1. An improved structure of heat sink is combined with the base and the structure of the closed mini pipeline; the length and width of said base are in accordance with some machine elements causing waste heat for connecting closely with said machine elements as a whole; by way of the cooling effect produced when the solution in the pipeline of the structure of closed mini pipeline connecting with said base circulate and change manually in the liquid state and steam, which makes some machine elements causing waste heat cooling.
The claims below are in addition to those above.
All refrences to claim(s) which appear below refer to the numbering after this setence.
1. A missile with a tube, which tube encircles part of the missile and is able to rotate relative to the encircled part of the missile, and at least one fin is connected to the tube, which at least one fin is connected to the tube such that the at least one fin is able to be rotated in a pivoting manner relative to the tube, and which missile comprises a plurality of sections and a means to rotate the at least one fin, which sections can be separated, and which means to rotate the at least one fin is such that separation of the sections is able to cause rotation of the at least one fin in a pivoting manner relative to the tube.
2. The missile of claim 1 wherein at least one additional fin is connected to the tube, and which at least one additional fin is connected to the tube such that the at least one additional fin is able to be rotated in a pivoting manner relative to the tube, and which missile comprises a means to rotate the at least one additional fin such that separation of the said sections is able to cause rotation of the at least one additional fin in a pivoting manner relative to the tube.
3. The missile of claim 2 wherein the means to rotate the at least one fin and the means to rotate the at least one additional fin are such that separation of the said sections is able to cause rotation of the at least one fin in a pivoting manner relative to the tube and rotation of the at least one additional fin in a pivoting manner relative to the tube, and such that the at least one fin can be caused to rotate in a pivoting manner in a same direction as a direction of rotation in a pivoting manner of the at least one additional fin relative to the tube.
4. The missile of claim 3 wherein the said same direction is such that rotation of the at least one fin is substantially in a same direction relative to the tube as a direction rotation of the at least one additional fin.