I am a new member.
I have a thought to design a new jet engine. The combustion in current jet engine is under consistent high pressure created by compressor. A lot of energy out off from combustion cabinet is used to drive turbine for compressor. But I know the efficiency of compressor is very low and the compressor is very heavy, its weight occupies 70% of total engine. My idea is to adopt closed combustion type to increase pressure. It consist of several same components cooperate to get steady propulsion. By the closed combustion, we can get high pressure easily. Meanwhile the total weight is much smaller. It also utilizes the other advantage of closed combustion
in mixture gas : easily igniting, burning rapidly.easy to get high pressure. On the other side I must overcome the weakness: the stress on some parts isn’t consistent and regulate difficultly in different work condition. I have thought methods to solve them basically. I have applied for a Chinese patent ZL95237295.9 Name: the jet propulsion with the closed combustion type.
The main advantage are: the new jet engine is lighter and has more whole efficiency than current jet engine.
I hope you think if it is feasible?
I beg you propose your idea and tell me how to promote it into market.
My E-mail:
qumf@163.com
