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قديم 06-11-2009, 06:50 AM  
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الصورة الرمزية Tarig Elsheikh
Tarig Elsheikh Tarig Elsheikh غير متواجد حالياً
A 320 Technician
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تاريخ التسجيل: 25 - 01 - 2008
المشاركات: 791
شكر غيره: 4
تم شكره 28 مرة في 24 مشاركة
معدل تقييم المستوى: 2172
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مشاهدة أوسمتي

Tarig Elsheikh Tarig Elsheikh غير متواجد حالياً
A 320 Technician
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الصورة الرمزية Tarig Elsheikh

مشاهدة ملفه الشخصي
تاريخ التسجيل: 25 - 01 - 2008
المشاركات: 791
شكر غيره: 4
تم شكره 28 مرة في 24 مشاركة
معدل تقييم المستوى: 2172
Tarig Elsheikh يستحق الثقة والتقديرTarig Elsheikh يستحق الثقة والتقديرTarig Elsheikh يستحق الثقة والتقديرTarig Elsheikh يستحق الثقة والتقديرTarig Elsheikh يستحق الثقة والتقديرTarig Elsheikh يستحق الثقة والتقديرTarig Elsheikh يستحق الثقة والتقديرTarig Elsheikh يستحق الثقة والتقديرTarig Elsheikh يستحق الثقة والتقديرTarig Elsheikh يستحق الثقة والتقديرTarig Elsheikh يستحق الثقة والتقدير
افتراضي رد: ما معنى compressor stall ؟؟

This characteristic has been called both " Surge " and " Stall " in the past , but is more properly called SURGE when it is response of the entire engine. The word stall applies to the action occuring at each individual compressor blade. Compressor surge , also called Compressor stall , is a phenomenon which is difficult to understand because it is usually caused by complex combination of factors . The basic cause of compressor surge is fairly simple , each blade in an axial flow compressor is a miniature airplane wing which , when subjected to a higher angle of attack , will stall just as an airplane stalls. Surge may define as results from an unstable air condition within the compressor. Pilot or engine operator has no instrument to tell him that one or more blades are stalling. He must wait until the engine surges to know that. The unstable condition of air is often caused from air piling up in the rear stages of the compressor. Surge may become sufficiently pronounce to cause lound bangs and engine vibration. In most case , this condition is of short duration , and will either correct itself or can be corrected by retarding the throttle or power lever to Idle and advanncing it again , slowly. Among other things , to minimize the tendency of a compressor to surge , the compressor can be "unload" during certain operating conditions by reducing the pressure ratio across the compressor for any giving airflow. One method of doing this is by bleeding air from the middle or toward the rear of the compressor. In dual axial compressor engines , air is often bled from between the low and the high pressure compressor. Air bleed ports are located in the compressor section. These ports are fitted with automatic , overboard bleed valves which usually operate in a specified range of engine RPM. Some large engine have been provided with variable-angle stators ( variable stators) in a few of the forward compressor stages. The angle of these vanes change automatically to prevent the choking of the downstream compressor stages as engine operating conditions vary.
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