HYBRID AIRFOIL FOR A GAS TURBINE ENGINE
    1.
    发明公开

    公开(公告)号:EP3640435A1

    公开(公告)日:2020-04-22

    申请号:EP19214582.9

    申请日:2013-03-19

    摘要: A hybrid airfoil (142) for a gas turbine engine comprises a leading edge portion (148), a trailing edge portion (150) and an intermediate portion (151) between said leading edge portion (148) and said trailing edge portion (150). The leading edge portion (148) is made of a first material, the trailing edge portion (150) is made of a second material, and the intermediate portion (151) is made of a third material. At least two of said first material, said second material and said third material are different materials. A a portion (115) between said leading edge portion and said intermediate portion includes a pocket (127) that receives a non-metallic portion (102A). A connection interface is established between said leading edge portion (148) and said non-metallic portion (102A).

    NONDESTRUCTIVE MULTISPECTRAL VIBROTHERMOGRAPHY INSPECTION SYSTEM AND METHOD THEREFOR

    公开(公告)号:EP3531124A1

    公开(公告)日:2019-08-28

    申请号:EP19159151.0

    申请日:2019-02-25

    摘要: A nondestructive multispectral vibrothermography inspection system includes a fixture (210) to retain a component (84), an ultrasonic excitation source (220) directed toward the component (84) retained within the fixture (210), a sensor (230) directed toward the component (84) retained within the fixture (210), and a multispectral thermography system (240) directed toward the component (84) retained within the fixture (210). A method for nondestructive multispectral vibrothermography inspection of a component (84), includes generating ultrasonic excitations in a component (84) over a broad range of frequencies; determining a spectral signature in the component (84) from the excitations; comparing the spectral energy signature against database (270) of correlations between vibrational frequencies of a multiple of components and the spectral energy distribution thereof, and classifying the component (84) based on the database data.

    PARTICLE SEPARATOR FOR AN ADDITIVE MANUFACTURING SYSTEM AND METHOD OF OPERATION
    9.
    发明公开
    PARTICLE SEPARATOR FOR AN ADDITIVE MANUFACTURING SYSTEM AND METHOD OF OPERATION 审中-公开
    粒子对于系统用于操作助剂生产和方法

    公开(公告)号:EP3094411A1

    公开(公告)日:2016-11-23

    申请号:EP15737134.5

    申请日:2015-01-15

    IPC分类号: B03B4/00

    摘要: A aerodynamic particle separator for an Additive Manufacturing System (AMS) has an air supply device to entrain a mixed powder in an airstream flowing through a housing. Each particle in the mixed powder is imparted with a momentum dependent upon the particle weight and size. Utilizing this momentum characteristic, the heavier particles are capable of crossing streamlines of the airstream at a bend portion of the housing and the lighter particles generally stay within the streamlines. Utilizing this dynamic characteristic, the particles of specific weight ranges are collected through respective offtake holes in the housing and controllably fed to a spreader of the AMS.

    摘要翻译: 关于添加剂制造系统(AMS)甲空气动力学颗粒分离器具有在空气供应装置在流过壳体气流夹带混合粉末。 在混合粉末每个粒子被赋予依赖于粒子的重量和尺寸的势头。 利用该特性动量,较重的颗粒能够在所述壳体的所述流线内的弯曲部和较轻的颗粒基因反弹停留交叉的气流的流线。 利用该动态特性,比重范围的粒子通过在壳体respectivement承购孔收集并可控地供给到AMS的吊具。