Chapter 264 (1/2)

Two months passed in the twinkling of an eye in Wang Bin's busy life. At this time, it is golden autumn and September. In this month, Wang Bin and their Tiangong technology, in addition to the large bypass fan engine that has been successfully developed in the test run.

Wang Bin's Tiangong technology has developed another engine, and like the previous fan engine, the engine developed this time is also a fan engine.

And the channel of this fan engine is larger than that of the engine they have developed before.

Of course, a more natural fan means that the greater the thrust ratio of the engine, the greater the fuel consumption. However, since this engine is the same as the previous engine, it is also an engine with large bypass ratio. Naturally, it is impossible for the aircraft to fly at supersonic speed. After all, the turbofan engine with large bypass ratio cannot fly at supersonic speed.

However, as a civil aviation engine, I don't want to have the ability to fly at supersonic speed.

In addition, during this period of time, Wang Bin's rocket engine R & D Laboratory of Tiangong technology has finally completed the construction and even the installation of various internal equipment with the efforts of the military engineering forces day and night.

At the same time, at this time, the rocket launch pad of Tiangong technology has been almost built. According to Wang Bin's estimation, the military engineering force can complete the construction of the launch pad in half a month.

Of course, in addition to these achievements in construction, Wang Bin's company has also made achievements in many other aspects. For example, the tg-s1 aeroengine, that is, the turbofan, which has already started full-life test run, has accumulated 6000 hours of test run at this time, This can be similar to the service life of the tg001 engine that Wang Bin and his team have successfully developed before.

However, according to their prediction, the service life of this engine will far exceed that of the turbojet engine they developed before, at least more than double that of the tg001 engine, that is, the first overhaul time will be at least 10000 hours.

If you add three renovations until scrapping, the whole life of this engine will be at least 40000 or 50000 hours, which means that it is definitely far enough for a civil aviation engine.

The tg-s2 turbofan engine, which has just been developed, adopts more advanced technology and better bearings at the time of design. Therefore, according to the data, the service life of this engine will be longer than that of the previous S1 model. According to the data, it can be delivered for at least 15000 hours.

In addition, in terms of turbojet engine, after continuous improvement in the past two months, the performance of tg001 engine has also been qualitatively improved. First, as an engine, it is naturally in terms of thrust.

The maximum non afterburner thrust of the improved engine has reached 16.5 tons, and the maximum afterburner thrust has reached 20 tons up and down. The tail nozzle of the engine can also achieve the vector disguised function.

Finally, there is the problem of fuel consumption and engine life. In terms of fuel consumption, although after improvement, the fuel consumption of the engine when starting the maximum thrust has increased, the fuel consumption of the engine in cruise state is not so large, but less than before.