# US 8,540,479 B2 · Active retractable seal for turbo machinery and related method > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 8,540,479 B2 - Document ID: US8540479B2 - Status: Granted - Kind: B2 - Application number: 11/652,076 - Filed: 2007-01-11 - Published: 2008-07-17 - Granted: 2013-09-24 - Earliest claimed: 2007-01-11 - Assignees: General Electric Company - Applicants: Shorya Awtar; Timothy R. Kemp; Kurt N. Laurer; Frederick G. Baily - Inventors: Shorya Awtar; Timothy R. Kemp; Kurt N. Laurer; Frederick G. Baily - Web page: https://patentgrep.com/patent/US8540479B2 ## CPC - F01D 11/025: {Seal clearance control; Floating assembly; Adaptation means to differential thermal dilatations} - F01D 11/122: {with erodable or abradable material (blades having cutting or grinding tips F01D5/20)} - F01D 11/127: {with a deformable or crushable structure, e.g. honeycomb} - F01D 11/22: by mechanically actuating the stator or rotor components, e.g. moving shroud sections relative to the rotor - F05D 2240/56: Brush seals - F05D 2240/57: Leaf seals - F05D 2240/59: Lamellar seals - Y02T 50/60: Efficient propulsion technologies, e.g. for aircraft - F01D: NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES (machines or engines for liquids F03; non-positive displacement pumps F04D) - F05D: INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS - Y02T: CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION ## Abstract An active retractable seal assembly for use between rotating and non-rotating turbo machinery components including: a plurality of seal rings mounted to the non-rotating component, the seal rings movable toward and away from the rotating component between respective closed and open positions as a function of pressure drop across the seal rings, wherein the seal rings are normally in the open position; and a fluid bypass circuit for directing fluid around one or more of the plurality of seal rings to reduce the pressure drop across the one or more of the seal rings, thereby causing the one or more seal rings to move towards the open position under the action of spring(s) or actuator(s). ## Claims ### Claim 1 An active retractable seal assembly for use between rotating and non-rotating turbomachinery components comprising: at least one seal ring mounted to the non-rotating component, said at least one seal ring movable toward and away from the rotating component between respective closed and open positions as a function of pressure drop across the seal ring said at least one seal ring biased toward said open position by one or more actuators; a fluid bypass circuit for directing fluid around said at least one seal ring to reduce the pressure drop across the seal ring; wherein said fluid bypass circuit includes a conduit extending from an inlet at a location upstream of said at least one seal ring and terminating at an outlet location downstream of said at least one seal ring, and wherein a bypass control valve is located in said fluid bypass circuit, between said inlet and said outlet, said control valve enabling active control of pressure drop across the seal ring such that said at least one seal ring can be moved via said one or more actuators to said open position during operation and under any operating conditions of the turbomachinery. ### Claim 2 (depends on 1) The seal assembly of claim 1 wherein said bypass control valve is controlled manually. ### Claim 3 (depends on 1) The seal assembly of claim 1 wherein said bypass control valve is programmed for automatic operation. ### Claim 4 (depends on 1) The seal assembly of claim 1 wherein said rotating component comprises a rotor shaft. ### Claim 5 (depends on 1) The seal assembly of claim 1 wherein said stationary component comprises one of a shell, casing, packing head, diaphragm or shroud hanger. ### Claim 6 (depends on 1) The seal assembly of claim 1 wherein said one or more actuators comprises one or more springs. ### Claim 7 (depends on 1) The seal assembly of claim 1 wherein said at least one seal ring comprises at least two arcuate segments. ### Claim 8 (depends on 1) The seal assembly of claim 1 wherein said at least one seal ring comprises a plurality of seal rings and wherein said bypass circuit directs fluid around at least two of said plurality of seal rings. ### Claim 9 A retractable seal assembly for use between a turbine stator and a turbine rotor component of a turbine, the seal assembly comprising: a plurality of seal rings mounted to said turbine stator, each ring having at least two arcuate seal segments movable toward and away from said turbine rotor between respective closed and open positions as a function of pressure drop in a fluid flowing axially along said rotor; and a fluid bypass circuit for directing fluid around one or more of said plurality of seal rings to thereby reduce the pressure drop across said one or more of said seal rings; wherein said fluid bypass circuit includes a conduit extending from an inlet at a location upstream of said at least one seal ring and terminating at an outlet location downstream of said at least one seal ring, and wherein a bypass control valve is located in said fluid bypass circuit, between said inlet and said outlet, said control valve enabling active control of pressure drop across said at least one seal ring such that said at least one seal ring can be moved via said one or more actuators_to said open position during operation and under any operating condition of the turbomachinery. ### Claim 10 (depends on 9) The retractable seal assembly of claim 9 wherein said bypass control valve is controlled manually. ### Claim 11 (depends on 9) The retractable seal assembly of claim 9 wherein said bypass valve is programmed for automatic operation. ### Claim 12 (depends on 9) The retractable seal assembly of claim 9 wherein said seal segments are biased toward said open position by at least two springs associated with each segment.