Method for operating a turbo-machine having overload protection and turbo-machine comprising a device for carrying out said method

Patent metadata

Field	Value
Publication number	US-10415422-B2
Application number	US-201415024457-A
Country	US
Kind code	B2
Filing date	Sep 5, 2014
Priority date	Sep 30, 2013
Publication date	Sep 17, 2019
Grant date	Sep 17, 2019

Abstract

A turbo-machine is provided having at least one turbo-machine stage, wherein overload protection of the rotating shaft is provided by the method and, to protect the rotating shaft against overload, a measurement of a torsional stress of the rotating shaft is carried out during operation of the rotating shaft. The torsional stress is measured via a measurement of the torque of the rotating shaft. The torque is preferably measured magneto-elastically. By using the measured torque of the rotating shaft, the development of the torque is forecast. On the basis of the forecast produced, the turbo-machine stage or operating parameters of the turbo-machine is/are regulated. Further a turbo-machine is provided comprising at least one turbo-machine stage which has at least one rotating shaft, wherein the turbo-machine has a device for carrying out the method.

First claim

The invention claimed is:

1. A method for operating a turbomachine comprising:
providing at least one turbomachine stage which has at least one rotary shaft,
providing overload protection for the rotary shaft, wherein the overload protection includes sensing a torsional stress in the rotary shaft by measuring a torque of the rotary shaft using a contactless measurement method during operation of the rotary shaft, wherein the contactless measurement method utilizes at least one magnetoelastic torque sensor,
wherein the overload protection for the rotary shaft is accomplished through the following steps:
a) predicting a development of a future torque of the rotary shaft based on the measured torque of the rotary shaft, and
b) changing at least one operating parameter of the turbomachine stage based on the prediction.

2. The method as claimed in claim 1 , wherein the predicting a future development of a torque of the rotary shaft includes determining if the predicted torque of the rotary shaft at a future time exceeds a permissible torque limit value for the rotary shaft.

3. The method as claimed in claim 2 , wherein the at least one operating parameter of the turbomachine stage is changed such that the permissible torque limit value for the rotary shaft is complied with.

4. The method as claimed in claim 3 , wherein the permissible torque limit value for the rotary shaft acts as an alarm such that when the predicted torque of the rotary shaft at a future time exceeds the permissible limit value, the at least one operating parameter of the turbomachine stage is changed.

5. The method as claimed in claim 1 , wherein the measuring the torque of the rotary shaft is performed continuously over time.

6. The method as claimed in claim 1 , further comprising:
providing a multistage turbomachine having at least one further turbomachine stage used as the turbomachine, the further turbomachine stage having at least one further rotary shaft, and
providing overload protection for the further rotary shaft,
wherein the providing overload protection for the further rotary shaft includes sensing a further torsional stress in the further rotary shaft during operation of the further rotary shaft.

7. The method as claimed in claim 1 , wherein the at least one operating parameter includes at least one of a volumetric flow rate at the turbomachine stage of a fluid with which the flow machine stage is operated and a torque with which the rotary shaft of the turbomachine stage is driven.

8. The method as claimed in claim 1 , wherein the turbomachine is selected from the group consisting of gas turbine, steam turbine, turbocharger, pump, compressor and hydro turbine.

9. A turbomachine comprising:
at least one turbomachine stage, wherein the at least one turbomachine stage has at least one rotary shaft,
a contactless torque sensor arranged at the rotary shaft, wherein the contactless torque sensor is a magnetoelastic toque sensor, wherein the magnetoelastic toque sensor measures the torque of the rotary shaft,
wherein the turbomachine is configured to perform the method of claim 1 .

10. The turbomachine as claimed in claim 9 , wherein the turbomachine has at least one further turbomachine stage having at least one further rotary shaft.

11. The turbomachine as claimed in claim 10 , further comprising a second contactless torque sensor arranged at the at least one further rotary shaft.

12. The turbomachine as claimed in claim 9 , wherein the turbomachine is selected from the group consisting of gas turbine, steam turbine, turbocharger, pump, compressor and hydro turbine.

Assignees

• Siemens Ag

Inventors

• Brummel Hans-Gerd
• Grieshaber Dirk
• Maier Carl Udo
• Pfeifer Uwe
• De Bruyn Huub

Classifications

• F01D21/00

  Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for · CPC title

• G01L3/102

  involving magnetostrictive means (magnetostrictive sensors H10N35/101) · CPC title

• F01D21/14 Primary

  responsive to other specific conditions · CPC title

• F05D2220/32

  in gas turbines · CPC title

• F04D29/32

  for axial flow pumps · CPC title