GAS TURBINE VANE BODY WITH INSTRUMENTATION
An instrumented vane body (62) is provided that includes a suction side and pressure side outer walls (76, 80), an interior cavity (90), at least one supply conduit (100), a plurality of sensors (108), and a plurality of sensor ports (104). The suction and pressure side outer walls (76, 80) extend c...
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| creator | MARTIN, Thomas J KUCZEK, Andrzej E CROTEAU, Paul F |
| description | An instrumented vane body (62) is provided that includes a suction side and pressure side outer walls (76, 80), an interior cavity (90), at least one supply conduit (100), a plurality of sensors (108), and a plurality of sensor ports (104). The suction and pressure side outer walls (76, 80) extend chordwise between leading and trailing edges (64, 66) and between inner and outer radial ends (68, 70). The supply conduit (100) is in fluid communication with the interior cavity (90), and is in communication with the interior cavity (90) through at least one of the inner or outer radial ends (68, 70). The sensor ports (104) are disposed in the leading edge (64) and each is configured to receive a sensor (108), and are spaced apart from one another. Each sensor port (104) is in fluid communication with at least one vent aperture (92), and each is configured to permit core gas to enter that sensor part and exit the vane body (62) through the at least one vent aperture (92). |
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The suction and pressure side outer walls (76, 80) extend chordwise between leading and trailing edges (64, 66) and between inner and outer radial ends (68, 70). The supply conduit (100) is in fluid communication with the interior cavity (90), and is in communication with the interior cavity (90) through at least one of the inner or outer radial ends (68, 70). The sensor ports (104) are disposed in the leading edge (64) and each is configured to receive a sensor (108), and are spaced apart from one another. 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The suction and pressure side outer walls (76, 80) extend chordwise between leading and trailing edges (64, 66) and between inner and outer radial ends (68, 70). The supply conduit (100) is in fluid communication with the interior cavity (90), and is in communication with the interior cavity (90) through at least one of the inner or outer radial ends (68, 70). The sensor ports (104) are disposed in the leading edge (64) and each is configured to receive a sensor (108), and are spaced apart from one another. 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The suction and pressure side outer walls (76, 80) extend chordwise between leading and trailing edges (64, 66) and between inner and outer radial ends (68, 70). The supply conduit (100) is in fluid communication with the interior cavity (90), and is in communication with the interior cavity (90) through at least one of the inner or outer radial ends (68, 70). The sensor ports (104) are disposed in the leading edge (64) and each is configured to receive a sensor (108), and are spaced apart from one another. Each sensor port (104) is in fluid communication with at least one vent aperture (92), and each is configured to permit core gas to enter that sensor part and exit the vane body (62) through the at least one vent aperture (92).</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre ; ger |
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| subjects | BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MEASURING MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PHYSICS STEAM ENGINES TESTING TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR WEAPONS |
| title | GAS TURBINE VANE BODY WITH INSTRUMENTATION |
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