Abstract: Methods, systems, and computer program products for detecting and correcting integration issues and errors between different computer systems are disclosed. For example, a computer-implemented method may include collecting transaction data for each one of a plurality of respective merchants where the transaction data is associated with service integration between computer systems associated with the respective merchants and one or more service provider computer systems, analyzing the transaction data across a plurality of respective issue detection models, generating for each one of the plurality of merchants action data corresponding to one or more of the respective issue detection models based on the analyzing, and providing each one of the plurality of merchants with the respective generated action data.

Abstract: Methods, systems, and computer program products for detecting and correcting integration issues and errors between different computer systems are disclosed. For example, a computer-implemented method may include collecting transaction data for each one of a plurality of respective merchants where the transaction data is associated with service integration between computer systems associated with the respective merchants and one or more service provider computer systems, analyzing the transaction data across a plurality of respective issue detection models, generating for each one of the plurality of merchants action data corresponding to one or more of the respective issue detection models based on the analyzing, and providing each one of the plurality of merchants with the respective generated action data.

Abstract: An air-line safeguard for use with an air-line connection comprising a first connector and an opposing connector, wherein the first connector comprises a tongue, an interface, and a shaft and wherein the opposing connector comprises an opposing tongue, an opposing interface and an opposing shaft, the safeguard comprising of at least one body that removably attaches to and accommodates the first air-line connector and extends between the shaft and the tongue of the first connector and least partially between the opposing tongue and the opposing shaft of the opposing connector to prevent the first connector from substantially rotating relative to the opposing connector.

Abstract: An air-line safeguard for use with an air-line connection comprising a first connector and an opposing connector, wherein the first connector comprises a tongue, an interface, and a shaft and wherein the opposing connector comprises an opposing tongue, an opposing interface and an opposing shaft, the safeguard comprising of at least one body that removably attaches to and accommodates the first air-line connector and extends between the shaft and the tongue of the first connector and least partially between the opposing tongue and the opposing shaft of the opposing connector to prevent the first connector from substantially rotating relative to the opposing connector.

Abstract: Methods, systems, and computer program products for detecting and correcting integration issues and errors between different computer systems are disclosed. For example, a computer-implemented method may include collecting transaction data for each one of a plurality of respective merchants where the transaction data is associated with service integration between computer systems associated with the respective merchants and one or more service provider computer systems, analyzing the transaction data across a plurality of respective issue detection models, generating for each one of the plurality of merchants action data corresponding to one or more of the respective issue detection models based on the analyzing, and providing each one of the plurality of merchants with the respective generated action data.

Abstract: An airline couple that provide consumers a way to keep air lines connected while driving. The first airline couple includes a first airline connector extending forward, an airline clip including a planar rectangular tab that includes a pair of apertures disposed on the planar rectangular tab and a second airline connector extending back towards the airline clip, the airline clip is wrapped around the first airline connector and the second airline connector. The airline couple includes a piece of putty wrapped around each end of a first airline connector and a second airline connector, the piece of putty hardens between each end of the first airline connector and the second airline connector securing each end of the first airline connector and the second airline connector.

Abstract: A sensing coil assembly and method for attaching a sensing coil to a support structure are provided for a fiber optic gyroscope. The method comprises affixing a first support surface of the support structure to a first mounting surface of the sensing coil via a first preformed adhesive, and affixing a second support surface of the support structure to a second mounting surface of the sensing coil via a second preformed adhesive. The sensing coil assembly comprises a support structure having first and second support surfaces and having a substantially cylindrical hub coupled between the first and second opposing surfaces, an optical fiber coil surrounding at least a portion of the substantially cylindrical hub, and first and second preformed adhesive patterns affixing the optical fiber coil to the first and second opposing surfaces. The first support surface opposes the second support surface.

Abstract: Adhesive system and method are provided for affixing a fiber optic coil to a hub with an adhesive in a fiber optic gyroscope. The adhesive system comprises a fiber optic coil, a substantially cylindrical hub configured to couple with the fiber optic coil, and an array of adhesive dots affixing the fiber optic coil to the substantially cylindrical hub. The method comprises forming an array of adhesive dots on an outer surface of the hub, and affixing the fiber optic coil to the outer surface of the hub via the array of adhesive dots.