Target/stem connection utilizing a diffusion enhancer for x-ray tube
anode assemblies
    13.
    发明授权
    Target/stem connection utilizing a diffusion enhancer for x-ray tube anode assemblies 失效
    使用X射线管阳极组件的扩散增强器的靶/茎连接

    公开(公告)号:US5530733A

    公开(公告)日:1996-06-25

    申请号:US272064

    申请日:1994-07-08

    IPC分类号: H01J35/10

    摘要: An improved high performance x-ray system having a rotating anode therein which includes an improved target/stem connection and a coating, operatively positioned between the target and the stem, for enhancing the diffusion therebetween to reduce tube failure due to anode assembly imbalance comprising a metallic target and a metal stem bonded to provide a composite rotating x-ray tube target is disclosed. An insert of an alloy, for example, titanium alloy, is placed between the target layer, the stem and a coating, operatively positioned between the target and the stem, for enhancing the diffusion therebetween and then bonded thereto to produce a composite x-ray tube target/stem having a high remelt temperature and bond strength which retains its balance throughout the manufacturing process and during x-ray tube operations is also disclosed.

    摘要翻译: 改进的高性能x射线系统,其中具有旋转阳极,其包括改进的靶/杆连接和可操作地定位在靶和杆之间的涂层,用于增强其间的扩散,以减少由于阳极组件不平衡引起的管故障,包括 公开了金属靶和结合以提供复合旋转X射线管靶的金属杆。 将合金例如钛合金的插入件放置在目标层,杆和可操作地定位在靶和杆之间的涂层之间,以增强它们之间的扩散,然后结合到其上以产生复合X射线 还公开了具有高重熔温度和粘合强度的管靶/杆,其在整个制造过程中和在x射线管操作期间保持其平衡。

    Clad structural member with NbTiAl low Hf alloy cladding and niobium
base metal core
    14.
    发明授权
    Clad structural member with NbTiAl low Hf alloy cladding and niobium base metal core 失效
    具有NbTiAl低Hf合金包层和铌基金属芯的包层结构件

    公开(公告)号:US5426001A

    公开(公告)日:1995-06-20

    申请号:US953700

    申请日:1992-09-30

    IPC分类号: C22C47/00 C22C49/10 C22C1/09

    摘要: Composite structures having a higher density, stronger reinforcing niobium based alloy embedded within a lower density, lower strength niobium based cladding alloy are provided. The cladding is preferably an alloy having a niobium and titanium base according to the expression:Nb.sub.balance --Ti.sub.40-48 --Al.sub.12-22 --Hf.sub.0.5-6.The reinforcement may be in the form of plates, sheets or rods of the higher strength, higher temperature niobium based reinforcing alloy. The same crystal form is present in both the matrix and the reinforcement and is specifically body centered cubic crystal form.

    摘要翻译: 提供了具有较高密度,更强的增强铌基合金嵌入较低密度的复合结构,较低强度的铌基包层合金。 包层优选为根据以下表达式的具有铌和钛基的合金:Nbbalance-Ti40-48-Al12-22-Hf0.5-6。 加强件可以是较高强度,较高温度的铌基增强合金的板,片或棒的形式。 在基质和强化物中都存在相同的晶体形式,特别是体心立方晶体形式。

    Clad structural member with NbTiAl high Hf alloy cladding and niobium
base metal core
    15.
    发明授权
    Clad structural member with NbTiAl high Hf alloy cladding and niobium base metal core 失效
    包层结构件,NbTiAl高Hf合金包层和铌基底金属芯

    公开(公告)号:US5306570A

    公开(公告)日:1994-04-26

    申请号:US953911

    申请日:1992-09-30

    IPC分类号: C22C49/10 C22C1/09

    摘要: Composite structures having a higher density, stronger reinforcing niobium based alloy embedded within a lower density, lower strength niobium based cladding alloy are provided. The cladding is preferably an alloy having a niobium and titanium base according to the expression:Nb balance-Ti32-45-Al-3-18-Hf-8-15.The reinforcement may be in the form of plates, sheets or rods of the higher strength, higher temperature niobium based reinforcing alloy. The same crystal form is present in both the matrix and the reinforcement and is specifically body centered cubic crystal form.

