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公开(公告)号:US20180051360A1
公开(公告)日:2018-02-22
申请号:US15237976
申请日:2016-08-16
Applicant: United Technologies Corporation
Inventor: Dilip M. Shah , Alan D. Cetel , Venkatarama K. Seetharaman
CPC classification number: C22C1/03 , B22D21/005 , B22D27/04 , C22C19/00 , C22C19/03 , C22C19/056 , C30B11/00 , C30B29/52
Abstract: A formable nickel based superalloy composition including a two phase γ/γ′ precipitation hardenable nickel base superalloy with a sum of primarily γ′ forming elements in atom % is in the range of about 10-16, forming about a 40-64 volume % of the γ′ precipitate, cast in form of a single crystal.
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公开(公告)号:US09802248B2
公开(公告)日:2017-10-31
申请号:US14905904
申请日:2014-07-11
Applicant: United Technologies Corporation
Inventor: John J. Marcin, Jr. , Steven J. Bullied , Dilip M. Shah , Alan D. Cetel
IPC: B22D25/02 , B22D27/04 , B22D19/00 , B22D19/16 , B22C9/10 , B22C9/04 , B22C21/14 , B22C7/02 , B22C9/06 , B22C9/24 , B22D15/00 , B22D21/02 , B22D29/00
CPC classification number: B22D25/02 , B22C7/02 , B22C9/043 , B22C9/06 , B22C9/10 , B22C9/101 , B22C9/108 , B22C9/24 , B22C21/14 , B22D15/00 , B22D19/00 , B22D19/0072 , B22D19/16 , B22D21/025 , B22D27/045 , B22D29/00 , B22D29/001
Abstract: A method for casting an article comprises a first region and a second region. The method comprises casting an alloy in a shell, the shell having a casting core protruding from a first metal piece; and deshelling and decoring to remove the shell and core and leave the first region formed by the first piece and the second region formed by the casted alloy.
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公开(公告)号:US20170088926A1
公开(公告)日:2017-03-30
申请号:US14867232
申请日:2015-09-28
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Dilip M. Shah , Alan D. Cetel , Venkatarama K. Seetharaman
CPC classification number: C22F1/10 , C22C19/056
Abstract: A process includes solution heat treating a nickel based superalloy with greater than about 40% by volume of gamma prime precipitate to dissolve the gamma prime precipitate in the nickel based superalloy; cooling the nickel based superalloy to about 85% of a solution temperature measured on an absolute scale to coarsen the gamma prime precipitate such that a precipitate structure is greater than about 0.7 micron size; and wrought processing the nickel based superalloy at a temperature below a recrystallization temperature of the nickel based superalloy. A material includes a nickel based superalloy with greater than about 40% by volume of gamma prime precipitate in which the precipitate structure is greater than about 0.7 micron size.
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公开(公告)号:US20160325387A1
公开(公告)日:2016-11-10
申请号:US15211238
申请日:2016-07-15
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Edward R. Szela , Daniel A. Bales , Alan D. Cetel
IPC: B23P6/04 , B23K9/04 , B23K10/02 , B23K26/34 , B23K31/02 , F01D9/02 , C22C19/07 , C22C19/03 , C22F1/10 , F01D5/00 , F01D5/12 , B23K1/00 , B23K35/30
CPC classification number: B23P6/045 , B23K1/0018 , B23K9/04 , B23K10/027 , B23K26/34 , B23K31/02 , B23K35/3033 , B23K35/3046 , B23K2101/001 , B23K2103/08 , B23P6/007 , C22C19/03 , C22C19/057 , C22C19/07 , C22F1/10 , C23C4/01 , C23C4/18 , C23C28/02 , C23C30/00 , F01D5/005 , F01D5/12 , F01D5/288 , F01D9/02 , F05D2220/30 , F05D2230/31 , F05D2230/40 , F05D2230/80 , F05D2230/90 , F05D2300/229 , Y10T29/49318
Abstract: A method for repairing, refurbishing, or replacing a turbine engine component or sub-component includes the steps of providing a turbine engine component or sub-component having a site to be repaired, refurbished, or replaced providing a repair or replacement material having a sulfur content, which sulfur content is less than 10 ppm, and applying the repair or replacement material to the site on the turbine engine component to effect the repair, the refurbishment, or the replacement.
Abstract translation: 一种用于修理,翻新或更换涡轮发动机部件或子部件的方法包括提供具有待修理,翻新或替换的部位的涡轮发动机部件或子部件的步骤,提供具有硫的修复或更换材料 含量小于10ppm的含量,以及将修理或更换材料应用于涡轮发动机部件上的部位进行修理,翻新或更换。
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公开(公告)号:US20160222801A1
公开(公告)日:2016-08-04
申请号:US14916310
申请日:2014-08-13
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: John J. Marcin , Steven J. Bullied , Dilip M. Shah , Alan D. Cetel
CPC classification number: F01D5/28 , B23K20/02 , B23K2101/001 , B23K2103/08 , F01D5/147 , F05D2220/32 , F05D2230/236 , F05D2240/307 , F05D2300/175 , F05D2300/607
Abstract: A blade (60; 60-2) comprises an airfoil (61) and an attachment root (63). The blade has a tipward zone (80; 80-2; 80-2, 81) and a rootward zone (82; 82-2, 81; 82). The rootward zone has a single crystal structure. The tipward zone has a single crystal structure. The crystalline orientations of the rootward zone and tipward zone are at least 15° out of registry with each other.
