VEINE INSTRUMENTEE DE TURBOMACHINE

An annular air flow passage, particularly for a turbine engine, comprising two radially internal and external annular walls. A measuring element is elongated in a direction between the internal and external annular walls, and a first of the internal or external ends of the element is fixed rigidly t...

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Hauptverfasser:	LEROUX, ANDRE, PIERRE, JEAN, XAVIER, BADER, VALENTINE, LUCETTE, ROUSSELIN, STEPHANE, GIORDAN, JEREMY
Format:	Patent
Sprache:	fre
Schlagworte:	MEASURING PHYSICS TESTING TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR
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creator	LEROUX, ANDRE, PIERRE, JEAN, XAVIER BADER, VALENTINE, LUCETTE ROUSSELIN, STEPHANE GIORDAN, JEREMY
description	An annular air flow passage, particularly for a turbine engine, comprising two radially internal and external annular walls. A measuring element is elongated in a direction between the internal and external annular walls, and a first of the internal or external ends of the element is fixed rigidly to a first of the internal or external walls. The element includes at least one tubular cavity extending along the element and supplied with pressurized fluid.
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subjects	MEASURING PHYSICS TESTING TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR
title	VEINE INSTRUMENTEE DE TURBOMACHINE
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