An improvement is provided to a pressurized close-cycle machine that has a cold-end pressure vessel and is of the type having a piston undergoing reciprocating linear motion within a cylinder containing a working fluid heated by conduction through a heater head by heat from an external thermal source. The improvement includes a heat exchanger for cooling the working fluid, where the heat exchanger is disposed within the cold-end pressure vessel. The heater head may be directly coupled to the cold-end pressure vessel by welding or other methods. A coolant tube is used to convey coolant through the heat exchanger.

The heat engine with transfer-expansion and regeneration (1) includes a compressor (2) which compresses gases in a high-pressure regeneration line (6) of a regeneration heat exchanger (5) from which they emerge preheated via a high-pressure regenerator outlet line (9) which has a heat source (12) that superheats the gases, the latter being then transferred by an admission metering valve (24) operated by a metering valve actuator (25) into a transfer-expansion chamber (16) formed in particular by an expansion cylinder (13) and an expansion piston (15), the gases leaving the chamber (16) after having been expanded via an expanded gas exhaust line (26) and thanks to an exhaust valve (31) operated by an exhaust valve actuator (32) before being cooled down in a low-pressure regeneration line (7) of the regeneration heat exchanger (5).

The heat engine with transfer-expansion and regeneration (1) includes a compressor (2) which compresses gases in a high-pressure regeneration line (6) of a regeneration heat exchanger (5) from which they emerge preheated via a high-pressure regenerator outlet line (9) which has a heat source (12) that superheats the gases, the latter being then transferred by an admission metering valve (24) operated by a metering valve actuator (25) into a transfer-expansion chamber (16) formed in particular by an expansion cylinder (13) and an expansion piston (15), the gases leaving the chamber (16) after having been expanded via an expanded gas exhaust line (26) and thanks to an exhaust valve (31) operated by an exhaust valve actuator (32) before being cooled down in a low-pressure regeneration line (7) of the regeneration heat exchanger (5).

The invention relates to a Membrane Stirling Engine. The inventors propose a Membrane Stirling Engine, with working gas, with a hot part and with a cold part, where the working gas of the Stirling engine is found both in its hot part as well as its cold part in the membrane skins, which have two ends, whereby they are closed on one end hermetically and on the other end they are open, where they lead into the hot or cold space of a regenerator chamber with their open end tightly sealed.

The invention relates to a Membrane Stirling Engine. The inventors propose a Membrane Stirling Engine, with working gas, with a hot part and with a cold part, where the working gas of the Stirling engine is found both in its hot part as well as its cold part in the membrane skins, which have two ends, whereby they are closed on one end hermetically and on the other end they are open, where they lead into the hot or cold space of a regenerator chamber with their open end tightly sealed.

Aircraft with an emission-free drive and method for emission-free driving of an aircraft. The aircraft includes an aircraft thruster structured and arranged to generate thrust force on the aircraft, an aircraft lift device structured and arranged to generate lift on the aircraft, and a heat engine, which is structured and arranged to convert thermal energy into kinetic energy to drive the aircraft thruster, that includes at least one flat-plate Stirling engine drivable by solar thermal radiation.

Aircraft with an emission-free drive and method for emission-free driving of an aircraft. The aircraft includes an aircraft thruster structured and arranged to generate thrust force on the aircraft, an aircraft lift device structured and arranged to generate lift on the aircraft, and a heat engine, which is structured and arranged to convert thermal energy into kinetic energy to drive the aircraft thruster, that includes at least one flat-plate Stirling engine drivable by solar thermal radiation.

Aircraft with an emission-free drive and method for emission-free driving of an aircraft. The aircraft includes a drive device structured and arranged to generate thrust, a lift device structured and arranged to generate lift, and a heat engine structured and arranged to convert thermal energy into kinetic energy to drive the drive device. The heat engine includes at least one flat-plate Stirling engine drivable by solar thermal radiation.

Aircraft with an emission-free drive and method for emission-free driving of an aircraft. The aircraft includes a drive device structured and arranged to generate thrust, a lift device structured and arranged to generate lift, and a heat engine structured and arranged to convert thermal energy into kinetic energy to drive the drive device. The heat engine includes at least one flat-plate Stirling engine drivable by solar thermal radiation.

A free piston Stirling engine with a heat exchanger that has an inner component part assembled within an outer component part. The outer component part has a tubular outer wall and circumferentially spaced ridges that extend radially inward from the tubular outer wall and are separated from each other by inward opening slots. The inner component part has a tubular inner wall and circumferentially spaced ridges that extend outward from the inner tubular wall and are separated from each other by outward opening slots. The ridge widths of the outer and inner component parts are less than the slot widths of the corresponding slots into which they fit. The two component parts are assembled with the ridges of each component part extending into the slots of the other component part to form gas passages between interfacing sidewall surfaces of the ridges.