会员体验
专利管家(专利管理)
工作空间(专利管理)
风险监控(情报监控)
数据分析(专利分析)
侵权分析(诉讼无效)
联系我们
交流群
官方交流:
QQ群: 891211   
微信请扫码    >>>
现在联系顾问~
热词
    • 5. 发明申请
    • Thermal control of gas turbine engine rings for active clearance control
    • 用于主动间隙控制的燃气轮机发动机环的热控制
    • US20070140839A1
    • 2007-06-21
    • US11303688
    • 2005-12-16
    • Michael BucaroRafael RuizRobert AlbersScott EstridgeRoger Wartner
    • Michael BucaroRafael RuizRobert AlbersScott EstridgeRoger Wartner
    • F04D29/58
    • F01D11/24
    • A gas turbine engine thermal control apparatus includes at least one annular spray tube having spray holes oriented to impinge thermal control air onto a fillet between an outer casing and a forward thermal control ring and, in a more particular embodiment, into a center of the fillet. The apparatus may include an annular segmented stator shroud attached to the outer casing and circumscribing radial outer blade tips of turbine blades of a turbine rotor. A thermal air distribution manifold encircling a portion of the outer casing includes an annular supply tube connected in fluid supply relationship to plenums of header assemblies. The annular spray tube is connected to at least one of the plenums and may be elongated radially inwardly and axially. Baffles attached to radially outwardly facing surfaces of the panels may be contoured to form exhaust passages having exhaust passage inlets and outlets between the baffles and the panels.
    • 燃气涡轮发动机热控制装置包括至少一个具有喷射孔的环形喷射管,所述喷射孔定向成将热控制空气冲击到外壳和向前热控制环之间的圆角上,并且在更具体的实施例中,进入圆角的中心 。 该装置可以包括附接到外壳并且包围涡轮转子的涡轮叶片的径向外叶片尖端的环形分段定子罩。 环绕外壳的一部分的热空气分配歧管包括以流体供应关系连接到集管组件的气室的环形供应管。 环形喷射管连接到至少一个通气室,并且可以径向向内和轴向地伸长。 附接到面板的径向向外表面的挡板可以被轮廓化以形成排气通道,其具有在挡板和面板之间的排气通道入口和出口。
    • 8. 发明授权
    • Method and apparatus for controlling fluid leakage through gas turbine engines
    • 用于控制通过燃气涡轮发动机的流体泄漏的方法和装置
    • US06932567B2
    • 2005-08-23
    • US10326028
    • 2002-12-19
    • Robert Joseph AlbersMarcia Jean BoyleRafael Ruiz
    • Robert Joseph AlbersMarcia Jean BoyleRafael Ruiz
    • F01D11/00F01D11/02F16J15/34
    • F16J15/3448F01D11/003F01D11/02
    • A method for controlling fluid leakage between a first pressure region and a second pressure region within a gas turbine engine using a first sealing member and a second sealing member. The first sealing member is movably coupled to a portion of the gas turbine engine, and a space defined generally between a portion of the first sealing member and a portion of the second sealing member fluidly couples the first pressure region to the second pressure region. The method includes moving the first sealing member towards the second sealing member using fluid pressure within a portion of the engine, and, using the first and second sealing members, substantially controlling fluid leakage between the first pressure area and the second pressure area through the space generally without contacting the first sealing member with the second sealing member.
    • 一种使用第一密封构件和第二密封构件来控制燃气涡轮发动机内的第一压力区域和第二压力区域之间的流体泄漏的方法。 第一密封构件可移动地联接到燃气涡轮发动机的一部分,并且通常在第一密封构件的一部分和第二密封构件的一部分之间限定的空间将第一压力区域流体耦合到第二压力区域。 该方法包括使用发动机的一部分内的流体压力将第一密封构件朝向第二密封构件移动,并且使用第一和第二密封构件,通过空间基本上控制第一压力区域和第二压力区域之间的流体泄漏 通常不使第一密封构件与第二密封构件接触。