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Match Document Document Title
US20150152785 AIR INTAKE HOOD FOR TURBINE INLET FILTER HOUSE  
An air intake hood for channeling an incoming air flow downward in a filter house. The intake hood includes an inlet that is inclined.
US20130305684 DEBRIS DISCOURAGER  
A debris discourager for a gas turbine engine is rotatable about an engine axis and extends between a fore end and an aft end. A portion of the debris discourager includes a non-uniform surface...
US20120023895 APPARATUS AND FILTERING SYSTEMS RELATING TO COMBUSTORS IN COMBUSTION TURBINE ENGINES  
A combustor for a combustion turbine engine, the combustor that includes: a chamber defined by an outer wall and forming a channel between windows defined through the outer wall toward a forward...
US20110138770 ANTI-ICING SYSTEM USING RADIANT INFRARED ENERGY FROM TURBINE EXHAUST FLUES  
An exhaust flue is provided for use with a gas turbine engine. The exhaust flue is oriented to channel exhaust gases from a core engine of the gas turbine engine. The exhaust flue includes a...
US20110173986 Adaptive Gas Turbine Vane Separator System and Method  
An adaptive vane separator system is provided for use with an inlet filter house of a gas turbine engine system. The vane separator system is coupled to the inlet filter house. The vane separator...
US20110047959 AIR PARTICLE SEPARATOR FOR A GAS TURBINE ENGINE  
An assembly for separating debris from a pressurization air flow adjacent to a bearing compartment seal includes a baffle and a capture annulus. The baffle is disposed in the pressurization air...
US20110277442 Seal for Gas Turbine Filter  
A turbine filter seal assembly may include a first mounting flange with a channel extending about a first air opening, a seal with an enlarged portion compressed into the channel, and a second...
US20150113938 WEATHER HOOD WATER REMOVAL SYSTEM AND METHOD FOR ASSEMBLY  
An air intake system for use with a gas turbine is provided. The air intake system includes a weather hood coupled to a filter house. The air intake system also includes a prefilter assembly...
US20110146294 AIRPLANE ENGINE DEFLECTOR SYSTEMS  
A protective deflector for airplane engines system is disclosed herein comprising a turbine-covering screen assembly which may be installed to an airplane engine turbine housing by a securable...
US20100313542 JET ENGINE SCREEN  
The present invention relates to a jet screen designed to protect a jet engine comprising: a conical shaped perimeter; a concaved metal grid within the perimeter; and a plurality of bolts, said...
US20110179763 Particle separator and debris control system  
A gas turbine engine system includes an air inlet, an inlet particle separator located at the air inlet and having a blower selectively driven by a variable output motor, and a controller for...
US20090266048 Turbine Air-Intake Filter  
A turbine air-intake filter for removal of particles from an air stream entering a gas turbine comprises a composite filter media (10) being made from a membrane filtration layer (20) comprising a...
US20080141649 SEGMENTED INERTIAL PARTICLE SEPARATORS AND METHODS OF ASSEMBLING TURBINE ENGINES  
A method for assembling a turbine engine including a compressor is disclosed. The method includes coupling an inlet including an inertial particle separator (IPS) and a first surface that is...
US20090145101 PARTICLE SEPARATOR FOR TIP TURBINE ENGINE  
A particle separator (20) for a tip turbine engine (10) includes a generally conical inclined leading surface (24) leading to a maximum radius (25) and a tapered trailing surface (56) having a...
US20140077039 Heated Screen For Air Intake Of Aircraft Engines  
An aircraft includes a fuselage and wings mounted on opposite sides of the fuselage for sustained forward flight. An engine is mounted in the fuselage or at least one of the wings and includes an...
US20080072606 Adaptive inertial particle separators and methods of use  
A method for operating a gas turbine engine including a compressor is provided. The method includes defining a predetermined concentration, placing at least one sensor in an inlet of the gas...
