Apparatus for measuring the temperature of a gas flow traversing

Measuring and testing – Gas analysis – Moisture content or vapor pressure

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G01K 1100

Patent

active

042791537

ABSTRACT:
Apparatus is disclosed which is intended to measure the temperature of a flow traversing a blade grid, for example the valve blades of a turbojet turbine. This apparatus comprises a temperature sounder lodged within a gas escape circuit provided in a blade. In-flight monitoring of the gas temperature in an aircraft turbojet is possible with the present invention.

REFERENCES:
patent: 3098387 (1963-07-01), Corbett

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