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DEVICE FOR STABILIZING THE ENGINE INJECTION FLOW IN ENGINE STANDS AND / OR FOR REDUCING FLOW SAVINGS AND PRESSURE FLUCTURES IN ENGINE ENTRY IN STATIONS, DEVICE FOR SUPPORTING STATIONS FOR AIRCRAFT GEARWAYS, AND USE OF A DEVICE
DEVICE FOR STABILIZING THE ENGINE INJECTION FLOW IN ENGINE STANDS AND / OR FOR REDUCING FLOW SAVINGS AND PRESSURE FLUCTURES IN ENGINE ENTRY IN STATIONS, DEVICE FOR SUPPORTING STATIONS FOR AIRCRAFT GEARWAYS, AND USE OF A DEVICE
The invention relates to a device for stabilizing the engine inlet flow in static tests of engines and/or for reducing stall and pressure fluctuations in the engine inlet in static tests, wherein the device can comprise a lower half surrounding part for the engine and wherein the device can comprise an upper half surrounding part for the engine. The upper half surrounding piece can also be composed of partially surrounding parts, for example segments.
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