Abstract:
A gas turbine engine includes a flex mount for a fan drive gear system. A very high speed fan drive turbine drives the fan drive gear system.
Abstract:
A gas turbine engine includes a flex mount for a Fan Drive Gear System defined by a lateral and transverse stiffness relationship. Epicyclic gearboxes with planetary or star gear trains may be used in gas turbine engines for their compact designs and efficient high gear reduction capabilities. Planetary and star gear trains generally include three gear train elements: a central sun gear, an outer ring gear with internal gear teeth, and a plurality of planet gears supported by a planet carrier between and in meshed engagement with both the sun gear and the ring gear.
Abstract:
A gas turbine engine includes a shaft defining an axis of rotation. An outer turbine rotor directly drives the shaft and includes an outer set of blades. An inner turbine rotor has an inner set of blades interspersed with the outer set of blades. The inner turbine rotor is configured to rotate in an opposite direction about the axis of rotation from the outer turbine rotor. A splitter gear system couples the inner turbine rotor to the shaft and is configured to rotate the inner set of blades at a faster speed than the outer set of blades.
Abstract:
Un cojinete de fricción (44) que comprende:un cuerpo central (57) que se extiende axialmente adaptado para ser soportado en cada extremo exterior; unprimer pasaje (54) que se extiende en general axialmente a través de una porción del cuerpo central (57); unfiltro (58) dispuesto en comunicación con el primer pasaje (54) y configurado para atrapar residuos de unlíquido lubricante que fluye a través de él; y un segundo pasaje (60) en comunicación de fluido con el primerpasaje (54) y el filtro (58) y una superficie exterior del cuerpo central (57) para permitir el suministro del líquidolubricante filtrado a él;caracterizado por:un pasador de alineación (52) que fija el cojinete de fricción (44) con respecto a un soporte (48) y conello alinea angularmente el segundo pasaje en una posición predeterminada con respecto a unengranaje de estrella (38), un engranaje anular (40) y un engranaje solar (42) y con respecto a unacarga de cojinete aplicada para asegurar la distribución adecuada de la película lubricante a lo largo dela superficie exterior del cuerpo central (57) en uso.
Abstract:
A coupling system for connecting a sun gear to a shaft within a planetary gear train, includes a sun gear coupling connecting the sun gear to the shaf t. The sun gear coupling has at least one undulant flexible section joined to a n inflexible spindle for accommodating misalignment between the sun gear and the shaft. The flexible section comprises a cylindrical ring having a diamet er greater than the diameter of the spindle, and joined to the spindle by two longitudinally spaced apart diaphragms. The juncture between the diaphragms, the ring, and the spindle is curved in cross section on an outer side to improve flexibility and minimize stress concentrations, and the inner sides of the diaphragms are straight edges which result in a non-symmetric contour of the diaphragm walls.
Abstract:
A gearbox assembly for a gas turbofan engine includes a sun gear rotatable about an axis and a plurality of intermediate gears driven by the sun gear. A baffle disposed between at least two of the plurality of intermediate gears includes a first gap distance within a first gap portion and a second gap distance within a second gap portion. The first gap portion is disposed between the baffle and one of the intermediate gears away from the meshed interface with the sun gear and the second gap portion is disposed near the interface with the sun gear. The first gap distance within the first gap portion is different than the second gap distance within the second gap portion to define a desired lubricant flow path.
Abstract:
An example epicyclic gear train assembly includes a flexure pin received by a carrier. The flexure pin and the carrier respectively include first and second pin apertures configured to receive a retainer pin. The flexure pin further includes a lubricant conduit separate from the first pin aperture.
Abstract:
A gas turbine engine includes a fan and a compressor. A combustor drives a turbine, including a first turbine with a shaft to drive the compressor. A fan drive turbine drives the fan through a speed reduction. A sensor senses a speed of rotation of the fan and communicates sensed speed information to a control. The control develops an expected speed for the fan. A problem is identified should the sensed speed be less than the expected speed by more than a predetermined amount. A method is also described.