Integral Turbine Center Frame
    31.
    发明申请

    公开(公告)号:US20190249570A1

    公开(公告)日:2019-08-15

    申请号:US15892735

    申请日:2018-02-09

    Abstract: Turbine center frames are provided. For example, a turbine center frame comprises an annular outer case and an annular hub. The hub is defined radially inward of the outer case such that the outer case circumferentially surrounds the hub. The turbine center frame further comprises an annular fairing extending between the outer case and the hub, a ligament extending from the fairing to the outer case to connect the fairing to the outer case, a plurality of struts extending from the hub to the outer case, and a boss structure defined on an outer surface of the outer case. The outer case, hub, fairing, ligament, plurality of struts, and boss structure are integrally formed as a single monolithic component. For instance, the turbine center frame is additively manufactured as an integral structure, and methods for manufacturing turbine center frames also are provided.

    COMPONENTS CONFIGURED TO AUTONOMOUSLY DETECT AND ACCOMMODATE STRUCTURAL CHANGES

    公开(公告)号:US20190041280A1

    公开(公告)日:2019-02-07

    申请号:US15667091

    申请日:2017-08-02

    Abstract: A component has a first structural configuration and a second structural configuration. The component includes a sensor assembly including a plurality of interconnected structural members defining a plurality of load paths. A first structural member and a second structural member define a first load path when the component is in the first structural configuration. The first structural member and a third structural member define a second load path when the component is in the second structural configuration. The second load path is configured to bypass the second structural member. The sensor assembly is configured to detect a characteristic of the component that changes when the component switches between the first structural configuration and the second structural configuration.

    COMPONENTS INCLUDING STRUCTURES HAVING DECOUPLED STRUCTURAL STIFFNESS AND MASS DENSITY

    公开(公告)号:US20190030879A1

    公开(公告)日:2019-01-31

    申请号:US15663341

    申请日:2017-07-28

    Abstract: A component is provided. The component includes a structure including a plurality of unit cells joined together, each unit cell of the plurality of unit cells having a mass density substantially similar to the mass density of every other unit cell of the plurality of unit cells. The plurality of unit cells includes a first portion of unit cells having a characteristic dimension and a first portion average stiffness, the characteristic dimension of the first portion of unit cells having a first value. The plurality of unit cells also includes a second portion of unit cells having the characteristic dimension and a second portion average stiffness, the characteristic dimension of the second portion of unit cells having a second value different from the first value, wherein the second portion average stiffness differs from the first portion average stiffness.

    EROSION-SHIELDED TURBINE BLADES AND METHODS OF MANUFACTURING THE SAME

    公开(公告)号:US20240229648A9

    公开(公告)日:2024-07-11

    申请号:US17973198

    申请日:2022-10-25

    CPC classification number: F01D5/005 B23P6/007 F05D2230/10 F05D2230/22

    Abstract: A method of manufacturing an erosion-shielded turbine blade includes providing a turbine blade for use with a rotary machine. The turbine blade includes an airfoil extending between a root and a tip. The airfoil includes a pressure side and an opposite suction side, and each of the pressure and suction sides extends between a leading edge and a trailing edge. The method also includes printing a green body part by an additive manufacturing process by selectively depositing a binder solution across a particulate erosion-resistant material, and sintering the green body part to produce a post-sintering erosion shield that includes densified erosion-resistant material. The method also includes coupling the erosion shield to the leading edge of the turbine blade.

    System and method for identifying distortion-compensation threshold for sintering parts with complex features

    公开(公告)号:US11620421B2

    公开(公告)日:2023-04-04

    申请号:US17162219

    申请日:2021-01-29

    Abstract: A system includes a memory module configured to store a computer model of a part for manufacturing with an additive manufacturing machine, and a processor communicatively coupled to the memory module. The processor is configured to receive the computer model, discretize the computer model into a mesh, predict a deformation behavior the plurality of nodes of the mesh under a simulated sintering process, determine a buckling factor for the part based on the predicted deformation behavior of the mesh, determine whether the buckling factor exceeds a threshold, in response to determining that the buckling factor exceeds the threshold, export the computer model to the additive manufacturing machine for pre-build processing, and in response to determining that the buckling factor does not exceeds the threshold, output, to a display of the system, at least one of an alert that the part is unstable or the buckling factor.

    SYSTEMS AND METHOD FOR PREDICTING DISTORTION OF GREEN BODY PARTS DURING SINTERING

    公开(公告)号:US20220143922A1

    公开(公告)日:2022-05-12

    申请号:US17092524

    申请日:2020-11-09

    Inventor: Ananda Barua

    Abstract: A method of predicting a post-sintering geometry of a green body part includes determining stress differentiating material properties of a material configuration of the green body part by physically measuring the stress differentiating material properties of the material configuration and identifying a plurality of stress regions in the green body part via a first sintering analysis of the green body part. Each stress region is associated with a portion of the green body part subjected to a particular stress state during sintering. The method also includes assigning different sets of stress differentiating material properties to each of the plurality of stress regions to form a stress-simulated green body part and predicting the post-sintering geometry via a second sintering analysis of the stress-simulated green body part.

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