Burner pressure transducer

A sensor for measuring gas pressure in a gas turbine engine. The sensor is positioned to receive pressurized gas and measure the pressure. A thermally insulating material mounts the sensor spaced from conductive portions of the engine. A heater is mounted on a plurality of sides of the sensor to pro...

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Bibliographic Details
Main Author LEBRON JOSE M
Format Patent
LanguageEnglish
Published 09.04.2013
Subjects
BLASTING
ENGINE PLANTS IN GENERAL
HEATING
INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS
INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04
LIGHTING
MACHINES OR ENGINES IN GENERAL
MEASURING
MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER,MECHANICAL EFFICIENCY, OR FLUID PRESSURE
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
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Summary:A sensor for measuring gas pressure in a gas turbine engine. The sensor is positioned to receive pressurized gas and measure the pressure. A thermally insulating material mounts the sensor spaced from conductive portions of the engine. A heater is mounted on a plurality of sides of the sensor to provide heat thereto. A thermal blanket covers the heater to prevent loss of sensor heat.
Bibliography:Application Number: US201213353517