Abstract: A rotor for an aircraft is described having: a support angularly fixed with respect to an axis and housing a power source; a unit rotatable about axis and housing an electrical load of the resistive type; and a power supply system for the electrical load and comprising: a first transformer electrically interposed between the power source and the load; the first transformer comprises: a first winding arranged on the support and a second winding arranged on the unit, a stator carried by the support, rotationally fixed with respect to axis and to which the first winding is fixed; and a rotor operatively connected to the unit and to which the second winding is fixed; the power supply system comprises a capacitive circuit electrically connected to the first transformer, so as to reduce the reactive power absorbed by the rotary transformer.

Abstract: Wearable device having one or more impact sensors and at least one unit transmitting a detected signals to a remote station, the device being composed of an inner glove wearable under a martial art glove.

Abstract: A control system (50, 100) is for wind power plants including aerogenerators (10) provided with DC modular converters (40). The control system (50, 100) includes devices for receiving at least a voltage signal coming from a DC medium voltage line (MTDC) electrically connected to the converters (40) and a mechanical torque signal (CRIF) produced by the aerogenerators (10) and controls AC-DC conversion modules (40a?-40a??) of the plant. The modules have electronic devices driven by impressed voltage and producing on their outputs a respective partial continuous voltage (Vdci). For each aerogenerator (10) there are secondary control stages (100) and a single main control stage (50). Each of the secondary control stages (100) supplies control signals to a respective AC-DC conversion module (40a?-40a??) and is designed to keep the partial continuous voltage (Vdci) at a constant value.

Abstract: A control system (50, 100) is for wind power plants including aerogenerators (10) provided with DC modular converters (40). The control system (50, 100) includes devices for receiving at least a voltage signal coming from a DC medium voltage line (MTDC) electrically connected to the converters (40) and a mechanical torque signal (CRIF) produced by the aerogenerators (10) and controls AC-DC conversion modules (40a?-40a??) of the plant. The modules have electronic devices driven by impressed voltage and producing on their outputs a respective partial continuous voltage (Vdci). For each aerogenerator (10) there are secondary control stages (100) and a single main control stage (50). Each of the secondary control stages (100) supplies control signals to a respective AC-DC conversion module (40a?-40a??) and is designed to keep the partial continuous voltage (Vdci) at a constant value.

Abstract: A modular converter 30 for converting the electric power produced by aerogenerators, designed to be used within a wind-power plant, which is equipped with: input terminals 30a designed to be connected to an electric-power generator 3 of a single-phase or multiphase type; output terminals 30b; and control devices 36 for controlling the power of the electric-power generator 3. The modular converter has multiple modules 31 designed to receive on their inputs 31.1 alternating electric current and to produce on the respective outputs 31.2a, 31.2b direct electric current to be distributed within the wind-power plant, and, moreover, the control devices 36 receive a signal from the modules 31 and act on the electric-power generator 3.

Abstract: A modular converter 30 for converting the electric power produced by aerogenerators, designed to be used within a wind-power plant, which is equipped with: input terminals 30a designed to be connected to an electric-power generator 3 of a single-phase or multiphase type; output terminals 30b; and control devices 36 for controlling the power of the electric-power generator 3. The modular converter has multiple modules 31 designed to receive on their inputs 31.1 alternating electric current and to produce on the respective outputs 31.2a, 31.2b direct electric current to be distributed within the wind-power plant, and, moreover, the control devices 36 receive a signal from the modules 31 and act on the electric-power generator 3.

Abstract: A sleeve to be drawn over a rotary support in order to define a blanket cylinder of an indirect or offset printing machine, this cylinder cooperating with a lithographic plate cylinder from which it receives the date to be printed and with a substrate onto which said data are transferred, said substrate moving between the blanket cylinder and a pressure cylinder, the sleeve comprising an inner cylindrical portion to be drawn over the aforesaid rotary support and having its surface covered by a layered structure comprising at least one compressible layer and an incompressible outer layer arranged to cooperate directly with the lithographic plate and with the substrate to be printed; the layered structure being composed at least partly of polyurethane material.

