Abstract: Methods, apparatus, and device, such as a blood bag envelope, that protects a blood bag during storage and/or transport. The blood bag envelope holds a blood bag or a metal cassette that contains the blood bag. The envelope includes multiple panels. The multiple panels include a top panel, a first edge panel, a second edge panel, a front panel and a bottom panel. The multiple panels are configured to fold to form the enclosure to hold the blood bag. The envelope includes a first fastening device connected to an inner surface of the top panel. The envelope includes a suspension device that is suspended from the first fastening device. The suspension device is configured to suspend the blood bag within the enclosure when the multiple panels are folded to form the enclosure.

Abstract: Methods, apparatus, and device, such as a blood bag envelope, that protects a blood bag during storage and/or transport. The blood bag envelope holds a blood bag or a metal cassette that contains the blood bag. The envelope includes multiple panels. The multiple panels include a top panel, a first edge panel, a second edge panel, a front panel and a bottom panel. The multiple panels are configured to fold to form the enclosure to hold the blood bag. The envelope includes a first fastening device connected to an inner surface of the top panel. The envelope includes a suspension device that is suspended from the first fastening device. The suspension device is configured to suspend the blood bag within the enclosure when the multiple panels are folded to form the enclosure.

Abstract: A lean blowout protection system and method is provided that facilitates improved lean blowout protection while providing effective control of turbine engine speed. The lean blowout protection system and method selectively and gradually biases the lean blowout (LBO) schedule based on current engine data. This facilitates improved lean blowout protection while providing effective control of turbine engine speed and temperature.

Abstract: A lean blowout protection system and method is provided that facilitates improved lean blowout protection while providing effective control of turbine engine speed. The lean blowout protection system and method selectively and gradually biases the lean blowout (LBO) schedule based on current engine data. This facilitates improved lean blowout protection while providing effective control of turbine engine speed and temperature.

Abstract: A lean blowout protection system and method is provided that facilitates improved lean blowout protection while providing effective control of turbine engine speed. The lean blowout protection system and method selectively and gradually biases the lean blowout (LBO) schedule based on current engine data. This facilitates improved lean blowout protection while providing effective control of turbine engine speed and temperature.

Abstract: Control logic, and a method implemented by the control logic, compensates for mismatched inter turbine temperatures between two gas turbine engines and displays a biased inter turbine temperature (ITT) reading to the pilot without jeopardizing the need to be properly informed of the health of all engines and the relationship engine temperature compared to the maximum allowed temperature. A temperature compensation value is added to the lower inter turbine temperature to thereby increase the ITT to a value that is substantially equal to the higher ITT value. As a result, any potential nuisance or distraction that the flight crew may experience from displaying the mismatch is eliminated.

Abstract: A lean blowout protection system and method is provided that facilitates improved lean blowout protection while providing effective control of turbine engine speed. The lean blowout protection system and method selectively and gradually biases the lean blowout (LBO) schedule based on current engine data. This facilitates improved lean blowout protection while providing effective control of turbine engine speed and temperature.

Abstract: Control logic, and a method implemented by the control logic, compensates for mismatched inter turbine temperatures between two gas turbine engines and displays a biased inter turbine temperature (ITT) reading to the pilot without jeopardizing the need to be properly informed of the health of all engines and the relationship engine temperature compared to the maximum allowed temperature. A temperature compensation value is added to the lower inter turbine temperature to thereby increase the ITT to a value that is substantially equal to the higher ITT value. As a result, any potential nuisance or distraction that the flight crew may experience from displaying the mismatch is eliminated.

Abstract: Disclosed herein is a method for moving a plurality of telecommunications customers from an ILEC to a CLEC, the CLEC having a plurality of telecommunication lines, the method comprising: screening the customers; performing loop tests on the telecommunications lines; assigning physical and logical network inventory; provisioning one or more features for the customer; pre-wiring the telecommunications lines to a switch at a central office; generating a UNE-L order to the ILEC; receiving confirmation of an LNP request by the ILEC; activating the telecommunication lines; and generating an activate order to a NPAC.

Abstract: Disclosed herein is a method for moving a plurality of telecommunications customers from an ILEC to a CLEC, the CLEC having a plurality of telecommunication lines, the method comprising: screening the customers; performing loop tests on the telecommunications lines; assigning physical and logical network inventory; provisioning one or more features for the customer; pre-wiring the telecommunications lines to a switch at a central office; generating a UNE-L order to the ILEC; receiving confirmation of an LNP request by the ILEC; activating the telecommunication lines; and generating an activate order to a NPAC.