公开(公告)号：US20180361471A1

公开(公告)日：2018-12-20

申请号：US15417873

申请日：2017-01-27

Applicant: United Technologies Corporation

Inventor： Pantcho P. Stoyanov ,  Christopher W. Strock ,  Thomas J. Watson

IPC: B22F1/00 ,  C23C24/04 ,  F01D5/28

CPC classification number: B22F1/0059 ,  B22F2301/052 ,  B22F2301/15 ,  B22F2301/205 ,  B22F2303/01 ,  B22F2303/05 ,  B22F2999/00 ,  C23C4/06 ,  C23C24/04 ,  F01D5/288 ,  F05D2230/90 ,  F05D2300/611

Abstract: A coated article comprising: a substrate; and a coating on the substrate comprising: a metallic matrix comprising, by weight: Al as a largest constituent; 3.0-6.0 Cr; 1.5-4.0 Mn; 0.1-3.5 Co; and 0.3-2.0 Zr; and a filler and optionally porosity.

公开(公告)号：US20140241897A1

公开(公告)日：2014-08-28

申请号：US13625956

申请日：2012-09-25

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Daniel A. Bales ,  Thomas J. Watson

IPC: F04D29/18 ,  F04D29/20

CPC classification number: F04D29/18 ,  B23K1/0018 ,  B23P15/04 ,  F01D5/147 ,  F04D29/023 ,  F04D29/20 ,  F04D29/324 ,  F05D2220/36 ,  F05D2230/237 ,  F05D2300/133 ,  F05D2300/173 ,  F05D2300/174

Abstract: A fan blade includes first and second titanium portions that are secured to one another with an aluminum alloy braze. A method of manufacturing a fan blade includes providing first and second titanium portions, applying an aluminum alloy braze to at least one of the first and second titanium portions, and heating the fan blade to melt the aluminum alloy braze and join the first and second portions to one another to provide a fan blade with an airfoil exterior contour.

Abstract translation: 风扇叶片包括用铝合金钎焊彼此固定的第一和第二钛部分。 制造风扇叶片的方法包括提供第一和第二钛部分，将铝合金钎焊施加到第一和第二钛部分中的至少一个，并且加热风扇叶片以熔化铝合金钎焊并将第一和第二部分 彼此提供具有翼型外形轮廓的风扇叶片。

公开(公告)号：US10508321B2

公开(公告)日：2019-12-17

申请号：US15022514

申请日：2014-09-05

Applicant: United Technologies Corporation

Inventor： Thomas J. Watson ,  Iuliana Cernatescu

IPC: C22C1/04 ,  B22F3/14 ,  B22F3/20 ,  B22F3/24 ,  C22C21/00 ,  C22F1/04

Abstract: Dispersion strengthened aluminum-cerium-manganese alloys containing from about 0.05 to about 23.0 weight percent cerium and about 0.03 to about 9.5 weight percent manganese exhibit mechanical properties that make them useful alloys as a result of age hardening for extended periods at temperatures between 350° C. (662° F.) and 450° C. (842° F.).

公开(公告)号：US20180216626A1

公开(公告)日：2018-08-02

申请号：US15928246

申请日：2018-03-22

Applicant: United Technologies Corporation

Inventor： Daniel A. Bales ,  Thomas J. Watson

IPC: F04D29/18 ,  F04D29/32 ,  F01D5/14 ,  F04D29/02 ,  F04D29/20 ,  B23K1/00 ,  B23P15/04

CPC classification number: F04D29/18 ,  B23K1/0018 ,  B23P15/04 ,  F01D5/147 ,  F04D29/023 ,  F04D29/20 ,  F04D29/324 ,  F05D2220/36 ,  F05D2230/237 ,  F05D2300/133 ,  F05D2300/173 ,  F05D2300/174

Abstract: A fan blade includes first and second titanium alloy portions that are secured to one another with an aluminum alloy braze that contains manganese. The first titanium alloy portion includes ribs, a root, and at least a portion of an exterior airfoil contour of the fan blade. The second titanium alloy portion includes another portion of the exterior airfoil contour. The ribs are secured to the second titanium alloy portion with the aluminum alloy braze. The first titanium alloy portion includes a tip, and leading and trailing edges. The second titanium alloy portion has a perimeter that is arranged inboard of the root, the tip and the leading and trailing edges.

公开(公告)号：US20160305255A1

公开(公告)日：2016-10-20

申请号：US15100663

申请日：2014-11-19

Applicant: United Technologies Corporation

Inventor： Iuliana Cernatescu ,  Thomas J. Watson ,  James O. Hansen ,  David Ulrich Furrer ,  Randy P. Salva

IPC: F01D5/28 ,  C30B29/52 ,  F01D5/14

CPC classification number: F01D5/28 ,  C30B29/52 ,  F01D5/147 ,  F05D2220/36 ,  F05D2250/74 ,  F05D2300/173 ,  F05D2300/605 ,  F05D2300/606 ,  Y02T50/673

Abstract: An airfoil includes an airfoil body that extends at least between leading and trailing edges, first and second sides, and radially inner and outer ends. The airfoil body includes an aluminum alloy that has a controlled crystallographic texture with respect to a predefined three-dimensional coordinate system. The airfoil can be used in the fan of a gas turbine engine.

