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File:NDT test of an V2500 engine blade route.jpg

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Description
English: NDT, Ultrasonic Testing (UT) on blade roots of a V2500 IAE aircraft engine. Step 1: The UT probe is placed on the root of the blades to be inspected with the help of a special aircraft tool (video probe). Step 2: Instrument settings are input. Step 3: The probe is scanned over the blade root. In this case, an indication (peak in the data) through the red line (or gate) indicates a good blade; an indication to the left of that range indicates a crack.
Türkçe: V2500 IAE uçak motorunun pal köklerinin NDT İncelemesi (Ultrasonik). 1. Adım: Özel bir boroskop aracı vasıtasıyla NDT probunu incelemenin yapılacağı pal köküne yerleştir. 2. Adım: NDT Cihazını doğru dalga değerine ayarla. 3.Adım: Probu incelemenin yapılacağı noktaya ayarla ve en yüksek inceleme dalgasının kırmızı çizgi ile belirlenmiş normal değerler içinde kaldığını gözlemle. Eğer kalıyorsa, pal sağlamdır, kırmızı çizginin dışında ve sol tarafında ise pal kökünde çatlak var demektir.
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Author Plenumchamber

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26 June 2007

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current10:43, 26 June 2007Thumbnail for version as of 10:43, 26 June 20072,400 × 600 (648 KB)Plenumchamber~commonswiki{{Information |Description= NDT test of blade rouths of V2500 IAE Aircraft Engine. ''Step 1'': Place the special NDT probe on the routh of the blades to be inspected by the help of a special boroscope tool. ''Step2'': Set the NDT Tool for the

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