Darrick Klingler

发明人： Matthew Stephen Casavant ,  Brett Darrick Klingler

IPC分类号： F01D25/24 ,  B23P11/00 ,  F16J15/02

CPC分类号： F01D25/243 ,  F05D2240/55 ,  F05D2260/31 ,  Y10T29/49863

摘要： A seal for a turbine casing is provided. The turbine casing includes a plurality of sections joined at flanges provided on each section. Each flange includes a bore and a counterbore. The seal comprises a compression sleeve seal having a length that is greater than a counterbore-to-counterbore length of two flanges; a fastener configured to extend through the compression sleeve seal; and a nut threadable on each end of the fastener. The compression sleeve seal is compressible between each flange and each nut to create a first seal and is radially extensible to create a second seal against each bore.

摘要翻译： 提供了一种用于涡轮机壳体的密封件。 涡轮机壳体包括在每个部分上设置的法兰处连接的多个部分。 每个凸缘包括孔和沉孔。 密封件包括压缩套筒密封件，该密封件的长度大于两个凸缘的沉孔至沉孔长度; 紧固件，其构造成延伸穿过所述压缩套筒密封件; 以及在紧固件的每一端上可螺纹的螺母。 压缩套筒密封件在每个凸缘和每个螺母之间是可压缩的，以产生第一密封件并且可径向延伸以产生抵靠每个孔的第二密封件。

公开(公告)号：US20120257958A1

公开(公告)日：2012-10-11

申请号：US13428684

申请日：2012-03-23

申请人： Giles D. NORTON

发明人： Giles D. NORTON

IPC分类号： F01D25/00

CPC分类号： F04D29/083 ,  F01D5/025 ,  F04D29/644 ,  F05D2260/30 ,  F05D2260/31

摘要： A windage shield 2 for an array of fasteners 34, the shield 2 comprising a channel 4 for accommodating portions of the fasteners 34 extending into a fluid flow path. The windage shield 2 also comprises a closure flap 12 which extends between opposite side walls 8, 10 of the channel 4 to enclose the interior of the channel 4. The closure flap 12 is displaceable away from at least one of the side walls 8, 10 to provide access to at least one of the fastener portions 34.

摘要翻译： 用于紧固件阵列34的防风罩2，护罩2包括用于容纳延伸到流体流动路径中的紧固件34的部分的通道4。 防风罩2还包括在通道4的相对的侧壁8,10之间延伸的封闭翼片12，以封闭通道4的内部。封闭翼片12可以远离至少一个侧壁8,10 以提供对至少一个紧固件部分34的通路。

公开(公告)号：US20110274541A1

公开(公告)日：2011-11-10

申请号：US13127836

申请日：2009-09-29

申请人： Olivier Belmonte ,  Thomas Langevin ,  Stevan Le Goff

发明人： Olivier Belmonte ,  Thomas Langevin ,  Stevan Le Goff

IPC分类号： F01D25/28

CPC分类号： F01D5/066 ,  F01D25/243 ,  F01D25/246 ,  F05D2260/30 ,  F05D2260/31 ,  Y02T50/671

摘要： A radial annular flange including in inner or outer periphery alternating solid portions including orifices for passing fastener bolts, and hollow portions having bottoms that are substantially flat. The bottom of at least one keying hollow portion is situated radially inside, or outside, respectively, a circle centered on the axis of the flange and externally, or respectively internally, tangential to the orifices. Two hollow portions are situated on either side of the keying hollow portion having bottoms of concave curved shapes situated radially on the outside, or respectively on the inside, relative to the flat bottoms of the other hollow portions.

