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US20150167468 LOW-PRESSURE TURBINE  
A double-flow low-pressure partial turbine is provided herein, wherein the exhaust steam of the first flow and the exhaust steam of the second flow are deflected in a common direction within the...
US20130302158 EXHAUST-GAS TURBOCHARGER  
An exhaust-gas turbocharger (1) having a turbine housing (2), and having an exhaust manifold (3) connected to the turbine housing (2). At least one adapter ring (4, 5) is arranged between the...
US20140112771 FAN ASSEMBLING STRUCTURE AND HEAT DISSIPATING DEVICE  
The invention provides a fan assembling structure and a heat dissipating device. The fan assembling structure comprises a first assembling board for assembling a fan thereon and a second...
US20130272870 MICA-BASED SEALS FOR GAS TURBINE SHROUD RETAINING CLIP  
A gas turbine, a gas turbine shroud, and a method for sealing a gas turbine shroud with a non-metallic seal are provided. The gas turbine shroud includes an inner shroud and an outer shroud. A...
US20130209250 TRANSITION PIECE SEAL ASSEMBLY FOR A TURBOMACHINE  
A transition piece seal assembly includes a first seal, and a second seal joined to the first seal. The second seal being spaced from the first seal to define a coolant passage.
US20140119910 TURBINE EXHAUST HOOD AND RELATED METHOD  
A turbine exhaust hood and related method of installation is disclosed. In one embodiment, the turbine exhaust hood includes: a housing having an end wall, the end wall including a first portion...
US20120027580 FAN MODULE AND FAN RAIL THEREOF  
A fan module and a fan rail thereof are provided. The fan module includes a fan, two fan rails and a holder. The fan rails are respectively disposed at opposite sides of the fan, and each of the...
US20140079545 FAN ASSEMBLING STRUCTURE AND FAN DEVICE HAVING THE SAME  
The disclosure provides a fan assembling structure and a fan device having the same. The fan comprises a frame having an upper board, a lower board and a circular connector, and blades disposed in...
US20130287565 TEC Mount Redundant Fastening  
A mounting apparatus for a turbine exhaust case (TEC) is provided. The mounting apparatus may include a neck, support links and a plurality of fastening pins. The neck may include an upper portion...
US20110189037 Pump Assembly For Evaporative Cooler  
A pump assembly for circulating water in an evaporative cooler is provided. The pump assembly may include a housing which defines a cavity. The pump assembly may also include an impeller received...
US20150167586 ASSEMBLY FOR HOLDING THE INTERFACE OF A FRONT FRAME OF A NACELLE AND A TURBOJET ENGINE CASING  
The present disclosure relates to a holding assembly to hold a front frame of a thrust reverser to a turbojet engine casing. The assembly includes at least one connecting flange connecting the...
US20120219415 METALLIC ANNULAR CONNECTION STRUCTURE FOR AIRCRAFT TURBOMACHINE  
A metallic annular connection structure between two parts for an aircraft turbomachine, with an arbitrary half-section including two primary branches and a base forming a first U opening up in the...
US20140140839 TURBINE CASING WITH SERVICE WEDGE  
A turbine casing is provided and includes first and second turbine casing shells configured to be removably coupled to one another. At least one of the first and second turbine casing shells is...
US20150167498 JOINT BETWEEN COMPONENTS  
A joint assembly between a first gas turbine engine casing and a second gas turbine casing, the first gas turbine engine casing having a plurality of circumferentially spaced attachment points and...
US20150098816 SYSTEM AND METHOD FOR CONTROLLING BACKBONE BENDING IN A GAS TURBINE ENGINE  
A flexible coupling for a gas turbine engine includes a fan hub frame having a first flange and a core engine having a second flange. The first flange includes a first plurality of fingers...
US20150204348 FAN HOUSING WITH ENCIRCLING RINGS  
The invention discloses a fan housing with encircling rings, comprising a front housing and a rear housing, wherein the front and rear housings are respectively provided with a circular encircling...
US20120148392 COMPOSITE FAN CONTAINMENT CASE ASSEMBLY  
A fan case for a gas turbine engine includes a composite fan containment case having an outer surface, a front and a rear. An attachment flange and a mounting ring are respectively provided on the...
