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| Patent # | Description |
|---|---|
| 2016/0201507 |
ENGINE COMPONENT FOR A GAS TURBINE ENGINE An engine component for a gas turbine engine includes a film-cooled wall having a hot surface facing hot combustion gas and a cooling surface facing a cooling... |
| 2016/0201506 |
TURBINE EXHAUST CYLINDER/ TURBINE EXHAUST MANIFOLD BOLTED STIFFENING RIBS Disclosed are a casing arrangement and a method to reduce vibrations in a gas turbine casing. The casing arrangement includes a turbine exhaust cylinder... |
| 2016/0201505 |
Fan Cases and Manufacture Methods A turbine engine fan case (48) comprises a composite body member (300) circumscribing an axis (500) and having an annular mounting portion (310, 410), a... |
| 2016/0201504 |
UNISON RING SELF-CENTRALIZERS AND METHOD OF CENTRALIZING A centralizing assembly for an engine having a plurality or rotatable vanes is provided including an engine casing and at least one unison ring disposed... |
| 2016/0201503 |
FRANGIBLE AIRFOIL A frangible airfoil that mitigates adverse conditions associated with release of material resulting from impact damage to the composite blade is provided, the... |
| 2016/0201502 |
INTEGRAL PART WEAR INDICATOR SYSTEM, METHOD AND APPARATUS A part comprising a one or more removable wear indicators is provided. The part may be a stator segment comprising a plurality of airfoils. The stator segment... |
| 2016/0201501 |
METHOD FOR TESTING AN OVERSPEED PROTECTION APPARATUS OF A SINGLE-SHAFT
SYSTEM A method for testing an overspeed protection apparatus of a single-shaft system that includes: a) operating the system at nominal speed and under electrical... |
| 2016/0201500 |
METHOD FOR OPERATING A STEAM TURBINE WITH TWO STEAM SUPPLY LINES A steam turbine arrangement and a method for operating a steam turbine, wherein the steam turbine is supplied with steam via a first valve in a first steam... |
| 2016/0201499 |
VANE ARM ASSEMBLY An assembly for operating a device, such as a variable vane, has an arm, a stem to which the arm is connected, the stem having a slot, and a member having a... |
| 2016/0201498 |
SEAL COATING A method of forming a coating includes disposing a substrate having a plurality of protrusions on a seal and layering a topcoat over the protrusions. The... |
| 2016/0201497 |
GAS TURBINE AND MOUNTING METHOD An insert element fastens to an annular segment body of a turbine of a gas turbine. The annular segment body has a recess on a hot-gas side. The insert element... |
| 2016/0201496 |
GAS TURBINE AND MOUNTING METHOD A gas turbine includes an insert element for fastening to a ring segment body of a turbine of the gas turbine. The ring segment body has a recess on a hot gas... |
| 2016/0201495 |
GAS TURBINE AND MOUNTING METHOD A gas turbine includes a turbine having a rotor blade row and a ring that is arranged around the rotor blade row and is made up of multiple ring segments. An... |
| 2016/0201494 |
SLIDING SEAL The present disclosure relates generally to a sliding seal between two components. The sliding seal includes a carrier having one or more cavities formed... |
| 2016/0201493 |
BIFURCATED SLIDING SEAL The present disclosure relates generally to a sliding seal between two components. The sliding seal includes a first seal section and an uncoupled second seal... |
| 2016/0201492 |
TANGENTIAL ON-BOARD INJECTION VANES A tangential on-board injection (TOBI) system for gas turbine engines includes a first endwall and a second endwall radially spaced apart from the first... |
| 2016/0201491 |
VARIABLE AREA TURBINE ARRANGEMENT WITH SECONDARY FLOW MODULATION A variable area turbine arrangement according to an exemplary aspect of the present disclosure includes, among other things, a variable vane assembly and a... |
| 2016/0201490 |
