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Solar Turbines Incorporated patents


Recent patent applications related to Solar Turbines Incorporated. Solar Turbines Incorporated is listed as an Agent/Assignee. Note: Solar Turbines Incorporated may have other listings under different names/spellings. We're not affiliated with Solar Turbines Incorporated, we're just tracking patents.

ARCHIVE: New 2018 2017 2016 2015 2014 2013 2012 2011 2010 2009 | Company Directory "S" | Solar Turbines Incorporated-related inventors


 new patent  Injector head with a resonator for a gas turbine engine

A fuel injector for a combustor of a gas turbine engine is disclosed herein. In embodiments, the fuel injector includes an injector head adjoining a stem. ... Solar Turbines Incorporated

 new patent  Start biased liquid fuel manifold for a gas turbine engine

A fuel distribution manifold for a gas turbine engine is disclosed herein. The fuel distribution manifold includes a manifold body, a stage divider, and a plurality of manifold outlet ports. ... Solar Turbines Incorporated

 new patent  Ventilation panel with panel silencer for a turbine package enclosure

A ventilation panel for an enclosure of an industrial machine is disclosed herein. In embodiments, the ventilation panel includes a panel silencer and a fire damper assembly. ... Solar Turbines Incorporated

Flanged component for a gas turbine engine

A flanged component for a gas turbine engine is disclosed herein. The flanged component includes a flange body with a flange mating surface and a plurality of threaded features. ... Solar Turbines Incorporated

Swirl brakes for compressors with teeth-on-rotor seals

A device and method for reducing swirl in a gas compressors is provided. The device can include a tubular or annular seal body having an abradable interior surface for use in forming a seal. ... Solar Turbines Incorporated

Injector resonator for a gas turbine engine

A fuel injector for a combustor of a gas turbine engine is disclosed herein. In embodiments, the fuel injector includes an injector head, a stem, a fuel passage, a fitting, a fuel inlet, and a resonator. ... Solar Turbines Incorporated

Sump tank for a gas turbine engine

A sump tank for use with a gas turbine engine in offshore conditions is disclosed. In embodiments, the sump tank includes two circuitous lubricant flow paths. ... Solar Turbines Incorporated

Modular testing fixture

A testing fixture for testing a component of an industrial machine is disclosed herein. The testing fixture includes a fixture block and a component interfacing fixture that fastens to the fixture block. ... Solar Turbines Incorporated

System and method for measuring bending mode frequencies

A system and method for controlling bending modes of a rotor assembly is disclosed. The rotor assembly can be supported by one or more bearings in an integrated machine. ... Solar Turbines Incorporated

Modular compression plant

A building structure for operating turbomachinery equipment is disclosed. The building structure includes a first pre-fabricated structure, a second pre-fabricated structure, and a connector attaching the first pre-fabricated substructure to the second pre-fabricated substructure. ... Solar Turbines Incorporated

Method for manufacturing compressor components

A method forming a metallic structure having two or more portions is provided. The method can include providing a first layer of metal-forming material and then applying energy of a first power level to a first area of the first layer of metal-forming material to form a first portion of the metallic structure having a first density. ... Solar Turbines Incorporated

Turbine assembly and method for flow control

A turbine assembly of an engine is disclosed. The turbine assembly includes a nozzle ring for receiving exhaust gases from a combustion chamber having a plurality of guide vanes for guiding the exhaust gases, a stator ring disposed downstream to the nozzle ring, and a rotor disposed circumferentially within the stator ring. ... Solar Turbines Incorporated

Method for improving turbine compressor performance

A method and device for retrofitting a gas turbine engine for improved hot day performance are disclosed. The method can include removing a first selected stator bladerow from the plurality of compressor stages, the first selected stator bladerow having a first inlet swirl angle and including a first plurality of fixed stator vanes. ... Solar Turbines Incorporated

Method for determining vibratory contact stress at a blade attachment

A modal analysis is performed on a blade and disk assembly of a turbomachine, including creating a finite element model of the blade and disk assembly made up of a plurality of nodes corresponding to points on the blade and disk assembly and characterized by a simplifying assumption of a rigidly attached connection between the blade and disk. The modal analysis also includes selecting a target vibration frequency at which a target amplitude of vibration has been one of measured or estimated for a target node during operation, and deriving modal velocity vectors from the target amplitude at the target node. ... Solar Turbines Incorporated

10/12/17 / #20170292386

Wrapped serpentine passages for turbine blade cooling

A turbine blade for a gas turbine engine may include at least two wrapped, serpentine-shaped internal cooling paths. A first one of the serpentine-shaped internal cooling paths may include a first passage that extends radially along a leading edge of the turbine blade from adjacent a root end of the turbine blade to adjacent a tip end of the turbine blade. ... Solar Turbines Incorporated

10/12/17 / #20170292385

Rotation enhanced turbine blade cooling

A turbine blade for a gas turbine engine may include an outer, peripheral wall extending along a suction side and a pressure side of the blade from a leading edge to a trailing edge of the blade and from a root end to a tip end of the blade, a substantially vertical bifurcating internal wall extending between the leading edge and the trailing edge of the blade in between the suction side and the pressure side of the blade, a plurality of pressure side cooling fluid passages defined between the peripheral wall on the pressure side of the blade and the bifurcating internal wall and extending at least part way from the root end to the tip end of the blade, and a plurality of suction side cooling fluid passages defined between the peripheral wall on the suction side of the blade and the bifurcating internal wall and extending at least part way from the tip end to the root end of the blade. At least one of the pressure side cooling fluid passages may receive fresh cooling fluid from a cooling fluid inlet opening at the root end of the blade and direct the cooling fluid radially upwardly toward the tip end of the blade, across a top side of the bifurcating internal wall, and down through at least one of the plurality of suction side cooling fluid passages.. ... Solar Turbines Incorporated

