公开(公告)号：US09683454B1

公开(公告)日：2017-06-20

申请号：US15196189

申请日：2016-06-29

Applicant: General Electric Company

Inventor： David Ernest Welch ,  Kristopher John Frutschy ,  Edward Leo Kudlacik

IPC: G01B11/14 ,  F01D17/02 ,  G01B7/14 ,  G01B15/00

CPC classification number: F01D17/02 ,  F01D17/18 ,  F05D2220/31 ,  F05D2270/804 ,  F05D2270/821 ,  F05D2300/17 ,  F16K1/443 ,  F16K37/0033 ,  F16K37/0041 ,  G01B7/14 ,  G01B11/14 ,  G01B15/00 ,  G01B21/16

Abstract: A method for monitoring non-rotating turbomachine parts includes the step of measuring displacement of at least one turbomachine part. A monitoring step monitors displacement of the turbomachine part with a non-contact type sensor. A collecting step collects data regarding the displacement of the turbomachine part. An analyzing step analyzes the data to determine if the displacement exceeds a predetermined threshold range. The non-contact type sensor may be attached to the turbomachine by a rod formed of a material having a low coefficient of thermal expansion, and a target may be attached to a stationary structure in close proximity to the non-contact type sensor.

公开(公告)号：US20170130733A1

公开(公告)日：2017-05-11

申请号：US15310943

申请日：2015-05-13

Applicant: GENERAL ELECTRIC TECHNOLOGY GMBH

Inventor： Filippo CAPPUCCINI ,  Stefania STRAMARE ,  Marco ROMANELLI ,  Marco ANSELMI ,  Riccardo PAOLETTI ,  Alessio BANDINI

IPC: F04D29/22 ,  F04D29/043 ,  F04D29/053 ,  F04D29/62 ,  C25D3/04 ,  C23C18/16 ,  C23C4/12 ,  B05D1/12 ,  C23F11/00 ,  C25D3/12 ,  F04D29/28 ,  C23C18/32

CPC classification number: F04D29/2294 ,  B05D1/12 ,  C23C4/12 ,  C23C18/1633 ,  C23C18/32 ,  C23F11/00 ,  C25D3/04 ,  C25D3/12 ,  F01D5/34 ,  F01D25/007 ,  F04D29/023 ,  F04D29/043 ,  F04D29/053 ,  F04D29/266 ,  F04D29/28 ,  F04D29/624 ,  F04D29/628 ,  F05D2230/90 ,  F05D2260/95 ,  F05D2300/132 ,  F05D2300/16 ,  F05D2300/17 ,  F05D2300/171 ,  F05D2300/611

Abstract: A method for preventing corrosion of an impeller-shaft assembly of a turbomachine comprises the steps of assembling an impeller on a shaft in order to define an impeller-shaft assembly; plating the assembly by inserting the assembly into a plating bath; and coating at least a first predefined surface on the impeller and a second predefined surface on the shaft wherein the coating step is performed by spraying the predefined surfaces.

公开(公告)号：US20170022831A9

公开(公告)日：2017-01-26

申请号：US14687173

申请日：2015-04-15

Applicant: Pratt & Whitney Canada Corp.

Inventor： ERIC DUROCHER ,  GUY LEFEBVRE

IPC: F01D9/04 ,  B22F3/22 ,  B22F3/00 ,  B22F5/00 ,  B22F3/10

CPC classification number: F01D9/04 ,  B22F3/004 ,  B22F3/10 ,  B22F3/225 ,  B22F5/009 ,  B22F5/10 ,  B22F2005/103 ,  F01D11/24 ,  F05D2220/32 ,  F05D2230/22 ,  F05D2230/31 ,  F05D2230/40 ,  F05D2240/11 ,  F05D2260/20 ,  F05D2300/10 ,  F05D2300/17

Abstract: A turbine shroud segment is metal injection molded (MIM) about a low melting point material insert. The low melting point material is dissolved using heat during the heat treatment cycle required for the MIM material, thereby leaving internal cooling passages in the MIM shroud segment without extra manufacturing operation.

Abstract translation: 涡轮机护罩段是关于低熔点材料插入件的金属注射模制（MIM）。 在MIM材料所需的热处理循环期间，使用热量溶解低熔点材料，从而在MIM护套段内留下内部冷却通道，而无需额外的制造操作。

公开(公告)号：US20160326896A1

公开(公告)日：2016-11-10

申请号：US14704406

申请日：2015-05-05

Applicant: General Electric Company

Inventor： Joshua Brian Jamison

IPC: F01D9/04 ,  F01D25/00

CPC classification number: F01D9/042 ,  F01D5/284 ,  F01D9/041 ,  F01D25/005 ,  F05D2220/32 ,  F05D2230/642 ,  F05D2240/128 ,  F05D2250/42 ,  F05D2250/711 ,  F05D2260/36 ,  F05D2300/17 ,  F05D2300/50212 ,  F05D2300/6033 ,  Y02T50/672 ,  Y02T50/673

Abstract: A turbine component assembly for a gas turbine engine includes: a first component having a first coefficient of thermal expansion and including an end face; a second component including a mating surface abutting the end face; and a fastener having a second coefficient of thermal expansion different from the first coefficient of thermal expansion, the fastener including a shank engaging the second component and an enlarged head engaging a mounting slot in the first component; wherein the mating surface and the end face shaped to permit relative pivoting movement between the first and second components.

