What is the Liu Ding shedding of J- 10?

In the photo, the screws unscrewed in the screw holes are quick-release screws, not rivets, but also protrude around the fuselage patch, which can be opened. For the convenience of maintenance, the J 10 aircraft has been designed and manufactured in a modular way for a long time. If you pay attention to the photos, you will find many patches near or around the engine. Regardless of the United States and Russia, any aircraft, including the expanded Su 35 and F22, have the same maintenance and inspection of engines.

1. These are all graphs of J 10.

2. Those "nails" are J 10 electrostatic discharge brushes, which are used to prevent static electricity (lightning can't be prevented), lead out charges, and prevent aircraft failures caused by charge accumulation and cloud discharge.

The fuselage of 3.3. F22/F35 has a skin, so no rivets can be seen. At present, laser welding technology is still immature. It seems that it is only used on Airbus 380 and top-class RVs (such as Audi A8 and A8), and F22 is only partially used.

4. It can be clearly seen from this picture that the so-called stick (stiffener) of J 10 is actually a spoiler, which is irregularly distributed and guides the airflow to the canard.

As a 3rd generation/3rd generation semi-fighter, it is unnecessary and impossible to adopt too many top technologies. After all, it can only be put into use after mass production. However, the aerodynamic design in the late 1980s doomed its inherent deficiency in stealth performance. Of course, it can wait for technological progress and cost reduction before launching subsequent models. (Cheng Fei has the most experience in this field, just look at the J-7 series. )

6. As a transitional model, 6.J 10/0 is destined to have its main market outside China. Seize the time and concentrate on the development of four generations is king.