Abstract translation: 叶片(60; 60-2)包括翼型件(61)和附接根部(63)。 叶片具有尖端区域(80; 80-2; 80-2,81)和向后区域(82; 82-2,81; 82)。 根部区域具有单晶结构。 顶端区域具有单晶结构。 根部区域和向前区域的结晶取向相互之间至少为15°。
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公开(公告)号:US20150328681A1
公开(公告)日:2015-11-19
申请号:US14651926
申请日:2013-12-13
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Steven J. Bullied , Dilip M. Shah , Alan D. Cetel , John J. Marcin
CPC classification number: B22D19/16 , B22D27/045 , F01D5/147 , F05D2230/211
Abstract: An alloy part is cast in a mold (280) having a part forming cavity (292, 294, 296). The method comprises pouring a first alloy into the mold. The pouring causes: a surface (550) of the first alloy in the part forming cavity to raise relative to the part forming cavity; a branch flow of the poured first alloy to pass upwardly through a first portion (304) of a passageway; and the branch flow to pass downwardly through a second portion (310), of the passageway; solidifying some of the first alloy in the passageway to block the passageway while at least some of the first alloy in the part forming cavity remains molten. A second alloy is poured into the mold atop the first alloy and solidified.
Abstract translation: 合金部件铸造在具有部分形成腔体(292,294,296)的模具(280)中。 该方法包括将第一合金倒入模具中。 浇注原因:部件形成腔中的第一合金的表面(550)相对于部件形成腔体升高; 倾倒的第一合金的分支流向上通过通道的第一部分(304); 并且所述分支流向下通过所述通道的第二部分(310); 固化通道中的一些第一合金以阻挡通道,同时部件形成空腔中的至少一些第一合金保持熔融。 将第二合金倒入第一合金顶部的模具中并固化。
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公开(公告)号:US10830357B2
公开(公告)日:2020-11-10
申请号:US14695981
申请日:2015-04-24
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Michael G. McCaffrey , Jeffrey M. Wittman , Dilip M. Shah , Alan D. Cetel , Timothy M. Davis , Mark J. Rogers
Abstract: The present disclosure relates to advanced materials, particularly single crystal grain structures including the formation of single crystal grain structures. Single crystal grain structures offer improved mechanical properties when used with individual components. Improving mechanical properties is favorable for components that are used in applications with high temperature, pressure, and stress. In these applications, mechanical failure is extremely undesirable. Individual components, such as seals, can be designed with a single crystal grain structure in a preferred direction. By selecting a preferred direction, and orienting the single crystal grain structure accordingly, the single crystal grain structure can improve the component's mechanical properties. Single crystal grain structure seals and the method of forming the seals, therefore, offer various improvements to individual components, specifically when the components are designed for high temperature, pressure, and stress applications.
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公开(公告)号:US20200255923A1
公开(公告)日:2020-08-13
申请号:US16715463
申请日:2019-12-16
Applicant: United Technologies Corporation
Inventor: Luke H. Rettberg , Alan D. Cetel
Abstract: An alloy comprises, by weight: nickel (Ni) as a largest constituent; 6.0% to 7.5% chromium; up to 5.0% cobalt; 5.3% to 6.5% aluminum; up to 5.0% rhenium; 3.7% to 7.0% tungsten; and 3.7% to 7.0% tantalum.
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公开(公告)号:US10576537B2
公开(公告)日:2020-03-03
申请号:US16267900
申请日:2019-02-05
Applicant: United Technologies Corporation
Inventor: Steven J. Bullied , Dilip M. Shah , Alan D. Cetel , John J. Marcin, Jr.
Abstract: A casting mold has a pour cone, a downsprue, and a part-forming cavity having a lower end and an upper end. The downsprue extends from the pour cone toward the part-forming cavity and has: a lower portion having a plurality of ports in communication with the part-forming cavity; and an upper portion telescoping relative to the lower portion and coupling the lower portion to the pour cone.
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公开(公告)号:US10369625B2
公开(公告)日:2019-08-06
申请号:US14731768
申请日:2015-06-05
Applicant: United Technologies Corporation
Inventor: Dilip M. Shah , Paul D. Genereux , Alan D. Cetel , John J. Marcin, Jr. , Steven J. Bullied , Mario P. Bochiechio , Kevin W. Schlichting , Bradford A. Cowles , Carl R. Verner , David U. Furrer , Venkatarama K. Seetharaman
IPC: B22D27/04 , B22D7/04 , B22D27/13 , C30B11/14 , F01D5/02 , F01D5/28 , F01D25/00 , F23R3/00 , C30B13/34 , C30B15/36 , C30B29/52 , C30B29/60 , B22D19/00 , B22D21/02 , B22D25/02 , C22C19/03 , F01D11/08 , F01D25/24 , F01D5/14 , F01D5/34
Abstract: A method for casting comprising: providing a seed, the seed characterized by: an arcuate form and a crystalline orientation progressively varying along an arc of the form; providing molten material; and cooling and solidifying the molten material so that a crystalline structure of the seed propagates into the solidifying material.
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