Patent References 1678065 1678066 1734216 2402841 3029064 Thermal actuated valve for clearance control Clearance control for gas turbine engine Seal clearance control system for a gas turbine Compressor structure adapted for active clearance control Method and replacement member for repairing a gas turbine engine vane assembly InventorsAssigneeApplicationNo. 631512 filed on 12/21/1990US Classes:415/116, WITH DIVERSELY ORIENTED INLET OR ADDITIONAL INLET FOR DIVERSE FLUID (E.G., HEATING, COOLING OR MIXED WORKING FLUID, ETC.)415/173.2, Selectively adjustable415/178Working fluid on at least one side of heat exchange wallExaminersPrimary: Look, Edward K.Assistant: Verdier, Christopher Attorney, Agent or FirmForeign Patent References
International ClassF01D 009/00AbstractImproved operation can be achieved from an enhanced gas turbine engine having a segmented annular shroud which radially expands and contracts to match the expansion and contraction of engine rotor blades. The segmented annular shroud is supported by a structure which includes an annular ring having two radially outwardly extending flanges, and forward and aft annular segmented brackets which attach the segmented shroud to the forward and aft side of the ring respectively. In a preferred embodiment of the invention, two circumferentially extending separate and distinct air impingement manifolds surrounds each of the outwardly extending flanges. Each manifold is provided with a valve for controlling the amount and temperature of the airflow entering each manifold. The air from each manifold then impinges upon each of the outwardly extending flanges, thereby controlling the radial movement of the corresponding shroud segments and the associated clearances with the rotor blade tips. The use of separate and distinct manifolds and the corresponding values which regulate the amount and temperature of airflow to each manifold allows individual shroud portions to be separately expanded or contracted.Field of SearchWITH PASSAGE IN BLADE, VANE, SHAFT OR ROTARY DISTRIBUTOR COMMUNICATING WITH WORKING FLUIDWITH DIVERSELY ORIENTED INLET OR ADDITIONAL INLET FOR DIVERSE FLUID (E.G., HEATING, COOLING OR MIXED WORKING FLUID, ETC.) Between blade edge and static part Selectively adjustable INCLUDING HEAT INSULATION OR EXCHANGE MEANS (E.G., FINS, LAGGING, ETC.) Working fluid on at least one side of heat exchange wall | |