HYBRID TORQUE BAR
    1.
    发明申请

    公开(公告)号:US20210332864A1

    公开(公告)日:2021-10-28

    申请号:US17370616

    申请日:2021-07-08

    Abstract: A hybrid torque bar for a brake assembly may comprise a base portion, a pin extending from a first end of the base portion, and a rail extending between the first end of the base portion and a second end of the base portion opposite the first end. The base portion may be formed using a first manufacturing process. At least one of the pin or the rail may be formed using a second manufacturing process. The second manufacturing process may comprise an additive manufacturing technique.

    HYBRID TORQUE BAR
    5.
    发明申请
    HYBRID TORQUE BAR 审中-公开

    公开(公告)号:US20190331178A1

    公开(公告)日:2019-10-31

    申请号:US15962680

    申请日:2018-04-25

    Abstract: A hybrid torque bar for a brake assembly may comprise a base portion, a pin extending from a first end of the base portion, and a rail extending between the first end of the base portion and a second end of the base portion opposite the first end. The base portion may be formed using a first manufacturing process. At least one of the pin or the rail may formed using a second manufacturing process. The second manufacturing process may comprise an additive manufacturing technique.

    HYBRID TORQUE TUBE
    7.
    发明申请
    HYBRID TORQUE TUBE 审中-公开

    公开(公告)号:US20200263747A1

    公开(公告)日:2020-08-20

    申请号:US16865635

    申请日:2020-05-04

    Abstract: A hybrid torque tube for a brake assembly may comprise a tube portion having a centerline axis, and a conical back-leg portion extending from the tube portion. A stator spline may be formed on a radially outward surface of the tube portion. A foot may be formed on a radially inward surface of the tube portion. The tube portion is formed using a first manufacturing process and at least one of the conical back-leg, stator spline, or foot is formed using additive manufacturing.

    LITHIUM FREE ELEVATED TEMPERATURE ALUMINUM COPPER MAGNESIUM SILVER ALLOY FOR FORGED AEROSPACE PRODUCTS
    9.
    发明申请
    LITHIUM FREE ELEVATED TEMPERATURE ALUMINUM COPPER MAGNESIUM SILVER ALLOY FOR FORGED AEROSPACE PRODUCTS 审中-公开
    无铅高温铝合金镁合金锻造气囊产品

    公开(公告)号:US20150322556A1

    公开(公告)日:2015-11-12

    申请号:US14461102

    申请日:2014-08-15

    CPC classification number: C22C21/16 C22C21/14 C22C21/18 C22F1/04 C22F1/057

    Abstract: A substantially lithium-free alloy may comprise copper from 4.8 wt. % to 5.4 wt. %, magnesium from 0.7 wt. % to 1.1 wt. %, silver from 0.55 wt. % to 0.7 wt. %, and lithium at or below 0.005 wt. %. The substantially lithium-free alloy may further comprise silver from 0.56 wt. % to 0.7 wt. %. The substantially lithium-free alloy may also comprise zirconium from 0.08 wt. % to 0.15 wt. %. The substantially lithium-free alloy may include titanium at or below 0.06 wt. %, iron at or below 0.1 wt. %, silicon at or below 0.08 wt. %, beryllium at or below 0.0001 wt. %, chromium at or below 0.05 wt. %, and zinc at or below 0.25 wt. %.

    Abstract translation: 基本上不含锂的合金可以包含4.8重量% %至5.4wt。 %,镁从0.7wt。 %至1.1wt。 %,银0.55重量% %至0.7wt。 %,锂等于或低于0.005wt。 %。 基本上不含锂的合金还可以包含0.56重量% %至0.7wt。 %。 基本上不含锂的合金还可以包含0.08重量% %〜0.15wt。 %。 基本上不含锂的合金可以包括等于或等于0.06wt。 %,铁等于或低于0.1wt。 %,硅或等于0.08重量% %,铍等于或低于0.0001wt。 %,铬等于或低于0.05wt。 %,锌等于或低于0.25wt。 %。

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