Seal apparatus for a turbomachine casing

    公开(公告)号:US11118594B2

    公开(公告)日:2021-09-14

    申请号:US16611269

    申请日:2018-05-02

    发明人: Daniel J. Griffin

    IPC分类号: F04D29/08 F01D1/06 F04D29/42

    摘要: A seal apparatus for a casing of a turbomachine. The seal apparatus may include an annular body having first and second annular body portions and an appendage. The second annular body portion may extend axially from the first annular body portion and may have an outer annular surface radially offset from an outer annular surface of the first annular body portion. The appendage may extend axially from the first annular body portion and may have an outer annular surface and an inner annular surface. The inner annular surface of the appendage and the outer annular surface of the second annular body portion may define an annular cavity therebetween, and at least a portion of the appendage may be configured to be displaced radially outward in order to maintain contact with first and second inner cylindrical surfaces of the casing during radial expansion of the casing.

    SEAL APPARATUS FOR A TURBOMACHINE CASING
    3.
    发明申请

    公开(公告)号:US20200166046A1

    公开(公告)日:2020-05-28

    申请号:US16611269

    申请日:2018-05-02

    发明人: Daniel J. Griffin

    IPC分类号: F04D29/08 F04D29/42

    摘要: A seal apparatus for a casing of a turbomachine. The seal apparatus may include an annular body having first and second annular body portions and an appendage. The second annular body portion may extend axially from the first annular body portion and may have an outer annular surface radially offset from an outer annular surface of the first annular body portion. The appendage may extend axially from the first annular body portion and may have an outer annular surface and an inner annular surface. The inner annular surface of the appendage and the outer annular surface of the second annular body portion may define an annular cavity therebetween, and at least a portion of the appendage may be configured to be displaced radially outward in order to maintain contact with first and second inner cylindrical surfaces of the casing during radial expansion of the casing.

    SEAL FOR A HIGH-PRESSURE TURBOMACHINE
    4.
    发明申请
    SEAL FOR A HIGH-PRESSURE TURBOMACHINE 有权
    密封用于高压涡轮机

    公开(公告)号:US20150016988A1

    公开(公告)日:2015-01-15

    申请号:US14317283

    申请日:2014-06-27

    申请人: Daniel J. Griffin

    发明人: Daniel J. Griffin

    IPC分类号: F04D29/16

    摘要: An annular seal is provided for use in a turbomachine. The annular seal may form a generally rectangular cross-section and may include an outer radial surface forming an outer sealing surface and defining at least one annular groove and a plurality of slots spaced circumferentially about the outer radial surface. Each slot may have an end terminating in the at least one annular groove. The annular seal may also include a first axial sidewall forming a sidewall sealing surface and a recessed portion and a second axial sidewall opposing the first axial sidewall. At least one annular groove and the plurality of slots may be configured to maintain a low pressure environment across at least a portion of the outer radial surface. The second axial sidewall, the recessed portion, and the inner radial surface may be configured to maintain a high pressure environment there across during operation of the turbomachine.

    摘要翻译: 提供用于涡轮机中的环形密封件。 环形密封件可以形成大致矩形的横截面并且可以包括形成外密封表面的外径向表面,并且限定至少一个环形槽和围绕外径向表面周向间隔开的多个槽。 每个槽可以具有终止于至少一个环形槽中的端部。 环形密封件还可以包括形成侧壁密封表面的第一轴向侧壁和与第一轴向侧壁相对的凹陷部分和第二轴向侧壁。 至少一个环形槽和多个狭槽可被构造成在外部径向表面的至少一部分上保持低压环境。 第二轴向侧壁,凹陷部分和内部径向表面可构造成在涡轮机操作期间保持横跨高压环境。

    Gas turbine engine systems involving rotor bayonet coverplates and tools for installing such coverplates
    5.
    发明授权
    Gas turbine engine systems involving rotor bayonet coverplates and tools for installing such coverplates 有权
    包括转子卡口盖板的燃气涡轮发动机系统和用于安装这种盖板的工具

    公开(公告)号:US08313289B2

    公开(公告)日:2012-11-20

    申请号:US11952367

    申请日:2007-12-07

    IPC分类号: F01D11/02

    摘要: Gas turbine engine systems involving rotor bayonet coverplates and tools for installing such coverplates are provided. In this regard, a representative turbine assembly for a gas turbine engine includes: a turbine disk operative to mount a set of turbine blades; and a coverplate having an annular main body portion and a spaced annular arrangement of tabs extending radially inwardly from the main body portion with open-ended gaps being located between the tabs, the tabs being operative to secure an inner diameter of the coverplate to the turbine disk.