09/28/17 / #20170276367

Fuel supply system for an engine

A fuel supply system for a combustion chamber having at least two combustion zones in which each combustion zone is arranged at a height different from the other includes a pair of fuel injectors that are configured to supply fuel to respective ones of the combustion zones. The pair of fuel injectors are disposed at different heights corresponding to the different heights of the combustion zones, each of the heights being taken in reference with one of a lower one of the fuel injectors and a horizontal midplane of the combustion chamber. ... Solar Turbines Incorporated

09/28/17 / #20170275190

System using heat energy to produce power and pure water

A system may be configured to use heat energy to produce power and potable water. The system may include an organic rankine cycle (orc) subsystem configured to receive heat energy from one or more sources and convert that heat energy into usable power. ... Solar Turbines Incorporated

08/31/17 / #20170248022

Airfoil for turbomachine and airfoil cooling method

An airfoil for a turbomachine such as a gas turbine engine includes a pressure side and a suction side, a flow-distributing forward wall and an inner cooling wall. A switchbacked passage extends through the airfoil, and the flow-distributing forward wall has a plurality of jetting orifices formed therein and connecting the switchbacked passage to a forward cavity. ... Solar Turbines Incorporated

08/24/17 / #20170241294

Exhaust system for gas turbine engine

An exhaust system for a gas turbine engine is provided. The exhaust system includes an exhaust diffuser having a diffuser axis. ... Solar Turbines Incorporated

08/24/17 / #20170241270

Airfoil for turbomachine and method of cooling same

An airfoil for a turbomachine such as a gas turbine engine includes a switchbacked passage for conveying cooling fluid, and flow-distribution passages in a forward wall so as to direct cooling fluid from the internal passage for back side impingement upon a leading edge of the airfoil. An inner cooling wall forms a passage for discharging the spent cooling air from a trailing edge of the airfoil after impingement, and cools one of a pressure side and a suction side of the airfoil by way of conduction. ... Solar Turbines Incorporated

08/17/17 / #20170234320

Real time rotation breakaway detection

A system and method for detecting the rotation breakaway of a spacer from a compressor rotor disk are disclosed herein. The method includes detecting a disk sensed feature and a spacer sensed feature on the compressor rotor disk and the spacer respectively. ... Solar Turbines Incorporated

08/10/17 / #20170227224

Fuel injector for combustion engine system, and engine operating method

A fuel injector for a combustion engine includes an injector body having formed therein a first passage structured to feed a fuel to an outlet of the injector body, and a second passage structured to feed air to the outlet of the injector body. Flow-directing surfaces are exposed to a flow of fuel through the first passage to induce swirl, and a flow segregator is positioned between the flows of fuel and air such that the air shrouds the swirling flow of fuel and inhibits migration of fuel radially outwardly from the fuel injector outlet.. ... Solar Turbines Incorporated

07/06/17 / #20170191667

Fuel injector with dual main fuel injection

A fuel injector for a gas turbine engine is disclosed. The fuel injector includes two primary tubes, a secondary tube, a primary gas gallery, and a secondary gas gallery. ... Solar Turbines Incorporated

07/06/17 / #20170191457

Fuel injector with a center body assembly for liquid prefilm injection

A center body assembly for a fuel injector is disclosed. The center body assembly defines a primary liquid passage, a liquid gallery, swirl slots, and a prefilm passage. ... Solar Turbines Incorporated

07/06/17 / #20170191428

Two stream liquid fuel lean direct injection

A method for lean direct injection of a liquid fuel from a fuel injector into a combustion chamber of a gas turbine engine is disclosed. The method includes injecting all of the liquid fuel into the combustion chamber through a pilot liquid fuel circuit during light off and during acceleration towards idle. ... Solar Turbines Incorporated

07/06/17 / #20170191421

Fuel injector with multi tube gas distribution

A fuel injector for a gas turbine engine is disclosed. The fuel injector includes a flange assembly with a distribution block, three main gas tubes, and an injector head. ... Solar Turbines Incorporated

02/09/17 / #20170039836

Monitoring system for a gas turbine engine

A method of monitoring a plurality of turbomachines is disclosed herein. In embodiments, the method includes a fleet data system receiving first event data from a first monitoring connection system and second event data from a second monitoring connection system. ... Solar Turbines Incorporated

02/09/17 / #20170038277

Monitoring system for a gas turbine engine

A system for monitoring a plurality of turbomachinery systems is disclosed herein. In embodiments, the system includes a monitoring system data provider, a plurality of monitoring system servers, and a monitoring device. ... Solar Turbines Incorporated

02/09/17 / #20170038276

Monitoring system for turbomachinery

A system for monitoring a plurality of turbomachinery systems is disclosed herein. In embodiments, the system includes a network remote management tools module, and a plurality of monitoring devices. ... Solar Turbines Incorporated

02/09/17 / #20170038275

Monitoring system for turbomachinery

A method of monitoring a gas turbine engine is disclosed herein. The method includes periodically receiving sensor data for the gas turbine engine at a monitoring device from a monitoring system server. ... Solar Turbines Incorporated

02/09/17 / #20170037742

Monitoring system for turbomachinery

A method of monitoring a plurality of turbomachines is disclosed herein. The method includes a fleet data system periodically receiving first event data from a first monitoring connection system and second event data from a second monitoring connection system. ... Solar Turbines Incorporated








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