Abstract translation: 一种用于燃气涡轮发动机的涡轮机部件组件，包括：具有第一热膨胀系数并包括端面的第一部件; 第二部件，包括邻接所述端面的配合表面; 以及具有与所述第一热膨胀系数不同的第二热膨胀系数的紧固件，所述紧固件包括接合所述第二部件的柄部和与所述第一部件中的安装槽接合的扩大头部; 其中所述配合表面和所述端面被成形为允许所述第一和第二部件之间的相对枢转运动。

公开(公告)号：US20160061040A1

公开(公告)日：2016-03-03

申请号：US14832296

申请日：2015-08-21

Applicant: Rolls-Royce Corporation

Inventor： Wade A. Vest

IPC: F01D5/02 ,  F01D25/00

CPC classification number: F01D5/02 ,  C25D1/02 ,  C25D1/08 ,  C25D5/56 ,  F01D5/323 ,  F01D25/005 ,  F04D29/023 ,  F04D29/322 ,  F05D2220/36 ,  F05D2230/24 ,  F05D2230/90 ,  F05D2250/191 ,  F05D2300/17 ,  F05D2300/433 ,  F05D2300/436 ,  F05D2300/605 ,  Y02T50/671 ,  Y02T50/672

Abstract: A fan slider for use in a fan assembly to push a fan blade radially outward of a rotating axis of the gas turbine engine. The fan slider may include a fan slider body coated with a nanocrystalline metallic coating and a slider spring.

Abstract translation: 一种用于风扇组件的风扇滑块，用于将风扇叶片径向向外推向燃气涡轮发动机的旋转轴线。 风扇滑块可以包括涂覆有纳米晶体金属涂层和滑块弹簧的风扇滑块体。

公开(公告)号：US20150354379A1

公开(公告)日：2015-12-10

申请号：US14297406

申请日：2014-06-05

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Amandine Miner ,  David K. Jan ,  Don Mittendorf ,  Jason Smoke

IPC: F01D5/30 ,  B23K1/00 ,  B23K31/02 ,  B23K20/02 ,  B23K20/00

CPC classification number: B23K20/028 ,  B23K1/00 ,  B23K1/0018 ,  B23K20/002 ,  B23K20/021 ,  B23K20/023 ,  B23K20/14 ,  B23K20/22 ,  B23K20/26 ,  B23K31/02 ,  B23K2101/001 ,  B23P15/006 ,  F01D5/3061 ,  F01D5/34 ,  F05D2220/323 ,  F05D2230/236 ,  F05D2230/60 ,  F05D2300/17 ,  F05D2300/606 ,  F05D2300/607 ,  Y10T29/49323

Abstract: Dual alloy turbine rotors and methods for manufacturing the same are provided. The dual alloy turbine rotor comprises an assembled blade ring and a hub bonded to the assembled blade ring. The assembled blade ring comprises a first alloy selected from the group consisting of a single crystal alloy, a directionally solidified alloy, or an equi-axed alloy. The hub comprises a second alloy. The method comprises positioning a hub within a blade ring to define an interface between the hub and the blade ring. The interface is a non-contacting interface or a contacting interface. The interface is enclosed by a pair of diaphragms. The interface is vacuum sealed. The blade ring is bonded to the hub after the vacuum sealing step.

Abstract translation: 提供双合金涡轮转子及其制造方法。 双合金涡轮转子包括组装的叶片环和结合到组装的叶片环的轮毂。 组装的叶片环包括选自单晶合金，定向凝固合金或等轴合金的第一合金。 轮毂包括第二合金。 该方法包括将轮毂定位在叶片环内以限定轮毂和叶片环之间的界面。 该接口是非接触式界面或接触界面。 接口由一对隔膜包围。 界面被真空密封。 在真空密封步骤之后，叶片环结合到轮毂上。

公开(公告)号：US20150321249A1

公开(公告)日：2015-11-12

申请号：US14651911

申请日：2013-12-13

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Dilip M. Shah ,  Alan D. Cetel

IPC: B22D25/02 ,  B22D21/06 ,  C22C19/05 ,  F01D5/28

CPC classification number: B22D25/02 ,  B22D19/16 ,  B22D21/025 ,  B22D21/06 ,  B22D27/045 ,  C22C19/057 ,  F01D5/14 ,  F01D5/147 ,  F01D5/28 ,  F05D2220/30 ,  F05D2230/21 ,  F05D2230/211 ,  F05D2300/131 ,  F05D2300/132 ,  F05D2300/133 ,  F05D2300/135 ,  F05D2300/17 ,  F05D2300/606 ,  F05D2300/609 ,  Y10T403/478

Abstract: A method is provided for casting an article such as a blade having an attachment root and an airfoil, the airfoil having a proximal end and a distal end. The method comprises introducing a molten alloy into a mold; and varying a composition of the introduced alloy during the introduction so as to produce a compositional variation.

