Renewables-2017

Dr. Gábor Szabó, President Dr. László Antos, Executive Director Hungarian Association for Innovation Dr. István Blazsek, President Dr. Ivan Budai, Director Hungarian Chemical Industry Association   Dr. Roland Feketa, President IPE – Association of Industrial, Science, Innovation and Technology Parks Dear gentlemen, 19.09.2017 Danube countries using their nearness to Black sea and its unique potential for very cheap, simple and clean energy production, they can reach fuel and electricity independency, with a help of Ukrainian outsourcing and my fresh looked innovations, while Ukraine has high professional engineers and workers and extremely low cost of labor. A small international group can promote it, and I ask you to help me in your separate country. Disclosure for experts [ (1a), (3) and (4) need some additional time for R & D. All costs are correlating each to others and corresponding here to Black sea conditions] (1) electricity by 0.

Arrays of Lattices of small HAWTs lifted high in the sky Author: David Judbarovski, principle inventor, engineering and engineering systems, retired engineer, Israel email: judbarovski@gmail.com , CV see in Linkedin.com (David Judbarovski) Earlier versions goes me back to about 10 years ago Numerous small HAWTs (horizontal axis wind turbines) combined in a lattice, the said lattices are jointed each to another as a chain. Such device transforms wind kinetic energy in electricity. A total HAWT proportionally of its dimension is lighter and cheaper, so correspondingly the electricity production is cheaper. Being lifted in the sky, the wind velocity is bigger following exponential Hellmann law, while the HAWT power is in cube of wind velocity being more than 10 m/s at 500-900 m above open ocean surface. Low point of such device be fixed by a rope to a float stabilized in constant position.. The lion share of such electricity cost is a cost of electric generator of 30 Wat

Breakthrough novel aircraft versus helicopters Author: David Judbarovski, principle inventor, engineering and engineering systems, retired engineer, Israel judbarovski@gmail.com , CV see in Linkedin.com (David Judbarovski) 2016-2017, 10 th September 10, 2017 Specifications comparison (my concept vs. Mi-17, Russia, for example) Capacity: 26 troops, or 12 stretchers, or 4000 kg vs. 24/12/4000 Take-off weight (max): 5300 kg vs. 13000 kg Speed (cruise): 720 km/h vs. 260 km/h Range (till operational point and back: 2.3 hours, 1700 km vs. 3.0 hours, 800 km Max. on duty at the sky : 20 hours, 150 km/h vs. about 3.5 hours   Runway: 40 meters (about 4000 km range for landing) vs. zero Power plant: 2600 kW vs. 4800 kW Service ceiling: 0-10,000 m vs. 6000 m Target at any point of Iran can be hit by Israel from the West (2500 km max.) or from the South (2000 km max.), while Tomahawk (missile) is 1300 -1600 kg and 2500 km range