ADAPTIVE CORE ENGINE

A gas turbine engine having an adaptive core (10) capable of maintaining a substantially constant core pressure ratio while having a variable flow rate is disclosed. In one aspect, the adaptive core composes a front block compressor (30) and a rear block compressor (40). L'invention porte sur u...

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Bibliographische Detailangaben
1. Verfasser:	JOHNSON, JAMES, EDWARD
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT PUMPS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS WEAPONS
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Beschreibung
Zusammenfassung:	A gas turbine engine having an adaptive core (10) capable of maintaining a substantially constant core pressure ratio while having a variable flow rate is disclosed. In one aspect, the adaptive core composes a front block compressor (30) and a rear block compressor (40). L'invention porte sur un moteur à turbine à gaz possédant un noyau central adaptatif (10) capable de maintenir un rapport de pression de noyau central sensiblement constant tout en présentant un débit variable. Dans un aspect, le noyau central adaptatif constitue un compresseur de bloc avant (30) et un compresseur de bloc arrière (40).