Abstract translation: 翼型件包括至少在前缘和后缘之间延伸的翼型件本体，第一和第二侧以及径向内端和外端。 翼型体包括相对于预定义的三维坐标系具有受控的结晶组织的铝合金。 翼型可用于燃气轮机的风扇。

公开(公告)号：US20160230252A1

公开(公告)日：2016-08-11

申请号：US15022514

申请日：2014-09-05

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Thomas J. Watson ,  Iuliana Cernatescu

IPC: C22C1/04 ,  B22F3/14 ,  B22F3/24 ,  B22F3/20 ,  C22C21/00 ,  C22F1/04

CPC classification number: C22C1/0416 ,  B22F3/14 ,  B22F3/20 ,  B22F3/24 ,  B22F2998/10 ,  C22C1/0491 ,  C22C21/00 ,  C22F1/04 ,  B22F9/082 ,  B22F2003/145

Abstract: Dispersion strengthened aluminum-cerium-manganese alloys containing from about 0.05 to about 23.0 weight percent cerium and about 0.03 to about 9.5 weight percent manganese exhibit mechanical properties that make them useful alloys as a result of age hardening for extended periods at temperatures between 350° C. (662° F.) and 450° C. (842° F.).

Abstract translation: 含有约0.05至约23.0重量百分比的铈和约0.03至约9.5重量％的锰的分散强化的铝 - 铈 - 锰合金表现出机械性能，使得它们是有用的合金，作为在350℃之间的温度下长时间硬化的结果 （662°F）和450℃（842°F）。

公开(公告)号：US09394805B2

公开(公告)日：2016-07-19

申请号：US13714779

申请日：2012-12-14

Applicant: United Technologies Corporation

Inventor： James O. Hansen ,  Thomas J. Garosshen ,  Thomas J. Watson

IPC: F01D25/00 ,  F01D5/30

CPC classification number: F01D25/00 ,  B64D45/02 ,  F01D5/30 ,  F01D5/3007 ,  F01D25/007 ,  F05D2220/36 ,  F05D2270/54 ,  Y02T50/671 ,  Y02T50/673

Abstract: A rotor has a rotor body with at least one slot receiving a blade. The blade has an outer surface, at least at some areas, formed of a first material and having an airfoil extending from a dovetail. The dovetail is received in the slot. A diode is in contact with a portion of the dovetail formed of a second material that is more electrically conductive than the first material. The diode is in contact with a rotating element that rotates with the rotor. The rotating element is formed of a third material. The first material is less electrically conductive than the third material. The diode and the rotating element together form a ground path from the portion of the dovetail into the rotor. An engine and a fan blade are also disclosed.

Abstract translation: 转子具有转子体，其具有至少一个容纳刀片的槽。 至少在某些区域，叶片具有由第一材料形成并具有从燕尾形延伸的翼型件的外表面。 燕尾接收在槽中。 二极管与由与第一材料相比更导电的第二材料形成的燕尾形部分接触。 二极管与转子一起旋转的旋转元件接触。 旋转元件由第三材料形成。 第一种材料比第三种材料导电性差。 二极管和旋转元件一起形成从燕尾榫部分到转​​子的接地路径。 还公开了一种发动机和风扇叶片。

公开(公告)号：US20140083080A1

公开(公告)日：2014-03-27

申请号：US13714779

申请日：2012-12-14

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： James O. Hansen ,  Thomas J. Garosshen ,  Thomas J. Watson

IPC: F01D25/00 ,  F01D5/30

CPC classification number: F01D25/00 ,  B64D45/02 ,  F01D5/30 ,  F01D5/3007 ,  F01D25/007 ,  F05D2220/36 ,  F05D2270/54 ,  Y02T50/671 ,  Y02T50/673

Abstract: A rotor has a rotor body with at least one slot receiving a blade. The blade has an outer surface, at least at some areas, formed of a first material and having an airfoil extending from a dovetail. The dovetail is received in the slot. A diode is in contact with a portion of the dovetail formed of a second material that is more electrically conductive than the first material. The diode is in contact with a rotating element that rotates with the rotor. The rotating element is formed of a third material. The first material is less electrically conductive than the third material. The diode and the rotating element together form a ground path from the portion of the dovetail into the rotor. An engine and a fan blade are also disclosed.

Abstract translation: 转子具有转子体，其具有至少一个容纳刀片的槽。 至少在某些区域，叶片具有由第一材料形成并具有从燕尾形延伸的翼型件的外表面。 燕尾接收在槽中。 二极管与由与第一材料相比更导电的第二材料形成的燕尾形部分接触。 二极管与转子一起旋转的旋转元件接触。 旋转元件由第三材料形成。 第一种材料比第三种材料导电性差。 二极管和旋转元件一起形成从燕尾榫部分到转​​子的接地路径。 还公开了一种发动机和风扇叶片。