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    • 1. 发明授权
    • Gap control system for turbine engines
    • 涡轮发动机间隙控制系统
    • US07234918B2
    • 2007-06-26
    • US11014271
    • 2004-12-16
    • Dieter BrillertWayne GiddensHarald HoellRobert W. SunshineJuergen HermelerHans-Thomas Bolms
    • Dieter BrillertWayne GiddensHarald HoellRobert W. SunshineJuergen HermelerHans-Thomas Bolms
    • F01D11/08
    • F01D11/001F01D11/025
    • Embodiments of the invention relate to a system and method for controlling the size of gaps in a turbine engine. In many instances, it is desirable to minimize the size of the gaps between neighboring rotating and stationary components in a turbine engine, such as between a disc cover plate and a proximate pre-swirler. According to embodiments of the invention, each component can be provided with a sealing surface. The sealing surfaces can be angled relative to the axis of rotation. The sealing surfaces are spaced from each other so as to form a gap therebetween. The sealing surfaces may or may not be substantially parallel. As a result of such configuration, the size of the gap can be controlled by axial and radial movement of the components. For example, the gap between the cover plate and the pre-swirler can be adjusted by axially movement of the rotor.
    • 本发明的实施例涉及一种用于控制涡轮发动机中的间隙尺寸的系统和方法。 在许多情况下,期望使涡轮发动机中的相邻旋转和静止部件之间的间隙的尺寸最小化,例如在盘盖板和邻近预旋流器之间。 根据本发明的实施例,每个部件可以设置有密封表面。 密封表面可以相对于旋转轴线成角度。 密封表面彼此间隔开,以便在它们之间形成间隙。 密封表面可以或可以不基本上平行。 作为这种构造的结果,可以通过部件的轴向和径向运动来控制间隙的尺寸。 例如,盖板和预旋流器之间的间隙可以通过转子的轴向运动来调节。
    • 2. 发明申请
    • Gap control system for turbine engines
    • 涡轮发动机间隙控制系统
    • US20060133927A1
    • 2006-06-22
    • US11014271
    • 2004-12-16
    • Dieter BrillertWayne GiddensHarald HoellRobert SunshineJuergen HermelerHans-Thomas Bolms
    • Dieter BrillertWayne GiddensHarald HoellRobert SunshineJuergen HermelerHans-Thomas Bolms
    • F04D29/08
    • F01D11/001F01D11/025
    • Embodiments of the invention relate to a system and method for controlling the size of gaps in a turbine engine. In many instances, it is desirable to minimize the size of the gaps between neighboring rotating and stationary components in a turbine engine, such as between a disc cover plate and a proximate pre-swirler. According to embodiments of the invention, each component can be provided with a sealing surface. The sealing surfaces can be angled relative to the axis of rotation. The sealing surfaces are spaced from each other so as to form a gap therebetween. The sealing surfaces may or may not be substantially parallel. As a result of such configuration, the size of the gap can be controlled by axial and radial movement of the components. For example, the gap between the cover plate and the pre-swirler can be adjusted by axially movement of the rotor.
    • 本发明的实施例涉及一种用于控制涡轮发动机中的间隙尺寸的系统和方法。 在许多情况下,期望使涡轮发动机中的相邻旋转和静止部件之间的间隙的尺寸最小化,例如在盘盖板和邻近预旋流器之间。 根据本发明的实施例,每个部件可以设置有密封表面。 密封表面可以相对于旋转轴线成角度。 密封表面彼此间隔开,以便在它们之间形成间隙。 密封表面可以或可以不基本上平行。 作为这种构造的结果,可以通过部件的轴向和径向运动来控制间隙的尺寸。 例如,盖板和预旋流器之间的间隙可以通过转子的轴向运动来调节。
    • 4. 发明授权
    • Arrangement for axially securing rotating blades in a rotor, sealing element for such an arrangement, and use of such an arrangement
    • 用于将旋转叶片轴向固定在转子中的布置,用于这种布置的密封元件以及这种布置的使用
    • US08105041B2
    • 2012-01-31
    • US11991439
    • 2006-08-21
    • Dieter BrillertHarald HoellArmin HülfenhausClaus Vögelin
    • Dieter BrillertHarald HoellArmin HülfenhausClaus Vögelin
    • F01D5/32
    • F01D5/3015F05D2250/70F05D2260/30
    • An arrangement is presented for axially securing rotating blades in a rotor, having a shaft collar on whose external circumference rotating blade securing grooves which extend in the axial direction of the rotor are provided. At one end side face of the shaft a projection is arranged in the region of the securing grooves, in which projection a circumferential groove which is open radially towards the outside is provided and said projection having securing grooves which are arranged in each rotating bade, sheet-metal-shaped sealing elements which each engage in the circumferential groove and in the securing groove and form an end side sealing ring in the circumferential direction being provided for axially securing the rotating blades, and at least one of the sealing elements comprising a sheet metal strip which is attached to said sealing ring in order to secure the sealing elements against displacement in the circumferential direction.
    • 提出了一种用于将旋转叶片轴向固定在转子中的布置,其具有轴套,在其上设置有在转子的轴向方向上延伸的外圆周旋转叶片固定槽。 在轴的一端侧面设置突起,在突出部分设置有朝径向向外侧开口的圆周槽,并且所述突起具有设置在每个旋转板中的固定槽 金属形的密封元件,其各自接合在周向槽中和固定槽中并且在周向上形成端侧密封环,用于轴向地固定旋转叶片,并且至少一个密封元件包括钣金 条带,其附接到所述密封环,以便确保密封元件在周向方向上的位移。
    • 8. 发明申请
    • Non-Positive-Displacement Machine and Rotor for a Non-Positive-Displacement Machine
    • 非正位移机和非正位移机的转子
    • US20080159864A1
    • 2008-07-03
    • US10593030
    • 2005-03-10
    • Harald Hoell
    • Harald Hoell
    • F01D5/02
    • F01D5/026F01D5/048F01D5/088F01D25/12F05D2260/4031
    • The invention relates to a rotor for a non-positive-displacement machine provided with a hollow shaft, which is arranged coaxial to the rotation axis, is supported, on both sides and on the face, on two axially opposed sections of the rotor, and which encloses an inner hollow space. In order to provide a rotor for a non-positive-displacement machine, which has a higher serviceable life and is less susceptible to mechanical defects, the invention provides that the hollow shaft, in the axial direction of the rotor, is formed from a number of adjoining rings, and the rings are outwardly sealed against one another an with regard to the sections of the hollow space. Each ring has an I-shaped cross-section and the web of the I shape extends in the radial direction of the rotor.
    • 本发明涉及一种非正排量机的转子,其具有与旋转轴同轴设置的中空轴,在转子的两个轴向相对的部分的两侧和面上被支撑,以及 其包围内部中空空间。 为了提供具有较高使用寿命并且不易受机械缺陷的非正排量机的转子,本发明提供了一种空心轴,其在转子的轴向方向上由多个 邻接的环,并且环相对于中空空间的部分彼此向外密封。 每个环具有I形横截面,并且I形腹板在转子的径向方向上延伸。