US20080310951 TURBINE COOLING AIR CENTRIFUGAL PARTICLE SEPARATOR  
A centrifugal particle separator (202) is provided for removing particles such as dust particles from the compressed airflow (110) prior to reaching and cooling the turbine blades (122, 124, 126)...
US20120000176 FOG AND MIST CATCHING APPARATUS  
An apparatus is provided and includes an inlet, including a peripheral wall formed to define a pathway along which gaseous, fluidic and particulate matter flow and two or more nets sequentially...
US20090320441 INFLATABLE SEAL ASSEMBLY BETWEEN AN ENGINE INLET AND A VEHICLE  
An inflatable sealing assembly for sealing between an intake section of a turbine engine and an air inlet ring of a vehicle. The inflatable sealing assembly including a seal holder coupled to the...
US20090302150 TUBULAR AIR TRANSPORT VEHICLE  
An air transport vehicle of the present invention comprises a tubular body, said body comprising an upper half and a lower half. The upper half is positioned above the lower half and connected...
US20120125009 AIRCRAFT SAFETY DEVICE SYSTEMS  
An aircraft system comprising a deflector assembly including, a base having mounting apertures; an inner ring concentrically positioned within an outer ring, the inner ring and the outer ring have...
US20070119146 Retarding and filter cleaning method and system  
A filter cleaning system is provided for a gas turbine engine including a compressor section and a combustor section. A mechanism is operatively connected to the gas turbine engine and is...
US20090139200 TURBOENGINE AIR INTAKE PROVIDED WITH A CONTROLLED FILTER SYSTEM  
An air intake (2) for a turbine engine, and a method implemented by the air intake (2) are disclosed. The air intake (2) is provided with a filter system (10) including foldable filter elements...
US20140123621 ACTUATED BYPASS HOOD FOR GAS TURBINE AIR INLET SYSTEM AND METHODS  
An inlet hood for use with a gas turbine or compressor air inlet system includes a frame and at least one pre-filter pivotably held by the frame in an operating position. The pre-filter is...
US20090126337 RETROFIT DIRT SEPARATOR FOR GAS TURBINE ENGINE  
A dirt separator may be retrofit into existing gas turbine engines since it is formed of circumferentially separate pieces which may be assembled together in the gas turbine engine.
US20100162682 INLET PARTICLE SEPARATOR SYSTEM FOR A GAS TURBINE ENGINE  
Embodiments include an inlet particle separator system for a gas turbine engine. The inlet particle separator system includes an inertial particle separator that separates incoming air into a...
US20090044512 DIRT SEPARATOR FOR COMPRESSOR DIFFUSER IN GAS TURBINE ENGINE  
A compressor diffuser for a gas turbine engine is provided with a dirt separator. The dirt separator ensures the air having moved downstream of the compressor section, and moving toward the...
US20140260183 VARIABLE CYCLE INTAKE FOR REVERSE CORE ENGINE  
A gas generator for a reverse core engine propulsion system has a variable cycle intake for the gas generator, which variable cycle intake includes a duct system. The duct system is configured for...
US20120131900 INLET PARTICLE SEPARATOR SYSTEM  
An inlet particle separator system is provided. The system includes an axial flow separator for separating air from an engine inlet into a first flow of substantially contaminated air and a second...
US20110016845 AIRCRAFT ENGINE PROTECTION DEVICE  
A jet engine intake guard includes an engine sleeve located within the nacelle of the engine; a primary deflection screen located at a front portion of the sleeve and having a first circular frame...
US20130000271 ENGINE SHIELD  
One example embodiment includes an engine shield for protecting a jet engine intake. The engine shield includes a base, a first support and a second support. The first and second supports include...
US20110001003 FILTERING DEVICE WITH INTEGRATED BYPASS FOR AN AIR INLET  
A filtering device for an engine or a for power unit with a radial air intake, includes a ring-shaped filter for covering the radial air intake, characterised in that the ring-shaped filter...
US20120124961 Filter Cartridge Assembly For Use With Turbine Engine Systems  
A filter cartridge assembly includes a first filter including a first cavity defined therein and a second filter coupled to the first filter. The second filter includes a second cavity defined...
