Housing for a turbo-machine working as an energy exchanger with isochoric combustion

In a turbo-machine which works as an energy exchanger with isochoric combustion and which consists essentially of a rotor (1) with cells (2), of a rotor housing enclosing its circumference and of housings (3a, 3b) closing off the end faces of the rotor (1) and having ducts (4), the rotor housing enc...

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Bibliographische Detailangaben
1. Verfasser:	ALTHAUS, ROLF., FLAWIL, CH
Format:	Patent
Sprache:	eng ; ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES COMBUSTION ENGINES IN GENERAL CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS INTERNAL-COMBUSTION PISTON ENGINES LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPING OF FLUID BY DIRECT CONTACT OF ANOTHER FLUID OR BYUSING INERTIA OF FLUID TO BE PUMPED PUMPS FOR LIQUIDS OR ELASTIC FLUIDS SIPHONS STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	In a turbo-machine which works as an energy exchanger with isochoric combustion and which consists essentially of a rotor (1) with cells (2), of a rotor housing enclosing its circumference and of housings (3a, 3b) closing off the end faces of the rotor (1) and having ducts (4), the rotor housing enclosing the circumference is a thin-walled supporting spacer housing (5) which is arranged at a short distance from the rotor (1) and which is encased by a non-supporting insulating housing (6) which reflects thermal radiation, for example is metallised, the axial rotor position being capable of being positioned by a regulating system (7) in such a way that the gap width (8) between the two end faces of the rotor (1) and the housings (3a, 3b) is constant at all the operating points. As a result, the losses can be reduced and the efficiency of the machine increased.