Centering attachment of a compressor housing cover

Patent metadata

Field	Value
Publication number	US-9291073-B2
Application number	US-201113825035-A
Country	US
Kind code	B2
Filing date	Sep 22, 2011
Priority date	Sep 22, 2010
Publication date	Mar 22, 2016
Grant date	Mar 22, 2016

Abstract

A casing is provided having a longitudinal axis of a turbomachine, the axis extending along a rotor. The casing includes at least one jacket part extending along the longitudinal axis and at least one end-face cover. The cover is surrounded by the jacket part at least with a part of the axial extension of the cover. In order to reduce the need for radial clearance, without compromising the availability or safety of the operation of the machine, the cover has radial clearance with respect to the jacket part and at least two separate guide elements of the cover are provided on the jacket part in two different circumferential positions with respect to the longitudinal axis. The respective guide elements are designed such that they block a respective movement of the cover in the circumferential direction at least unidirectionally.

First claim

The invention claimed is:

1. A casing with a longitudinal axis of a turbomachine extending alon a rotor the casin comprising:
at least one jacket part which extends along the longitudinal axis, and
at least one end-face cover,
wherein the casing has a horizontal parting line parallel to the longitudinal axis, which cover is surrounded by the jacket part at least by way of part of its axial extension,
wherein the cover has a radial clearance in relation to the jacket part and in that at least two separate guide elements of the cover are provided on the jacket part at two different circumferential positions with reference to the longitudinal axis,
wherein the at least two separate guide elements are respectively configured in such a manner that they block a movement of the cover in the circumferential direction at least in a unidirectional manner,
wherein a centering device is provided on the casing, the centering device having two supporting faces which abut against contact faces of the cover,
wherein the supporting faces and contact faces are configured in such a manner that a horizontal movement of the cover perpendicular with respect to the longitudinal axis is blocked in a bidirectional manner, and
wherein the cover includes at least one shaft seal, via which a circumferential gap between the rotor and the opening of the cover is sealable.

2. A casing with a longitudinal axis of a turbomachine extending along a rotor, the casing comprising:
at least one jacket part which extends along the longitudinal axis, and
at least one end-face cover,
wherein the casing has a horizontal parting line parallel to the longitudinal axis, which cover is surrounded by the jacket part at least by way of part of its axial extension,
wherein the cover has a radial clearance in relation to the jacket part and in that at least two separate guide elements of the cover are provided on the jacket part at two different circumferential positions with reference to the longitudinal axis,
wherein the at least two separate guide elements are respectively configured in such a manner that they block a movement of the cover in the circumferential direction at least in a unidirectional manner,
wherein a centering device is provided on the casing, the centering device having two supporting faces which abut against contact faces of the cover,
wherein the supporting faces and contact faces are configured in such a manner that a horizontal movement of the cover perpendicular with respect to the longitudinal axis is blocked in a bidirectional manner, and
wherein the cover has a first supporting face which extends in the circumferential direction and cooperates in a sealing manner with a second supporting face on the jacket part, wherein a surface normal of the second supporting face points into the interior of the casing and a surface normal of the first supporting face is directed in the opposite direction such that an excessive pressure in the interior of the casing presses the two supporting faces against one another.

3. A casing with a longitudinal axis of a turbomachine extending along a rotor, the casing comprising:
at least one jacket part which extends along the longitudinal axis, and
at least one end-face cover,
wherein the casing has a horizontal parting line parallel to the longitudinal axis, which cover is surrounded by the jacket part at least by way of part of its axial extension,
wherein the cover has a radial clearance in relation to the jacket part and in that at least two separate guide elements of the cover are provided on the jacket part at two different circumferential positions with reference to the longitudinal axis,
wherein the at least two separate guide elements are respectively configured in such a manner that they block a movement of the cover in the circumferential direction at least in a unidirectional manner,
wherein a centering device is provided on the casing, the centering device having two supporting faces which abut against contact faces of the cover,
wherein the supporting faces and contact faces are configured in such a manner that a horizontal movement of the cover perpendicular with respect to the longitudinal axis is blocked in a bidirectional manner, and
wherein the casing is a turbo-compressor casing.

4. The casing as claimed in claim 3 , wherein the cover has an opening for positioning the rotor extending through the opening axially.

5. The casing as claimed in claim 3 , wherein the at least two separate guide elements are arranged and configured such that they support the force due to the weight of the cover.

6. The casing as claimed in claim 3 , wherein the at least two separate guide elements are arranged in such a manner that in operation the clearance is produced concentrically with respect to the longitudinal axis.

7. The casing as claimed in claim 5 , wherein the at least two separate guide elements are arranged through the longitudinal axis along a horizontal and the centering device is arranged through the longitudinal axis along a vertical.

8. The casing as claimed in claim 3 , wherein the cover includes a radial bearing.

9. The casing as claimed in claim 1 , wherein the shaft seal included by the cover includes a dry gas seal.

10. The casing as claimed in claim 3 , wherein the at least two separate guide elements block a free vertical movement of the cover only on one side and the centering device blocks a horizontal free movement perpendicular with respect to the longitudinal axis of the cover in a bidirectional manner.

Assignees

• Naβ Dieter
• Siemens Ag

Inventors

• Naβ Dieter

Classifications

• F05D2220/40

  in turbochargers · CPC title

• F04D29/4206

  especially adapted for elastic fluid pumps · CPC title

• F04D29/102

  especially adapted for elastic fluid pumps · CPC title

• F04D29/083

  especially adapted for elastic fluid pumps · CPC title

• F01D25/24 Primary

  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 title