圖17-3一個典型的壓氣機進口噴水系統
an increase in the maximum rotational speed of the engine, thus providing further additional thrust, Where methanol is used with the water, the turbine inlet temperature is restored, or partially restored, by the burning of the methanol in the combustion chamber.
COMPRESSOR INLET INJECTION
5. The compressor inlet injection system shown in fig. 17-3 is a typical system for a turbo-propeller engine. When the injection system is switched on, water/methanol mixture is pumped from an aircraft-mounted tank to a control unit. The control unit meters the flow of mixture to the compressor inlet through a metering valve that is operated by a servo piston. The servo system uses engine oil as an operating medium, and a servo valve regulates the
6.控制裝置的高壓滑油開關控制桿與油門控制系統以這樣一種方式相互連接:油門移向起飛位置前,滑油開關是關閉的,是一節流活門也是關閉的,這就防止混合液流入壓氣機進口。當油門移動到起飛位置時,才打開滑油開關,滑油壓力通過伺服活門后借助伺服活塞將節流活門打開。
微動電門
水噴嘴
低壓水
高壓水
冷卻水
高壓空氣
滑油
燃油噴嘴
系統排放活門
節流活塞
排放活門
渦輪泵
排氣限制器
軸承冷卻水流
到燃油流量調節器
單向和水傳感活門
來自水箱
排放
通氣
單向活門
滑油箱
空氣冷卻水流量
空氣進口限制器
排放活門
高壓壓氣機空氣
水流量傳感裝置
水切斷活門
Water injection
圖17-4 一個典型的燃燒室噴水系統
Fig. 17-4 A typical combustion chamber injection system.
supply of oil. The degree of servo valve opening is set by a control system that is sensitive to propeller shaft torque oil pressure and to atmospheric air pressure acting on a capsule assembly.
6. The control unit high pressure oil cock control lever is interconnected to the throttle control system in such a manner that, until the throttle is moved towards the take-off position, the oil cock remains closed, and thus the metering valve remains closed, preventing any mixture flowing to the compressor
inlet Movement of the throttle control to the take-off position opens the oil cock, and the oil pressure passes through the servo valve to open the metering valve by means of the servo piston.
COMBUSTION CHAMBER INJECTION
7. The combustion chamber injection system shown in fig. 17-4 is a typical system for a turbo-jet engine. The coolant flows from an aircraft-mounted tank to an air-driven turbine pump that delivers it to a water flow sensing unit. The water passes from the
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sensing unit to each fuel spray nozzle and is sprayed from two jets onto the flame tube swirl vanes, thus cooling the air passing into the combustion zone. The water pressure between the sensing unit and the discharge jets is sensed by the fuel control system, which automatically resets the engine speed governor to give a higher maximum engine speed.
8. The water flow sensing unit opens only when the correct pressure difference is obtained between 8.水流傳感裝置只在壓氣機出口空氣壓力和水壓之間獲得正常的壓差時才打開。當發動機油門桿移動到起飛位置時,該系統才進入工作狀態,使微動開關工作并為渦輪泵選擇供氣量。
9.傳感裝置也作為一個單向活門,用以防止空氣壓力從噴水孔反饋回來,并在水流動時,用指示燈亮來顯示它。
燃燒室噴水
7.圖17-4所示的燃燒室噴水系統是一個用于渦輪噴氣發動機典型的系統。冷卻劑從安裝在飛機的水箱流入空氣驅動的渦輪泵中,渦輪泵再把冷卻劑送到水流傳感器裝置。氺通過傳感裝置,流到每個燃油噴嘴并從每個噴嘴上的兩個噴水孔噴射到火焰筒漩渦葉片上,這樣便冷卻進入到燃燒區域的空氣。在傳感裝置與噴水孔之間由燃燒控制統感測。它自動調整發動機轉速調節器,產生出一個更高的最大發動機轉速。
Water injection
compressor delivery air pressure and water pressure. The system is brought into operation when the engine throttle lever is moved to the take-off position, causing microswitches to operate and select the air supply for the turbine pump.
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