Abstract: A method and apparatus of controlling movement of an aircraft. A turn path off of a planned route for an aircraft comprising a turn to direct the aircraft to an intercept point on the planned route is determined. A planned route indicator depicting the planned route, a turn path indicator depicting the turn path, and an aircraft position indicator indicating a position of the aircraft are displayed to an operator of the aircraft at the same time on a turn guidance display. Deviation limit indicators for the planned route, the turn path, or both, may be displayed on the turn guidance display. Indicator characteristics of the deviation limit indicators may be changed in response to aircraft deviations from the planned route or the turn path by more than the deviation limits. The turn guidance display is used to control the movement of the aircraft to follow the turn path.

Abstract: A dual pressure respiratory assistance device including a gas source which supplies a flow of gas into an air tube having a bubbler branch and a patient branch. A first tube that is connected to the bubbler branch is at least partially submerged in a fluid. An oscillatory relief valve cycles between first and second configurations. The relief valve includes an oscillating member which captures gas released through at least one hole in the first tube when the oscillating member is in a first position. The gas in the oscillating member causes the oscillating member to rise to a second position, wherein gas is released from the oscillating member and the at least one hole is blocked when the oscillating member reaches the second position.

Abstract: A dual pressure respiratory assistance device including a gas source which supplies a flow of gas into an air tube having a bubbler branch and a patient branch. A first tube that is connected to the bubbler branch is at least partially submerged in a fluid. An oscillatory relief valve cycles between first and second configurations. The relief valve includes an oscillating member which captures gas released through at least one hole in the first tube when the oscillating member is in a first position. The gas in the oscillating member causes the oscillating member to rise to a second position, wherein gas is released from the oscillating member and the at least one hole is blocked when the oscillating member reaches the second position.

Abstract: A method and apparatus of controlling movement of an aircraft. A turn path off of a planned route for an aircraft comprising a turn to direct the aircraft to an intercept point on the planned route is determined. A planned route indicator depicting the planned route, a turn path indicator depicting the turn path, and an aircraft position indicator indicating a position of the aircraft are displayed to an operator of the aircraft at the same time on a turn guidance display. Deviation limit indicators for the planned route, the turn path, or both, may be displayed on the turn guidance display. Indicator characteristics of the deviation limit indicators may be changed in response to aircraft deviations from the planned route or the turn path by more than the deviation limits. The turn guidance display is used to control the movement of the aircraft to follow the turn path.

Abstract: System and methods are provided for driving one or more light emitting diodes (LEDs) to reduce audible noise. An example system includes a switching component, a system controller, and a current generator. The switching component is configured to receive a dimming signal with a predetermined dimming frequency and configured to switch on or off the one or more LEDs in response to the dimming signal, the predetermined dimming frequency being outside a frequency band of the audible noise. The system controller is configured to receive a feedback signal related to a LED current that flows through the one or more LEDs and configured to generate a drive signal. Additionally, the current generator is configured to receive the drive signal, to generate a charging current to store energy during a charging period and to generate the LED current during a discharging period.

Abstract: System and methods are provided for driving one or more light emitting diodes (LEDs) to reduce audible noise. An example system includes a switching component, a system controller, and a current generator. The switching component is configured to receive a dimming signal with a predetermined dimming frequency and configured to switch on or off the one or more LEDs in response to the dimming signal, the predetermined dimming frequency being outside a frequency band of the audible noise. The system controller is configured to receive a feedback signal related to a LED current that flows through the one or more LEDs and configured to generate a drive signal. Additionally, the current generator is configured to receive the drive signal, to generate a charging current to store energy during a charging period and to generate the LED current during a discharging period.

Abstract: System and methods are provided for driving one or more light emitting diodes (LEDs) to reduce audible noise. An example system includes a switching component, a system controller, and a current generator. The switching component is configured to receive a dimming signal with a predetermined dimming frequency and configured to switch on or off the one or more LEDs in response to the dimming signal, the predetermined dimming frequency being outside a frequency band of the audible noise. The system controller is configured to receive a feedback signal related to a LED current that flows through the one or more LEDs and configured to generate a drive signal. Additionally, the current generator is configured to receive the drive signal, to generate a charging current to store energy during a charging period and to generate the LED current during a discharging period.

Abstract: A visual/graphical air traffic display tool to aid flight crews in determining future heading/track and position of ownship based on current climb rate, bank angle and groundspeed under current meteorological conditions. The tool displays symbols which indicate the predicted future position and heading/track of ownship on a traffic display unit. The tool is also capable of using ownship's predicted position and information received from surrounding traffic to identify a future conflict at ownship's predicted position and then display a future conflict warning on the traffic display unit. In one embodiment, the future conflict warning takes the form of a change in the coloration of the ownship position and heading/track indicator being displayed.

Abstract: A visual/graphical air traffic display tool to aid flight crews in determining future heading/track and position of ownship based on current climb rate, bank angle and groundspeed under current meteorological conditions. The tool displays symbols which indicate the predicted future position and heading/track of ownship on a traffic display unit. The tool is also capable of using ownship's predicted position and information received from surrounding traffic to identify a future conflict at ownship's predicted position and then display a future conflict warning on the traffic display unit. In one embodiment, the future conflict warning takes the form of a change in the coloration of the ownship position and heading/track indicator being displayed.

Abstract: A method for achieving and maintaining spacing between aircraft may include receiving by a following aircraft information related to a lead aircraft. The information is useable for achieving and maintaining spacing by the following aircraft from the lead aircraft. The method may also include determining spacing of the following aircraft from the lead aircraft. The method may additionally include receiving by the following aircraft a vertical profile for the traffic management environment. The method may further include automatically controlling throttle settings to achieve and maintain spacing by the following aircraft from the lead aircraft while maintaining the vertical profile of the following aircraft in response to an automatic spacing mode being enabled.

