TURBINE ENGINE SHROUD SEGMENT, HANGER AND ASSEMBLY

PROBLEM TO BE SOLVED: To provide a turbine engine shroud segment (10) including a surface exposed to high-temperature engine gas stream, a segment hanger and a shroud assembly. SOLUTION: A segment projecting portion (26) includes segment support surfaces (28, 30) spacedly arranged circumferentially....

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Bibliographische Detailangaben
Hauptverfasser:	BULMAN DAVID EDWARD, ALFORD MARY ELLEN
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OFGENERAL APPLICATION ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEAT EXCHANGE IN GENERAL HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES NON-POSITIVE DISPLACEMENT PUMPS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS STEAM ENGINES WEAPONS
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