A turbine engine system includes a heat source, a heat exchanger, a cooling medium inlet and a cooling medium outlet. The heat source includes a first passage. The heat exchanger includes a second passage and a third passage. The first and the second passages are configured in a closed loop circuit. The third passage is configured between the inlet and the outlet in an open loop circuit.

A bonded dissimilar material heat transfer assembly is provided. The assembly comprises a frame component, a thin stamped component and at least one dissimilar metal component having means for heat transfer and having a higher thermal conductivity than the frame component and stamped component. The heat transfer assembly includes a novel geometry such that distortion caused by mismatch of thermal expansion rates does not affect the normally planar shape of the assembly. Such a construction leads to higher thermal performance, lighter weight, less cost, and higher reliability than similar prior art heat exchanger assemblies.

An aspect of a method of forming a heat exchanger includes providing a metal body, removing material from the metal body to partially create a set of cooling passages, filling the partially created set of cooling passages with sacrificial material, forming a remainder of the set of cooling passages such that a set of fully formed cooling passages for the heat exchanger are defined, and removing the sacrificial material from the cooling passages.

An external combustion engine including a burner element, a heater head, a piston cylinder containing a piston, a cooler and a crankcase. The crankcase includes a crankshaft, a piston rod connected to the piston, a drive mechanism for converting the linear motion of the piston rod to rotary motion of the crankshaft and a linear cross-head bearing that is connected rigidly to the piston rod at one end and to the drive mechanism at the other end. Also the external combustion engine includes a piston clearance seal and a piston rod seal unit that has floating rod seals. The piston includes a inner dome to reduce axial heat transfer via radiation and convection.

An annular venturi burner assembly and Stirling engine. The annular venturi burner injects fuel into combustion air flowing axially through a port with an annular cross section. The fuel enters the annular cross-section from the outside diameter. The flow of air through the annular section creates suction that draws the fuel through the ports. A venturi bushing directs the flow of fuel to provide improved and more uniform mixing of fuel and air.

A turbine engine system includes a heat source, a heat exchanger, a cooling medium inlet and a cooling medium outlet. The heat source includes a first passage. The heat exchanger includes a second passage and a third passage. The first and the second passages are configured in a closed loop circuit. The third passage is configured between the inlet and the outlet in an open loop circuit.

A heat exchanger includes a frame and a plurality of coil passes disposed within the frame. The plurality of coil passes is configured to direct a flow of a refrigerant therethrough to transfer heat with an air flow passing over the heat exchanger. The plurality of coil passes include a U-bend disposed between first and second linear portions of the plurality of coil passes to redirect the refrigerant from a first longitudinal end of the heat exchanger to a second longitudinal end of the heat exchanger. Additionally, a first plurality of fins is disposed on an outer surface the U-bend.

A system and method for a multistage condenser is described that reduces problems associated with temperature and pressure differential strains on tubes above and below a dead tube. Instead of connecting the dead tube to the I/O manifold, a physical separation is created. The physical separation can be created by shortening the dead tube, coring a portion of the I/O manifold where the dead tube is received, independent I/O manifolds, or other means.

An exhaust gas recirculation cooler may include a housing having a coolant inlet opening into an inlet region and a coolant outlet, and a plurality of cooling tubes arranged in the housing next to one another to form a tube row, each cooling tube connecting an exhaust gas inlet and outlet. At least two tube rows with one arranged on top of another and spaced from each other may form a tube block. Exhaust gas may be flowable through an inside of each cooling tube, and a coolant flow may be able to be circulated outside of the cooling tubes within the housing and flowable through an annular space enclosing the tube block in a circumferential direction. A flow guide arrangement for guiding the coolant in the interior of the tube block may be arranged in the housing lying against at least portions of one of the tube rows.

A bonded dissimilar material heat transfer assembly is provided. The assembly comprises a frame component, a thin stamped component and at least one dissimilar metal component having means for heat transfer and having a higher thermal conductivity than the frame component and stamped component. The heat transfer assembly includes a novel geometry such that distortion caused by mismatch of thermal expansion rates does not affect the normally planar shape of the assembly. Such a construction leads to higher thermal performance, lighter weight, less cost, and higher reliability than similar prior art heat exchanger assemblies.