# US 9,752,509 B2 · Method for controlling coupling of shafts between a first machine and a second machine using rotation speeds and angles > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 9,752,509 B2 - Document ID: US9752509B2 - Status: Granted - Kind: B2 - Application number: 14/010,669 - Filed: 2013-08-27 - Published: 2015-03-05 - Granted: 2017-09-05 - Earliest claimed: 2013-08-27 - Assignees: Siemens Energy, Inc. - Applicants: Peter Jon Clayton; Joseph David Hurley; Albert C. Sismour, Jr.; Melissa A. Batis-Carver - Inventors: Peter Jon Clayton; Joseph David Hurley; Albert C. Sismour, Jr.; Melissa A. Batis-Carver - Web page: https://patentgrep.com/patent/US9752509B2 ## CPC - F02C 7/36: Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user ({F02C3/107 - F02C3/13 and} F02C7/32 take precedence; couplings for transmitting rotation F16D; gearing in general F16H) - F01K 23/101: {Regulating means specially adapted therefor (F01K23/105, F01K23/108 take precedence)} - F01K 23/16: all the engines being turbines (F01K23/14 takes precedence) - F05D 2270/023: of different spools or shafts - Y02E 20/16: Combined cycle power plant [CCPP], or combined cycle gas turbine [CCGT] - F02C: GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS (construction of turbines F01D; jet-propulsion plants F02K; construction of compressors or fans F04; generating combustion products of high pressure or high velocity F23R; using gas turbines in compression refrigeration plants F25B11/00) - F01K: STEAM ENGINE PLANTS; STEAM ACCUMULATORS; ENGINE PLANTS NOT OTHERWISE PROVIDED FOR; ENGINES USING SPECIAL WORKING FLUIDS OR CYCLES (gas-turbine or jet-propulsion plants F02; nuclear power plants, engine arrangements therein G21D) - F05D: INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS - Y02E: REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION ## Abstract A method for controlling coupling between a first machine including a first rotating shaft having an associated first positional phase angle defined by a first shaft indicia and a second machine including a second rotating shaft having an associated second positional phase angle defined by a second shaft indicia. A rotational speed and rotational angle of the first shaft are monitored, and rotation of the second shaft is controlled by bringing the second shaft to a predetermined rotational speed relative to the first shaft speed. Acceleration of the second shaft is controlled such that the second shaft indicia is within a predetermined angle relative to the first shaft indicia upon the second shaft being brought to the predetermined rotational speed, at which point the first and second shafts are coupled such that the second shaft indicia is within the predetermined angle relative to the first shaft indicia. ## Claims ### Claim 1 A method for controlling coupling between a first machine and a second machine, the first machine including a first rotating shaft having a first shaft indicia and the second machine including a second rotating shaft having a second shaft indicia, the method comprising: monitoring a rotational speed and rotational angle of the first shaft; controlling rotation of the second shaft comprising: determining a first positional phase angle of the first rotating shaft, determining a second positional phase angle of the second rotating shaft, determining a relative phase angle between the first positional phase angle and the second positional phase angle, controlling the rotational speed of the first shaft constantly at a synchronous speed, accelerating the second shaft to a predetermined rotational speed relative to the synchronous speed of the first shaft, reducing the acceleration of the second shaft when a rotational speed of the second shaft is approaching the synchronous speed so that the second positional phase angle is slowly changing, waiting until the second positional phase angle is within a predetermined relative phase angle to the first positional phase angle, and coupling the first and second shafts at the same time when the second shaft is brought to the predetermined rotational speed and the second positional phase angle is within the predetermined relative phase angle, wherein the first positional phase angle of the first shaft is determined by a first once per revolution sensor sensing a position of the first shaft indicia at each rotation of the first shaft, and wherein the second positional phase angle of the second shaft is determined by a second once per revolution sensor sensing a position of the second shaft indicia at each rotation of the second shaft. ### Claim 2 (depends on 1) The method of claim 1, wherein the first machine is a gas turbine and the second machine is a steam turbine. ### Claim 3 (depends on 2) The method of claim 2, wherein exhaust gases from gas turbine are used to power the steam turbine to effect rotation of the second shaft. ### Claim 4 (depends on 1) The method of claim 1, wherein, during the step of controlling rotation of the second shaft, the first shaft rotates at a substantially constant speed and the speed of the second shaft is increased. ### Claim 5 (depends on 1) The method of claim 1, wherein the predetermined rotational speed comprises a normal operating speed of the first shaft. ### Claim 6 (depends on 1) The method of claim 1, wherein the first and second shaft indicia each comprise one of a notch and a tooth. ### Claim 7 (depends on 1) The method of claim 1, wherein the first and second shafts are coupled together at the predetermined relative phase angle to effect a reduction in vibration in the first and second machines. ### Claim 8 (depends on 7) The method of claim 7, wherein vibrational vectors of the first and second shafts offset each other when coupled together to effect a substantially balanced combined shaft. ### Claim 9 A method for controlling coupling between a gas turbine and a steam turbine in a combined cycle power plant, the gas turbine including a first rotating shaft having a first shaft indicia and the steam turbine including a second rotating shaft having a second shaft indicia, the method comprising: monitoring a rotational speed and rotational angle of the first shaft; controlling rotation of the second shaft comprising: determining a first positional phase angle of the first rotating shaft, determining a second positional phase angle of the second rotating shaft, determining a relative phase angle between the first positional phase angle and the second positional phase angle, controlling the rotational speed of the first shaft constantly at a synchronous speed, accelerating the second shaft to a predetermined rotational speed relative to the synchronous speed of the first shaft, reducing the acceleration of the second shaft when a rotational speed of the second shaft is approaching the synchronous speed so that the second positional phase angle is slowly changing, waiting until the second positional phase angle is at a predetermined relative phase angle to the first positional phase angle, and coupling the first and second shafts at the same time when the second shaft is brought to the predetermined rotational speed and the second positional phase angle is at the predetermined relative phase angle, wherein a position of the first shaft indicia at each rotation of the first shaft is sensed by a first once per revolution sensor to determine the first positional phase angle of the first shaft and a position of the second shaft indicia at each rotation of the second shaft is sensed by a second once per revolution sensor to determine the second positional phase angle of the second shaft. ### Claim 10 (depends on 9) The method of claim 9, wherein exhaust gases from gas turbine are used to power the steam turbine to effect rotation of the second shaft. ### Claim 11 (depends on 9) The method of claim 9, wherein the predetermined rotational speed comprises a normal operating speed of the first shaft. ### Claim 12 (depends on 9) The method of claim 9, wherein the first and second shaft indicia each comprise one of a notch and a tooth. ### Claim 13 (depends on 9) The method of claim 9, wherein the first and second shafts are coupled together at the predetermined relative phase angle to effect a reduction in vibration in the first and second machines. ### Claim 14 (depends on 13) The method of claim 13, wherein vibrational vectors of the first and second shafts offset each other when coupled together to effect a substantially balanced combined shaft.