    摘要翻译: 提供涉及转子卡口盖板的燃气涡轮发动机系统和用于安装这种盖板的工具。 在这方面,用于燃气涡轮发动机的代表性的涡轮组件包括:涡轮盘,其可操作地安装一组涡轮叶片; 以及具有环形主体部分和间隔开的从所述主体部分径向向内延伸的环形布置的盖板,其中开口间隙位于所述突片之间,所述突出部可操作以将所述盖板的内径固定到所述涡轮机 磁盘。

    Seal for a high-pressure turbomachine
    6.
    发明授权
    Seal for a high-pressure turbomachine 有权
    密封用于高压涡轮机

    公开(公告)号:US09303655B2

    公开(公告)日:2016-04-05

    申请号:US14317283

    申请日:2014-06-27

    申请人: Daniel J. Griffin

    发明人: Daniel J. Griffin

    IPC分类号: F04D29/16 F04D29/42 F04D17/12

    摘要: An annular seal is provided for use in a turbomachine. The annular seal may form a generally rectangular cross-section and may include an outer radial surface forming an outer sealing surface and defining at least one annular groove and a plurality of slots spaced circumferentially about the outer radial surface. Each slot may have an end terminating in the at least one annular groove. The annular seal may also include a first axial sidewall forming a sidewall sealing surface and a recessed portion and a second axial sidewall opposing the first axial sidewall. At least one annular groove and the plurality of slots may be configured to maintain a low pressure environment across at least a portion of the outer radial surface. The second axial sidewall, the recessed portion, and the inner radial surface may be configured to maintain a high pressure environment there across during operation of the turbomachine.

    摘要翻译: 提供用于涡轮机中的环形密封件。 环形密封件可以形成大致矩形的横截面并且可以包括形成外密封表面的外径向表面,并且限定至少一个环形槽和围绕外径向表面周向间隔开的多个槽。 每个槽可以具有终止于至少一个环形槽中的端部。 环形密封件还可以包括形成侧壁密封表面的第一轴向侧壁和与第一轴向侧壁相对的凹陷部分和第二轴向侧壁。 至少一个环形槽和多个狭槽可被构造成在外部径向表面的至少一部分上保持低压环境。 第二轴向侧壁,凹陷部分和内部径向表面可构造成在涡轮机操作期间保持横跨高压环境。

    SLIDABLE COVER FOR CASING ACCESS PORT
    7.
    发明申请
    SLIDABLE COVER FOR CASING ACCESS PORT 有权
    用于进出口的滑动盖

    公开(公告)号:US20100239419A1

    公开(公告)日:2010-09-23

    申请号:US12407909

    申请日:2009-03-20

    IPC分类号: F04D29/40 F04D29/60 F01D25/24

    CPC分类号: F04D27/0215 F04D29/441

    摘要: A closure device for a casing having at least one access opening wherein the closure device includes a cover member movably disposed within an interior chamber of the casing so as to be slidably displaceable along or in the direction of a casing central axis between an open and a closed position, the cover member being spaced at least partially axially from the access opening in the open position so as to permit access to the interior chamber and generally extending across and substantially obstructing the at least one access opening in the closed position.

    摘要翻译: 一种用于壳体的封闭装置,具有至少一个进入开口,其中所述封闭装置包括可移动地设置在所述壳体的内部腔室内的盖构件,以便沿着或沿着壳体中心轴线的方向可滑动地移位, 所述盖构件在所述打开位置中至少部分地与所述进入开口轴向间隔开,以便允许进入所述内部室并且大体上在所述关闭位置中延伸并且基本上阻挡所述至少一个进入开口。

    Programmable calculator having string variable editing capability
    8.
    发明授权
    Programmable calculator having string variable editing capability 失效
    具有字符串变量编辑功能的可编程计算器

    公开(公告)号:US4180854A

    公开(公告)日:1979-12-25

    申请号:US837771

    申请日:1977-09-29

    IPC分类号: G06F15/02 G06F3/02 G06F3/14

    CPC分类号: G06F15/02

    摘要: A programmable calculator employs modular read-write and read-only memories separately expandable to provide additional program and data storage functions within the calculator oriented toward the environment of the user and two sixteen bit LSI NMOS central processing units. One of the central processing units (LPU) is employed to perform language syntaxing, arithmetic, and general supervision of program execution. The second central processing unit (PPU) is employed for managing input/output operations. Communication between the two central processing units is accomplished by an arrangement through which the two central processing units share a common portion of memory. The calculator also includes a keyboard having a full complement of alphanumeric keys for entering programs and data into the calculator and for otherwise allowing the user to control operation of the calculator. The calculator further includes a CRT that can be operated in either an alphanumeric mode or a graphics mode, two magnetic tape transports that permit the user to store information into and to retrieve information from the user portion of the calculator read-write memory, and an 80-column thermal printer utilizing a print head that includes 560 thermal print resistors arranged in a single horizntal row.

