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This standard, designated ASTM D2155-18 (Reapproved 2024), establishes a definitive procedure for assessing the fire resistance of hydraulic fluids used in aircraft applications. The core objective is the determination of the autoignition temperature (AIT) of the hydraulic fluid in air at one atmosphere pressure. This laboratory method quantifies the specific temperature at which a fluid will spontaneously ignite in the absence of an external ignition source, a critical safety parameter for fluids operating near hot engine or brake components.
| 🟦 Parameter | 📏 Specification | 🎯 Requirement |
|---|---|---|
| Test Vessel | 200 mL Erlenmeyer Flask | Borosilicate Glass |
| Injection Device | Hypodermic Syringe | Precise metered sample volume |
| Test Atmosphere | Air | 1 atm pressure |
| Observation Room | Darkened | Ensure clear flame visibility |
| Observation Period | 5 minutes | Post sample injection |
| Ignition Evidence | Sudden appearance of a flame | Inside the flask |
| Reported Result | Autoignition Temperature (AIT) | Lowest flask temperature for ignition |
The specific apparatus of a 200 mL borosilicate glass Erlenmeyer flask is not arbitrary. The standard emphasizes that the volume of the vessel is particularly important, as lower autoignition temperatures are achieved in larger vessels. The vessel material (borosilicate glass) is also an important controlled factor that directly influences the measured result. The test is conducted in a darkened room to allow the operator to clearly observe the sudden appearance of a flame inside the flask, which is the definitive indicator of autoignition.
During the test, a small metered sample is injected using a hypodermic syringe. The operator must observe the flask for a full 5 minutes following injection before a negative result can be recorded for that specific temperature and sample volume combination. The “ignition time lag” (the time in seconds between sample insertion and the appearance of flame) is a critical observation for documenting the kinetic behavior of the oxidation reaction.
Autoignition is formally defined as the ignition of a material commonly in air resulting from heat liberation due to the exothermic oxidation reaction, occurring specifically in the absence of an external ignition source such as a spark or flame (Section 2.1.1). The autoignition temperature is therefore the minimum temperature at which this occurs under the specified conditions of this test method (Section 2.1.2).
It is crucial to recognize that this test method is not designed for evaluating materials which are capable of exothermic decomposition (Section 4.3). Furthermore, the temperatures determined by this method are those at which air oxidation leads to ignition and can be expected to vary with test pressure and oxygen concentration. All reported values must comply with the standard, where inch-pound units are the primary standard of measurement.
| 📚 Terminology | 📖 Definition per ASTM D2155 |
|---|---|
| Autoignition | Ignition in air due to heat from the exothermic oxidation reaction, without an external ignition source (spark or flame). |
| Autoignition Temperature | The minimum temperature at which autoignition occurs under the specified conditions of the test. |
| Ignition | The initiation of combustion. |
| Ignition Time Lag | The time lapse between the application of heat (specifically sample insertion) and the ignition of the material, measured in seconds. |
It measures the Autoignition Temperature (AIT) of an aircraft hydraulic fluid. This is the minimum temperature at which the fluid will spontaneously ignite in air at one atmosphere pressure without an external ignition source, specifically using a 200 mL borosilicate glass flask and hypodermic syringe injection methodology.
Autoignition is definitively identified by the sudden appearance of a flame inside the heated Erlenmeyer flask. The test is conducted in a darkened room to maximize the visibility of this ignition event. The observer must watch the flask for up to 5 minutes following the injection of the sample.
The vessel volume and material are critical controlled variables. The standard explicitly states that the volume of the vessel is particularly important because lower autoignition temperatures are generally achieved in larger vessels. The specific material (borosilicate glass) is also a critical factor to ensure repeatability and reproducibility across different testing laboratories.
No. This test method is specifically designed for assessing the fire resistance of aircraft hydraulic fluids. Furthermore, Section 4.3 explicitly states that this test method is not designed for evaluating materials that are capable of exothermic decomposition, as the standard test conditions and interpretations do not apply to such materials.