摘要翻译： 径向环形凸缘，其包括在内部或外部周边，交替的实心部分包括用于通过紧固件螺栓的孔口，以及具有基本上平坦的底部的中空部分。 至少一个键合中空部分的底部分别径向地位于或位于围绕凸缘的轴线的中心的圆周上，或者分别位于与孔口相切的内部。 两个中空部分位于键合中空部分的任一侧，具有相对于另一个中空部分的平坦底部径向位于外侧或分别在内侧的凹形弯曲形状的底部。

公开(公告)号：US20110243722A1

公开(公告)日：2011-10-06

申请号：US12749971

申请日：2010-03-30

申请人： Richard M. Murphy ,  Matthew S. Gleiner

发明人： Richard M. Murphy ,  Matthew S. Gleiner

IPC分类号： F01D9/02 ,  B23P15/02

CPC分类号： F01D9/042 ,  F01D25/246 ,  F05D2230/642 ,  F05D2240/80 ,  F05D2250/62 ,  F05D2260/31 ,  F05D2260/941 ,  Y10T29/49336

摘要： A fixed vane section for a gas turbine engine includes an anti-rotation slot that receives a pin for maintaining a desired position while providing for movement encountered during operation. The example anti-rotation slot includes a compound radius on inner surfaces to reduce stresses encountered during operation.

摘要翻译： 用于燃气涡轮发动机的固定叶片部分包括防旋转槽，其接收销以保持期望位置，同时提供在操作期间遇到的运动。 示例性防旋转槽包括内表面上的复合半径，以减少操作期间遇到的应力。

公开(公告)号：US07510380B2

公开(公告)日：2009-03-31

申请号：US11213178

申请日：2005-08-26

申请人： Mohsiul Alam ,  Scott J. Freestone ,  Walter L. Meacham ,  Paul B. Talbert

发明人： Mohsiul Alam ,  Scott J. Freestone ,  Walter L. Meacham ,  Paul B. Talbert

IPC分类号： F01D5/02

CPC分类号： F01D5/025 ,  F01D5/027 ,  F01D5/066 ,  F05D2230/64 ,  F05D2260/15 ,  F05D2260/31

摘要： The present invention provides apparatus and methods for balancing stacked components of rotating machinery, such as in a gas turbine engine. Unlike conventional processes and devices for balancing stacked components, the present invention may use a single non-parallel spacer for obtaining an acceptable and repeatable component group balance. The non-parallel spacer may be used to compensate for rotor bow and the associated imbalance of the rotor group. By indexing a spacer with non-parallel faces, situated terminally at the end of the stack adjacent to the nut, rotor balance can be achieved without disassembly of the rotor group and clocking of its individual components. A spacer may also be disposed at any one or more of the interfaces between various components in the stack.

摘要翻译： 本发明提供了用于平衡诸如在燃气涡轮发动机中的旋转机械的堆叠部件的装置和方法。 与用于平衡堆叠部件的常规工艺和装置不同，本发明可以使用单个非平行间隔件来获得可接受和可重复的部件组平衡。 非平行间隔件可用于补偿转子弓和转子组的相关不平衡。 通过将具有非平行面的间隔物分度，位于与螺母相邻的堆叠的端部处，可以实现转子平衡而不拆卸转子组并对其各个部件进行计时。 间隔物也可以设置在堆叠中各种组分之间的任何一个或多个界面处。

公开(公告)号：US20240352870A1

公开(公告)日：2024-10-24

申请号：US18687520

申请日：2022-11-30

申请人： MITSUBISHI HEAVY INDUSTRIES, LTD.

发明人： Satoshi Kumagai ,  Shunsuke Mizumi ,  Koji Ishibashi ,  Keisuke Uchino

IPC分类号： F01D21/00 ,  F01D25/24 ,  G01M3/26

CPC分类号： F01D21/003 ,  F01D25/243 ,  G01M3/26 ,  F05D2260/31 ,  F05D2260/83

摘要： A method for estimating a flange surface pressure distribution includes: a reference model receiving step of receiving a three-dimensional reference shape model of a rotary machine; a measured coordinate receiving step of receiving measured three-dimensional coordinate data at a plurality of positions on an upper flange surface and a lower flange surface when a casing is in an open state; a condition receiving step of receiving a tightening torque and an elastic coefficient of a plurality of bolts, elastic coefficients and weights of an upper-half casing and a lower-half casing, and the like; a modified model creating step of creating a three-dimensional modified shape model by modifying the three-dimensional reference shape model based on the measured three-dimensional coordinate data at the plurality of positions; and a pressure distribution estimating step of obtaining, by using the three-dimensional modified shape model and under the conditions received in the condition receiving step, a pressure distribution of a flange surface in a fastened state.

