9988910 | Staggered core printout | Jan 30, 15 | Jun 05, 18 | United Technologies Corporation |
9982629 | cycle with independent shafts for combustion cycle elements and propulsion elements | Jun 17, 16 | May 29, 18 | Rolls-Royce Corporation; Rolls-Royce North American Technologies Inc.; |
9976480 | Fluid intake system | Dec 11, 14 | May 22, 18 | SNECMA |
9976448 | Regenerative thermodynamic power generation cycle systems, and methods for operating thereof | May 29, 15 | May 22, 18 | General Electric Company |
9970360 | Gas turbine engine configured to shape power output | Jan 31, 13 | May 15, 18 | SIEMENS AKTIENGESELLSCHAFT |
9964034 | Methods for producing a fuel gas stream | Mar 27, 15 | May 08, 18 | ExxonMobil Upstream Research Company |
9964038 | Supersonic caret inlet system leading edge slat for improved inlet performance at off-design flight conditions | Mar 16, 15 | May 08, 18 | The Boeing Company |
9963241 | Airplane with a fuel cell device | Oct 29, 14 | May 08, 18 | Airbus Defence and Space GmbH |
9964307 | Interface heat shield for a combustor of a gas turbine engine | Sep 30, 13 | May 08, 18 | United Technologies Corporation |
9964309 | Gas turbine engine combustor with CMC heat shield and methods therefor | Dec 22, 14 | May 08, 18 | General Electric Company |
9957897 | Gimbal tube systems for tangential onboard injectors | Mar 19, 15 | May 01, 18 | United Technologies Corporation |
9957918 | Gas turbine engine front architecture | Aug 28, 07 | May 01, 18 | United Technologies Corporation |
9957893 | Combustor and gas turbine provided with same | Mar 14, 12 | May 01, 18 | MITSUBISHI HITACHI POWER SYSTEMS, LTD. |
9951721 | Three-stream gas turbine engine architecture | Oct 21, 14 | Apr 24, 18 | United Technologies Corporation |
9945249 | Ventilation of a piece of electronic equipment of a turbomachine | Jul 31, 14 | Apr 17, 18 | SNECMA |
9938895 | Dual reheat topping cycle for improved energy efficiency for compressed air energy storage plants with high air storage pressure | Nov 13, 13 | Apr 10, 18 | Dresser-Rand Company |
9938898 | Geared turbofan bearing arrangement | Jul 29, 11 | Apr 10, 18 | United Technologies Corporation |
9927125 | Two-circuit injector for a turbine engine combustion chamber | Sep 23, 13 | Mar 27, 18 | Turbomeca |
9927124 | Fuel nozzle for axially staged fuel injection | Mar 26, 15 | Mar 27, 18 | ANSALDO ENERGIA SWITZERLAND AG |
9915200 | System and method for controlling the combustion process in a gas turbine operating with exhaust gas recirculation | Jan 19, 15 | Mar 13, 18 | ExxonMobil Upstream Research Company, GENERAL ELECTRIC COMPANY, |