Abstract: A brush seal assembly for sealing a gap between a first component and a second component, comprising: a body; bristles extending from the body; and an extension from the body, the extension having an elongated slot therein. The slot, when the brush seal assembly mounts between the first and second components, allows the brush seal assembly to float within the gap. An axial brush seal assembly, comprising: a body; bristles extending from the body; and means for allowing movement of the brush seal assembly in an axial direction within the gap. An apparatus, comprising: a first component; a second component spaced from the first component in an axial direction; and an axial brush seal assembly movably mounted between the first and second components. The brush seal assembly can move in said axial direction.

Abstract: A template for evaluating a part, comprising: a surface having a shape corresponding to the part; and at least one element on the surface corresponding to a desired location of a feature on the part. A method of evaluating a part, comprising the steps of: providing a template having a shape corresponding to the part and at least one element thereon corresponding to a desired location on the part; associating the template with the part; and using the element to determine whether the feature is at the desired location.

Abstract: A brush seal including a back plate, side plate and bristle ring is disclosed wherein the brush seal is secured together entirely through the use of removable fasteners. The back plate may be provided with a circumferential lip thereby providing a surface against which the head of a fastener can be used to compress the back plate against the side plate and thus capture the bristle ring therebetween. The brush seal can thereby be manufactured from disparate materials which could not be manufactured if welding were required.

Abstract: A flow directing device of a gas turbine engine, comprising: an airfoil having a leading edge, trailing edge, suction side and pressure side; a wall abutting the airfoil; and a fillet between the airfoil and wall. The fillet has an enlarged section at the leading edge, along the suction and pressure sides, and towards the trailing edge. The device could be part of a vane segment. In addition to eliminating a horseshoe vortex, the device also reduces heat load on the airfoil by directing the cooler gas from the proximal end of the airfoil to the hotter gas at the medial section of the airfoil.

Abstract: A method of operating a gas turbine engine for testing, comprising: providing an aircraft on a tarmac, the aircraft having a gas turbine engine with an inlet; selecting a power setting for the engine that is capable of producing a vortex between the inlet and the tarmac; and inhibiting formation of the vortex. A suppressor for preventing a vortex between an inlet of a gas turbine engine on an aircraft and a tarmac. The suppressor comprises: a base facing the tarmac; and an inclined surface extending in a direction from the tarmac towards the inlet at an angle to the base. The suppressor prevents formation of the vortex.

Abstract: A blade for a turbine engine having a centerline. The blade comprises: a root section extending at an angle relative to the centerline; and an airfoil section extending from the root section. The root section is directly adjacent said airfoil section. In other words, the blade is neckless. The blade is part of a rotor assembly, and is preferably a fan blade.

Abstract: A valve assembly for supplying cooling air to a nozzle of a gas turbine engine. The nozzle can move between a first configuration and a second configuration. The valve assembly includes a first member having openings that receive cooling air. The valve assembly also includes a second member having openings. The second member resides adjacent the first member to receive the cooling air from the first member. Finally, the valve assembly includes actuator for moving the first member from a first position, which allows a first flow rate of cooling air to pass through the openings, to a second position, which allows a second flow rate of cooling air to pass through the openings. The second flow rate is less than the first flow rate.

Abstract: An apparatus for friction welding a workpiece to a substrate, comprising an actuator producing a linear oscillating motion, a platform for supporting the workpiece, and a slide mechanism between the actuator and the platform. The slide mechanism converts the linear oscillating motion of the actuator into an arcuate oscillating motion of the platform. The slide could comprise a base and a guide engaging the platform.

Abstract: A catalyst bed assembly, comprising: an outer housing having an open interior, an inlet leading to the open interior, and an outlet from the open interior; a catalyst bed in the open interior; and a gap between the outer housing and the catalyst bed. The open interior receives material from the inlet. A portion of the material enters the catalyst bed to expose said material to a catalyst so that the material and the catalyst react and create heat within the catalyst bed assembly. A remainder of the material enters the gap between the outer housing and the catalyst bed to cool the catalyst bed assembly. The catalyst bed assembly could be part of a turbopump assembly. The turbopump assembly would further include a nozzle downstream of the outlet; a turbine downstream of the nozzle; and a pump driven by said turbine.

Abstract: A fixture for securing a workpiece, which includes: a base; a plurality of locators on the base for accepting the workpiece; a plurality of arms, each secured to the base at a pivot point; and a lever for actuating the arms against the workpiece. The arms positively position the workpiece against the locators. The fixture is part of an electrical discharge machining (EDM) apparatus, which also includes a tank and a holder for supporting an electrode in said tank. The lever actuates towards a front of the tank.

Abstract: A fuel nozzle, comprising an inlet for receiving fuel and an outlet for discharging fuel. The outlet intersects a longitudinal centerline of the nozzle and produces a skewed spray pattern. A fuel injector having a fuel nozzle outlet such that a fluid discharged from a swirler produces a crescent-shaped spray pattern in the fuel. A burner section of a gas turbine engine comprising a combustion chamber and fuel injectors. At least one of the fuel injectors produces a skewed flame pattern in the combustion chamber that overlaps with a flame pattern from an adjacent fuel injector. A method of improving stability of a flame in a burner section of a gas turbine engine in which at least one of the fuel injectors produces a skewed flame pattern in the burner section to create a fuel non-uniformity, the flame pattern also overlapping with an adjacent flame pattern.

