FIELD: engines and pumps.
SUBSTANCE: turbojet axial compressor housing is furnished with fixed blades and multiple working blades revolving about lengthwise axis. Radial outer ends of working blades are arranged nearby housing inner side. Housing annular element facing one blade of said multiple working blades 20 makes housing machining zone facing said blades. Said zone has closed groove extending above housing inner wall limited angular sector.
EFFECT: prevented pressure pulsations caused by break-away rotation.
18 cl, 8 dwg
Authors
Dates
2013-08-10—Published
2008-02-20—Filed