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| Number | Title | Issue Date |
| 7189057 | Turbine shroud segment attachment A turbine shroud segment attachment with a casing (1) and several shroud segments (2) arranged in the casing (1), wherein the individual shroud segments (2) are located in the casing (1) with a circumferential clearance (3) ... | 03/13/2007 |
| 7176696 | Method of detecting and eliminating foreign bodies in a flow of tobacco In a method of detecting and eliminating foreign bodies in tobacco, a flow of tobacco advances first through a preparation zone where it is gathered into a continuous ribbon of tobacco filler, then through a forming station at which the filler is used to fashion a c... | 02/13/2007 |
| 7100868 | Method for the control of aero gas turbine engines The exchange, removal or addition, as applicable, of media and/or power between the individual shafts of an engine, between individual engines and between the engines and the aircraft provides for additional degrees of freedom, enabling engine parameters to be addre... | 09/05/2006 |
| 7059133 | Dilution air hole in a gas turbine combustion chamber with combustion chamber tiles A gas turbine combustion chamber includes combustion chamber tiles 3 attached to a supporting structure 6 of the gas turbine combustion chamber, with each tile possessing at least one dilution air hole 4 which is flush with a dilution air hole o... | 06/13/2006 |
| D521374 | Hinged-lid packet | 05/23/2006 |
| 7043333 | Device for checking the position of a spindle in a machine tool In a machine tool with a spindle capable of motion along at least three axes x, y, and z, the position of the spindle is checked by a device that operates utilizing electromagnetic signals sent out by four emitters, located externally of the machine tool, and picked... | 05/09/2006 |
| 7033131 | Fan blade for a gas-turbine engine For material reduction, a fan blade made of solid material for a gas-turbine engine is provided in the area of the blade tip with at least one cavity (5) extending from the face of the blade tip. Thus, apart from the aspect of weight saving, the vibration amp... | 04/25/2006 |
| 7028653 | Roller rocker mounting mechanism A roller rocker mounting mechanism for an internal combustion engine valve actuating mechanism includes a first rocker stand having a first locating boss and a second rocker stand having a second locating boss. An indexing link has a first portion separably attachab... | 04/18/2006 |
| 7025201 | Pack of rigid type for tobacco products and a relative method of manufacture A rigid pack of substantially parallelepiped appearance for tobacco products appears as a container (5) with an open top end (6), surmounted by a lid (7) hinged to the container (5) and rotatable between positions in which the top end ( | 04/11/2006 |
| 7022095 | Sport bandage The invention relates to a sports brace comprising an elastic woven or knitted fabric, which for a sport of the kind that is performed using the arm or hand can be secured to the applicable arm or wrist (2) of the person using it by means of a closure (4 | 04/04/2006 |
| 7021431 | Disk brake caliper mounting bracket A disk brake caliper mounting bracket is attachable to an axle tube to mount a brake caliper to the axle tube with a desired positioning and alignment. The bracket includes an axle tube mounting portion and a brake caliper mounting portion. The axle tube mounting po... | 04/04/2006 |
| 7011495 | Fluid flow machine (turbomachine) with increased rotor-stator ratio A fluid-flow machine (turbomachine) includes at least one rotor equipped with blades and at least one stator equipped with vanes, the rotor being supported in a casing by means of a rotating shaft. A form of annulus is provided whose cross-sectional area in a stage ... | 03/14/2006 |
| 7003939 | Method for the adaption of the operation of a staged combustion chamber for gas turbines This invention relates to a fuel injection system for a staged combustion chamber (1) of a gas turbine aero-engine, in which a certain quantity of fuel is permanently supplied to the pilot burner(s) (3) and in which fuel is apportioned to the main burn... | 02/28/2006 |
| 7002172 | Electronic safety system for the avoidance of an overspeed condition in the event of a shaft failure An electronic safety system for the detection of a shaft failure and for the interruption of the energy supply to the shaft includes at least one measuring light guide (13) which is firmly routed in the shaft longitudinal direction, co-rotates with the shaft ... | 02/21/2006 |
| 6976462 | Double roller cam follower A double roller cam follower includes a longitudinal beam having a first end and a second end, a cam roller rotationally mounted on the beam for engaging a cam lobe and a valve stem roller rotationally mounted on the second end of the beam for engaging a valve stem.... | 12/20/2005 |
| 6949055 | Machine tool A machine tool consists in a pair of slide ways set apart one from another and extending parallel with a longitudinal axis, a machining station between the slide ways, presenting a first zone and a second zone adjacent one to the other, and a traveling gantry set in... | 09/27/2005 |