MULTI-FUNCTION BOSS FOR A TURBINE EXHAUST CASE A turbine exhaust case frame (100) comprises an inner ring (104), an outer ring (102), and a plurality of load-bearing struts (106). The inner ring is... |
| 2016/0201489 |
CRIMPED INSERT FOR IMPROVED TURBINE VANE INTERNAL COOLING An insert tube of a turbine vane is disclosed. The insert tube includes a pressure side wall, a suction side wall opposite and spaced apart from the pressure... |
| 2016/0201488 |
VANE ASSEMBLY WITH TRAPPED SEGMENTED VANE STRUCTURES A vane assembly includes inner and outer rings, a plurality of segmented vane structures circumferentially-spaced around a central axis and between the inner... |
| 2016/0201487 |
SLIDING BAFFLE INSERTS A vane includes a vane body extending from a root to an opposed tip along a longitudinal axis and first and second baffle bodies. The vane body defines a... |
| 2016/0201486 |
Extruded profile for manufacturing a blade of an outlet guide vane An extruded profile for manufacturing a blade of an outlet guide vane of a turbine engine. A cross-sectional area has an axial length LAX and a thickness D/LAX... |
| 2016/0201485 |
Support Buttress An airfoil of a turbine engine may have internal passages to permit the travel of cooling air through the airfoil. Multiple airfoils may be formed together in... |
| 2016/0201484 |
TURBINE WHEEL WITH CLAMPED BLADE ATTACHMENT A turbine wheel for use in a gas turbine engine having a plurality of blades attached to a rotor disk. Each blade is formed from a composite comprising ceramic... |
| 2016/0201483 |
TURBINE WHEEL WITH CLAMPED BLADE ATTACHMENT A turbine wheel for use in a gas turbine engine having a plurality of blades attached to a rotor disk. Each blade is formed from a composite comprising ceramic... |
| 2016/0201482 |
ALUMINUM AIRFOIL WITH TITANIUM COATING An airfoil includes an aluminum airfoil body with a pressure side, suction side, leading edge and trailing edge; and a titanium foil layer covering at least... |
| 2016/0201481 |
METHOD OF FABRICATING A REINFORCING EDGE FOR A BLADE AND REINFORCING EDGE
OBTAINED BY THE METHOD A method of fabricating a reinforcing edge (10') of a turbine engine blade (70) in which there is provided a blank (10) of the reinforcing edge and an... |
| 2016/0201480 |
AIRFOIL WITH AN INTEGRALLY STIFFENED COMPOSITE COVER An airfoil according to an exemplary aspect of the present disclosure includes, among other things, a main body extending between a leading edge and a trailing... |
| 2016/0201479 |
CMC AIRFOIL WITH MONOLITHIC CERAMIC CORE An airfoil includes a core having a first surface, a skin having a second surface disposed over at least a portion of the first surface of the core, and at... |
| 2016/0201478 |
BRAIDED BLADES AND VANES HAVING DOVETAIL ROOTS A gas turbine engine composite article having a composite article airfoil extending outwardly to an article root to an article airfoil tip. Within the article... |
| 2016/0201477 |
GAS TURBINE ENGINE AIRFOIL CROSSOVER AND PEDESTAL RIB COOLING ARRANGEMENT A gas turbine engine component includes spaced apart walls that provide a cooling passage that extends in a first direction. A cross-over rib joins the walls... |
| 2016/0201476 |
AIRFOIL FOR A TURBINE ENGINE An airfoil for a turbine engine includes a cooling cavity and a cooling fluid supply cavity which supplies cooling fluid to the cooling cavity through a... |
| 2016/0201475 |
COOLING FOR GAS TURBINE ENGINE COMPONENTS A gas turbine engine component includes a body with a wall surrounding an interior cavity. The wall has opposed interior and exterior surfaces. The interior... |
| 2016/0201474 |
GAS TURBINE ENGINE COMPONENT WITH FILM COOLING HOLE FEATURE A gas turbine engine component includes a wall that provides an exterior surface and an interior flow path surface. A film cooling hole extends through the... |
