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时间:2010-05-30 14:30来源:蓝天飞行翻译 作者:admin
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L.V.D.T. signal to the motor is cancelled and the system stabilizes at the new setting.
17. The electronic E.P.R. system utilizes two vibrating cylinder pressure transducers which sense the engine air pressures and vibrate at frequencies relative to these pressures. From these vibration frequencies electrical signals of E.P.R. are computed and are supplied to the E.P.R. gauge and electronic engine control system (Part 10).
Engine torque
18.
Engine torque is used to indicate the power that is developed by a turbo-propeller engine, and the indicator is known as a torquemeter. The engine torque or turning moment is proportional to the horse-power and is transmitted through the propeller reduction gear.

19.
A torquemeter system is shown in fig. 12-4. In this system, the axial thrust produced by the helical gears is opposed by oil pressure acting on a number of pistons; the pressure required to resist the axial thrust is transmitted to the indicator.

20.
In addition to providing an indication of engine power; the torquemeter system may also be used to automatically operate the propeller feathering system if the torquemeter oil pressure falls due to a power failure. It is also used, on some installations, to assist in the automatic operation of the water injection system to restore or boost the take-off power at high ambient temperatures or at high altitude airports (Part 17).


Engine speed
21. All engines have their rotational speed (r.p.m.) indicated. On a twin or triple-spool engine, the high pressure assembly speed is always indicated; in most instances, additional indicators show the speed of the low pressure and intermediate pressure assemblies.

22. Engine speed indication is electrically transmitted from a small generator, driven by the engine, to an indicator that shows the actual revolutions per minute (r.p.m.), or a percentage of the maximum engine speed (fig. 12-5). The engine speed is often used to assess engine thrust, but it
图12-5 发动机转速指示器及发电机
26.除了提供转子转速的指示之外,转速探头中感应的电流可以用来电亮仪表板上的警告灯,向驾驶员指示转子组件正在转动。这在发动机起动时特别重要,因为它通知驾驶员何时打开燃油开关,来向发动机供油。该灯与起动电路相连,因而仅仅在起动过程中才亮。
25.转速探头位于压气机机匣上,与音轮对齐。音轮是压气机轴上经机械加工的部分。每转一圈音轮外圆上的齿通过探头一次,通过改变探头中线圈的磁通量而诱导出一股电流。电流的大小由磁通量的变化率控制,因而与发动机转速直接相关。
23.发动机转速发电机供应三相交流电,其频率取决于发动机转速。发电机的输出频率控制指示器中的同步马达的转速,位于鼓筒或阻力杯中的磁铁组件的旋转导致鼓筒的运动,进而转动指示器的指针。
 
24.在没有其它设备来驱动发电机的场合,可以采用可变磁阻式转速探头,它与一个音轮相接,产生感应电流,经放大后送入指示器(图12-6)。本方法可以用于提供发动机的转速指示,而不需有单独驱动的发电机以及其相应的传动机构,因而减少了发动机的部件和运动零件的数量。
涡轮燃气温度
 
27.始终要指示排气温度,以保证在任一特定的工作状态下,能够检查涡轮组件的温度。而且,通常还备有一个自动燃气温度控制系统,保证最大燃气温度不致被超过(第10章)。
Controls and instrumentation


28.涡轮燃气温度(T.G.T.)有时用排气燃气温度(E.G.T.)或喷管温度(J.P.T)来表示。它是发动机工作中的关键参数,因而提供该温度的指示极为重要。按照理想,应当测定涡轮进口温度(T.E.T.)。但是涉及到高温,这是不现实的。但是涡轮中的温度降是按已知的方式变化的,所以涡轮出口温度通常由适当安排的热电偶测量。作为代替方式,也可以测量涡轮组件中间级的温度,如图12-7所示。

29.用于将温度信号传到指示器的热电偶探头由两种不同的金属丝构成,在一个金属套管内部连接在一起。套管上的一些传导孔允许排气流流过接点。用于制造热电偶丝的材料通常是镍铬和镍铝合金。

30.这些探头在燃气流中的配置要保证能获得良好的平均温度读数,通常将探头连在一起构成一个并联电路。在电路(图12-8)上连接一个指示器,它基本上是一个毫伏计,其读数按摄氏度作了标定。

Fig. 12-6  Variable-reluctance speed probe图12-6 可变磁阻式转速探头和音轮
and phonic wheel.
does not give an absolute indication of the thrust being produced because inlet temperature and pressure conditions affect the thrust at a given engine speed.
23.
The engine speed generator supplies a three-phase alternating current, the frequency of which is dependent upon engine speed. The generator output frequency controls the speed of a synchronous motor in the indicator, and rotation of a magnet assembly housed in a drum or drag cup induces movement of the drum and consequent movement of the indicator pointer,

24.
Where there is no provision for driving a generator, a variable-reluctance speed probe, in conjunction with a phonic wheel, may be used to induce an electric current that is amplified and then transmitted to an indicator (fig. 12-6). This method can be used to provide an indication of r.p.m. without the need for a separately driven generator, with its associated drives, thus reducing the number of components and moving parts in the engine.

25.
 
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