公开(公告)号：US12065947B2

公开(公告)日：2024-08-20

申请号：US18090197

申请日：2022-12-28

申请人： General Electric Company

发明人： Ravindra Shankar Ganiger ,  Sam J. Stoughton ,  Kevin Lee Kirkeng ,  Jacob P. Miller ,  Reddi Hari Prasad Reddy Mylapalli ,  Paul Trimby ,  Jaeyong Kim

IPC分类号： F01D5/22 ,  F02C7/28

CPC分类号： F01D5/225 ,  F02C7/28 ,  F05D2240/55 ,  F05D2250/283 ,  F05D2260/31 ,  F05D2260/96

摘要： Methods, apparatus, systems and articles of manufacture are disclosed. An inner shroud damper for a gas turbine engine includes: at least one carrier including a joint to couple to an inner shroud, the at least one carrier having a first side and a second side, and at least one mass damper coupled to the at least one carrier.

公开(公告)号：US20240229826A9

公开(公告)日：2024-07-11

申请号：US17970910

申请日：2022-10-21

申请人： Coil Master Corporation

发明人： Marco Giglio

IPC分类号： F04D29/60 ,  F04D25/16 ,  F04D29/40

CPC分类号： F04D29/602 ,  F04D25/166 ,  F04D29/403 ,  F05D2260/31

摘要： A modular fan array includes a fan assembly having a fan wheel, a fan motor, and a mounting bracket. The fan wheel has a diameter. The assembly includes a frame having at least a pair of vertical members having a spacing therebetween. The spacing is greater than the fan wheel diameter. The mounting bracket includes a motor mount portion and a pair of rearwardly and outwardly extending legs. The motor mount portion includes an opening in which the motor is mounted. The rearwardly and outwardly extending legs each have a first angled section angled relative to the motor mount portion and second frame mount portion. The frame mount portions extend outwardly from the angled portions and parallel to the motor mount portion. The frame mount portions are removably secured to the frame.

公开(公告)号：US20240209753A1

公开(公告)日：2024-06-27

申请号：US18287387

申请日：2022-06-21

申请人： MITSUBISHI HEAVY INDUSTRIES ENGINE & TURBOCHARGER, LTD.

发明人： Youji AKIYAMA ,  Nariaki SEIKE ,  Takuya EHANA

IPC分类号： F01D25/24

CPC分类号： F01D25/243 ,  F05D2230/13 ,  F05D2250/60 ,  F05D2260/31

摘要： A casing that is for a rotating machine and that is configured such that a plurality of housings are linked together, the casing comprising: a first housing including a first connection part that protrudes outward in a radial direction of the rotating machine and that has a first surface extending along the radial direction; a second housing including a second connection part that protrude outward in the radial direction and that has a second surface extending along the radial direction and being in contact with the first surface; and at least one fastening device that fastens the first connection part and the second connection part in the axial direction of the rotating machine, wherein at least one of the first surface or the second surface includes, at least at a portion thereof, a rough surface region having formed therein a plurality of laser irradiation marks formed by irradiation with laser light.

公开(公告)号：US20240200495A1

公开(公告)日：2024-06-20

申请号：US18539813

申请日：2023-12-14

申请人： Rolls-Royce plc

发明人： Zahid M. HUSSAIN ,  Vasileios Kyritsis

IPC分类号： F02C7/18 ,  F02C9/18

CPC分类号： F02C7/18 ,  F02C9/18 ,  F05D2240/14 ,  F05D2260/213 ,  F05D2260/31 ,  F05D2260/606

摘要： A thermal management system for a gas turbine engine includes a plurality of inlet and outlet vanes extending from a bypass inner wall towards an outer cowl, a plurality of first removable shims, a plurality of second removable shims, and a third removable shim. Each first removable shim extends between and engages the outer cowl and a corresponding inlet vane. Each second removable shim extends between and engages the outer cowl and a corresponding outlet vane. The third removable shim extends between and engages a heat exchanger and the outer cowl. Each of the plurality of first removable shims, each of the plurality of second removable shims, and the third removable shim is removable for positionally adjusting the outer cowl relative to the bypass inner wall.