IP Library Granted Patent US 10,774,673
Granted Patent B2
US 10,774,673 · App. 15/566,483 · Granted Sep 15, 2020

Guide vane adjustment device and turbomachine

Inventor: Lennart Leopold (Berlin, DE)
Assignee: MAN Energy Solutions SE
F01D17/162F01D9/041F01D17/00F01D17/167F04D29/563F04D29/566F01D5/02F05D2260/50
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Quick Facts
Patent No.
US 10,774,673
App. No.
15/566,483
Granted
Sep 15, 2020
Kind
B2
Abstract

Guide vane adjusting device for a flow machine to rotate guide vanes, with a driveshaft, and a control ring that transmits rotation of the driveshaft to rotate the guide vanes. The driveshaft is directly coupled with one of the guide vanes to be directly rotatable by the driveshaft without the intermediary of the control ring. The directly driven guide vane is articulately coupled with the control ring via a transmission lever. The other guide vanes are indirectly rotatable with the intermediary of the control ring. The control ring is displaceable in circumferential and axial direction such that forces at coupling points between the control ring and the transmission levers coupled with the control ring run perpendicular to the transmission levers.

Claims (23)

1. A guide vane adjusting device for a flow machine, the guide vane adjusting device configured to rotate a plurality of guide vanes, the plurality of guide vanes arranged to form a guide vane ring around a guide vane axis of the guide vane ring, the guide vane adjusting device comprising:

a driveshaft directly coupled to one of the plurality of guide vanes of the guide vane ring at a radially outer portion of the one guide vane such that the one guide vane is directly rotated by the driveshaft, the driveshaft configured to be coupled to and driven by a drive motor;

a control ring arranged radially outside the plurality of guide vanes and configured to transmit a rotation of the driveshaft to rotate all of the plurality of guide vanes of the guide vane ring except the one guide vane directly coupled to the driveshaft, such that the one guide vane directly coupled to the driveshaft is directly rotated by the driveshaft without the control ring as an intermediary;

a multiple-part transmission lever configured to articulatedly couple the control ring to the driveshaft and the one guide vane that is directly rotated by the driveshaft, wherein a first segment of the multiple-part transmission lever is rigidly coupled with one of the drive shaft and the one guide vane that is directly rotated by the driveshaft, and a second segment of the multiple-part transmission lever is articulatedly coupled with the control ring, and such that the first segment of the multiple-part transmission lever is articulatedly coupled with the second segment of the multiple-part transmission lever,

wherein a pair of joint bearings are configured to couple the first segment of the multiple-part transmission lever to the second segment of the multiple-part transmission lever, and an individual third joint bearing is configured to couple the second segment of the multiple-part transmission lever to the control ring, wherein the individual third joint bearing is axially offset from the pair of joint bearings with respect to the driveshaft,

wherein the driveshaft is indirectly coupled with all of the plurality of guide vanes of the guide vane ring except the one guide vane directly coupled to the driveshaft, such that the plurality of guide vanes indirectly coupled with the driveshaft are indirectly rotated with the control ring as an intermediary;

respective additional single-part transmission levers configured to articulatedly couple the control ring to respective radially outer portions of the plurality of guide vanes that are indirectly rotated by the driveshaft,

wherein the control ring is displaceable in a circumferential direction and in an axial direction such that forces exerted at coupling points between the control ring and the respective additional single-part transmission levers run perpendicular to the respective additional single-part transmission levers with respect to the circumferential direction of the control ring,

wherein the additional single-part transmission levers are elastically deformable and configured to articulatedly couple the control ring to the driveshaft and the one guide vane that is directly rotated by the driveshaft, wherein a first segment of the respective additional single-part transmission lever is rigidly coupled with one of the driveshaft and the one guide vane that is directly rotated by the driveshaft, and a second segment of the respective additional single-part transmission lever is articulatedly coupled with the control ring, such that the first segment of the respective additional single-part transmission lever is radially in line with the second segment of the respective additional single-part transmission lever for each respective guide vane that is indirectly coupled with the driveshaft.

2. The guide vane adjusting device according to claim 1 , wherein each of the additional single-part transmission levers are provided with a respective joint bearing formed between the respective additional single-part transmission lever and the control ring.

