METHOD AND DEVICE FOR THRUST EQUILIBRATING TURBOSUPERCHARGER

PROBLEM TO BE SOLVED: To improve the partial load and idling characteristics of a turbosupercharger equipped with a device for thrust equilibration. SOLUTION: A connection between a high pressure range 16 of a turbosupercharger and a range 21 of the turbosupercharger, being lower in pressure than th...

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Bibliographic Details
Main Authors LICHTNER FRANK, LOOS MARKUS
Format Patent
LanguageEnglish
Published 21.03.2000
Edition7
Subjects
AIR INTAKES FOR JET-PROPULSION PLANTS
ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
BLASTING
COMBUSTION ENGINES
COMBUSTION ENGINES IN GENERAL
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES
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
STEAM ENGINES
WEAPONS
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Summary:PROBLEM TO BE SOLVED: To improve the partial load and idling characteristics of a turbosupercharger equipped with a device for thrust equilibration. SOLUTION: A connection between a high pressure range 16 of a turbosupercharger and a range 21 of the turbosupercharger, being lower in pressure than the range 16, is wholly opened in time of the full-load of the turbosupercharger, and in time of partial load, it is almost closed at the very least and in time of idling, it is completely closed. Therefore, a device constituted as an exhaust passage for thrust equilibration is equipped with a closing member 30.
Bibliography:Application Number: JP19990236049