| 6945053 | Lean premix burner for a gas turbine and operating method for a lean premix burner A lean premix burner for a gas turbine having at least one fuel supply ring 4 fitted with primary fuel nozzles 8 and additional secondary fuel nozzles 9, and a method of operation for this lean premix burner. ... | 09/20/2005 |
| 6938753 | Transfer unit for containers Containers are transferred from a first conveyor operating at a first height to a second conveyor operating at a second height by a rotary unit equipped with a plurality of grippers designed to take up and support each successive container by the neck. The grippers ... | 09/06/2005 |
| D508850 | Hinged-lid packet | 08/30/2005 |
| 6929121 | Blank for rigid hinge-lid type wrappers for tobacco products and a procedure for manufacturing such wrappers A rigid type wrapper (1) with a hinged lid (13) is fashioned from a flat diecut blank (42) presenting a treated face and an untreated face and comprising a main portion (45) destined to form the container (11) and the lid (13 | 08/16/2005 |
| 6921079 | Hydraulic seal arrangement A hydraulic seal arrangement 5 between two shafts 1, 2 rotating relatively to each other, particularly in the same sense of rotation, of especially a gas turbine engine, where the radially outer shaft 2 has an annulus 5a extending ... | 07/26/2005 |
| 6910400 | Machine tool In a machine tool comprising a spindle mounting slide which is driven by a linear electric motor and which runs in a vertical direction in a slideway, the slide is equipped with a counterweighting device comprising an elastic element and a roller chain, the rigidity... | 06/28/2005 |
| 6902362 | Machine tool In an automatic machine tool (1) comprising a spindle mounting slide (4) which is driven by a linear electric motor (9) in a vertical direction (V) in a slideway (8), the slide (4) is equipped with a counterweight device (13... | 06/07/2005 |
| 6901756 | Device for the injection of fuel into the flow wake of swirler vanes A device for the injection of fuel into the combustion chamber of a gas turbine includes at least one swirler (1) arranged in an air path with at least one swirler vane (2) and with at least one fuel injection nozzle (3), wherein the fuel inject... | 06/07/2005 |
| 6901757 | Heat shield arrangement with sealing element A heat shield arrangement includes several tiles 1 and several fasteners 6 for attaching the tiles at a spaced distance to a wall 2 to form an interspace 4 between the wall and the tiles which can be supplied with cooling air. At least on... | 06/07/2005 |
| 6901721 | Unit for overwrapping packets Packets are overwrapped in a cellophaner unit equipped with a wheel by which the packets are directed through an assembly station together with leaves of wrapping material and toward a folding station where the leaves are bent around the packets, also a suction roll... | 06/07/2005 |
| 6892533 | Automatic transmission An automatic transmission includes a stator support shaft having an internal axial bore for receiving an input shaft, a forward engagement portion for engaging a stator of a torque converter, and a central engagement portion for engaging a stator support and transfe... | 05/17/2005 |
| 6877953 | Gas turbine A gas turbine with a compressor area has a rotor shaft 2 to carry rotor blades 1 and a casing 4 to carry stator vanes 3, with the related rotor blades 1 and stator vanes 3 forming an axial clearance space 5 between on... | 04/12/2005 |
| D503616 | Hinged-lid packet | 04/05/2005 |
| D502871 | Hinged-lid packet | 03/15/2005 |
| 6863497 | Stator vane span attachment for a gas turbine A stator vane span attachment for a gas turbine having a casing 1 in which several stator vane spans 2 are located, wherein means 3 are provided for restraining the stator vane spans 2 against the casing 1. ... | 03/08/2005 |
| 6858056 | Oil separator An oil separator includes a casing 1 and a rotor 2, said rotor being arranged rotatably within said casing and having a flow chamber 3 through which oil-laden air 4 can pass, with porous material being arranged in the flow chamber 3 | 02/22/2005 |
| 6817189 | Arrangement for the cooling of the casing of an aircraft gas turbine engine This invention relates to an arrangement for the cooling of the casing 1 of an aircraft gas turbine with a bypass duct 2 and at least one cooling air tube 3, this cooling air tube 3 having its inlet 4 arranged in the bypass duct | 11/16/2004 |
| 6810671 | Method for the fuel supply and a fuel supply system for aircraft equipped with at least one aero gas turbine The invention relates to a method for the fuel supply of an aero gas turbine installed in an aircraft and to a fuel supply system. In order to avoid negative effects by out-gassed air in the fuel lines, the invention provides for an increased flow rate of the fuel i... | 11/02/2004 |
| 6790000 | Shroud for the roots of variable stator vanes in the high-pressure compressor of a gas turbine A shroud for the support of vane roots 1 of variable stator vanes 2 in the high-pressure compressor of a gas turbine includes a forward shroud segment 3 and a rearward shroud segment 4, each with an axially open annulus 5 forming a... | 09/14/2004 |
