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Blade off testing or blade out testing is a specific form of air safety testing required by the Federal Aviation Administration and other safety agencies to certify safety performance of jet engines. The tests require engine manufacturers to carry out at least two tests of the engine, to make sure that the engine can survive a compressor or fan blade…
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blade engine turbine containment engines rotor aircraft compressor testing failure safety 33 test requirements aviation blade-out blades required united states
| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| Blade off testing | Purpose | Ensures that failure of rotating fan and compressor blades in turbine engines does not cause consequential failures in critical aircraft systems | 1.00 | infobox |
| Blade off testing | Year started | 1964 (1964) | 1.00 | infobox |
| aramid fiber | instance of | the soft wall generally uses a resilient outer containment layer made from a composite material | 0.80 | text |
| which requires a larger space to allow the composite layer to expand slightly | instance of | the soft wall generally uses a resilient outer containment layer made from a composite material | 0.80 | text |
| Blade off testing | related to Europe | The | 0.60 | section |
| Blade off testing | related to Europe | Compressor | 0.60 | section |
| Blade off testing | related to Europe | Turbine Blade Failure | 0.60 | section |
| Blade off testing | related to Europe | Subpart | 0.60 | section |
| Blade off testing | related to Europe | Section | 0.60 | section |
| Blade off testing | related to Europe | Joint Aviation Requirements | 0.60 | section |
| Blade off testing | related to Europe | Engines | 0.60 | section |
| Blade off testing | related to Europe | JAR-E | 0.60 | section |
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