Combustor for gas turbine
    3.
    发明授权
    Combustor for gas turbine 失效
    燃气轮机燃烧器

    公开(公告)号:US4926645A

    公开(公告)日:1990-05-22

    申请号:US387146

    申请日:1989-07-31

    IPC分类号: F02C7/22 F23R3/40

    CPC分类号: F23R3/40

    摘要: A catalytic combustor for a gas turbine comprises catalyst layers arranged in two stages in a direction of gas flow. Fuel supply nozzles are disposed close to and upstream of the downstream catalyst layer. A substantially constant amount of fuel is supplied from the fuel supply nozzles to form pilot flames by the downstream catalyst layer, which are above 1000 degrees C. and below 1500 degrees C. Combustible component having passed through the upstream catalyst layer is burned by the pilot flames.

    摘要翻译: 用于燃气轮机的催化燃烧器包括沿气流方向分成两级的催化剂层。 燃料供给喷嘴设置在下游催化剂​​层附近和上游。 从燃料供给喷嘴供给大致恒定量的燃料,通过下游催化剂​​层形成先导火焰,该催化剂层高于1000℃,低于1500℃。通过上游催化剂层的可燃组分被飞行员 火焰

    Method for producing a ceramic-coated blade of gas turbine
    4.
    发明授权
    Method for producing a ceramic-coated blade of gas turbine 失效
    燃气轮机陶瓷涂层刀片的制造方法

    公开(公告)号:US06521293B1

    公开(公告)日:2003-02-18

    申请号:US09511187

    申请日:2000-02-23

    IPC分类号: C23C1630

    摘要: A ceramic-coated blade of a gas turbine and a method of producing the same, in which the thickening of an Al2O3 layer at the interface between a ceramic layer and a primary layer is sufficiently prevented for a long period of time, thereby positively suppressing the separation of the ceramic layer. Using powder of MCrAlY alloy (Co—32%Ni—21%Cr—8%Al—0.5%Y), a primary layer (alloy coating layer) is formed on a surface of a substrate made of a heat-resistant Ni base alloy (Rene'-80). Further, a heat-resistant ceramic layer, comprising a mixture of ion-conductive ZrO2—8wt. %Y2O3 ceramic and insulative ceramic (e.g. Al2O3), is formed on the alloy coating layer. This mixture has a columnar structure in which columnar crystals are grown by a gas phase in a direction of a thickness of the coating, or a porous structure in which flattened particles brought about from molten particles caused to fly at high velocity are laminated.

    摘要翻译: 燃气轮机的陶瓷涂覆刀片及其制造方法,其中在陶瓷层和主层之间的界面处的Al 2 O 3层的增厚被充分地长时间地防止,从而积极地抑制 分离陶瓷层。 使用MCrAlY合金(Co-32%Ni-21%Cr-8%Al-0.5%Y)的粉末,在由耐热Ni基合金制成的基板的表面上形成一层(合金涂层) (Rene'-80)。 此外,还包括耐热陶瓷层,其包含离子传导性ZrO 2 -8wt。 %Y 2 O 3陶瓷和绝缘陶瓷(例如Al 2 O 3)形成在合金涂层上。 该混合物具有柱状结构,其中柱状结晶通过气相在涂层的厚度方向上生长,或多层结构,其中由熔融颗粒引起的高速飞行的扁平颗粒被层压。

    Method of non-destructively estimating life of ceramic member
    6.
    发明授权
    Method of non-destructively estimating life of ceramic member 失效
    无损估计陶瓷构件寿命的方法

    公开(公告)号:US5625153A

    公开(公告)日:1997-04-29

    申请号:US572891

    申请日:1995-12-18

    IPC分类号: G01N33/38 G01N3/00

    CPC分类号: G01N33/388

    摘要: A method of estimating non-destructively the life expectancy of ceramic members, at least a surface layer of which is made of ceramics, is disclosed. The method comprises measuring a variation in at least one of physical characteristics of said ceramic members including color, grain size, electroconductivity and Young's modulus and estimating the life expectancy of the ceramic members on the basis of the predetermined relationship between the life of said ceramics and the physical characteristics. The method is excellent in estimation of the life expectancy of ceramic members of gas turbines or nuclear fusion reactor since the life expectancy of the members to be inspected can easily be estimated in a short time without fracturing the members.