| 2016/0201473 |
TURBINE BLADE HAVING FILM COOLING HOLE ARRANGEMENT A turbine blade includes a platform that has a platform leading edge and trailing edge joined by two platform circumferential sides. An airfoil extends... |
| 2016/0201472 |
VANE, GAS TURBINE PROVIDED WITH THE SAME, METHOD OF MANUFACTURING VANE,
AND METHOD OF REMODELING VANE A retainer that protrudes from an inner shroud of a vane to a radially inner side and extends in a circumferential direction is formed with an opening that... |
| 2016/0201471 |
FAN BLADE ASSEMBLY The present disclosure relates generally to a fan blade assembly. In an embodiment, the fan blade assembly includes an airfoil having a forward edge covered by... |
| 2016/0201470 |
INTEGRALLY BLADED ROTOR HAVING AXIAL ARM AND POCKET An integrally bladed rotor includes a monolithic rotor body that has a bore portion, a rim, and a web that joins the bore portion and the rim. A plurality of... |
| 2016/0201469 |
MATEFACE SURFACES HAVING A GEOMETRY ON TURBOMACHINERY HARDWARE Turbomachinery hardware, used in a rotor assembly and a stator assembly, including an airfoil portion including a leading edge, a trailing edge, a pressure... |
| 2016/0201468 |
TURBINE AIRFOIL The present invention is an aerodynamically efficient turbine airfoil that includes a first endwall, a second endwall, a stacking axis, an aspect ratio, a... |
| 2016/0201467 |
BLADE OUTER AIR SEAL WITH COOLING HOLES A blade outer air seal (BOAS) for a turbomachine can include a BOAS body including a plurality of cooling holes defined in substantial conformance with a set... |
| 2016/0201466 |
COATING POCKET STRESS REDUCTION FOR ROTOR DISK OF A GAS TURBINE ENGINE A rotor is provided for a gas turbine engine. The rotor includes a rim that extends transverse to the web. The rim has a rotor spacer arm which defines a... |
| 2016/0201465 |
TURBINE ROTOR MATERIAL FOR GEOTHERMAL POWER GENERATION AND METHOD FOR
PRODUCING THE SAME A turbine rotor material for geothermal power generation containing C: 0.20 to 0.30 mass %, Si: 0.01 to 0.2 mass %, Mn: 0.5 to 1.5 mass %, Cr: 2.0 to 3.5 mass... |
| 2016/0201464 |
INTAKE/OUTLET PIPE OPTIMIZATION METHOD FOR ROTARY ENGINE An intake/outlet pipe optimization method includes the steps of providing a rotary engine, measuring the pressure in an operation of the engine, designing the... |
| 2016/0201463 |
FLUID DEVICE OUTPUT SHAFT WITH COATING A fluid device includes a housing defining a central bore, a plurality of commutator holes that extend radially outward from the central bore and a plurality... |
| 2016/0201462 |
Non-Coaxial Multi-Axial Rotating Mechanism A mechanism whereby fluid can be pumped by the addition of mechanical power to a shaft, or conversely, shaft power may be extracted from a fluid by forcing a... |
| 2016/0201461 |
Piston Unit and Hydrostatic Radial-Piston Machine A piston unit includes a piston which has a rolling element seat configured to rotatably support a rolling element. The rolling element seat has a bearing... |
| 2016/0201460 |
AN ARTIFICIAL DAM OF DISTRIBUTED COAL MINE UNDERGROUND RESERVOIR AND ITS
CONSTRUCTING METHOD The present disclosure provides an artificial dam of a distributed coal mine underground reservoir and its constructing method. The artificial dam comprises a... |
| 2016/0201459 |
MOBILE CONVEYOR DEVICE FOR THE DELIVERY OF TUNNEL LINERS A system for folding and deploying liners within tunnels includes a mobile conveyor device having a base frame including a plurality of wheels supporting a... |
| 2016/0201458 |
PLATFORM DEVICE FOR SAMPLING AND CHEMICAL REACTION SPECTROPHOTOMETRY OF
DRILLING FLUID A spectrometric analysis system for use with a drilling and production system including a first inlet configured to receive an aliquot of downhole drilling... |
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