Method for constructing a standard environment of oxygen concentration in an aircraft fuel tank

By constructing the external, internal, and fuel gas environments of the aircraft fuel tank and using a standard gas replacement method to create a standard oxygen concentration environment, the problem of calibrating oxygen concentration testing equipment in the flight environment was solved, thus achieving the reliability and accuracy of the equipment and meeting the requirements for flight test evaluation of the aircraft fuel system.

CN115924116BActive Publication Date: 2026-06-09CHINESE FLIGHT TEST ESTAB

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
CHINESE FLIGHT TEST ESTAB
Filing Date
2022-12-14
Publication Date
2026-06-09

AI Technical Summary

Technical Problem

Existing oxygen concentration testing equipment is mainly used in the biological and petroleum fields, and lacks the conditions for calibration in flight environments, making it difficult to guarantee the reliability and accuracy of aircraft fuel tank oxygen concentration testing equipment.

Method used

The external, internal, and fuel gas environments of the aircraft fuel tank were constructed. A standard oxygen concentration standard environment was formed using a standard gas replacement method. The temperature, pressure, and fuel gas state of the fuel tank under flight conditions were simulated, and the oxygen concentration testing equipment was calibrated.

Benefits of technology

It enables the calibration of oxygen concentration testing equipment in flight environments, ensuring the reliability and accuracy of the testing equipment under complex conditions and meeting the needs of flight test evaluation of aircraft fuel systems.

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Abstract

The application discloses a method for constructing a standard oxygen concentration environment in an aircraft fuel tank, and comprises the following steps: step 1, constructing an external environment of the aircraft fuel tank, wherein the aircraft fuel tank is a fuel tank simulated through experiments; step 2, constructing an internal environment of the aircraft fuel tank; step 3, constructing an oil and gas environment of the fuel tank; and step 4, constructing a standard oxygen concentration environment of the fuel tank. The technical scheme of the embodiment of the application solves the problem that calibration conditions are lacked for an aircraft fuel tank oxygen concentration testing device.
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