US20140147270 Aircraft Nacelle Comprising A Reinforced Connection Between An Air Intake And A Means Of Propulsion  
An aircraft nacelle includes an air intake, connected to a means of propulsion, which defines a longitudinal direction, an outer wall, an inner duct including an annular flange connected, by means...
US20110070080 FIXING APPARATUS FOR FAN  
A fixing apparatus includes two receiving boxes, and a plurality of elastic members. The receiving boxes are covered to each other, to receive a fan. The plurality of elastic members is...
US20140064957 GAS TURBINE FAN CASING HAVING A BELT FOR FASTENING EQUIPMENT  
The invention relates to a gas turbine fan casing (10) comprising an annular casing wall (12) centered on a longitudinal axis (X-X) of the casing and at least one fastening belt (100) mounted on...
US20100329837 SYSTEM AND METHOD FOR ALIGNING TURBINE COMPONENTS  
Embodiments include a system having a turbine support key having a set of key segments selectively stackable together in a plurality of combinations to adjust a thickness between turbine supports...
US20130309085 COMPRESSOR CASE OVERHAUL  
A longitudinally-split compressor case of a gas turbine engine is overhauled to inhibit leakage between case segments that have been distorted. Grooves are machined in mating surfaces of the case...
US20110014038 WIND TURBINE WITH SKELETON-AND-SKIN STRUCTURE  
A wind turbine comprises a turbine shroud and optionally an ejector shroud. The turbine shroud and/or the ejector shroud include a skeleton support structure, with a skin covering at least a...
US20130202430 GAS TURBINE ENGINE FAN CASING HAVING A FLANGE FOR FASTENING PIECES OF EQUIPMENT  
The invention provides a fan casing for a gas turbine engine, the casing having a substantially cylindrical portion that terminates at one end in an annular flange made of composite material. The...
US20150056070 MULTI SURFACE BLOCKER DOOR SYSTEM AND APPARATUS  
A multi-surface blocker door system for a thrust reverser of an aircraft is provided. The system may comprise one or more first blocker doors coupled to the inner fixed structure. The first...
US20140099198 DUCT ASSEMBLY  
A duct for a gas turbine engine system is used to convey exhaust gas and bypass air away from the engine system, towards an exhaust nozzle. The duct includes an inlet face having at least two...
US20140093371 MID-TURBINE FRAME HEAT SHIELD  
A heat shield for a mid-turbine frame has a conical body, including at least one axial retention feature, at least one circumferential retention feature, and at least one radial retention feature.
US20080063542 FAN FOR GENERATING AIR FLOW  
A fan for generating an air flow by rotating an impeller with a motor is provided. A cylindrical outer side surface of a rotor of the motor is press-fitted to an inner side surface of the impeller...
US20110158801 FAN FRAME AND HEAT DISSIPATION APPARATUS USING THE SAME  
A fan frame for a heat dissipation apparatus is provided. The fan frame includes an outer frame, an inner frame sleeved in the outer frame and slidable relative to the outer frame, a latching...
US20090232651 Inner Turbine Shell Support Configuration and Methods  
Embodiments of the present disclosure relate to a turbine which includes an outer shell, an inner shell connected to and surrounded by the outer shell in generally concentric relation therewith,...
US20120121408 TURBINE TRANSITION COMPONENT FORMED FROM A TWO SECTION, AIR-COOLED MULTI-LAYER OUTER PANEL FOR USE IN A GAS TURBINE ENGINE  
A cooling system for a transition duct for routing a gas flow from a combustor to the first stage of a turbine section in a combustion turbine engine is disclosed. The transition duct may have a...
US20150016989 AXIAL FLOW FAN  
An axial flow fan is provided. The axial flow fan includes an impeller and a fan frame. The impeller has a maximum outer diameter. The fan frame includes a first body and a second body. The first...
US20110250066 Peripheral Control Ejector  
A system for augmenting ducted fan thrust is provided, the system including a peripheral ejector comprised of inner and outer cowling members. With the addition of actuators mounted between the...
