RECIRCULATION STRUCTURE FOR A TURBOCOMPRESSOR

Canada Patent

PATENT NO 2496543
APP PUB NO CA-2496543-A1
SERIAL NO

2496543

Stats

Importance

Loading Importance Indicators... loading....

Abstract

See full text

Disclosed is a recirculation structure for a turbocompressor, comprising an annular chamber which is arranged in the area of the free blade ends (25 to 28) of a blade ring and radially borders the main flow channel (29 to 32), and a plurality of guiding elements (37 to 40) which are disposed inside the annular chamber and are spread across the circumference thereof. Said annular chamber allows the flow to penetrate in the circumferential direction in the front and/or rear area. The guiding elements are connected in a fixed manner to at least one wall of the annular chamber but are detached everywhere else. The tips of the guiding elements, which face the annular chamber, run on and/or near the contour of the main flow channel while axially overlapping the free blade ends or axially bordering the area of the free blade ends.

Loading the Abstract Image... loading....

First Claim

See full text

Family

Loading Family data... loading....

Patent Owner(s)

  • Owner owned or assignment not recorded

International Classification(s)

Inventor(s)

  • No Inventor to display

Cited Art Landscape

Load Citation