Nandor
Nandor Klatsmanyi, Berowra AU
Patent application number | Description | Published |
---|---|---|
20120150424 | DESTINATION ARRIVAL ESTIMATES AUTO-NOTIFICATION BASED ON CELLULAR SYSTEMS - The present, in one embodiment, is directed to a method for determining vehicular speeds over various travel routes that includes the steps: | 06-14-2012 |
Nandor Koeteles, Bremgarten CH
Patent application number | Description | Published |
---|---|---|
20130028685 | ARRANGEMENT FOR FORMING A BAND LOOP AND METHOD AND DEVICE FOR MANUFACTURING PEEL-OFF LIDS - When handling a foil band ( | 01-31-2013 |
Nandor Koszo, Shalier Park AU
Patent application number | Description | Published |
---|---|---|
20150204085 | WALL ASSEMBLY AND A BUILDING STRUCTURE INCLUDING THE WALL ASSEMBLY - A wall assembly for forming an external wall on a building structure is disclosed. The wall assembly comprises a cladding and a plurality of vertical formwork members spaced along the wall assembly, and a horizontal formwork member extending along the top of the wall assembly. The formwork members are elongate profiles having a substantially constant cross sectional shape and they are arranged so that with the cladding they form an interconnected formwork defining a formwork space. A cementitious material cast within the formwork space is interconnected and forms a single underlying structural frame within the constructed wall assembly. The assembly includes connectors extending between the vertical and horizontal formwork members and the cladding on which they are mounted. Each connector extends from the cladding through the formwork space to the formwork member and is cast within the cementitious material. A method of building a wall assembly is also disclosed. | 07-23-2015 |
Nandor Vestroci, Debrecen HU
Patent application number | Description | Published |
---|---|---|
20110180672 | Airplane with aerodynamic stall-prevention layout and pertinent longitudinal stability arrangement - General purpose airplane with a swept back wing provided with a sharp leading edge as to cause flow separation and stall of the wing in cases where the limits of the regular flight envelope are exceeded in terms of angle of attack, and as a result to cause the front part of the airplane to move downward, said airplane also having positive lift-producing horizontal stabilizer provided with rounded leading edge, which does not stall at this point, therefore holds the tail in level during the process, all together acting to restore the original flight attitude. The horizontal stabilizer is essentially a straight (or similar) wing with a steeper lift-coefficient curve as that of the swept-back wing, therefore, in case of an un-commanded pitch-up of the airplane the greater increase of lift on the horizontal stabilizer together with its greater moment arm provides the stabilizing force to counter such pitching. | 07-28-2011 |