Passive clearance control system for gas turbomachine

A turbomachine system comprising:

• a compressor portion;
• a turbine portion operatively connected to the compressor portion, the turbine portion including a turbine casing, a plurality of stators fixedly mounted to the turbine casing, and a plurality of rotating airfoils rotatably supported in the turbine casing;
• an intake system fluidically coupled to the compressor portion, the intake system being operative to condition a flow of intake air to the compressor portion;
• an exhaust system fluidically connected to the turbine portion, the exhaust system being operative to condition a flow of exhaust gases passing from the turbine portion;
• a load operatively connected to one of the turbine portion and the compressor portion;
• a combustor assembly including at least one combustor fluidically connecting the compressor portion and the turbine portion, wherein the compressor portion, turbine portion, and combustor assembly are enclosed within a shell of the turbomachine;
• a compressor discharge cavity arranged in the compressor portion within the shell of the turbomachine for directing a fluid having a fluid parameter indicative of a desired operational mode of the turbomachine from the compressor portion to the turbine portion;
• a passive clearance control system operatively arranged in the turbomachine system, the passive clearance control system including at least one passive flow modulating device mounted in the compressor discharge cavity within the shell of the turbine and being responsive to the fluid parameter, and at least one cooling channel extending from the compressor discharge cavity through the turbine casing, the at least one passive flow modulating device selectively passing the fluid from the compressor discharge cavity through the at least one cooling channel to adjust a clearance between the plurality of stators and the plurality of rotating airfoils;
• wherein the fluid parameter comprises a temperature or a pressure of the fluid in the compressor discharge cavity the at least one passive flow modulating device comprises at least one first passive flow modulating device and at least one second passive flow modulating device, the at least one first passive flow modulating device including one of a temperature actuated valve and a pressure actuated valve, the at least one second passive flow modulating device including the other one of the temperature actuated valve and the pressure actuated valve.

A method of adjusting rotor blade-to-stator clearance in a turbomachine comprising:

• exposing at least one flow modulating device to a fluid parameter of a fluid in an internal sensing cavity of the turbomachine, the fluid parameter indicative of a desired operating mode of the turbomachine, wherein the sensing cavity comprises a compressor discharge cavity disposed within a shell of the turbomachine;
• and
• the at least one flow modulating device actuating in response to the fluid parameter at least one passive flow modulating device in response to the fluid parameter;
• and
• passing the fluid from the sensing cavity to one or more cooling channels extending through a casing of a turbine portion to passively adjust rotor blade-to-stator clearance in turbine portion;
• wherein the fluid parameter comprises a temperature or a pressure of the fluid in the compressor discharge cavity within the shell of the turbomachine, and wherein the at least one passive flow modulating device is mounted in the sensing cavity within the shell of the turbomachine and comprises at least one first passive flow modulating device and at least one second passive flow modulating device, the at least one first passive flow modulating device including one of a temperature actuated valve and a pressure actuated valve, the at least one second passive flow modulating device including the other one of the temperature actuated valve and the pressure actuated valve.