METHOD OF AND DEVICE TO PREVENT SURFACE OF AIRCRAFT DOUBLE-FLOW TURBOJET ENGINE AT TAKE-OFF REGIME

FIELD: aircraft industry; turbojet engines. ^ SUBSTANCE: according to proposed method, intensive cooling of high-pressure compressor housing is carried out by flow from external circuit at relative velocity of lambda>0.1 for 0.2.t0< t

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Bibliographische Detailangaben
1. Verfasser:	SEMERNJAK L.I
Format:	Patent
Sprache:	eng ; rus
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 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: aircraft industry; turbojet engines. ^ SUBSTANCE: according to proposed method, intensive cooling of high-pressure compressor housing is carried out by flow from external circuit at relative velocity of lambda>0.1 for 0.2.t0< t