COMPONENTS FOR COMPRESSORS HAVING ELECTROLESS COATINGS ON WEAR SURFACES
    124.
    发明申请
    COMPONENTS FOR COMPRESSORS HAVING ELECTROLESS COATINGS ON WEAR SURFACES 有权
    具有耐磨表面的电镀涂层的压缩机组件

    公开(公告)号:US20150118090A1

    公开(公告)日:2015-04-30

    申请号:US14527484

    申请日:2014-10-29

    Abstract: Carbon dioxide compressors having one or more coatings with wear surfaces having electroless surface coatings are provided. Alternatively, propane compressors are contemplated having wear surface coatings. The coating is electrolessly applied and may comprise nickel and wear resistant particles, such as boron nitride. The electroless surface coatings for use with compressor machines improve corrosion and wear resistance, as well as anti-friction properties for compressors processing CO2 or C3H8 containing refrigerants. In certain aspects, a scroll machine has an Oldham coupling and/or lower bearing comprising aluminum and has an electroless surface coating comprising nickel boron nitride particles disposed on one or more wear surfaces. In other aspects, a reciprocating compressor has a wear surface, such as on a connecting rod and/or piston coated with an electrolessly applied nickel and boron nitride particle layer. Methods for making the electroless surface coatings are also provided.

    Abstract translation: 提供具有一个或多个具有无电镀表面的耐磨表面的涂层的二氧化碳压缩机。 或者,预期丙烷压缩机具有磨损表面涂层。 该涂层是无电镀的,并且可以包括镍和耐磨颗粒,例如氮化硼。 用于压缩机的无电镀表面涂层可提高耐腐蚀和耐磨性,以及压缩机加工含CO2或C3H8制冷剂的抗摩擦性能。 在某些方面,涡旋机具有包含铝的十字联轴器和/或下轴承,并且具有包含设置在一个或多个磨损表面上的氮化镍颗粒的无电表面涂层。 在其他方面,往复式压缩机具有磨损表面,例如涂覆有无电镀镍和氮化硼颗粒层的连杆和/或活塞上。 还提供了制备无电表面涂层的方法。

    NICKEL-BASED SUPERALLOY AND ARTICLES

    公开(公告)号:US20140119979A1

    公开(公告)日:2014-05-01

    申请号:US13665280

    申请日:2012-10-31

    Abstract: A nickel-based superalloy composition includes from about 5 to about 7 wt % aluminum, from about 4 to about 8 wt % tantalum, from about 3 to about 8 wt % chromium, from about 3 to about 7 wt % tungsten, from 1 to about 5 wt % molybdenum, from 1.5 to about 5 wt % rhenium, from 5 to about 14 wt % cobalt, from about 0 to about 1 wt % hafnium, from about 0.01 to about 0.03 wt % carbon, from about 0.002 to about 0.006 wt % boron, and balance nickel and incidental impurities. The composition may exhibit a sustained peak low cycle fatigue life at 1800° F./45 ksi of at least about 4000 cycles. The nickel-based superalloy composition may be used in single-crystal or directionally solidified superalloy articles, such as a blade, nozzle, a shroud, a splash plate, and a combustor of a gas turbine engine.

    ROOTS PUMP AND EXHAUST METHOD
    127.
    发明申请
    ROOTS PUMP AND EXHAUST METHOD 审中-公开
    车辆泵和排气方法

    公开(公告)号:US20130336828A1

    公开(公告)日:2013-12-19

    申请号:US13779965

    申请日:2013-02-28

    Inventor: Takashi OHTA

    Abstract: According to one embodiment, a roots pump includes a first roots pump, a second roots pump, and a connection passage. The first roots pump includes a first casing which has a first pump chamber. The second roots pump includes a second casing which has a second pump chamber. The connection passage connects an exhaust hole which is provided in the first pump chamber to an intake hole which is provided in the second pump chamber.

    Abstract translation: 根据一个实施例,根泵包括第一根泵,第二根泵和连接通道。 第一根泵包括具有第一泵室的第一壳体。 第二根泵包括具有第二泵室的第二壳体。 连接通道将设置在第一泵室中的排气孔连接到设置在第二泵室中的进气孔。

    Thruster and Spacecraft
    128.
    发明申请
    Thruster and Spacecraft 有权
    推进器和航天器

    公开(公告)号:US20130305687A1

    公开(公告)日:2013-11-21

    申请号:US13834493

    申请日:2013-03-15

    Abstract: A thruster designed to produce thrust by introducing a propellant to a catalyst layer from a propellant valve via a propellant introduction member and spurting out a gas resulting from decomposition of the propellant occurring on the catalyst layer, wherein the thruster comprises a chamber of an Ni alloy for holding the catalyst layer inside, the propellant introduction member is made of an Ni alloy and connects the propellant valve and the chamber, and a propellant valve flange of a Ti alloy with a plurality of columns of a Ti alloy is arranged between the chamber and the propellant valve to support the chamber by the columns.

    Abstract translation: 一种推进器,设计用于通过推进剂引入构件将推进剂从推进剂阀引入催化剂层并喷出由催化剂层上发生的推进剂分解产生的气体,从而产生推力,其中推进器包括Ni合金室 为了将催化剂层保持在内部,推进剂引入构件由Ni合金制成,并连接推进剂阀和腔室,并且在腔室和腔室之间设有具有多列Ti合金的Ti合金推进剂阀法兰 推进剂阀由柱支撑室。

    NICKEL-BASED SUPERALLOY AND PARTS MADE FROM SAID SUPERALLOY
    130.
    发明申请
    NICKEL-BASED SUPERALLOY AND PARTS MADE FROM SAID SUPERALLOY 审中-公开
    基于镍的超级合金和部分由超级合资公司组成

    公开(公告)号:US20120183432A1

    公开(公告)日:2012-07-19

    申请号:US13391454

    申请日:2010-08-20

    CPC classification number: C22C19/056 C22C1/023 C22F1/10 F05C2201/0466

    Abstract: A nickel superalloy has the following composition, the concentrations of the different elements being expressed as wt-%: Formula (I), the remainder consisting of nickel and impurities resulting from the production of the superalloy. In addition, the composition satisfies the following equation, wherein the concentrations of the different elements are expressed as atomic percent: Formula (II).

    Abstract translation: 镍超合金具有以下组成,不同元素的浓度以重量%表示:式(I),其余由镍和由制造超合金产生的杂质组成。 此外,组合物满足以下等式,其中不同元素的浓度以原子百分比表示:式(II)。

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