Abstract: A coated article is provided with a low-emissivity (low-E) coating on a glass substrate. The low-E coating includes an infrared (IR) reflecting layer between at least a pair of dielectric layers. The IR reflecting layer may be of silver or the like. The coating is designed so as to provide a highly transparent coated article that is thermally stable upon optional heat treatment and which can be made to have a low emissivity in a consistent manner. The coating is designed to have improved IR reflecting layer quality, and thus reduced tolerances with respect to manufacturability of desired emissivity values. The coated article may be used in monolithic window applications, IG window applications, or the like.

Abstract: A method which is suitable for a system having a frequency converter and a generator, both of which are connected to a power grid, includes obtaining sub-synchronous components of the grid voltage and determining damping current set points according to the sub-synchronous components to compensate for sub-synchronous resonances of the grid. Damping current set points are determined by receiving the sub-synchronous components of the grid voltage and returning damping current set points as outputs. A variable damping gain is adjusted according to the sub-synchronous frequency of the grid, such that the required compensation level can be adapted to the frequency converter for damping sub-synchronous resonance of the grid.

Abstract: A coated article is provided with a low-emissivity (low-E) coating on a glass substrate. The low-E coating includes an infrared (IR) reflecting layer between at least a pair of dielectric layers. The IR reflecting layer may be of silver or the like. The coating is designed so as to provide a highly transparent coated article that is thermally stable upon optional heat treatment and which can be made to have a low emissivity in a consistent manner. The coating is designed to have improved IR reflecting layer quality, and thus reduced tolerances with respect to manufacturability of desired emissivity values. The coated article may be used in monolithic window applications, IG window applications, or the like.

Abstract: A coated article is provided with a low-emissivity (low-E) coating on a glass substrate. The low-E coating includes an infrared (IR) reflecting layer between at least a pair of dielectric layers. The IR reflecting layer may be of silver or the like. The coating is designed so as to provide a highly transparent coated article that is thermally stable upon optional heat treatment and which can be made to have a low emissivity in a consistent manner. The coating is designed to have improved IR reflecting layer quality, and thus reduced tolerances with respect to manufacturability of desired emissivity values. The coated article may be used in monolithic window applications, IG window applications, or the like.

Abstract: A coated article is provided with a low-emissivity (low-E) coating on a glass substrate. The low-E coating includes an infrared (IR) reflecting layer between at least a pair of dielectric layers. The IR reflecting layer may be of silver or the like. The coating is designed so as to provide a highly transparent coated article that is thermally stable upon optional heat treatment and which can be made to have a low emissivity in a consistent manner. The coating is designed to have improved IR reflecting layer quality, and thus reduced tolerances with respect to manufacturability of desired emissivity values. The coated article may be used in monolithic window applications, IG window applications, or the like.

Abstract: A method which is suitable for a system having a frequency converter and a generator, both of which are connected to a power grid, includes obtaining sub-synchronous components of the grid voltage and determining damping current set points according to the sub-synchronous components to compensate for sub-synchronous resonances of the grid. Damping current set points are determined by receiving the sub-synchronous components of the grid voltage and returning damping current set points as outputs. A variable damping gain is adjusted according to the sub-synchronous frequency of the grid, such that the required compensation level can be adapted to the frequency converter for damping sub-synchronous resonance of the grid.

Abstract: Protection system for a power converter connected to a doubly fed induction generator having a rotor and a stator. The power converter includes a grid-side-converter, a machine-side-converter, a DC link between both converters, a chopper connected to the DC link, and a hardware protection system connected to the rotor of the generator. The protection system includes a first control unit for controlling the hardware protection system depending on the voltage in the DC link, a second control unit for controlling the chopper depending on the DC link voltage, and a third control unit for controlling both converters.

Abstract: Protection system for a power converter connected to a doubly fed induction generator having a rotor and a stator. The power converter includes a grid-side-converter, a machine-side-converter, a DC link between both converters, a chopper connected to the DC link, and a hardware protection system connected to the rotor of the generator. The protection system includes a first control unit for controlling the hardware protection system depending on the voltage in the DC link, a second control unit for controlling the chopper depending on the DC link voltage, and a third control unit for controlling both converters.

Abstract: Windows, including windows for an aircraft. The windows include a shade. The shade has variable light transmissive characteristics. The shade is entrained upon rollers so that it may roll across the lens window. The parts of the shade are nearly opaque and other parts are nearly transparent. The result is a shade that has varying optical density depending upon the position of the hand operated rollers or shade positioning mechanism.

Abstract: Windows, including windows for an aircraft. The windows include a shade. The shade has variable light transmissive characteristics. The shade is entrained upon rollers so that it may roll across the lens window. The parts of the shade are nearly opaque and other parts are nearly transparent. The result is a shade that has varying optical density depending upon the position of the hand operated rollers or shade positioning mechanism.

