Abstract: Systems and methods for utilizing a trimming device to trim an edge of a plastic card having round corners, are provided. The plastic card has an overlay laminated on a major surface of the plastic card. The periphery of the overlay overhangs the edge of the plastic card. The trimming device trims the overhanging part of the laminated overlay by moving the trimming device along the edge of the personalized document in a direction generally parallel to the major surface of the plastic card.

Abstract: A messaging system for managing messaging subscriptions. A messaging provider receives a request to subscribe a user's message account to a subscription system. The messaging provider associates the subscription system with the user's message account to indicate to the messaging provider that the user has subscribed to receive messages from the subscription system. The messaging provider also communicates an identifier for the message account to the subscription system, which is used by the subscription system in sending messages to the user's message account. By subscribing to receive messages from subscription systems via the messaging provider in this manner, the messaging provider is automatically notified of the subscription systems that a user has subscribed to, enabling the messaging provider to more accurately determine how incoming messages should be handled.

Abstract: Methods and systems for controlling fuel tank flammability control systems are disclosed herein. In one embodiment, a system for use with an aircraft or other vehicle includes a flammability control system and a controller operably coupled to the flammability control system. The flammability control system can be configured to control the development of flammable vapors in a fuel tank of the vehicle. The controller can be configured to receive one or more signals relating to a condition of the fuel tank and control operation of the flammability control system at least partially in response to the one or more fuel tank condition signals. In another embodiment, the controller can be configured to receive one or more signals relating to an operational phase of the aircraft and control operation of the flammability control system at least partially in response to the one or more aircraft operation signals.

Abstract: An inerting system (10) for an aircraft (12) includes one or more fuel tank circuits (15) associated with fuel tanks (16). An air source (17) supplies pressurized air. A heat exchanger (56) cools the pressurized air. An air separation module (46) is in fluid communication with the heat exchanger (56) and separates inerting gas from the pressurized air. A controller (40) controls flow of the inerting gas from the air separation module (46) to the fuel tanks (16).

Abstract: Methods and systems for controlling fuel tank flammability control systems are disclosed herein. In one embodiment, a system for use with an aircraft or other vehicle includes a flammability control system and a controller operably coupled to the flammability control system. The flammability control system can be configured to control the development of flammable vapors in a fuel tank of the vehicle. The controller can be configured to receive one or more signals relating to a condition of the fuel tank and control operation of the flammability control system at least partially in response to the one or more fuel tank condition signals. In another embodiment, the controller can be configured to receive one or more signals relating to an operational phase of the aircraft and control operation of the flammability control system at least partially in response to the one or more aircraft operation signals.

Abstract: Systems and methods are disclosed for teaching a person how to perform a task within a computer program with at least one graphical user interface object. A script is formulated that contains step-by-step instructions indicating to a person how to perform a task within a computer program through interacting with at least one graphical user interface object of the computer program. The script is formulated by reference to an entity map, which contains programming instructions for accessing at least one graphical user interface object of the program to perform a step of the task. The script is executed by displaying a partial graphical overlay on top of an actual, non-simulated graphical user interface of the program. Each graphical user overlay instructs a user how to provide pertinent user input to graphical user interface objects of the computer program.

Abstract: Methods and systems for controlling fuel tank flammability control systems are disclosed herein. In one embodiment, a system for use with an aircraft or other vehicle includes a flammability control system and a controller operably coupled to the flammability control system. The flammability control system can be configured to control the development of flammable vapors in a fuel tank of the vehicle. The controller can be configured to receive one or more signals relating to a condition of the fuel tank and control operation of the flammability control system at least partially in response to the one or more fuel tank condition signals. In another embodiment, the controller can be configured to receive one or more signals relating to an operational phase of the aircraft and control operation of the flammability control system at least partially in response to the one or more aircraft operation signals.

Abstract: Methods and systems for controlling fuel tank flammability control systems are disclosed herein. In one embodiment, a system for use with an aircraft or other vehicle includes a flammability control system and a controller operably coupled to the flammability control system. The flammability control system can be configured to control the development of flammable vapors in a fuel tank of the vehicle. The controller can be configured to receive one or more signals relating to a condition of the fuel tank and control operation of the flammability control system at least partially in response to the one or more fuel tank condition signals. In another embodiment, the controller can be configured to receive one or more signals relating to an operational phase of the aircraft and control operation of the flammability control system at least partially in response to the one or more aircraft operation signals.

Abstract: An inerting system (10) for an aircraft (12) includes one or more fuel tank circuits (15) associated with fuel tanks (16). An air source (17) supplies pressurized air. A heat exchanger (56) cools the pressurized air. An air separation module (46) is in fluid communication with the heat exchanger (56) and separates inerting gas from the pressurized air. A controller (40) controls flow of the inerting gas from the air separation module (46) to the fuel tanks (16).

Abstract: A graphics printer apparatus and method using sensors to detect the position of a work piece relative to a print head. A single drive motor driving the feed rollers and a print roller.

Abstract: A printer apparatus including a print head assembly and a transport belt for transporting a workpiece such as a plastic card through the printer apparatus. The transport belt includes a surface self-adhering to a surface of the plastic card. In a preferred embodiment, the printer apparatus includes a print head which is moved across a surface of the card while printing on the card. The printer apparatus includes a print head controller for interfacing between at least one microprocessor and at least one continuous tone print head, the number of print intensities either fixed or selected by the microprocessor.