Abstract: A set-top box (STB) receives a router reboot or reset activation code generated by an Operations Support System (OSS) that manages a first network. The STB activates a router reboot or reset function based on the received activation code, and identifies, upon activation of the router reboot or reset function, a model of a router connected to the STB. The STB generates a router reboot or reset command based on the identified model of the router and sends the generated router reboot or reset command to the router to cause the router to perform a reboot or reset process.

Abstract: A set-top box (STB) receives a router reboot or reset activation code generated by an Operations Support System (OSS) that manages a first network. The STB activates a router reboot or reset function based on the received activation code, and identifies, upon activation of the router reboot or reset function, a model of a router connected to the STB. The STB generates a router reboot or reset command based on the identified model of the router and sends the generated router reboot or reset command to the router to cause the router to perform a reboot or reset process.

Abstract: An article of manufacture having a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in a TABLE 1. Wherein X and Y are distances in inches which, when connected by smooth continuing arcs, define airfoil profile sections at each distance Z in inches. The profile sections at the Z distances being joined smoothly with one another to form a complete airfoil shape.

Abstract: An article of manufacture having a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in a TABLE 1. Wherein X and Y are distances in inches which, when connected by smooth continuing arcs, define airfoil profile sections at each distance Z in inches. The profile sections at the Z distances being joined smoothly with one another to form a complete airfoil shape.

Abstract: Eleventh stage stator vanes for a compressor comprise airfoil profiles substantially in accordance with Cartesian coordinate values of x, Y and Z set forth in inches in Table I, wherein the Z coordinate values are perpendicular distances from planes normal to a radius from the compressor centerline and containing the X and Y values with the Z value commencing at zero in the X, Y plane at a radial aerodynamic section of the airfoil. X and Y are coordinate values defining the airfoil profile at each distance Z. The X, Y and Z values may be scaled to provide a scaled-up or scaled-down airfoil section for each stator vane.