Abstract: Systems and methods for intelligent tool detection are described. One embodiment includes a remote server, a processing system communicatively coupled to the remote server, and a tool tray communicatively coupled to the processing system. The tool tray is configured to store a plurality of tools, and to detect whether a tool has been removed from the tool tray. The tool tray is configured to communicate information associated with the removal of the tool to the processing system. The processing system is configured to communicate the information to the remote server.

Abstract: Systems and methods for intelligent tool detection are described. One embodiment includes placing a tool in a tool tray, and detecting a presence of the tool. Information associated with the presence of the tool is communicated to a processing system communicatively coupled to the tool tray. The tool is removed from the tool tray, and the removal is detected. Communication associated with the removal of the tool is communicated to the processing system. A distinction between information associated with the tool being present in the tool tray and information associated with the tool being removed from the tool tray is learned.

Abstract: Systems and methods for intelligent tool detection are described. One embodiment includes a remote server, a processing system communicatively coupled to the remote server, and a tool tray communicatively coupled to the processing system. The tool tray is configured to store a plurality of tools. The processing system is configured to detect whether a tool has been removed from the tool tray, and to communicate information associated with the removal of the tool to the remote server.

Abstract: Methods and arrangements are described for controlling transitions between firing fractions during skip fire operation of an engine in order to help smooth the transitions. Generally, firing fractions transitions are implemented gradually, preferably in a manner that relatively closely tracks manifold filling dynamics. In some embodiments, the commanded firing fraction is altered each firing opportunity. Another approach contemplates altering the commanded firing fraction by substantially the same amount each firing opportunity for at least a portion of the transition. These approaches work particularly well when the commanded firing fraction is provided to a skip fire controller that includes an accumulator functionality that tracks the portion of a firing that has been requested, but not delivered, or vice versa.

Abstract: Methods and arrangements are described for controlling transitions between firing fractions during skip fire operation of an engine in order to help smooth the transitions. Generally, firing fractions transitions are implemented gradually, preferably in a manner that relatively closely tracks manifold filling dynamics. In some embodiments, the commanded firing fraction is altered each firing opportunity. Another approach contemplates altering the commanded firing fraction by substantially the same amount each firing opportunity for at least a portion of the transition. These approaches work particularly well when the commanded firing fraction is provided to a skip fire controller that includes an accumulator functionality that tracks the portion of a firing that has been requested, but not delivered, or vice versa.

Abstract: Methods and arrangements are described for controlling transitions between firing fractions during skip fire operation of an engine in order to help smooth the transitions. Generally, firing fractions transitions are implemented gradually, preferably in a manner that relatively closely tracks manifold filling dynamics. In some embodiments, the commanded firing fraction is altered each firing opportunity. Another approach contemplates altering the commanded firing fraction by substantially the same amount each firing opportunity for at least a portion of the transition. These approaches work particularly well when the commanded firing fraction is provided to a skip fire controller that includes an accumulator functionality that tracks the portion of a firing that has been requested, but not delivered, or vice versa.

Abstract: Methods and arrangements are described for controlling transitions between firing fractions during skip fire operation of an engine in order to help smooth the transitions. Generally, firing fractions transitions are implemented gradually, preferably in a manner that relatively closely tracks manifold filling dynamics. In some embodiments, the commanded firing fraction is altered each firing opportunity. Another approach contemplates altering the commanded firing fraction by substantially the same amount each firing opportunity for at least a portion of the transition. These approaches work particularly well when the commanded firing fraction is provided to a skip fire controller that includes an accumulator functionality that tracks the portion of a firing that has been requested, but not delivered, or vice versa.

Abstract: A condensate extractor assembly is provided for collecting and evacuating condensate from inside a charge air cooler in an internal combustion engine assembly. The condensate extractor assembly includes a sump that is attached to or formed in the charge air cooler. The sump is adapted to drain and collect condensate from the charge air cooler. A hose is fluidly coupled at one end to the sump, and fluidly coupled at a second end to the intake manifold. The hose is configured to evacuate condensate from the sump and distribute it directly to the intake manifold in response to the pressure gradient generated by the engine assembly when in an on-state. The hose defines an orifice that restricts the flow of air and condensate through the hose. A filter is fluidly coupled to the hose, fluidly intermediate the orifice and the sump member.

Abstract: A condensate extractor assembly is provided for collecting and evacuating condensate from inside a charge air cooler in an internal combustion engine assembly. The condensate extractor assembly includes a sump that is attached to or formed in the charge air cooler. The sump is adapted to drain and collect condensate from the charge air cooler. A hose is fluidly coupled at one end to the sump, and fluidly coupled at a second end to the intake manifold. The hose is configured to evacuate condensate from the sump and distribute it directly to the intake manifold in response to the pressure gradient generated by the engine assembly when in an on-state. The hose defines an orifice that restricts the flow of air and condensate through the hose. A filter is fluidly coupled to the hose, fluidly intermediate the orifice and the sump member.