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Nondestructive Test Manual 无损检测手册简介

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cular to the radius surface. If the crack direction is not known, move the
probe along and across the radius as shown in Detail XIII.
(e) Edges: When you do an inspection near the edge of a part, use a
nonconductive straightedge to keep the probe the same distance from the edge of the
part. See Detail X to see how to examine a part near the edge. See Detail XI to examine
the edge of a part.
(4). Make a mark at the locations that cause signals that are more than 20 percent
of the display above the balance point.
NOTE; To find the end of the crack, continue to move the probe across the crack
until there is no more crack signal.
(5). Frequently do a check of the instrument calibration as follows:
NOTE: Do not adjust the gain.
(a) Put the probe on the reference standard to get a signal from the notch.
(b) Compare the signal you got from the notch during calibration with the signal
you get now.
(c) If the signal has changed 10 percent or more, do the calibration and
inspection again.
六、检查结果Inspection Results
A. Fast upscale signals that are more than 50 percent of the signal height from
the reference notch are signs of defects.
B. Compare the signal that occurs during the inspection to the signal you got
from the notch in the reference standard.
NOTE: The signal from a crack can have less horizontal movement than the
signal from the notch in the reference standard. See Detail VIII.
(1) To find the end of a crack, continue to move the probe across the crack until
there is no more crack signal.
(2) To make an estimate of the depth of a crack that is less than 0.02 inch (0.5
mm) deep, compare the horizontal movement of the crack signal to the horizontal
movement of the reference standard notch.A reference standard with notches that are
less than 0.02 inch(0.5 mm) deep can also be used.
C. The conditions specified below can also cause defect signals:
(1).The probe is moved too close to an edge. Use a nonconductive straightedge
to keep the probe the same distance from the edge.
(2).A worn probe coil. Put a piece of tape on the surface of the probe coil or
get a new probe and calibrate the instrument again.
(3) Local changes in material conductivity. Compare the signal to the
signal from the reference standard. Signals from conductivity changes will be
slower than the signal from the reference standard.
D. Do one of the procedures that follow to make sure a signal is the result of
a defect.
(1)Remove the surface finish and do a visual inspection with 10-power (or
higher) magnification and sufficient light.
(2) Do a penetrant inspection of the area as specified in Standard Overhaul Practices
Manual, Subject 20-20-02, " Penetrant Inspection Methods".
二. A320 系列飞机无损检测手册简介
下面再介绍有关AIRBUS NTM 的使用

 


在NTM 中,按照各类方法进行了分类,也采用了按ATA 章节进行查询,
在AIRBUS NTM 中,各种无损检测方法的章节代码与BOEING NDTM 的表示略有差别,在
使用时应注意区分:
PART1 - GENERAL
PART2 - X-RAY
PART3 - GAMMA RAY
PART4 - ULTRASONIC
PART5 - RESONANCE FREQUENCY
PART6 - EDDY CURRENT
PART7 - MAGNETIC PARTICLE
PART8 - PENETRANT
PART9 - VISUAL
PART10 - THERMOGRAPHIC
在不同手册中使用的缩写有不同的含义,在使用时应注意区别。
与BOEING NTM 一样,在AIRBUS NTM 手册前言部分的介绍(Introduction)和有效飞
机清单(AIRPLANE ALLOCATION LIST),对使用者非常有用,通过查阅飞机的生产序号、型
号等信息,对在手册使用时不同的有效性有所帮助,如:
在涉及不同的发动机选型时,涉及对不同发动机适用的吊舱结构等应注意有效性选择:
在具体工作中,还应注意对选择方法对应的不同程序的应用:
在AIRBUS NTM 各个检查程序中与BOEING NTM 类似,均按照下列结构,对检测程序给出
了详细步骤指导工作者进行相应的检测工作:
1. 检查的结构和区域(COMPONENT OR AREA TO BE INSPECTED)
2. 可能存在的损伤(DESCRIPTION OF POSSIBLE DAMAGE)
3. 引用文件(RELATED DOCUMENTS)
4. 设备和器材(EQUIPMENT AND MATERIALS)
5. 检查准备(PREPARATION FOR INSPECTION)
6. 设备标定、校准(INSTRUMENT CALIBRATION)
7. 检查步骤(INSPECTION PROCEDURE)
8. 验收标准(ACCEPTANCE CRITERIA)
9. NDT 后处理(FINAL NDT REQUIREMENTS)
其它手册中涉及NDT 检测的内容

 



对发动机和机载附件的修理与检查时,除参考除参考主机厂的NDT 手册及SOPM 外,还应
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