LOAD-BEARING SUPPORT OF TURBOJET ENGINE COMPRESSOR

FIELD: turbojet engine compressors using high-head and wide-chord moving blades. ^ SUBSTANCE: proposed load-bearing support of turbojet engine compressor is made in the form of hollow radial shell provided with longitudinal and transverse partitions dividing its space into separate cavities, each co...

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Bibliographische Detailangaben
Hauptverfasser:	KRITSKIJ VASILIJ JUR'EVICH, MARCHUKOV EVGENIJ JUVENAL'EVICH, SOROKIN ANDREJ ARTUROVICH, KUZNETSOV ANDREJ GENNAD'EVICH, ANDREEV ANATOLIJ VASIL'EVICH, DROZDENKO VIKTOR NIKOLAEVICH
Format:	Patent
Sprache:	eng ; rus
Schlagworte:	BLASTING HEATING 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:	FIELD: turbojet engine compressors using high-head and wide-chord moving blades. ^ SUBSTANCE: proposed load-bearing support of turbojet engine compressor is made in the form of hollow radial shell provided with longitudinal and transverse partitions dividing its space into separate cavities, each communicating with compressor flow path through at least one hole thereby reducing pressure fluctuation amplitude in gas-air path of compressor by several times. ^ EFFECT: reduced transient loads on structure, enhanced service life and operating reliability of compressor. ^ 1 cl, 4 dwg