We invented a new model of gas turbine engine for electricity production that is used in the aviation and is installed in the aircraft to supply the electricity inside.

Currently existing engines use part of the air that is passing throughout the engine to cool the turbines. Such cooling is needed, as otherwise the turbines/engine will be damaged by the very high temperature of the burning fuel. This method has two imperfections - part of the air is lost for cooling, and second - cooling the turbines reduces the efficiency of the engine itself.

We invented "self-cooling" gas turbine engine that does not take (do not need) part of air to be relocated, and that can work with the highest possible temperature of the burning fuel without damaging the turbines/engine itself. Thus, also working with higher than today efficiency.

Thus, our invention significantly increases: 1) The efficiency, 2) The life of the turbines/engine. At the same time the volume of the fuel needed remains t...
We invented a new model of gas turbine engine for electricity production that is used in the aviation and is installed in the aircraft to supply the electricity inside.

Currently existing engines use part of the air that is passing throughout the engine to cool the turbines. Such cooling is needed, as otherwise the turbines/engine will be damaged by the very high temperature of the burning fuel. This method has two imperfections - part of the air is lost for cooling, and second - cooling the turbines reduces the efficiency of the engine itself.

We invented "self-cooling" gas turbine engine that does not take (do not need) part of air to be relocated, and that can work with the highest possible temperature of the burning fuel without damaging the turbines/engine itself. Thus, also working with higher than today efficiency.

Thus, our invention significantly increases: 1) The efficiency, 2) The life of the turbines/engine. At the same time the volume of the fuel needed remains the same as today.


Our engine has:
- Lower weight (important for the aircraft)
- Simple but durable construction
- Simple and even less expensive materials versus currently used titanium and ceramic
- Lower CAPEX vs existing
- Lower OPEX vs existing


Our engine perfectly fits and can be "installed" in the aircraft by using the same (the existing) carrying chassis and constructions. The later are fully compatible. No need to modify the construction and/or the design of the airplane or part of it.

As a result, the Gross Margin for the aircraft manufacturer increases, higher prices can be offered to airlines (b2b clients) due to the benefits offered.

Our first (laboratory) prototype performed excellent. We need 3 months to build the second prototype (working in real environment), and another 3 months to test it, fine-tune it and finally test it again.

The claimed effect could be visible and measured immediately upon access to prototyping and test facilities that you provide.

We are currently not pitching financial investors since we prefer to settle strategic partnership which combines funding, testing facilities, mentoring and co-operation in further R&D and fine-tuning.

We have selected Madrid campus as primary choice, however we would be willing to also join Toulouse or Bangalore campus (we’d rather leave the choice to your sole consideration).
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Rennie Popcheva
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Rennie Popcheva Marketing Inventor. Founder at embrioo.com. Creative. Non-conventional thinker