For this reason, the wind turbine cabin is usually installed with air-guiding-flow devices to enhance ventilation, and reduce the cabin temperature. The actual application shows this method is
The destruction that sea or coastal waters wind-driven generator tend to receive humid air causes or aggravates the corrosion of metal device.And the wave bump is pulverized the salt fog that
is added to the air and the air/fuel mixture is ignited, increasing the working fluid temperature significantly. The combustion products move downstream through a turbine, which extracts
The result is difficulty in maintaining a sufficient volume of air to the engine intake to produce power, as well as to allow enough air to the fuselage for pressurization. These are the limiting factors for determining the design ceiling
Obviously the power extracted from the airflow by the turbine has been given to the airflow by the engines in the first place: so the wind turbine wouldn''t work "for free" but it would anyhow consume power from the main
Hence, the airflow was linearly related to the crosswind speed. As shown in Fig. 14 (d), for the crosswind facing intake-3 of the power room, intake-3 also experiences an air
The reason is that the wind blade rotating speed is very low with small frequency. In the range of noises from 500 Hz to 1000 Hz, the blades noise occupy the main range in the
摘要 为研究风力发电机组机舱散热性能,对某型号传统的风力发电机组机舱及舱内主要热源部件 (发电机、齿轮箱、电控柜等)按照相似准则进行物理建模与有限元建模。. 首先分析在一定的外界
ABSTRACT. The computer simulation software is used to simulate the actual environment in the wind turbine cabin, the electromagnetic and thermal simulation model of the transformer is
ABSTRACT. The computer simulation software is used to simulate the actual environment in the wind turbine cabin, the electromagnetic and thermal simulation model of the transformer is established, and the reasonable simulation
The engine inlet of a turbine engine is designed to provide a relatively distortion-free flow of air, in the required quantity, to the inlet of the compressor. [Figure 1] Many engines use inlet guide vanes (IGV) to help straighten the airflow and direct it into the first stages of the compressor.
An example of a turbine engine inlet A gas turbine engine consumes considerable more airflow than a reciprocating engine. The air entrance passage is correspondingly larger. Furthermore, it is more critical in determining engine and aircraft performance, especially at high airspeeds.
The air inlet ducts on engines mounted in this fashion are identical to air inlet ducts on wing-mounted engines; the duct is relatively short and is mounted directly to the engine. [Figure 3] Figure 2 . A Lockheed L-1011 Tristar is designed with wing-mounted engines and an engine in the vertical stabilizer.
Proper inlet design contributes materially to aircraft performance by increasing the ratio of compressor discharge pressure to duct inlet pressure. This is also referred to as the compressor pressure ratio. This ratio is the outlet pressure divided by the inlet pressure. The amount of air passing through the engine is dependent upon three factors:
The inlet also contains some sound-reducing materials that absorb the fan noise and make the engine quieter. Turboprops and turboshafts can use an inlet screen to help filter out ice or debris from entering the engine. A deflector vane and a heated inlet lip are used to prevent ice or large chunks from entering the engine.
The inlet varies according to the type of turbine engine. Small turboprop and turboshaft engines have a lower airflow than large turbofan engines which require a completely different type of inlet. Many turboprop, auxiliary power units, and turboshaft engines use screens that cover the inlet to prevent foreign object damage (FOD).
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