Abstract: An aircraft window having a generally rectangular frame with an inner lens. A first shade is movable with respect to the frame and capable of covering a portion of the inner lens. A second shade is also movable with respect to the frame and also capable of covering a portion of the inner lens. An intermediate lens or separation member lies between the first and second shades. Movement of the shades allows for independent and variable control over the light transmitted through the window.

Abstract: A vehicle window having a curved inner lens, a rectangular frame with frame members and a shade. The shade is a dual shade having a first fabric member and a second fabric member with a removable shade rail between the first and second fabric member. There also is a movable shade rail at the end of the second shade material. Cables attach to each end of the removable shade rails and through to separate handles. Moving the first handle will move the first moveable shade rail and the first fabric member up and down and moving the second handle will move the second moveable shade rail and the second fabric up and down. The fabric members have different light transmissive characteristics, one being more opaque then the other.

Abstract: Applicant discloses a modular window shade system for an aircraft or other vehicle. The window shade of the window is enclosed with an outer and inner lens and mounted to a frame. A handle is provided and a mechanism is provided where in moving a handle horizontally mounted to the frame will cause the shade to move vertically. The mechanism between the handle and the shade provides a mechanical advantage such that the handle moves a distance greater then the vertical travel of the shade.

Abstract: A vehicle window having a curved inner lens, a rectangular frame with frame members and a shade. The shade is a dual shade having a first fabric member and a second fabric member with a removable shade rail between the first and second fabric member. There also is a movable shade rail at the end of the second shade material. Cables attach to each end of the removable shade rails and through to separate handles. Moving the first handle will move the first moveable shade rail and the first fabric member up and down and moving the second handle will move the second moveable shade rail and the second fabric up and down. The fabric members have different light transmissive characteristics, one being more opaque then the other.

Abstract: A window apparatus for use within an aircraft interior. This window having at least one shade frame, at least one shade attached to the shade frame at its top and a moveable shade rail attached at its bottom, a first and second lens assembly where the first lens assembly has first lens and the second lens assembly has a second lens, the first and second lenses being mountable to the shade frame such that they form a double convex configuration, and means for moving the shade between a substantially open position and a substantially closed position.

Abstract: A vehicle window having a curved inner lens, a rectangular frame with frame members and a shade. The shade is a dual shade having a first fabric member and a second fabric member with a removable shade rail between the first and second fabric member. There also is a movable shade rail at the end of the second shade material. Cables attach to each end of the removable shade rails and through to separate handles. Moving the first handle will move the first moveable shade rail and the first fabric member up and down and moving the second handle will move the second moveable shade rail and the second fabric up and down. The fabric members have different light transmissive characteristics, one being more opaque then the other.

Abstract: A window apparatus for use within an aircraft interior. This window having at least one shade frame, at least one shade attached to the shade frame at its top and a moveable shade rail attached at its bottom, a first and second lens assembly where the first lens assembly has first lens and the second lens assembly has a second lens, the first and second lenses being mountable to the shade frame such that they form a double convex configuration, and means for moving the shade between a substantially open position and a substantially closed position. The first and second lenses may have the same dimensions and/or be rectangular in shape. The first lens may have a length of at least 40 inches, a width of at least 30 inches, and an area of at least 1200 square inches. The shade may be pleated, tubular in shape, and have means for maintaining the horizontal alignment of the shade rail.

Abstract: An electrically driven motor capable of smoothly and efficiently raising and lowering a shade of an aircraft window. The aircraft window includes a spool which can slide axially. A cord is tied to one end of the spool, routed around the frame of the window and back to the second end of the spool. Between the first and second ends of the cord, it is tied into a shade rail. The shade rail is attached to the shade and when the shade rail moves up and down, the shade opens and closes. The spool is energized by the electric motor and, when moving in the first direction, causes one end of the spool to take up cord, thus causing the shade rail to move up and the other window to open and, when the electric motor is reversed, the take-up side of the spool becomes the unwind side and the unwind side becomes the take-up side, with the shade moving towards a closed, or down, position.

Abstract: The present invention relates to a modular window unit for an aircraft comprising a nonopaque lens and a reveal, the reveal joining the lens, as well as a shade comprising a multiplicity of discrete elongated panels, each panel cooperating with one another and being movable between an open and a closed position. The panels lay one next to the other to substantially cover the lens when the window shade is closed and, in an open position, lay stacked atop each other to substantially uncover the lens. Electric motors are provided for moving the panels of the shade between the open and closed positions.

Abstract: The present invention relates to a modular window unit for an aircraft comprising a nonopaque lens and a reveal, the reveal joining the lens, as well as a shade comprising a multiplicity of discrete elongated panels, each panel cooperating with one another and being movable between an open and a closed position. The panels lay one next to the other to substantially cover the lens when the window shade is closed and, in an open position, lay stacked atop each other to substantially uncover the lens. Electric motors are provided for moving the panels of the shade between the open and closed positions.