METHOD OF FORMING GREEN PART AND MANUFACTURING METHOD USING SAME
    2.
    发明申请
    METHOD OF FORMING GREEN PART AND MANUFACTURING METHOD USING SAME 有权
    形成绿色部件的方法和使用该方法的制造方法

    公开(公告)号:US20160016329A1

    公开(公告)日:2016-01-21

    申请号:US14479738

    申请日:2014-09-08

    IPC分类号: B28B1/24 B28B11/08

    摘要: A method of manufacturing a part, including providing a green body made of powder injection molding material and connected to a solid support member partially contained in the green body. The support member is engaged with a retaining fixture of a machine tool. While supporting the green body through the engagement between the support member and the retaining fixture, the green body is machined to obtain a machined green part. The machined green part is debound and sintered. A method of forming a powder injection molding part in a green state including machining a molded body using a machine tool while supporting the blank with a retaining fixture, and a machining blank having a green body and a solid support member including one locating feature of a pair of complementary locating features snuggly engageable with one another are also discussed.

    摘要翻译: 一种制造零件的方法,包括提供由粉末注射成型材料制成的生坯并连接到部分包含在生坯中的固体支撑构件。 支撑构件与机床的保持夹具接合。 在通过支撑构件和保持夹具之间的接合来支撑生坯的同时,生坯被加工以获得加工的绿色部件。 机加工的绿色部分是脱模和烧结的。 一种形成绿色状态的粉末注射成型部件的方法,包括使用机床加工成型体,同时用保持固定装置支撑坯件;以及加工坯料,其具有生坯体和固体支撑部件,该加工坯料包括一个定位特征 还讨论了彼此紧密接合的一对互补定位特征。

    STRUCTURAL REINFORCEMENT STRUT FOR GAS TURBINE CASE
    4.
    发明申请
    STRUCTURAL REINFORCEMENT STRUT FOR GAS TURBINE CASE 有权
    用于气体涡轮机的结构加固钢筋

    公开(公告)号:US20130175327A1

    公开(公告)日:2013-07-11

    申请号:US13782140

    申请日:2013-03-01

    IPC分类号: F01D25/24

    CPC分类号: F01D25/24 F01D25/162

    摘要: A gas turbine engine case having a working fluid flow, includes inner and outer case portions defining an annular duct for directing the working fluid flow, and a plurality of struts positioned within the annular duct and extending between the inner and outer case portions. The struts are welded to the inner and outer case portions with a first weld along a peripheral line of the respective struts and with second weld, of fillet type, in selected locations for additionally connecting a portion of each strut to the respective inner and outer case portions.

    摘要翻译: 具有工作流体流动的燃气涡轮发动机壳体包括限定用于引导工作流体流动的环形管道的内外壳部分和定位在环形管道内并在内壳部分和外壳部分之间延伸的多个支柱。 支柱通过沿着相应支柱的周边线的第一焊接并且具有圆角型的第二焊接在选定的位置焊接到内外壳部分,用于将每个支柱的一部分附加到相应的内壳和外壳 部分。

    SYSTEM AND METHOD FOR JOINING COMPONENTS
    5.
    发明申请

    公开(公告)号:US20190061035A1

    公开(公告)日:2019-02-28

    申请号:US15686705

    申请日:2017-08-25

    IPC分类号: B23K1/20 B23K3/08 B23K11/11

    摘要: A system and method for joining components together by projection welding and brazing are disclosed. In one embodiment, the method makes use of one or more weld projections extending from a first component and one or more spacer projections extending from either or both of the components. The one or more weld projections are taller than the one or more spacer projections by a meltdown distance that permits projection welding of the first and second components and permits the one or more spacer projections to define a brazing gap between the first and second components after projection welding.

    METHOD OF WELDING CONDUIT COMPONENTS OF A HEAT EXCHANGER AND BACKING DEVICE THEREFORE

    公开(公告)号:US20190366464A1

    公开(公告)日:2019-12-05

    申请号:US16000430

    申请日:2018-06-05

    摘要: The method can include inserting a first portion of a backing device into a fluid aperture of a first conduit component, inserting a second portion of the backing device into a fluid aperture of a second conduit component, and bringing the second conduit component adjacent the first component over the backing device, fusion welding the first conduit component to the second conduit over the backing device, and removing the backing device by circulating a fluid inside the welded conduit components. The backing device can be made of a soluble material.

    GAS TURBINE ENGINE ROTOR
    7.
    发明申请

    公开(公告)号:US20180112542A1

    公开(公告)日:2018-04-26

    申请号:US15332313

    申请日:2016-10-24

    IPC分类号: F01D5/30

    摘要: A rotor for a gas turbine engine is described and includes a disc and a plurality of blades. The disc has opposite first and second end surfaces spaced apart by a peripheral surface circumferentially extending about the rotor, and a plurality of slots defined in the peripheral surface and each having a length extending between a first slot opening in the first end surface and a second slot opening in the second end surface. Each of the slots has a tapered shape with at least one dimension of a cross-sectional shape of the slot reducing along at least a portion of the length of the slot. The at least one dimension at the first slot opening is greater than the at least one dimension at the second slot opening. The blades having a complimentary root are received in the slots of the rotor.