Abstract: A valve and a heat exchanger apparatus for a gas turbine engine include a valve body having a valve seat and an actuation component including a plate formed from a set of metal layers and responsive to a change in at least one of a thermal condition and a pressure exerted thereon such that the plate moves and the valve moves between an opened and a closed position where a portion of the plate engages with the valve seat.

Abstract: A heat exchanger includes a core defining a first passageway and a second passageway. The core includes a plurality of unit cells coupled together. Each unit cell of the plurality of unit cells includes a first wall and a second wall. The second wall is spaced from the first wall. The first wall at least partially defines a first passageway portion and a second passageway portion. The second wall at least partially defines the second passageway portion. The second wall extends about the first wall such that the first passageway portion is nested within the second passageway portion.

Abstract: A heat exchanger includes a cooling air conduit having multiple baffles, a hot air conduit having multiple passes through the cooling air conduit and forming multiple intersections with the baffles, and multiple perforations extending through the baffles. A cooling air flow passes through the baffles, rather than strictly between the baffles, and improves heat-transfer characteristics of the heat exchanger.

Abstract: A heat exchanger is provided. The heat exchanger is formed of a spiral wound flow body (70) having a plurality of passages (76) ending therethrough for passage of a first fluid. The flow body is positioned within a housing (42) and a cross-flow of a second fluid passes between or across successive layers of the spiral wound flow body. The intermixing of the thermal energy of the cross-flowing second fluid and the first fluid provide improved heat exchange.

Abstract: A heat exchanger is provided having an integrally and seamlessly formed return manifold connecting multiple supply tubes and return tubes. The heat exchanger may also include a return manifold having one or more structures providing a flow restriction within or proximate the return manifold.

Abstract: The present innovation relates to a gas turbine engine comprising an engine core with a combustion section, a fuel circuit fluidly coupled to the combustion section, an oil circuit fluidly coupled to the engine core, and an oil heat exchanger comprising a portion of the fuel circuit forming part of the oil circuit.

Abstract: A heat exchanger includes a core defining a first passageway configured for a first fluid to flow through and a second passageway configured for a second fluid to flow through. The core includes a plurality of unit cells coupled together. Each unit cell of the plurality of unit cells includes a sidewall at least partly defining a first passageway portion, a second passageway portion, a plurality of first openings for the first fluid to flow through, and a plurality of second openings for the second fluid to flow through. Each unit cell of the plurality of unit cells is configured to enable the first fluid to combine and divide in the first passageway portion. Each unit cell is further configured to enable the second fluid to combine and divide in the second passageway portion.

Abstract: A heat exchanger apparatus including a surface cooler and a passive automatic retraction and extension system coupled to the surface cooler. The surface cooler having disposed therein one or more fluid flow channels configured for the passage therethrough of a heat transfer fluid to be cooled. The heat transfer fluid in a heat transfer relation on an interior side of said one or more fluid flow channels. The surface cooler including a plurality of fins projecting from an outer surface thereof. The passive automatic retraction and extension system including a thermal actuation component responsive to a change in temperature of at least one of the heat transfer fluid and a cooling fluid flow so as to actuate a change in a geometry of the surface cooler. Further disclosed is an engine including the heat exchanger apparatus.

Abstract: A spark plug having a shell defining a cavity, an insulator disposed within the cavity, and an electrode at least partially encapsulated by the insulator. The electrode may be formed from a ruthenium (Ru) electrode material having a columnar grain structure. Further, the ruthenium (Ru) electrode material may have a purity greater than 99.90 wt. percentage.

Abstract: A spark plug having a shell defining a cavity, an insulator disposed within the cavity, and an electrode at least partially encapsulated by the insulator. The electrode may be formed from a ruthenium (Ru) electrode material having a columnar grain structure. Further, the ruthenium (Ru) electrode material may have a purity greater than 99.90 wt. percentage.

Abstract: An ignition lead in an engine for conducting a large current and high voltage ignition pulse from an exciter to an igniter, which may then transform the pulse received from the ignition lead into an electrical spark, which ignites a fuel and air mixture in the combustor of the engine. The ignition lead may include a construction for improved electromagnetic shielding.

Abstract: An ignition lead in an engine for conducting a large current and high voltage ignition pulse from an exciter to an igniter, which may then transform the pulse received from the ignition lead into an electrical spark, which ignites a fuel and air mixture in the combustor of the engine. The ignition lead may include a construction for improved electromagnetic shielding.