US20140255183 TWIST PREVENTION FOR TURBOMACHINERY  
A twist prevention system for turbomachinery is disclosed. The twist prevention system has a first ring segment pair with a first radially inner ring segment and a first radially outer ring...
US20080159860 CONNECTING SYSTEM  
This invention relates to a system for connecting two ferrules of an axial compressor case. A ferrule comprises a female flange, while the other ferrule comprises a male flange. Both the female...
US20090123279 CONNECTION OF RADIAL ARMS TO A CIRCULAR SLEEVE VIA AXES AND SPACERS  
The connection assembly of an arm (10) to a sleeve (11) is carried out substantially by parts of axes (21) crossing the arm and the spacers (26) between the parts of axes and the sleeve and the...
US20140199167 COMPRESSOR HOUSING FOR AN AIR CYCLE MACHINE  
A compressor housing for an air cycle machine is provided. The compressor housing includes a body having a compressor volute configured to provide centrifugal compression in the air cycle machine....
US20150219246 Polymeric or Composite Interlocking Mount Assembly for Cable Harnesses and Fluid Tubes  
A kit for building a mount assembly for securing a tubular member to a support structure of a gas turbine engine is described. The kit may comprise a base unit including a bottom surface...
US20150176603 FAN ASSEMBLY  
A fan assembly in which all of the major structural components of the assembly are mechanically fastened together by non-welding means, such as mechanical fasteners, is disclosed. The disclosure...
US20140044538 CLAMPING RING FOR A TURBOMACHINE  
A turbomachine having a flow channel (6) and a housing (1, 2) which radially surrounds the flow channel, at least one sealing or lining element (11) being situated between the flow channel and the...
US20080226447 Removable Impeller for Fan  
The invention concerns a removable impeller (7) designed to be integrated in a fan (1), in particular for controlled mechanical ventilation, and configured in the shape of a wheel provided with a...
US20090060734 Blower housing of hydrogen recirculation device of fuel cell vehicle  
A blower housing of a hydrogen recirculation device for a fuel cell vehicle includes a plurality of cooling pins installed on a perimeter of a housing body installed in a fuel processing system of...
US20110070079 ANNULAR SEAL  
An annular seal positionable in a gap is disclosed herein. The annular seal includes a plurality of leaves positioned about a center axis. Each leaf extends to a distal end that is elastically...
US20080187438 AIR FLOW CHANNEL STRUCTURE FOR AIR COMPRESSOR  
An air flow channel structure for an air compressor is disclosed. The air flow channel structure comprises a shell and four flow channel sections, in which one of the flow channel sections is not...
US20150211550 VERTICAL PUMP HAVING DISCHARGE HEAD WITH FLEXIBLE ELEMENT  
A discharge head features at least one low-deflection component that substantially does not deflect in response to high piping forces applied in a direction perpendicular to the discharge head; at...
US20130129501 STUD RETENTION  
A gas turbine engine having two components attached together via a stud retention arrangement. The stud retention arrangement includes a stud having a shaft and an integral collar that is located...
US20080159858 SYSTEM FOR CONNECTING TWO SUBSTANTIALLY TUBULAR MEMBERS, A CASE COMPRISING SUCH A SYSTEM AND USE THEREOF  
A system for connecting two substantially tubular members, in particular ferrules of an axial compressor case, comprising two flanges, each comprising a proximal face and a distal face and...
US20080014085 Fan housing and wire clipping mechanism thereof  
A fan housing includes a first frame and a second frame. The first frame includes a clip member protruding toward the second frame, and a limit member connected with the clip member. The limit...
US20140133977 DEVICE FOR CONNECTING A FRONT FRAME TO A FAN CASING  
A device for connecting a front frame of a turbojet engine nacelle to a fan casing includes a locking pin connected to a first assembly flange and a retaining flange that is movably mounted and...
US20110158802 SHEAR RING CASING COUPLER DEVICE  
A coupler device is for connecting first and second casings to form a casing assembly with a central axis, each casing having an inner end disposed against the inner end of the other casing such...
Matches 1 - 50 out of 237 1 2 3 4 5 >