Abstract: A rocket propulsion system, comprising: a rocket engine; and a turbopump supplying fuel or oxidizer to the rocket engine. The turbopump can supply an; adjustable flow of the fuel or oxidizer to throttle the rocket engine. The turbopump includes a catalyst bed for decomposing a material to produce a discharge; a mixer section downstream of the catalyst bed for introducing an additional amount of the material to the discharge to produce an exhaust stream having a mass flow; a nozzle downstream of the mixer section; a turbine downstream of the nozzle; and a pump driven by the turbine. The additional amount of said material is selected to produce a desired amount of mass flow.

Abstract: An anti-rotation device for a fastener, comprising: a first coupling for engaging a first fastener; a second coupling for engaging a feature located near the first fastener; and a flexible connection between the first and second couplings. The flexible connection limits rotation of the first coupling relative to the second coupling. The anti-rotation device could be part of a kit which also includes a holder. The holder comprises: a first opening for receiving the first coupling and a second opening for receiving the second coupling. The spacing between the first and second openings corresponds to the distance between the first and second fasteners. The anti-rotation device allows the operator to tighten or loosen a third fastener corresponding to said first fastener without manually engaging the first fastener.

Abstract: A gas generator, comprising a catalyst section and a mixer section. The catalyst section has openings through which a material enters and reacts with a catalyst to decompose and to produce heat. The mixer section, located downstream of the catalyst section, introduces an additional amount of the material. The heat produced in the catalyst section is sufficient to decompose the additional amount of material introduce into the mixer section without exposure to said catalyst. The catalyst bed assembly could be part of a turbopump assembly. A nozzle downstream of the mixer section directs the exhaust towards a turbine. The turbine drives a pump. The amount of material added to the mixer is selected to produce a desired amount mass flow through the nozzle. Adding material to the mixer causes the turbopump to supply more fuel or oxidizer to a rocket engine. Thus, the rocket engine is throttleable.

Abstract: The present invention relates to a gas turbine engine jet noise suppressor which does not appreciably adversely impact engine thrust and performance. The jet noise suppressor includes a nozzle, having an arrangement thereon of tabs disposed on the downstream end of the nozzle, the tabs having a length and the angular offset with respect to the engine flow such that mixing occurs primarily at the interface of the engine flow and the ambient air. In addition, various construction details are developed for the tabs including tabs that are trapezoidal with tapered sides such that the tabs minimize adverse impact to engine performance.

Abstract: According to the present invention, a brush seal is provided having a side plate, a back plate, and a bristle pack disposed between the side plate and the back plate. The side plate is in contact with an upstream surface of the bristle pack. The back plate is in contact with a downstream surface of the bristle pack. The back plate includes a plurality of apertures positioned to provide a gas path through the back plate for gas exiting the bristle pack. In some embodiments, the back plate further includes an exit channel disposed in the back plate surface contiguous with the bristle pack, aligned with the apertures. In some embodiments, the radial length of the side plate in contact with the bristle pack is less than the radial length of the back plate in contact with the bristle pack.

Abstract: A method for inhibiting radial transfer of core gas flow away from a center radial region and toward the inner and outer radial boundaries of a core gas flow path within a gas turbine engine is provided that includes the steps of: (1) providing a flow directing structure that includes an airfoil that abuts a wall surface, said airfoil having a leading edge, a pressure side, and a suction side; and (2) increasing the velocity of the core gas flow in the area where the leading edge of the airfoil abuts the wall. Increasing the velocity of the core gas flow in the area where the leading edge of the airfoil abuts the wall impedes the formation of a pressure gradient along the surface of the airfoil that forces core gas from the center region of the core gas toward the wall. The apparatus includes apparatus for diverting core gas flow away from the area where the airfoil abuts the wall.

Abstract: An automated method and apparatus for electrode discharge machining wherein method includes moving the tool holder to the electrode loader, automatically mounting an electrode into the tool holder and then testing the electrode for conformance to geometric and dimension tolerances and testing the electrode for proper alignment in the tool holder and thus proper alignment relative to the workpiece just prior to moving the tool holder to the workpiece area for machining. The apparatus includes a moveable servomechanism with a tool holder, an electrode magazine, and a sensor module for testing an electrode mounted in the tool holder. The sensor module has a recess configuration of conductive material complimentary to the electrode such that the electrode will make contact with the conductive material when inserted into the sensor module if the electrode is out of tolerance or misaligned in the tool holder.

Abstract: Hold-Down element (1) for holding, in a clamping manner, an electrical and/or electronic component, such as a connector, onto a substrate. The hold-down element (1) comprising a first part (2) for engaging the substrate and a second part (5) for engaging the component to be mounted. The first part (2) having an essentially flat, elongate shape provided with a member (7) which is offset with respect to the raised member (7), so that the first part (2), under the influence of a force exerted thereon during the insertion of the hold-down element (1) in a mounting opening, can diverge in the opposite direction to the raised member (7) and can engage, in a clamping manner, the substrate by means of the divergent portion in the mounting opening. The hold-down element (1) may also be used as the connecting end of a component.

Abstract: An electrical connector assembly, comprising: a housing with an interior section, a front and a rear; a plurality of first contacts, and a plurality of second contacts. The first contacts have mating sections extending into the interior section and directed towards the rear of the housing. The second contacts have mating sections extending into the interior section and directed towards the front of the housing. The second contacts occupy three of the eight positions in the housing. In a modular jack arrangement, the second contacts occupy positions 3 and 5, and either position 1 or position 7. Cross-talk between the contacts is thereby reduced.