US20110277441 METHOD AND APPARATUS FOR AN AIR FILTER CARTRIDGE REPLACEMENT ASSEMBLY  
A method of assembling a filter replacement assembly for use with a gas turbine engine. The method includes coupling a first container to a filter wall that is included in an inlet air treatment...
US20150159560 SYSTEM AND METHOD FOR EXTRACTING FOREIGN MATTER IN GAS TURBINE  
A system for extracting foreign matter in a gas turbine is provided. The system includes a variable bleed valve (VBV) disposed between a booster and a high pressure compressor configured to bleed...
US20100326040 Bird and debris guand for a jet engine  
This guard can be built of this wire material and put in frame so that it fits In the air intake of the jet engine to stop any bird or a piece of debris being sucked in. This would include not...
US20090255230 GAS TURBINE  
A gas turbine having air cooling is provided with an effective measure for cleaning cooling air which is used in the turbine, which measure is particularly efficient. In order to allow...
US20130104518 Bird deflector and air replacement system  
A bird deflector and air replacement system for a jet engine, the bird deflector being conical or arcuate in shape as formed by suitable longitudinal and lateral interconnected bars, and the air...
US20120216505 AIRCRAFT  
A bird knocking-off rod of a bird knocking-off device is disposed outside a jet engine, in front of an air inlet of the jet engine and capable of rotating with a rotation area that is larger than...
US20110185700 Jet engine bird diverters  
This invention is a series of Jet engine bird diverters designed to attach to the side(s) of the jet engines and the leading edge of the jet engine housing or become an integral part of the...
US20150219010 FILTERING CHAMBER AND METHOD FOR MAINTAINING SAME  
A filtering chamber for a gas turbine having a combustor, compressor and air inlet duct, and a corresponding maintenance method is described. The filtering chamber includes a first chamber in an...
US20130213003 RETRACTABLE BIRD AND DEBRIS DEFLECTOR FOR AN AIRCRAFT JET ENGINE  
A retractable deflector to deflect birds and debris from an air intake duct of an aircraft jet engine. The duct has a forward opening for air receipt. The deflector includes a plurality of...
US20110000184 Method to protect jet engines from bird strikes  
The method of preventing the dangers of birds entering the jet engines of an airplane during take-off and landing by rotating a portion of the jet engines cowling to a blocking position in front...
US20150040535 INLET PARTICLE SEPARATOR SYSTEM WITH HUB AND/OR SHROUD SUCTION  
An inlet particle separator system for a vehicle engine includes a hub section, a shroud section, a splitter, and a hub suction flow passage. The shroud section surrounds at least a portion of the...
US20110011055 Jet engine air intake guard  
A jet engine air intake guard takes the circumstance into consideration to protect a jet-engine air intake structure from being damaged by birds or any other foreign objects, including meteoritic...
US20110238380 System And Method For Preventing Objects From Entering The Intake Of A Jet Engine  
A system for preventing objects from entering the intake of a jet engine including a deflector mounted to the turbine shaft and including a de-icing device to minimize collection of ice on the...
US20100180566 BIRD AND DEBRIS DEFLECTOR FOR AIRCRAFT JET ENGINES  
A retractable deflector serves to deflect birds and debris from an air intake duct of an aircraft jet engine. The intake duct has a central longitudinal axis and a forward opening for the receipt...
US20110030333 JET ENGINE PROTECTION SYSTEM  
A modern jet engine inlet protection system that protects against large birds and operates autonomously, that is dormant in routine aircraft operations, that automatically actuates its protective...
US20100287908 Jet engine shield and debris deflector  
A jet engine bird and debris shield device is disclosed that is designed as a deflector to deflect large birds, such as geese weighing in excess of eight pounds, and keep from entering the turbine...
US20130047622 PULSE FILTRATION APPARATUS  
A pulse filtration apparatus of a power plant including an air separation unit (ASU) and a gas turbine engine is provided. The apparatus includes a conduit to transmit fluid from the ASU to a...

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