Abstract: A gas path flow blocker comprising a plurality of vanes each comprising a forward portion and an aft portion defining a plurality of gas paths, a forward ring comprising a central axis about which is circumferentially disposed the plurality of forward portions, and an aft ring disposed about the central axis about which is circumferentially disposed the plurality of aft portions wherein the forward ring and the aft ring are moveable with respect to each other to at least partially block the flow of a gas through the gas paths.
Abstract: A seating device in the form of seat furniture or for placing on seat furniture. The device comprises a seating element which can be pivoted transversally to the seating direction in relation to a support element about at least one axis. The seating element can be moved in the seating direction (X) in relation to the support element by means of at least one actuatable regulating device, and a regulated self-locking position is fixed.
Abstract: An axial divergent section slot nozzle for an engine is provided. The nozzle has a plurality of spaced apart divergent flaps, at least one device for moving the divergent flaps to change a cross sectional area of the nozzle in a throat region, and a bridge member positioned intermediate adjacent ones of the flaps. The bridge member includes a bridge bracket and a sealing element joined to the bridge bracket. The sealing element has an upper surface. The bridge bracket has a lower surface which diverges from the upper surface of the sealing element. In a preferred embodiment of the present invention, the bridge bracket has a shape which allows variable slot size depending on nozzle throat jet area.
Type:
Grant
Filed:
March 26, 2004
Date of Patent:
August 29, 2006
Assignee:
United Technologies Corporation
Inventors:
Robert H. Bush, Sean Zamora, Harry Culver, Donald William Peters
Abstract: To further isolate imbalances in a rotating structure such as a gas turbine engine, an effective length between two bearings may exceed an actual length. This may be achieved via one or more tapering bearing supports associated with at least one of the bearings.
Abstract: A process for hydroprocessing a hydrocarbon feedstock, includes the steps of providing a hydrocarbon feed having an initial characteristic; providing a first hydrogen-containing gas; feeding the hydrocarbon feed and the first hydrogen-containing gas cocurrently to a first hydroprocessing zone so as to provide a first hydrocarbon product; providing a plurality of additional hydroprocessing zones including a final zone and an upstream zone; feeding the first hydrocarbon product cocurrently with a recycled gas to the upstream zone so as to provide an intermediate hydrocarbon product; and feeding the intermediate hydrocarbon product cocurrently with a second hydrogen-containing gas to the final zone so as to provide a final hydrocarbon product having a final characteristic which is improved as compared to the initial characteristic.
Type:
Grant
Filed:
May 23, 2002
Date of Patent:
August 29, 2006
Assignee:
Intevep, S.A.
Inventors:
Carlos Gustavo Dassori, Nancy Fernandez, Rosa Arteca, Carlos Castillo
Abstract: A bearing support for a rotor of an aircraft turbine engine which includes a front bearing and a front bearing support and bearing strut for securely attaching the front bearing, to the aircraft turbine engine support structure, wherein the front bearing support and bearing strut are integral with the aircraft turbine engine support structure.
Abstract: A vernier duct blocker comprising a plurality of vanes each having a width and comprising a forward portion and an aft portion defining a plurality of gas paths each of the plurality of vanes being separated by a plurality of widths, and a rotatably movable ring interposed between the forward portion and the aft portion comprising a plurality of openings each having a width, wherein the width of one of the plurality of vanes differs from the width of another one of the plurality of vanes.
Abstract: A gas turbine engine component, such as a high pressure turbine blade, has an airfoil portion, a platform, and micro-circuits within the platform for cooling at least one of a platform edge adjacent the pressure side of the airfoil portion and the trailing edge of the platform. The micro-circuits include a first micro-circuit on a suction side of the airfoil and a second micro-circuit on a pressure side of the airfoil. The micro-circuits within the platform achieve high thermal convective efficiency, high film coverage, and high cooling effectiveness.
Type:
Grant
Filed:
February 3, 2004
Date of Patent:
August 29, 2006
Assignee:
United Technologies Corporation
Inventors:
Frank Cunha, Keith Santeler, Bret Teller
Abstract: The invention relates to a rear parcel shelf system for a convertible vehicle with a hard folding roof. The system has a first retractable shelf. The inventive system also has a second shelf which is intended to be disposed under the bonnet of the rear boot when the roof is in the closed position and has a device for moving and guiding the second shelf towards the front of the vehicle in order to fill the space between the back of the corresponding seats and the front edge of the bonnet when the roof is in the folded position.
Type:
Grant
Filed:
July 10, 2003
Date of Patent:
August 22, 2006
Assignee:
Heuliez
Inventors:
Jean-Marc Guillez, Paul Queveau, Gerard Queveau
Abstract: If only an operating button 14 is pushed, an electrically opening and closing mechanism 1 disengages a first clutch K1 while engaging a second clutch K2 to operate an electrically driving means 2 to automatically open or close a second member (e.g., a liquid crystal display panel) 4 which is rotatable with respect to a first member (e.g., a body having a plurality of keys) 3. If the operating button 14 is pushed, the second member 4 automatically rotates to an optional angular position with respect to the first member 3, and if the operating button 14 is released (if the operating button 14 is returned to the original angular position by the spring force of a second spring 23), the first clutch K1 is engaged at the optional angular position to hold the attitude of the second member 4.
