Abstract: A laminate article includes a silicone pressure sensitive adhesive adhered to a silicone rubber article. A method for fabricating the laminate article is provided.

Abstract: A laminate includes a silicone pressure sensitive adhesive adhered to an article comprising a fluorosilicone rubber or a silicone foam. A method for fabricating the laminate is provided.

Abstract: A silicone release coating composition and method for its preparation and use are described. A release coating prepared by curing the silicone release coating composition has high immediate release force (>50 g/in). A release liner including the release coating is suitable for use as a transfer liner in processes for making composites articles, such as aircraft parts.

Abstract: A polydiorganosiloxane having both a silicon bonded aliphatically unsaturated group and a silicon bonded poly(meth)acrylate polymer or copolymer is useful in a polyorganosiloxane hybrid pressure sensitive adhesive composition that cures to form a polyorganosiloxane hybrid pressure sensitive adhesive. The polyorganosiloxane hybrid pressure sensitive adhesive composition can be wet-cast or dry-cast on a substrate and cured to form a polyorganosiloxane hybrid pressure sensitive adhesive article. An adhesive article including the polyorganosiloxane hybrid pressure sensitive adhesive is also disclosed.

Abstract: A laminate article includes a silicone pressure sensitive adhesive adhered to an article comprising a silicone rubber. A method for fabricating the laminate article is provided.

Abstract: A polydiorganosiloxane having both a silicon bonded aliphatically unsaturated group and a silicon bonded poly(meth)acrylate polymer or copolymer, and method for preparation of this polydiorganosiloxane are disclosed. The method preserves the aliphatically unsaturated groups when grafting the poly(meth)acrylate to the polydiorganosiloxane. This polydiorganosiloxane is useful in hydrosilylation reaction curable compositions, such as pressure sensitive adhesive compositions.

Abstract: A polydiorganosiloxane having a silicon bonded poly(meth)acrylate polymer or copolymer is useful in a polyorganosiloxane hybrid pressure sensitive adhesive composition that cures to form a polyorganosiloxane hybrid pressure sensitive adhesive. An adhesive article including the polyorganosiloxane hybrid pressure sensitive adhesive is also disclosed.

Abstract: A silicone release coating composition and method for its preparation and use are described. A release coating prepared by curing the silicone release coating composition has high immediate release force (>50 g/in). A release liner including the release coating is suitable for use as a transfer liner in processes for making composites articles, such as aircraft parts.

Abstract: A polydiorganosiloxane having both a silicon bonded aliphatically unsaturated group and a silicon bonded poly(meth)acrylate polymer or copolymer is useful in a polyorganosiloxane hybrid pressure sensitive adhesive composition that cures to form a polyorganosiloxane hybrid pressure sensitive adhesive. The polyorganosiloxane hybrid pressure sensitive adhesive composition can be wet-cast or dry-cast on a substrate and cured to form a polyorganosiloxane hybrid pressure sensitive adhesive article. An adhesive article including the polyorganosiloxane hybrid pressure sensitive adhesive is also disclosed.

Abstract: A polydiorganosiloxane having both a silicon bonded aliphatically unsaturated group and a silicon bonded poly(meth)acrylate polymer or copolymer, and method for preparation of this polydiorganosiloxane are disclosed. The method preserves the aliphatically unsaturated groups when grafting the poly(meth)acrylate to the polydiorganosiloxane. This polydiorganosiloxane is useful in hydrosilylation reaction curable compositions, such as pressure sensitive adhesive compositions.

Abstract: A secure communication management (SCM) computer device for providing secure data connections in an aviation environment which, includes safety of flight information, is provided. The SCM computer device includes a processor in communication with a memory. The processor is programmed to receive, from a first user computer device, a first data message for a first aircraft. The first data message is in a standardized data format. The processor is also programmed to analyze the first data message for potential cybersecurity threats. If the determination is that the first data message does not contain a cybersecurity threat, the processor is further programmed to convert the first data message into a first data format associated with the first aircraft and transmit the converted first data message to the first aircraft using a first communication protocol associated with the first aircraft.

Abstract: Diagnostic information for a program execution is provided, where the program is executable in a machine having a program stack for individual program elements. At least one program element is saved from the program stack into an event buffer as the at least one program element is executed. A historical event buffer associated with at least one runtime error is loaded, and a similarity between the event buffer and the historical event buffer is determined. It is requested that at least one type of diagnostic information be provided with the execution of the program in the event buffer when the determined similarity exceeds a threshold similarity.

Abstract: A secure communication management (SCM) computer device for providing secure data connections in an aviation environment which, includes safety of flight information, is provided. The SCM computer device includes a processor in communication with a memory. The processor is programmed to receive, from a first user computer device, a first data message for a first aircraft. The first data message is in a standardized data format. The processor is also programmed to analyze the first data message for potential cybersecurity threats. If the determination is that the first data message does not contain a cybersecurity threat, the processor is further programmed to convert the first data message into a first data format associated with the first aircraft and transmit the converted first data message to the first aircraft using a first communication protocol associated with the first aircraft.

Abstract: A secure communication management (SCM) computer device for providing secure data connections in an aviation environment which, includes safety of flight information, is provided. The SCM computer device includes a processor in communication with a memory. The processor is programmed to receive, from a first user computer device, a first data message for a first aircraft. The first data message is in a standardized data format. The processor is also programmed to analyze the first data message for potential cybersecurity threats. If the determination is that the first data message does not contain a cybersecurity threat, the processor is further programmed to convert the first data message into a first data format associated with the first aircraft and transmit the converted first data message to the first aircraft using a first communication protocol associated with the first aircraft.

Abstract: A secure communication management (SCM) computer device for providing secure data connections in an aviation environment which, includes safety of flight information, is provided. The SCM computer device includes a processor in communication with a memory. The processor is programmed to receive, from a first user computer device, a first data message for a first aircraft. The first data message is in a standardized data format. The processor is also programmed to analyze the first data message for potential cybersecurity threats. If the determination is that the first data message does not contain a cybersecurity threat, the processor is further programmed to convert the first data message into a first data format associated with the first aircraft and transmit the converted first data message to the first aircraft using a first communication protocol associated with the first aircraft.

Abstract: A pack with a variety of panels which can be deployed. A mid-panel is defined on the fabric housing. A head panel is attached to the mid-panel adapted to be folded and contained over the mid-panel. A leg panel is attached to the mid-panel adapted to be folded and contained over the mid-panel. The top finger loop is attached to the head panel and extends from the top. A bottom finger loop is attached to the leg panel extending from the bottom. Upon pulling the top finger loop and the bottom finger loop, the head panel and the leg panel, respectively, can be deployed from the fabric housing. A chest strap is deployable using an upper side finger loop. A waist strap is deployable using a lower side finger loop. The instant pack includes semi-rigid body boards contained over the mid-panel to add rigidity and enhance safety.

Abstract: A fuel fired, atmospheric water heater has a burner positioned inside a combustion chamber. All combustion air entering the combustion chamber must pass through a damper. The damper is operable to adjust the flow resistance to combustion air entering the combustion chamber. The damper is biased to a closed position such that during non-firing periods of the water heater, the damper significantly reduces the flow rate of combustion air being provided to the combustion chamber reducing standby heat loss. An actuator is in fluid communication with a fuel supply line such that when pressurized fuel is provided to the burner, the pressurized fuel causes the actuator to move the damper to an open position to permit operative combustion air delivery to the combustion chamber during firing periods of the water heater.