2016 - Published on GrabCAD some past research projects.
They are downloadable and viewable at this address:
Click here

2014-2015 - SEARCING activity in the electronic field,studing a device designed in collaboration with a friend (Ing. Conte Angelo), called WATCHDOG. It is designed to monitor the degenerative aging of most of TECHNICAL TEXTILES dedicated to the world of Sport, in particular, Aeronautical (parachute, paragliding , all type of harnesses, delta, balloons, etc.) and water (Kite surfing, windsurf, all types and sizes of sails, etc).
The Wathdog was created with the intention to protect the lives of people who play sports, by monitoring certain parameters vital own of the technical tissues.
The instrument was presented in France (Nice) during the Meeting ETSC (European Safety and Training Committee) in June 2014, and is now a mature product for the market. Have are now taking business negotiations with some communities and firms.
For information:

BLOG: Click here
Paragliding Forum: Click here
Free-Aero: Click here
FIVL: Click here

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2013-14 – SEARCHING Activity applied to the AIRBORNE WIND ENERGY field: Macrofeasibility study of a airborne wind energy generator type GROUND GEN, based onthe cycle YO-YO, MULTI TETHER. The Airborne Wind Energy technology is developing fast. These systems will be able to produce clean energy with a double capacity factor than a big wind turbine (the double hours of energy production), obtained with a structur 20 time lighter and cheaper. My challange is based to some inedit concepts on a new type of ground generator, having a big size (>1 MW), potentially able to solve the problems of actual projects. The literature on the topic AWE is now strongly consolidated around the world from study and prototypes, dissertations and scientific investigations.
ACTIVITIES DONE: A) A CAD feasibility study of the whole parts of the generator; B) The study concerning the new semirigid bimodal wing. Tight contacts with selected Engineers', just skilled in the AWE.


2012 – Start teaching of ERGONOMICS at the IED (Istituto Europeo Design)

2012 – A reference to the study on the wing carbon kite, with its attached image, appeared on the thesis in Mechanical Engineering Eng. Antonello Cherubini (p. 29) _and_Wind_Energy_Harvesting.pdf

2012-2013 - Collaboration with Bertone Style Center


2011 - RENEWABLE ENERGY FIELD - Closing collaboration with the Kite Gen project: 17 months after the start, some numbers related to the current project: over 3000 hours of CAD design dedicated to the study, construction and assembly of the first machine, built and being tested hundreds of parts, a second machine in working, the study and operational management of laboratory researchers in Stuttgart of a new semi-rigid wiing, having high-efficiency, aimed at the generation of the maximum energy from the wind at high altitude (” Ghiva

2010 – AVIATION FIELD: Collaboration (now closed) with the company Compact Compositi, on the high performance ULM named “Millenium Master, twin brother of the Blackshape Prime” Ghiva

2010 – AVIATION FIELD: SOLAR ENERGY PARAMOTOR: This project was created with the intent to understand what is the minimum threshold of power supplied by a micro electric motor, coupled to a propeller of large size, is really only usable on the flying machine seemingly simplest of all, the motor glider. This is intended to understand whether the main goal is technically attainable: the date from solar power, at least for the flight level.



Written both in Unigraphics than in CATIA V5, IAV is an archetype’s generator, and is able to verify quickly every type of vehicles architectures and to study from “0” the Base Design's phase. Aims to offer a range of useful services to large companies or to the Style Center that need to perform study and research, lowering costs for these activities. Held in a single product features of actual programs now existing, with this benefits: an immediate perception of the actions caused the change of each single parameter. A product reconfigurable and able to be developed on customer specifications.


The study and research is an attempt to demonstrate technically a concept I believe in: if you accept a project plan covering more investment, it may be possible to create a new product, while remaining within the confines imposed by the complex process scenarios design of a modern car. And in this case, it may be necessary to redefine the rules of economic assessment of a project in a broader perspective.

Some number: Max. Lenght (L103) = 3460 mm; Max. Width (W103) = 1880-1900 mm; Total Number. seats = N° 6, on two file (3+3) Baggage Volume wire hatbox = 650 dm2 Baggage Volume upper hip roof = 1670 dm2

Some number: Max. Lenght (L103) = 3460 mm; Max. Width (W103) = 1880-1900 mm; Total Number. seats = N° 6, on two file (3+3) Baggage Volume wire hatbox = 650 dm2 Baggage Volume upper hip roof = 1670 dm2