    摘要翻译: 提供了具有较高密度,更强的增强铌基合金嵌入较低密度的复合结构,较低强度的铌基包层合金。 根据Nb平衡-Ti32-45-Al-3-18-Hf-8-15的形式,包层优选为具有铌和钛基的合金。 加强件可以是较高强度,较高温度的铌基增强合金的板,片或棒的形式。 在基质和强化物中都存在相同的晶体形式,特别是体心立方晶体形式。

    Clad structural member with NbTiAlCr HF alloy cladding and niobium base
metal core
    17.
    发明授权
    Clad structural member with NbTiAlCr HF alloy cladding and niobium base metal core 失效
    包层结构件采用NbTiAlCr HF合金包层和铌基底金属芯

    公开(公告)号:US5273831A

    公开(公告)日:1993-12-28

    申请号:US953702

    申请日:1992-09-30

    摘要: Composite structures having a higher density, stronger reinforcing niobium based alloy embedded within a lower density, lower strength niobium based cladding alloy are provided. The cladding is preferably an alloy having a niobium and titanium base according to the expression:Nb.sub.balance -Ti.sub.27-40.5 -Al.sub.4.5-10.5 -Hf.sub.1.5-5.5 V.sub.0-6 Cr.sub.4.5-8.5 Zr.sub.0-1 C.sub.0-0.5,where each metal of the metal/metal composite has a body centered cubic crystal structure, andwherein the ratio of concentrations of Ti to Nb (Ti/Nb) is greater than or equal (.gtoreq.) to 0.5, andwherein the maximum concentration of the Hf+V+Al+Cr additives is less than or equal (.ltoreq.) to the expression:16.5+5.times.Ti/Nb.The reinforcement may be in the form of plates, sheets or rods of the higher strength, higher temperature niobium based reinforcing alloy. The same crystal form is present in both the matrix and the reinforcement and is specifically body centered cubic crystal form.

    摘要翻译: 提供了具有较高密度,更强的增强铌基合金嵌入较低密度的复合结构,较低强度的铌基包层合金。 包层优选为根据以下表达式具有铌和钛基的合金:Nbbalance-Ti27-40.5-Al4.5-10.5-Hf1.5-5.5V0-6Cr4.5-8.5Zr0-1C0-0.5,其中每种金属 的金属/金属复合体具有体心立方晶体结构,其中Ti与Nb的浓度比(Ti / Nb)大于或等于(> / =)至0.5,其中Hf的最大浓度 + V + Al + Cr添加剂与16.5 + 5×Ti / Nb的表达式小于或等于(<=)。 加强件可以是较高强度,较高温度的铌基增强合金的板,片或棒的形式。 在基质和强化物中都存在相同的晶体形式,特别是体心立方晶体形式。

    Material system for high temperature jet engine operation
    19.
    发明授权
    Material system for high temperature jet engine operation 失效
    高温喷气发动机运行材料系统

    公开(公告)号:US4904546A

    公开(公告)日:1990-02-27

    申请号:US331762

    申请日:1989-04-03

    申请人: Melvin R. Jackson

    发明人: Melvin R. Jackson

    摘要: A materials system is provided which is adapted for use in jet engines operable at high temperature and at lower density than possible with nickel base superalloys. A range of niobium base alloys is combined with a range of protective metallic coatings to provide a material system which permits a wide variety of alloy properties and performance characteristics to be combined in structural components of jet engines.

    摘要翻译: 提供了一种材料系统,其适用于在镍基超级合金的高温和低密度下可操作的喷气发动机。 一系列铌基合金与一系列保护性金属涂层结合,以提供允许各种合金性能和性能特性组合在喷气发动机的结构部件中的材料系统。