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    • 49. 发明授权
    • Antifoulant control process
    • 防污染控制过程
    • US06294078B1
    • 2001-09-25
    • US09611606
    • 2000-07-07
    • Alan D. EastmanRonald E. Brown
    • Alan D. EastmanRonald E. Brown
    • C01G916
    • C10G75/04
    • A process is provided by the invention which comprises: (a) providing a tubular reactor having an inlet and an outlet, a furnace for heating the reactor, and a cooler having an inlet in communication with the reactor outlet and also having an outlet; (b) introducing a substantially constant flow of feed gas comprising steam to the reactor inlet while the reactor is heated by the furnace to produce a predetermined and substantially constant reactor outlet temperature; and (c) controlling, during at least a portion of (b), the concentration of an antifoulant in the feed gas based on cooler outlet temperature.
    • 本发明提供了一种方法,其包括:(a)提供具有入口和出口的管式反应器,用于加热反应器的炉子和具有与反应器出口连通并具有出口的入口的冷却器; (b)当反应器被炉加热以产生预定且基本上恒定的反应器出口温度时,将包含蒸汽的基本恒定的进料气流引入反应器入口; 和(c)在(b)的至少一部分期间基于较冷的出口温度来控制进料气体中防污剂的浓度。
    • 50. 发明授权
    • Shaped-charge device with progressive inward collapsing jet
    • 具有逐渐向内折叠射流的成形装置
    • US5614692A
    • 1997-03-25
    • US497541
    • 1995-06-30
    • Ronald E. BrownMark E. Majerus
    • Ronald E. BrownMark E. Majerus
    • F42B1/028F42B1/02
    • F42B1/028
    • In a shaped-charge device, the liner is so shaped that bulges are formed in the jet without causing the jet to deviate from the central axis. The shaped-charge device includes a case defining an axisymmetrical forwardly-opening cavity uniformly disposed about a central axis; an axisymmetrical, homogeneous-material, liner of variable thickness defining a forwardly-opening cavity having a closed apex, with the cavity being uniformly disposed within the casing about the central axis; and explosive material symmetrically disposed between the casing and the liner. The liner is so shaped that in response to the explosive material being detonated to thereby explode, the liner is progressively collapsed inward by the exploding material to be formed into a fluid jet of the homogeneous liner material that is forwardly expelled at a varying velocity from the casing along the central axis, with the forward portion of the jet being squeezed from the apex of the collapsing liner. The rate of change of liner thickness with respect to liner axial position varies such that, after the formation of the forward portion of the jet, the velocity of the jet-forming material at at least one intermediate position within the jet varies so as to cause the material to bunch up to form a symmetrical bulge at each intermediate position within the jet, but not such that the velocity of the jet-forming material increases at any such intermediate position while the material is bunching up, thereby inhibiting the material from so bunching up as to cause the jet to deviate from the central axis.
    • 在成形装置中,衬套是这样的形状,使得在射流中形成凸起而不会使射流偏离中心轴线。 成形装置包括壳体,其限定围绕中心轴线均匀设置的轴对称正向开口空腔; 限定具有闭合顶点的向前开口腔的可变厚度的轴对称均匀材料衬里,其中空腔围绕中心轴线均匀地设置在壳体内; 和对称地设置在壳体和衬套之间的爆炸性材料。 内衬的形状是这样形状的:响应于爆炸材料被引爆而引起爆炸,衬套由于爆炸材料向内逐渐塌陷,以形成均匀衬垫材料的流体射流,该流体射流以不同速度向前排出 壳体沿着中心轴线,其中喷射器的前部从挤压衬套的顶点挤压。 衬套厚度相对于衬套轴向位置的变化率变化,使得在射流的前部形成之后,喷射形成材料在射流内的至少一个中间位置的速度变化,从而导致 这种材料在射流内的每个中间位置聚集形成对称的凸起,但不能使得在材料聚集时任何这样的中间位置喷射形成材料的速度增加,从而抑制材料的聚集 使飞机偏离中心轴。