Patent application number | Description | Published |
20120321453 | NON-MECHANICALLY FASTENED TOBI HEAT SHIELD - A high pressure turbine includes a stator, a rotor, a tangential on-board injector, and a heat shield. The rotor is located downstream of the stator and the tangential on-board injector directs cooling air to the rotor. The heat shield is retained by abutment with the stator and the tangential on-board injector. | 12-20-2012 |
20130000324 | INTEGRATED CASE AND STATOR - A gas turbine engine includes a compressor, a combustor section, and a turbine. The turbine includes an integrated case/stator segment that is comprised of a ceramic matrix composite material. | 01-03-2013 |
20130004314 | RADIAL SPLINE ARRANGEMENT FOR LPT VANE CLUSTERS - A full hoop stator vane cluster includes an inner hoop and an outer hoop both being substantially cylindrical and coaxial. A plurality of airfoils extend radially between the hoops, and a plurality of vane splines extend radially outward from the outer hoop for attaching the vane cluster to a gas turbine engine. | 01-03-2013 |
20130232768 | TURBINE ENGINE CASE MOUNT AND DISMOUNT - A method for mounting a gas turbine engine having a compressor section, a combustor section, a turbine section, a pylon and a rear mount bracket, includes positioning the mounting bracket between the gas turbine engine and the pylon. The mounting bracket is connected to the turbine case reacting a least a vertical load, a side load, a thrust load, and a torque load from the gas turbine engine through the mounting bracket. The mounting bracket is attached to the pylon reacting the same loads from the gas turbine engine. | 09-12-2013 |
20130233997 | TURBINE ENGINE CASE MOUNT - A mount for a turbine engine has a semi-circular yoke with a first leg and a second leg. The mount also has a stanchion with a cylindrical section attached to the yoke, and a conical section attached to the cylindrical section. A mounting bracket is attached to the conical section. | 09-12-2013 |