Ceramic Matrix Composite is an entire class of composite materials. GE is focusing on SiC-SiC composites. So if your question is "do we have SiC-SiC composites tech that we can apply to gas turbine engines.?", then the answer is: Not sure. In non-rotating components, such as in CFM-56 LEAP engine, maybe, if we spend some time doing R&D for it. But for use in turbine blades, defnitiely no, and not likely in the next couple of decades.
Shouldn't even be a question. Shinakereba naranai.
Not true. They have produced a Low Pressure Turbine and run it in a GE-414 engine. So its not as if they "haven't invested a dime." In fact, in CMC for hot sections alone, they have invested more than a Billion dollars over a period of decades. EPE is within their reach, only the funding is a problem for them. Similar to how Kaveri is within our reach, only funding is a problem. If they don't get funding for testing CMC blades in GE-414 EPE, they will most definitely get funding for testing CMC blades for an adaptive cycle engine (ADVENT) they are working on for their 6th generation fighters. They are clear on the strategic importance of gas turbine technology. India (the politicians) is not.
Fun fact: There are at least three Indian Americans involved in this endeavour. If GoI were Chinese, they would have paid these three Indian Americans handsomely to come back to India and work on these things here.
Dude what is the maximum airflow that MWF air intakes would even allow? 77 kg/sec? I think EPE requires some 85 kg/sec, which I suspect is more than what MWF intakes are being designed for. I am confused as to why GE-414 EPE is being discussed on MWF thread. I initially thought this was Kaveri engine thread.