3. The guide vane adjusting device according to claim 1 , wherein respective additional multiple-part transmission levers are used in lieu of the respective additional single-part transmission levers, the respective additional multiple-part transmission levers configured such that a first segment of the respective additional multiple-part transmission lever is rigidly coupled with a respective guide vane of the plurality of guide vanes, and a second segment of the respective additional multiple-part transmission lever is articulatedly coupled with the control ring.

4. The guide vane adjusting device according to claim 3 , wherein the first segment of the respective additional multiple-part transmission lever is articulatedly coupled with the second segment of the respective additional multiple-part transmission lever.

5. A flow machine comprising:

a stator having a plurality of guide vanes, the plurality of guide vanes arranged to form a guide vane ring around a guide vane axis of the guide vane ring; and

a guide vane adjusting device configured to adjust the plurality of guide vanes of the guide vane ring, the guide vane adjusting device comprising:

a driveshaft directly coupled to one of the plurality of guide vanes of the guide vane ring at a radially outer portion of the one guide vane such that the one guide vane is directly rotated by the driveshaft, the driveshaft configured to be coupled to and driven by a drive motor;

a control ring arranged radially outside the plurality of guide vanes and configured to transmit a rotation of the driveshaft to rotate all of the plurality of guide vanes of the guide vane ring except the one guide vane directly coupled to the driveshaft, such that the one guide vane directly coupled to the driveshaft is directly rotated by the driveshaft without the control ring as an intermediary;

a multiple-part transmission lever configured to articulatedly couple the control ring to the driveshaft and the one guide vane that is directly rotated by the driveshaft, wherein a first segment of the multiple-part transmission lever is rigidly coupled with one of the drive shaft and the one guide vane that is directly rotated by the driveshaft, and a second segment of the multiple-part transmission lever is articulatedly coupled with the control ring, and such that the first segment of the multiple-part transmission lever is articulatedly coupled with the second segment of the multiple-part transmission lever,

wherein a pair of joint bearings are configured to couple the first segment of the multiple-part transmission lever to the second segment of the multiple-part transmission lever, and an individual third joint bearing is configured to couple the second segment of the multiple-part transmission lever to the control ring, wherein the individual third joint bearing is axially offset from the pair of joint bearings with respect to the driveshaft,

wherein the driveshaft is indirectly coupled with all of the plurality of guide vanes of the guide vane ring except the one guide vane directly coupled to the driveshaft, such that the plurality of guide vanes indirectly coupled with the driveshaft are indirectly rotated with the control ring as an intermediary;

respective additional single-part transmission levers configured to articulatedly couple the control ring to respective radially outer portions of the plurality of guide vanes that are indirectly rotated by the driveshaft,

wherein the control ring is displaceable in a circumferential direction and in an axial direction such that forces exerted at coupling points between the control ring and the respective additional single-part transmission lever run perpendicular to the respective additional single-part transmission lever with respect to the circumferential direction of the control ring,

wherein the additional single-part transmission levers are elastically deformable and configured to articulatedly couple the control ring to the driveshaft and the one guide vane that is directly rotated by the driveshaft, wherein a first segment of the respective additional single-part transmission lever is rigidly coupled with one of the driveshaft and the one guide vane that is directly rotated by the driveshaft, and a second segment of the respective additional single-part transmission lever is articulatedly coupled with the control ring, such that the first segment of the respective additional single-part transmission lever is radially in line with the second segment of the respective additional single-part transmission lever for each respective guide vane that is indirectly coupled with the driveshaft.

Assignments (3)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 17, 2025
From: MAN ENERGY SOLUTIONS SE
To: EVERLLENCE SE
Reel/Frame 072914/0273 →
CHANGE OF NAME Recorded Aug 14, 2018
From: MAN DIESEL & TURBO SE
To: MAN ENERGY SOLUTIONS SE
Reel/Frame 046818/0806 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 17, 2017
From: LEOPOLD, LENNART
To: MAN DIESEL & TURBO SE
Reel/Frame 044158/0817 →
Priority Claims (1)
DE 10 2015 004 648 · Apr 15, 2015 · national
Continuity (1)
Related Publication 20180100407A1 · Apr 12, 2018