The TVC on J-10 is different from types used by Sukoi and Mig and F-16. Here is what I think. In the mean time I happily steel some of
@Hendrik_2000's nice photo.
1. In TVC nozzle of Su-35 and Pakfa (before article 30), the vector control part is marked (1). It is partially ball shaped. (2) is the converging part of the nozzle. (3) is the diverging part. The converging and diverging parts work in the same way as a conventional nozzle. The tilting of the nozzle is done by (1). This approach separated the work of converging and diverging from tilting. It is also heavier and longer than conventional counterpart.
2. In Mig OVT, F-16 AVEN, the Zhuhai model, European demonstrated TVC and article 30 of Su-50, the tilting are done by the paddles of converging and/or diverging. The
outside paddles are one pieces.
3. J-10's TVC is in the same category as items 2 above, but with different implementation. See the red circles in the following diagram. This does not exists in the all engines in 2. This required the
external paddles being constructed in
two pieces joined by a hinge. See the red lines in the diagram below and pictures of J-10 further down. Why does the designer make this choice? What difference can be made compared with all other implementation? Maximizing the tilting angle? Further shortening the length of nozzle?
Summary:
- Pre-article30 Sukoi TVC is in its own category. The rests are in another.
- J-10 TVC has a distinct feature than the rests in their category.
- There seems to be more than one type of TVC nozzle evaluated by PLAF.