    摘要翻译: 可编程计算器采用单独可扩展的模块化读写和只读存储器,在计算器内提供额外的程序和数据存储功能,面向用户环境和两个十六位LSI NMOS中央处理器。 中央处理单元(LPU)之一用于执行程序执行的语言语法,算术和一般监督。 第二个中央处理单元(PPU)用于管理输入/输出操作。 两个中央处理单元之间的通信由两个中央处理单元共享存储器的公共部分的布置来实现。 该计算器还包括具有全部字母数字键的键盘,用于将程序和数据输入到计算器中,并且否则允许用户控制计算器的操作。 计算器还包括可以以字母数字模式或图形模式操作的CRT,允许用户将信息存储到计算器读写存储器的用户部分并从其中检索信息的两个磁带传输,以及 80列热敏打印机利用包括布置在单个水平行中的560个热敏印刷电阻器的打印头。

    Gas Turbine Engine Systems Involving Rotor Bayonet Coverplates and Tools for Installing Such Coverplates
    9.
    发明申请
    Gas Turbine Engine Systems Involving Rotor Bayonet Coverplates and Tools for Installing Such Coverplates 有权
    涉及用于安装这种盖板的转子卡口盖板和工具的燃气轮机发动机系统

    公开(公告)号:US20090148295A1

    公开(公告)日:2009-06-11

    申请号:US11952367

    申请日:2007-12-07

    IPC分类号: F01D1/02

    摘要: Gas turbine engine systems involving rotor bayonet coverplates and tools for installing such coverplates are provided. In this regard, a representative turbine assembly for a gas turbine engine includes: a turbine disk operative to mount a set of turbine blades; and a coverplate having an annular main body portion and a spaced annular arrangement of tabs extending radially inwardly from the main body portion with open-ended gaps being located between the tabs, the tabs being operative to secure an inner diameter of the coverplate to the turbine disk.

    摘要翻译: 提供涉及转子卡口盖板的燃气涡轮发动机系统和用于安装这种盖板的工具。 在这方面,用于燃气涡轮发动机的代表性的涡轮组件包括:涡轮盘,其可操作地安装一组涡轮叶片; 以及具有环形主体部分和间隔开的从所述主体部分径向向内延伸的环形布置的盖板,其中开口间隙位于所述突片之间,所述突出部可操作以将所述盖板的内径固定到所述涡轮机 磁盘。

    Programmable calculator
    10.
    发明授权
    Programmable calculator 失效
    可编程计算器

    公开(公告)号:US4455618A

    公开(公告)日:1984-06-19

    申请号:US236394

    申请日:1981-02-20

    IPC分类号: G06F15/02

    CPC分类号: G06F15/02

    摘要: A programmable calculator employs modular read-write and read-only memories separately expandable to provide additional program and data storage functions within the calculator oriented toward the environment of the user and two sixteen bit LSI NMOS central processing units. One of the central processing units (LPU) is employed to perform language syntaxing, arithmetic, and general supervision of program execution. The second central processing unit (PPU) is employed for managing input/output operations. Communication between the two central processing units is accomplished by an arrangement through which the two central processing units share a common portion of memory. The calculator also includes a keyboard having a full complement of alphanumeric keys for entering programs and data into the calculator and for otherwise allowing the user to control operation of the calculator. The keyboard further includes a plurality of user-definable keys, some of which are pre-defined to have certain definitions at the time operating power is applied to the calculator.

    摘要翻译: 可编程计算器采用单独可扩展的模块化读写和只读存储器,在计算器内提供额外的程序和数据存储功能,面向用户环境和两个十六位LSI NMOS中央处理器。 中央处理单元(LPU)之一用于执行程序执行的语言语法,算术和一般监督。 第二个中央处理单元(PPU)用于管理输入/输出操作。 两个中央处理单元之间的通信由两个中央处理单元共享存储器的公共部分的布置来实现。 该计算器还包括具有全部字母数字键的键盘,用于将程序和数据输入到计算器中,并且否则允许用户控制计算器的操作。 键盘还包括多个用户可定义的键,其中一些键被预先定义为在操作电力被施加到计算器时具有某些定义。