Method for attaching the cover of a centrifugal compressor of a turbine engine, compressor cover implementing same and compressor assembly provided with such a cover

Patent metadata

Field	Value
Publication number	US-9409228-B2
Application number	US-201113880245-A
Country	US
Kind code	B2
Filing date	Oct 20, 2011
Priority date	Oct 21, 2010
Publication date	Aug 9, 2016
Grant date	Aug 9, 2016

Abstract

An attachment arrangement at a middle of a cover having an elastically deformable portion. The cover includes a concave shell including an inner surface spaced apart from the compressor including an impeller including blades by an attachment. The attachment includes one connection end at the middle of the shell, another end attached to a casing of the turbine engine, and an axisymmetric diaphragm having a generally frusto-conical configuration having an arm profile coupled to the end for attachment to the casing by a double-elbow joint having right and obtuse angles when in a rest position. The distance between the inner surface of the shell and upper edges of the blades can be held constant during operation with minimum clearance adjustment. The cover can be moved such that clearance between the cover and blades of the compressor impeller remains substantially constant and as low as possible.

First claim

The invention claimed is:

1. A method for attaching an impeller cover of a centrifugal compressor of a turbine engine, the cover including a concave shell and an axisymmetric connection forming an attachment between a junction formed substantially in a middle of the shell and a peripheral axial attachment holding the shell apart from the impeller, the method comprising:
arranging an elastically deformable portion including a radial rim and a double-elbow joint on the connection closer to a first end for attachment than to a second end for junction to the shell so that a distance between the shell and the impeller is held constant with minimal clearances at intermediate and transient speeds of the turbine engine,
wherein, at a rest position, the double-elbow joint includes a first elbow at a substantially right angle at a first end of the radial rim, and a second elbow at an obtuse angle at a second end of the radial rim, the first elbow being disposed radially outward of the second elbow.

2. An attaching method according to claim 1 , wherein the deformable portion is arranged near the first end for attachment of the connection.

3. An attaching method according to claim 1 , wherein the connection joins the shell according to a conformation that is substantially radial with regard to a curvature of the shell at the junction.

4. A cover for a centrifugal compressor of a turbine engine, the cover comprising:
a concave shell with an inner surface that can be arranged apart from the compressor including an impeller including blades by an attachment having a first junction end formed substantially in a middle of the shell and a second end that can be fixed to a turbine engine,
wherein the attachment includes an axisymmetric diaphragm of generally frusto-conical conformation that has an arm profile coupled together, at the second end for attachment, with the shell by a double-elbow joint having right and obtuse angles when in a rest position, the joint being arranged closer to the second end for attachment than to the first end for junction to the shell so that a distance between the inner surface of the shell and upper edges of the blades can be held constant during operation with minimal clearances at intermediate and transient speeds, and
wherein the double-elbow joint includes a radial rim in which a first elbow having a substantially right angle is provided at a first end of the radial rim and a second elbow having an obtuse angle is provided at a second end of the radial rim, the first elbow being disposed radially outward of the second elbow.

5. A cover for a centrifugal compressor according to claim 4 , wherein the diaphragm includes an axial annular connection between a radial attachment rim and the double-elbow joint.

6. A cover for a centrifugal compressor according to claim 4 , wherein the arm has a substantially rectilinear profile when in the rest position and an evolutionary thickness that increases near the junction end.

7. A cover for a centrifugal compressor according to claim 4 , wherein the arm has on average a thickness substantially lower than that of the shell of the cover.

8. An assembly of a cover and a centrifugal compressor of a turbine engine, the cover being configured according to claim 4 so that the cover stays at a constant distance from the compressor during operation and the cover can be fixed to a casing of the turbine engine.

Assignees

• Renard Beatrice Marie
• Marie Billotey Geoffroy Louis-Henri
• Turbomeca

Inventors

• Renard Beatrice Marie
• Marie Billotey Geoffroy Louis-Henri

Classifications

• F01D11/08 Primary

  for sealing space between rotor blade tips and stator (specially-shaped blade tips therefor F01D5/20) · CPC title

• F01D25/246

  Fastening of diaphragms or stator-rings · CPC title

• F04D29/162

  of a centrifugal flow wheel · CPC title

• F02C3/08

  the compressor comprising at least one radial stage (F02C3/10 takes precedence) · CPC title

• F04D29/4206

  especially adapted for elastic fluid pumps · CPC title