Impeller shroud of a centrifugal compressor

• US 4,264,271 A
• Filed: 03/15/1979
• Issued: 04/28/1981
• Est. Priority Date: 03/15/1979
• Status: Expired due to Term

• Current Assignee: Alliedsignal Inc. (Honeywell International Inc.)
• Original Assignee: Avco Corporation (Textron Inc)
• Inventors: Libertini, Zoltan L.
• Primary Examiner(s): Wilhite, Billy J.
• Application Number:
  US06/020,566
• Time in Patent Office: 775 Days
• Field of Search: 415/134, 415/170 A, 415/174
• US Class Current: 415/173.3
• CPC Class Codes: F01D 11/08 for sealing space between rotor blade tips and stator specially-shaped blade tips therefor F01D5/20
• CPC Class Codes: F01D 25/24 Casings modified for heating or cooling F01D25/14; Casing parts, e.g. diaphragms, casing fastenings casings for rotary machines or engines in general F16M ; special arrangements in stators dealing with breaking-off of part of rotor F01D21/045
• CPC Class Codes: F04D 29/441 especially adapted for elastic fluid pumps
• CPC Class Codes: F05D 2210/42 Axial inlet and radial outlet
• CPC Class Codes: F05D 2210/43 Radial inlet and axial outlet

Abstract

The shroud or stationary housing for the impeller of a centrifugal compressor includes inherent means for selectively controlling the displacement thereof during operation of the centrifugal compressor, and in a manner to substantially maintain uniform spacing or clearance between the shroud and the blade tips of the rotating impeller in order to achieve improved performance at both part and full power operating conditions. The shroud is preferably formed of a unitary member including an annular, concave disc portion substantially corresponding to the configuration of the tips of the blades of the impeller, with the annular concave disc portion being rigid and connected to a fixed flange support portion by a flexible, annular diaphragm which extends generally perpendicular to the shaft of the impeller. The annular diaphragm is sufficiently flexible such that during operation of the centrifugal compressor, the differential thermal and pressure forces generated along the length of the blades within the compressor cause deformation of the flexible diaphragm and a substantially linear movement of the rigid, concave disc portion relative to the flange support portion. The movement of the annular concave disc portion substantially corresponds to the change in configuration of the blades, thereby minimizing blade tip losses.

Claims

1. A shroud for the impeller of a centrifugal compressor wherein the shaft of said impeller is generally aligned with the air flow, said shroud comprising:

a rigid, annular concave disc portion substantially corresponding to the configuration of the tips of the blades of the impeller and spaced therefrom;

a flexible, annular diaphragm of a generally flattened, ring configuration having an inner and outer diameter, said diaphragm extending generally peripendicular to the shaft of the impeller, with the inner diameter of said diaphragm being connected to the annular concave disc portion intermediate the width thereof; and

a flange support portion connecting the flexible diaphragm to a fixed support frame, extending generally parallel to the shaft of said compressor and connected to the outer diameter of said flexible, annular diaphragm whereby, during operation of the centrifugal compressor, the differential thermal and pressure forces developed within the compressor cause a deformation of the flexible diaphragm and a corresponding displacement of said annular, concave disc portion relative to the flange support portion so as to maintain substantially uniform clearance between said annular concave disc portion and the blade tips.

2. A shroud for the impeller of a centrifugal compressor wherein the shaft of said impeller is generally aligned with the air flow as in claim 1 wherein said shroud is formed of a unitary member.

3. A shroud for the impeller of a centrifugal compressor wherein the shaft of said impeller is generally aligned with the air flow as in claim 1, wherein said flange support portion includes a first cylinder portion extending generally parallel to the impeller shaft and an apertured support connected adjacent one end thereof and extending peripendicular thereto, said apertured support being connected to the frame.

4. In combination with a centrifugal compressor, said centrifugal compressor including an impeller, the shaft of which is aligned with the air flow to the compressor, a shroud enveloping and spaced from the edges of the blades of said impeller, said shroud comprising:

a rigid, annular concave disc portion, the inner surface of which is juxtaposed to the edges of the blades of the impeller;

a flexible, annular diaphragm of a generally flattened, ring configuration having an inner diameter and an outer diameter, said flexible diaphragm extending generally peripendicular to the shaft of the impeller, with the inner diameter of said diaphragm being rigidly connected to the annular concave disc portion intermediate the length thereof; and

a flange support portion connecting the flexible diaphragm to a fixed support frame, said flange support portion including a cylinder portion extending generally parallel to the impeller shaft and an apertured support portion connected adjacent one end thereof and extending perpendicular thereto, said apertured support being connected to the frame whereby, during operation of the centrifugal compressor, the differential thermal and pressure forces developed within the compressor cause deformation of the flexible diaphragm and a corresponding axial and radial displacement of said annular, concave disc portion relative to the frame so as to maintain substantially uniform clearance between the annular concave disc portion and the juxtaposed blade edges.

5. The combination of claim 4 wherein said shroud is a unitary member.