Abstract: An impact tool, comprising: a shaft; a stop on the shaft; a slider movable on the shaft for striking the stop to create an impact force; and a handle on the slider to allow a user to move the slider. The handle isolates the impact force from the user by being movably attached to the slider.
Abstract: A drive control for controlling a gear system which is connected to a motor. The drive control comprises one or several sensors for detecting operationally specific parameters of the gear system, and a decentralized sensor evaluation unit. The sensor or each sensor is connected to the decentralized sensor evaluation unit for separate evaluation of information provided by the sensor or sensors.
Abstract: The present invention relates to a method for measuring the content of Lanthanides dissolved in uranium oxide, wherein the Lanthanides content in the nuclear fuel pellet is measured using the thermo gravimetric analysis which measures the weight variation caused by the oxidation and heat treatment of the nuclear fuel pellet. This method provides an advantage in that the Lanthanide content can be measured using relatively simple equipments such as an electric furnace and a balance.
Type:
Grant
Filed:
November 27, 2002
Date of Patent:
August 22, 2006
Assignees:
Korea Atomic Energy Research Institute, Korea Hydro & Nuclear Power Co., Ltd.
Abstract: A turbine blade for use in a gas turbine engine is provided. The turbine blade includes an airfoil portion having a tip end, a shroud attached to the tip end, which shroud has an outer surface, and a knife edge attached to an outer surface of the shroud. The knife edge has a pair of cutter blades protruding outwardly from the knife edge.
Abstract: The present invention relates to heat shield panels or liners to be used in combustors for gas turbine engines. The heat shield panels each comprise a hot side and a cold side and at least one isolated cooling chamber on the cold side. Each cooling chamber has a plurality of cooling film holes for allowing a coolant, such as air, to flow from the cold side to the hot side. A combustor having an arrangement of heat shield panels or liners is also described.
Type:
Grant
Filed:
May 16, 2002
Date of Patent:
August 22, 2006
Assignee:
United Technologies Corporation
Inventors:
Monica Pacheco-Tougas, Joseph D. Coughlan, III, James B. Hoke, Alan J. Goetschius
Abstract: A turbine engine augmentor has a centerbody within a gas flowpath. A flameholder is positioned in the flowpath outboard of the centerbody. A burner within the centerbody has an outlet for expelling combustion products of a first pilot fuel. A pilot fuel conduit has an outlet positioned to introduce a supplemental pilot fuel to the expelled combustion products.
Abstract: An apparatus for assembling a swash plate with pistons in a swash plate compressor of the present invention can automatically assemble the swash plate with double or single head pistons and shoes thereby improving workability and productivity. In the assembling apparatus, each of the pistons includes a swash plate-receiving section for receiving a pair of opposed shoes therein and having an insert groove for receiving the swash plate mounted on a rotational shaft and a piston body to be inserted into a cylinder bore of a cylinder block so that the swash plate is inserted into the insert grooves of the pistons. The assembling apparatus comprises a base plate, piston-loading means, piston-shifting means and rotating means.
Abstract: A gas turbine engine combustor has inboard and outboard walls. A forward bulkhead extends between the walls and cooperates therewith to define a combustor interior volume. In longitudinal section, a first portion of the combustor interior volume converges from fore to aft and a second portion, aft of the first portion converges from fore to aft more gradually than the first portion.
Type:
Grant
Filed:
October 9, 2003
Date of Patent:
August 22, 2006
Assignee:
United Technologies Corporation
Inventors:
Steven W. Burd, Albert K. Cheung, John T. Ols, Reid D. Smith, Irving Segalman
Abstract: A lightning strike mitigation system for protecting a surface includes an inner insulating layer adjacent a surface to be protected, an outer insulating layer, and an intermediate layer formed from an electrically conductive material between the inner and outer insulating layers. The inner and outer insulating layers may be formed from an ablative insulating material containing no metal fill, an ablative insulating material containing a 15% Ni fill, or an ablative insulating material containing a 30% Ni fill. The electrically conductive material may be a mesh material or a foil material formed from an electrically conductive material or materials.
Type:
Grant
Filed:
April 28, 2003
Date of Patent:
August 22, 2006
Assignee:
United Technologies Corporation
Inventors:
Brook Garrettson, Hugh M. Reynolds, James P. Hornick
Abstract: An average bidirectional flow tube, including a body having two side plates and upper and lower plates, a partition plate installed to be perpendicular to the side plates of the body so that front and rear ends of the tube are separated from each other, and two pairs of pressure impulse lines installed at front and rear positions of the partition plate. The upper and lower plates of the body each have a curvature to be in contact with an inner surface of a pipe in which the average bidirectional flow tube is installed, and each of the pressure impulse lines is installed to communicate with an interior of the pipe. Although a two-phase flow occurs in the pipe or the flow of the fluid flowing in the pipe is changed, an average flow rate of a fluid can be measured. Particularly, it is easy to measure an average flow rate of the fluid when the fluid flows at a low speed. Further, even when sudden pressure reduction occurs in the pipe, an additional cooling device is not required.