Zecca
Gabriele Zecca, Parma IT
Patent application number | Description | Published |
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20120279090 | SYSTEM FOR RECEIVING A USER - A system for removing moisture from a user's skin includes a casing having a first portion made of a material including hydrophilic and hydrophobic fibers configured to convey a liquid and/or vapor from outside to inside. The first portion configured to contact, or be near, a user's body part. The casing includes a second portion not configured to contact the body part, and at a third portion joining the first and second portions. The second and/or third portions are made of material configured to convey a liquid and/or vapor from inside to outside the casing. Padding, enclosed between the first and second portions, has a porous structure enabling the inside to be ventilated by vapor exiting the casing by contraction of a volume of the padding causing air to enter the casing by expansion in the volume of the padding. The porous structure has a resiliently compressible variable volume. | 11-08-2012 |
Joseph C. Zecca, San Diego, CA US
Patent application number | Description | Published |
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20160053719 | AUTOMATIC DEFLECTION LIMITING LATCHES FOR A THRUST REVERSER - A nacelle may include a pylon and a thrust reverser having an inner fixed structure. A locking mechanism may automatically engage and prevent relative movement between thrust reverser halves. A bumper may be coupled to the inner fixed structure. The locking mechanism may limit deflections between the thrust reverser and the pylon in response to a burst duct. A locking mechanism in the inner fixed structure may include a pressure relief door and an arrestor which hooks onto a retaining bar in a pylon bracket. The locking mechanism may allow the thrust reverser halves to be opened for access to the engine. | 02-25-2016 |
Joseph Christopher Zecca, San Diego, CA US
Patent application number | Description | Published |
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20100038475 | ICE PROTECTION SYSTEM FOR A MULTI-SEGMENT AIRCRAFT COMPONENT - An aircraft component includes a first segment having a first leading edge surface that extends to a first end of the first segment. The aircraft component also includes a second segment having a second leading edge surface that extends to a second end of the second segment. The second end is substantially adjacent to the first end of the first segment, and is connected to the first end. The first leading edge surface includes electrical resistance heating that extends to the first end of the first segment. In addition, the second leading edge surface includes electrical resistance heating that extends to the second end of the second segment. The electrical resistance heating is capable of providing ice protection heating immediately on either side of a juncture between the connected first and second ends. | 02-18-2010 |
20140034414 | ELECTRIC HEATER FOR INTEGRATION INTO AN AIRCRAFT ACOUSTIC PANEL - An electric heater ( | 02-06-2014 |
Luca Zecca, Sala Bolognese IT
Patent application number | Description | Published |
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20090107226 | FUEL VOLATILITY RECOGNITION METHOD DURING THE POST-CRANKING STEP OF AN INTERNAL COMBUSTION ENGINE - A fuel volatility recognition method during the post-cranking step of an internal combustion engine; the recognition method contemplates the steps of: starting the internal combustion engine; adjusting the enrichment of the mixture burnt in the cylinders of the internal combustion engine according to a previously determined historic fuel volatility value; detecting the time evolution of the angular speed of a crankshaft of the internal combustion engine during the post-cranking step; determining the noise contained in the angular speed of the crankshaft by filtering the angular speed itself by means of a high-pass filter; comparing the noise contained in the angular speed of the crankshaft against at least one predetermined threshold value; and recognizing the fuel volatility according to the result of the comparison between the noise contained in the angular speed of the crankshaft and the predetermined recognition threshold. | 04-30-2009 |