Invention Grant
- Patent Title: Compressor rotor with anti-vortex fins
-
Application No.: US15492281Application Date: 2017-04-20
-
Publication No.: US10012240B2Publication Date: 2018-07-03
- Inventor: Tibor Urac
- Applicant: PRATT & WHITNEY CANADA CORP.
- Applicant Address: unknown Longueuil, Quebec
- Assignee: PRATT & WHITNEY CANADA CORP.
- Current Assignee: PRATT & WHITNEY CANADA CORP.
- Current Assignee Address: unknown Longueuil, Quebec
- Agency: Norton Rose Fulbright Canada
- Main IPC: F04D29/66
- IPC: F04D29/66 ; F04D29/32 ; F02C6/08

Abstract:
A compressor rotor of a gas turbine engine includes a rotor body having a face adapted to face an adjacent rotor. The rotor body extends radially between an outer peripheral rim surface and an inner rim surface. The inner rim surface defines a bore of the rotor body. A plurality of blades extends radially from the outer peripheral rim surface. A plurality of anti-vortex fins extends axially from the face of the rotor body facing the adjacent rotor. The plurality of anti-vortex fins forms a plurality of open radial passageways. The plurality of anti-vortex fins extends axially to a predetermined thickness such that, when assembled with the second rotor, axial extremities of the plurality of anti-vortex fins being in close proximity with the adjacent rotor and the adjacent rotor closes the radial passageways. A method of providing a first rotor for assembly with a second facing rotor of a compressor rotor assembly is also presented.
Public/Granted literature
- US20170218980A1 COMPRESSOR ROTOR WITH ANTI-VORTEX FINS Public/Granted day:2017-08-03
Information query