• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-16 10:02来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

 (6)  The total vector sum of the trim balance weights and the weights installed for component (LPC) balance must not be more than the limits that follow:
 Fan Plane:  20 oz-inches (14,400 g.mm)
 NOTE:____ If it is necessary to add more correction weight, you must examine for incorrect assembly and part damage.
 (7)  Identify all the trim balance weights permanently with the letters "TB".
 NOTE:____ The balance weights installed on the fan hub during LPC balance are not identified wit the letters "TB".
 (8) (9)  This task gives the instructions for these subtasks: (a) Installation of engine equipment and external cables. (b) Listing of available fan plane counterweights. (c) Instruction of the installation of the counterweights. (d) Engine test requirements. (e) Supplemental PBS-4100 operation and setup information.Definitions: (a) Once Per Revolution N1 Speed Reference: Once every revolution a signal is received by the N1 speed transducer. The short tooth of the tachometer gear on the turbine shaft coupling makes the signal. (b) N1 Reference Mark: Ink mark on a fan blade or the hub which identifies the short tooth location.
 (c) (d)  1EL: The vibration of the low pressure rotor.Vibration Units: Vibration should be in mils (mm) and vibration velocity in inches per second (mm per second).
 1 mil = 0.001 inch (0.025 mm)

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 72-31-00
 ALL  ú ú N01 Page 522 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
(e)  Phase Angle Lag: If the low pressure rotor is not balanced, the vibration analyzer will give its angular location. The phase angle lag is the angle between the actual location of the unbalance and the location the analyzer shows.
 NOTE: This procedure uses phase measurement equipment that
____ measures from the N1 speed pulse to the vibration pulse (maximum). Measure positive angles, in this coordinate system, in the opposite direction from the direction in which the engine turns. Some phase measurement equipment, such as the MTI equipment, measure positive angles in the direction in which the engine turns (lead angle).
 (f)  
Phase Angle: The angle between the signal from the vibration transducer and the signal from the N1 speed reference. The speed reference is given once per revolution.

 (g)  
Sensitivity: The moment weight that causes 1.0 mil (0.025 mm) of vibration.

 (h)  
Once Per Revolution N1 Speed Reference: Once every revolution a signal is received by the N1 speed transducer. The short tooth of the tachometer gear on the turbine shaft coupling makes the signal. As an alternative procedure, use an optical tachometer for the once per revolution N1 speed reference.

 (i)  
N1 Reference Blade: Fan blade with an ink mark to identify the short tooth location.

 (j)  
Stable Vibration: A Stable Vibration is a vibration of which the vibration maximum does not change by more than one-fourth of the average vibration during 30 seconds of the engine operation.

 (k)  
Vibration Survey: To do a test and write the engine vibration data against the rotational speed during an engine acceleration or deceleration. This finds which engine speeds give the maximum vibration levels which are not permitted.

 (l)  
Trim Balance Survey: To do a test and write the vibration amplitude and phase angle data of the low rotor. The vibration amplitude is measured while the engine is stable at the peak vibration level. You can then calculate the correct weight.

 B.
Equipment

 (1)  
MTI 8900-6714 Engine Selector Switch Box,
 Mechanical Technology Inc.,
 968 Albany-Shaker Road,
 Latham, NY 12110


 (2)  
MTI 8115-6713 PBS Jumper Cable,
 Mechanical Technology


 (3)  
MTI 8900-5065 AVM Interface Cable, Mechanical Technology

 (4)  
MTI 7000-4133 Portable Balancing System - PBS-4100 ( This includes a Computer and Data Acquisition Unit (DAU), Mechanical Technology

 (5)  
PWA 85306 Puller - Pratt & Whitney

 (6)  
PWA 85307 Puller - Knocker, Pratt & Whitney


 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:747-400 AMM 飞机维护手册 发动机 ENGINE 1(124)