Abstract: An information handling system includes a unified communicator for initiating, via an application processor, a wireless link with a recipient user, a wireless adapter for communicating with a wireless link. The application processor executes instructions for determining one or more communication link options with the recipient user and determines an optimal wireless link from among the communication link options with the recipient user.

Abstract: An information handling system includes a unified communicator for initiating, via an application processor, a wireless link with a recipient user, a wireless adapter for communicating with a wireless link. The application processor executes instructions for determining one or more communication link options with the recipient user and determines an optimal wireless link from among the communication link options with the recipient user.

Abstract: A system and method for assembling a full interaction record for a meeting with non-realtime interaction is disclosed. The system and method may include recording a first plurality of data associated with the meeting to produce a meeting record at a first time, and determining whether to insert a placeholder in the meeting record at a point in the meeting record.

Abstract: An aircraft drain device (14) for interposition between a potable water line (e.g., the drain line from an ice drawer) and a gray water line leading to a drainmast or other external drain. The drain device (14) includes a housing (30), an inlet (36) adapted for connection to the potable water line, an outlet (38) adapted for connection to the gray water line, and a piston (40). The preferably floatable piston (40) is movable between a normal operation position, whereat potable water can flow to the drainmast, and a back-up operation position, whereat the potable water is protected from contact with the gray water. The drain device (14) can be constructed to prevent spillage (or leakage) during back-up operation.

Abstract: A deicing system (10) for preventing ice accumulation on an airfoil surface (14) of an aircraft (12). The system (10) can comprise a control module (66) which controls a valve (64) based on a pressure conditions within the deicer chambers (30), a reservoir (60) for providing pressurized inflation fluid to the deicer chambers (30), and/or a line (62) for providing the deflation suction for the airfoil's low-pressure side (18).