Abstract translation: 提供了一种用于铸造诸如具有附接根部和翼型的叶片的制品的方法，所述翼型件具有近端和远端。 该方法包括将熔融合金引入模具中; 并且在引入期间改变引入的合金的组成以产生组成变化。

公开(公告)号：US20140079557A1

公开(公告)日：2014-03-20

申请号：US13621551

申请日：2012-09-17

Applicant: Jeffrey A. LaRose ,  Charles R. Shambaugh, JR.

Inventor： Jeffrey A. LaRose ,  Charles R. Shambaugh, JR.

IPC: F03B3/12

CPC classification number: A61M1/1015 ,  A61M1/101 ,  A61M1/1012 ,  A61M1/1017 ,  A61M1/1029 ,  A61M1/1031 ,  A61M1/122 ,  A61M1/125 ,  A61M2205/02 ,  F04D29/026 ,  F04D29/181 ,  F05D2300/11 ,  F05D2300/143 ,  F05D2300/17 ,  F05D2300/507

Abstract: A magnetic impeller for a blood pump such as a magnetically driven, rotary ventricular assist device for pumping blood of a patient, the impeller comprising a magnetic alloy including platinum, cobalt, and boron.

Abstract translation: 一种用于血泵的磁性叶轮，例如用于泵送患者血液的磁驱动的旋转心室辅助装置，所述叶轮包括包含铂，钴和硼的磁性合金。

公开(公告)号：US20130343868A1

公开(公告)日：2013-12-26

申请号：US13532470

申请日：2012-06-25

Applicant: Sanjeev Kumar Jha ,  Sheo Narain Giri ,  Bhaskar Pemmi ,  Harish Bommanakatte ,  Rajesh Achudhan

Inventor： Sanjeev Kumar Jha ,  Sheo Narain Giri ,  Bhaskar Pemmi ,  Harish Bommanakatte ,  Rajesh Achudhan

IPC: F01D9/04 ,  F01D17/12 ,  F01D25/12

CPC classification number: F01D5/087 ,  F02C7/057 ,  F04D29/023 ,  F04D29/321 ,  F04D29/584 ,  F05D2300/17 ,  F05D2300/505

Abstract: Embodiments of the present application include a gas turbine system. The system may include a rotor wheel and one or more impeller vanes radially disposed on the rotor wheel. The system may also include one or more fluid passages defined by adjacent impeller vanes. The one or more fluid passages may be radially disposed across the rotor wheel. Moreover, the system may include one or more shape memory alloy valves disposed within each of the fluid passages. The one or more shape memory alloy valves may be configured to change shape to control a flow of fluid through the fluid passages.

Abstract translation: 本申请的实施例包括燃气轮机系统。 该系统可以包括转子轮和径向设置在转子轮上的一个或多个叶轮叶片。 系统还可以包括由相邻叶轮叶片限定的一个或多个流体通道。 一个或多个流体通道可以跨过转子轮径向地设置。 此外，系统可以包括设置在每个流体通道内的一个或多个形状记忆合金阀。 一个或多个形状记忆合金阀可以被配置为改变形状以控制通过流体通道的流体流动。

公开(公告)号：US20130101425A1

公开(公告)日：2013-04-25

申请号：US13654468

申请日：2012-10-18

Applicant: Hitachi, Ltd.

Inventor： Masahiko Arai ,  Hiroyuki Doi ,  Hideo Yoda ,  Katsumi Tanaka

IPC: F03B3/12

CPC classification number: F01D5/288 ,  B23K15/0006 ,  B23K15/0093 ,  B23K2101/001 ,  F01D5/28 ,  F05D2230/233 ,  F05D2300/11 ,  F05D2300/17

Abstract: Disclosed is a turbine blade including a turbine blade substrate including an iron-base alloy; an erosion shield plate including a Co-base alloy; and a shim including a Ni—Fe alloy, in which the erosion shield plate is fixed to a leading edge of the turbine blade substrate with the shim therebetween by an electron beam welding. Thus, a turbine blade having a highly reliable, bonded portion of an erosion shield, and a turbine rotor and a steam turbine using the turbine blade are provided.

Abstract translation: 公开了一种涡轮叶片，其包括具有铁基合金的涡轮叶片基板; 包括Co基合金的侵蚀屏蔽板; 以及包括Ni-Fe合金的垫片，其中通过电子束焊接，其间的垫片将侵蚀屏蔽板固定到涡轮叶片基板的前缘。 因此，提供了具有高度可靠的防腐蚀屏蔽部分的涡轮叶片，以及使用该涡轮机叶片的涡轮机转子和蒸汽轮机。