Abstract: Gas turbine engine systems and related methods involving thermally isolated retention are provided. In this regard, a representative method for attaching a gas turbine engine component includes using a fastener, varying in diameter along a length thereof, to prevent a portion of a component from being crimped between surfaces to which the component is attached such that the component moves relative to the surfaces responsive to thermal cycling of a gas turbine engine of which the surfaces and the component are constituent parts.

Abstract: A fluid coupling assembly has a single fluid connection, including a plate and at least a pair of nipples extending away from the plate in a first direction, and at least a pair of connection pipes connected to each of the nipples extending from the plate in a second opposed direction. The nipples include a thread at an outer periphery, a ramped surface spaced in a direction beyond the thread and towards the plate, and a ditch beyond the ramped surface. A fluid coupling has a thread at an inner periphery received on the thread on the nipple, and the coupling has a plurality of circumferentially spaced fingers spaced by grooves, with the fingers being snapped into the ditch and is biased against the ramped surface. The plate, at least a pair of nipples and at least a pair of connection pipes are all formed of an integral piece of metal.

Abstract: A fluid coupling assembly has a single fluid connection, including a plate and at least a pair of nipples extending away from the plate in a first direction, and at least a pair of connection pipes connected to each of the nipples extending from the plate in a second opposed direction. The nipples include a thread at an outer periphery, a ramped surface spaced in a direction beyond the thread and towards the plate, and a ditch beyond the ramped surface. A fluid coupling has a thread at an inner periphery received on the thread on the nipple, and the coupling has a plurality of circumferentially spaced fingers spaced by grooves, with the fingers being snapped into the ditch and is biased against the ramped surface. The plate, at least a pair of nipples and at least a pair of connection pipes are all formed of an integral piece of metal.

Abstract: Gas turbine engine systems and related methods involving thermally isolated retention are provided. In this regard, a representative method for attaching a gas turbine engine component includes using a fastener, varying in diameter along a length thereof, to prevent a portion of a component from being crimped between surfaces to which the component is attached such that the component moves relative to the surfaces responsive to thermal cycling of a gas turbine engine of which the surfaces and the component are constituent parts.

Abstract: Gas turbine engine systems and related methods involving thermally isolated retention are provided. In this regard, a representative method for attaching a gas turbine engine component includes using a fastener, varying in diameter along a length thereof, to prevent a portion of a component from being crimped between surfaces to which the component is attached such that the component moves relative to the surfaces responsive to thermal cycling of a gas turbine engine of which the surfaces and the component are constituent parts.

Abstract: Gas turbine engine systems and related methods involving thermally isolated retention are provided. In this regard, a representative method for attaching a gas turbine engine component includes using a fastener, varying in diameter along a length thereof, to prevent a portion of a component from being crimped between surfaces to which the component is attached such that the component moves relative to the surfaces responsive to thermal cycling of a gas turbine engine of which the surfaces and the component are constituent parts.