Abstract: System and methods are provided for driving one or more light emitting diodes (LEDs) to reduce audible noise. An example system includes a switching component, a system controller, and a current generator. The switching component is configured to receive a dimming signal with a predetermined dimming frequency and configured to switch on or off the one or more LEDs in response to the dimming signal, the predetermined dimming frequency being outside a frequency band of the audible noise. The system controller is configured to receive a feedback signal related to a LED current that flows through the one or more LEDs and configured to generate a drive signal. Additionally, the current generator is configured to receive the drive signal, to generate a charging current to store energy during a charging period and to generate the LED current during a discharging period.

Abstract: A method for filtering and presenting relevant aircraft traffic to a pilot may include determining a location and altitude of aircraft within a predetermined airspace relative to the pilot's own aircraft. The method may also include presenting a representation of the pilot's own aircraft and a representation of the location of each of the aircraft within the predetermined airspace in relation to the pilot's own aircraft on a display to the pilot. The method may additionally include filtering relevant aircraft within a selected filtering airspace relative to the pilot's own aircraft. The method may further include presenting the representation of the relevant aircraft within the selected filtering airspace in a selected format to distinguish the relevant aircraft within the selected filtering airspace from any other aircraft that may be presented in the display.

Abstract: A method for filtering and presenting relevant aircraft traffic to a pilot may include determining a location and altitude of aircraft within a predetermined airspace relative to the pilot's own aircraft. The method may also include presenting a representation of the pilot's own aircraft and a representation of the location of each of the aircraft within the predetermined airspace in relation to the pilot's own aircraft on a display to the pilot. The method may additionally include filtering relevant aircraft within a selected filtering airspace relative to the pilot's own aircraft. The method may further include presenting the representation of the relevant aircraft within the selected filtering airspace in a selected format to distinguish the relevant aircraft within the selected filtering airspace from any other aircraft that may be presented in the display.

Abstract: Electron generation apparatuses are disclosed that can include a power source coupled to a first electrode, and a switch between the power source and the first electrode. Mass spectrometry instruments are disclosed that can include a power source coupled to a first electrode, and a switch between the power source and the first electrode. Methods of generating electrons are provided that can include generating different voltage differentials across a cell, with at least one of the voltage differentials generating electrons from gaseous material, and discharging at least some of the electrons from the cell. Mass spectrometry methods are also provided that can include providing sample proximate a glow discharge ionization source, and generating a pulse of electrons from the ionization source according to an ionization parameter to ionize at least a portion of the sample.

Abstract: A system and method for introducing and analyzing a sample containing an analyte using an ion mobility spectrometer are described. The system includes a temperature module for adjusting the temperature of the sample according to temperature instructions received, and a split ratio module for adjusting the split ratio according to split ratio instructions received. An ion mobility analyzer determines an ion mobility of the analyte. The ion mobility analyzer collects a plasmagram of the analyte to identify and quantitate the analyte.

Abstract: A blowout preventer having a main body, a ram system with ram apparatus, a movement system with movable shaft apparatus connected to the ram apparatus, the ram apparatus movable from a first open-ram position to a second closed-ram position, the movable shaft apparatus including a locking shaft portion having a tapered portion, a locking system for selectively locking the ram apparatus in the closed position and having locking member apparatus having a primary tapered surface in contact with the locking shaft portion which is movable with the so that the primary tapered surface contacts the tapered portion of the locking shaft portion to releasably lock the movable shaft apparatus.

Abstract: The invention is a method of etching an integrated circuit (IC) structure that includes a metal hard mask layer. The etching of the metal hard mask layer is performed by first feeding a gas mixture comprising a fluorine containing gas and oxygen (O2) gas to a reactor. The method then proceeds to generate a plasma that etches the metal hard mask layer. The method can be applied to either performing a via etch or a trench etch. Additionally, the invention teaches the removal of a photoresist layer without affecting the metal hard mask layer.

Abstract: A system and method for introducing and analyzing a sample containing an analyte using an ion mobility spectrometer are described. The system includes a temperature module for adjusting the temperature of the sample according to temperature instructions received, and a split ratio module for adjusting the split ratio according to split ratio instructions received. An ion mobility analyzer determines an ion mobility of the analyte. The ion mobility analyzer collects a plasmagram of the analyte to identify and quantitate the analyte.

Abstract: A semiconductor manufacturing process wherein an organic anti-reflective coating (ARC) is plasma etched with selectivity to an underlying dielectric layer and/or overlying photoresist. The etchant gas is fluorine-free and includes a carbon-containing gas such as CO gas, a nitrogen-containing gas such as N2, an optional oxygen-containing gas such as O2, and an optional inert carrier gas such as Ar. The etch rate of the ARC can be at least 10 times higher than that of the underlying layer. Using a combination of CO and O2 with N2 and a carrier gas such as Ar, it is possible to obtain dielectric:ARC selectivity of at least 10. The process is useful for etching contact or via openings in damascene and self-aligned contact or trench structures.

Abstract: A semiconductor manufacturing process wherein an organic anti-reflective coating (ARC) is plasma etched with selectivity to an underlying dielectric layer and/or overlying photoresist. The etchant gas is fluorine-free and includes a carbon-containing gas such as CO gas, a nitrogen-containing gas such as N2, an optional oxygen-containing gas such as O2, and an optional inert carrier gas such as Ar. The etch rate of the ARC can be at least 10 times higher than that of the underlying layer. Using a combination of CO and O2 with N2 and a carrier gas such as Ar, it is possible to obtain dielectric:ARC selectivity of at least 10. The process is useful for etching contact or via openings in damascene and self-aligned contact or trench structures.