    摘要翻译: 公开了一种非破坏性地估计陶瓷构件的寿命的方法,陶瓷构件的至少表面层由陶瓷制成。 该方法包括测量所述陶瓷构件的物理特性中的至少一个的变化,包括颜色,晶粒尺寸,导电性和杨氏模量,并且基于陶瓷构件的寿命和陶瓷构件的寿命之间的预定关系来估计陶瓷构件的预期寿命 身体特征。 该方法在估计燃气轮机或核聚变反应堆的陶瓷构件的预期寿命方面是非常好的,因为待检查构件的预期寿命可以很容易地在短时间内被估计而不破坏构件。

    Reproducing apparatus with suspension supporting a floating-type head
with a bevelled slider
    9.
    发明授权
    Reproducing apparatus with suspension supporting a floating-type head with a bevelled slider 失效
    具有悬挂的再现装置,其支撑具有倾斜滑块的浮动头

    公开(公告)号:US5313445A

    公开(公告)日:1994-05-17

    申请号:US840905

    申请日:1992-02-25

    摘要: An information reproducing apparatus which has a rotating driver for rotating a disc-shaped recording medium, a floating-type head for reproducing information recorded in the recording medium while floating above the disc-shaped recording medium that is being rotated by the rotating driver, and a suspension, made of an elastic member, for supporting the floating-type head. The information reproducing apparatus is characterized in that the floating-type head has a slider which is floated by an air flow that is directed near the surface of the rotating disc-shaped recording medium, and that the slider has a bevelled portion at one side that faces the outer edge of the disc-shaped recording medium such that any contact between the slider and the ridge that exists along the outer edge area of the disc-shaped recording medium is virtually eliminated. Since the slider is virtually free from contacting the ridge that exists along the outer edge area of the disc-shaped recording medium, the storage capacity of the disc-shaped recording medium can be more effectively used.

    摘要翻译: 一种具有用于旋转盘形记录介质的旋转驱动器的信息再现装置,用于在浮动在由旋转驱动器旋转的盘形记录介质上方的同时再现记录在记录介质中的信息的浮动型头;以及 由弹性构件制成的用于支撑浮动头的悬架。 信息重放装置的特征在于,浮动式头部具有滑块,该滑块由朝向旋转的盘形记录介质的表面的空气流浮动,并且滑块在一侧具有倾斜部分, 面对盘状记录介质的外边缘,从而实质上消除了沿盘形记录介质的外边缘区域存在的滑块和凸脊之间的任何接触。 由于滑块实际上没有接触沿着盘形记录介质的外边缘区域存在的脊,所以可以更有效地使用盘形记录介质的存储容量。

    Combustor for gas turbine
    10.
    发明授权
    Combustor for gas turbine 失效
    燃气轮机燃烧器

    公开(公告)号:US4766721A

    公开(公告)日:1988-08-30

    申请号:US917973

    申请日:1986-10-14

    摘要: A combustor of two-stage combustion type in which fuel is supplied only from primary fuel nozzles for combustion only in primary combustion chamber under the operating condition where gas turbine load is low, and premixed mixture is supplied into a secondary combustion chamber provided on the downstream side of the primary combustion chamber for combustion in both the primary and secondary combustion chambers under the operating condition where the load is high. An air-bleed passageway opens on a downstream side of air holes for intaking secondary combustion air to be mixed with secondary fuel and communicates with the outside of the combustor. The air-bleed passageway is provided with a regulating valve and the secondary combustion air is bled at the minimum point of the load where the secondary fuel is supplied so that the fuel to air ratio of secondary premixed mixture may not be excessively lean, thereby reducing the production of non-burned components.

    摘要翻译: 一种二级燃烧式的燃烧器,其中,在燃气轮机负荷低的运行条件下,燃料仅从主燃料喷嘴供给燃料,仅在一级燃烧室中燃烧,并且将预混合物供给到设置在下游的二次燃烧室 在一次燃烧室中,在负载高的运行条件下在一次燃烧室和二次燃烧室中燃烧。 排气通道在气孔的下游侧开口,用于吸入与二次燃料混合的二次燃烧空气并与燃烧器的外部连通。 排气通道设置有调节阀,二次燃烧空气在供给二次燃料的负载的最小点处排出,使得二次预混混合物的燃料与空气的比例可能不会过度减少,从而减少 生产非烧成分。