Abstract: A sleeve to be drawn over a rotary support in order to define a blanket cylinder of an indirect or offset printing machine, this cylinder cooperating with a lithographic plate cylinder from which it receives the date to be printed and with a substrate onto which said data are transferred, said substrate moving between the blanket cylinder and a pressure cylinder, the sleeve comprising an inner cylindrical portion to be drawn over the aforesaid rotary support and having its surface covered by a layered structure comprising at least one compressible layer and an incompressible outer layer arranged to cooperate directly with the lithographic plate and with the substrate to be printed; the layered structure being composed at least partly of polyurethane material.

Abstract: A laminated printing blanket having compressible and resilient properties and a method for its production are provided. The compressible characteristics are provided by disposing an intermediate layer having substantially uniformly distributed voids of substantially uniform size between the base ply and the working surface of the printing blanket. The voids of the compressible intermediate layer are formed by introducing high melting point microspheres formed from thermoplastic resins into an elastomeric matrix, coating said microsphere containing elastomeric matrix upon an upper surface of the base ply and then vulcanizing the coated base ply at a temperature of between about 80-150° C. for between about one and six hours to form the compressible layer having substantially uniform compression characteristics. Once all of the layers of the blanket are stacked, a final vulcanization treatment at between about 132-160° C.

Abstract: A laminated printing blanket having compressible and resilient properties and a method for its production are provided. The compressible characteristics are provided by disposing an intermediate layer having substantially uniformly distributed voids of substantially uniform size between the base ply and the working surface of the printing blanket. The voids of the compressible intermediate layer are formed by introducing high melting point microspheres formed from thermoplastic resins into an elastomeric matrix, coating said microsphere containing elastomeric matrix upon an upper surface of the base ply and then vulcanizing the coated base ply at a temperature of between about 80-150.degree. C. for between about one and six hours to form the compressible layer having substantially uniform compression characteristics. Once all of the layers of the blanket are stacked, a final vulcanization treatment at between about 132-160.degree. C.

Abstract: The present invention relates to a digital printing blanket carcass for supporting a transfer layer having an outer surface which is capable of transferring electrostatic particles. This carcass includes an upper layer of a resilient material which can withstand a temperature of up to about 150.degree. C., such as silicone rubber, hydrogenated nitrile rubber, an acrylic rubber or a fluoroelastomer; a compressible layer of an elastomeric matrix material having a plurality of open or closed cells therein; and a fabric layer of a fiber material which can withstand a temperature of up to about 150.degree. C., such as carbon, boron, a metal, fiberglass, a polyimide, or an aromatic polyamide.

Abstract: A metal backed printing blanket for mounting on a cylinder that includes a gap. The blanket comprises a metal base plate having top and bottom surfaces and ends which include leading and trailing edges adapted for engaging the cylinder gap. The article further comprises a compressible, elastomeric printing blanket secured to the top surface of the base plate, but not to the ends, and having an upper face adapted for contact transfer of ink to a printable substrate. In addition, the blanket is provided with an anti-slip layer upon at least a portion of the top surface of at least one end of the base plate to facilitate retention of the base plate ends within the gap during rotation of the cylinder. The anti-slip layer has a coefficient of friction that is greater than that of the base plate and a thickness sufficient to permit insertion of the base plate edges and ends into the cylinder gap.

Abstract: A method of manufacturing a cylindrical compressible laminate using the floating knife or knife over roll spreading techniques to apply an inner compressible layer and outer or surface layer of a substantially incompressible material. The coating system includes a coating head to dispense an elastomeric material onto a rotating laminate and a knife blade that is parallel to the axis of rotation to distribute and spread a uniform coating of the elastomeric material. The knife blade can be raised incrementally on each rotation of the laminate so that an additional coating can be applied, until a layer of a desired thickness is obtained. In the preferred embodiment, the coatings are at least partially cured during each rotation.