Searching:
Search by keyword, patent number, inventor, assignee, city or state:
| Patent # | Description |
|---|---|
| 2011/0243768 |
MOTOR STATOR AND ROTARY COMPRESSOR According to one embodiment, a motor stator includes a substantially cylindrical stator iron core and insulators. The stator iron core includes a yoke, teeth,... |
| 2011/0243767 |
MOTOR-DRIVEN COMPRESSOR A motor-driven compressor is to be mounted to a first mounting of a vehicle. The compressor includes a compressor body that is electrically powered to draw in... |
| 2011/0243766 |
COMPRESSOR WITH TRANSMISSION A compressor includes a housing, a compression mechanism, an input shaft rotatable on an axis thereof, an output shaft for driving the compression mechanism, a... |
| 2011/0243765 |
MOTOR-DRIVEN COMPRESSOR The motor-driven compressor is mounted on a mounting of a vehicle. The motor-driven compressor includes a compressor body, a mounting, a damper and a fastener.... |
| 2011/0243764 |
MOTOR-DRIVEN COMPRESSOR The motor-driven compressor is mounted on a first mounting of a vehicle. The motor-driven compressor includes a compressor body, a second mounting, a first... |
| 2011/0243763 |
MOTOR-DRIVEN COMPRESSOR A motor-driven compressor is to be mounted to a first mounting of a vehicle. The compressor includes a housing having therein a compression mechanism that is... |
| 2011/0243762 |
MOTOR-DRIVEN CENTRIFUGAL COMPRESSOR A motor-driven centrifugal compressor includes a journal air bearing having a bump foil and a top foil for restraining a bearing shaft in a resting state and... |
| 2011/0243761 |
Pulsation Dampener for Gas Compressors Having Selectable Size Choke
Openings A gas flow pressure pulsation dampener includes a sealed housing having an inlet port, an outlet port a center section disposed between the inlet port and the... |
| 2011/0243760 |
Pressure Recovery Insert for Reciprocating Gas Compressor A method of reducing pulsations in a reciprocating compressor system, the system having nozzles between cylinders and filter bottles of the compressor system,... |
| 2011/0243759 |
CENTRIFUGAL PUMP APPARATUS A centrifugal blood pump apparatus includes an impeller provided in a blood chamber, a permanent magnet provided in one surface of the impeller, a permanent... |
| 2011/0243758 |
LIQUID RING PUMP WITH GAS SCAVENGE DEVICE A liquid ring pump having a channel including a first opening which opens into a first bucket formed by rotor blades. The first opening is located along an... |
| 2011/0243757 |
INVERTER CONTROL DEVICE FOR AC MOTOR AND ELECTRIC COMPRESSOR The present invention has an object to detect a three-phase AC motor current with high accuracy only with DC input current measuring means to a three-phase PWM... |
| 2011/0243756 |
METHOD FOR PRODUCING A BLADE BY CASTING AND BLADE FOR A GAS TURBINE A method is provided for producing a blade, by casting, for a gas turbine. The blade includes an elongate airfoil which extends in a blade longitudinal... |
| 2011/0243755 |
COOLED BLADE FOR A GAS TURBINE, METHOD FOR PRODUCING SUCH A BLADE, AND GAS
TURBINE HAVING SUCH A BLADE A blade for a gas turbine includes an airfoil extending in radial direction of the turbine or longitudinal direction of the blade, respectively, between a... |
| 2011/0243754 |
Pillow Block for Bed Plate of Wind Turbine A pillow block for a bed plate of a wind turbine is disclosed. In one embodiment, the pillow block includes a sleeve defining a generally horizontal centerline... |
| 2011/0243753 |
WIND TURBINE BLADE HAVING A FLOW GUIDING DEVICE WITH OPTIMISED HEIGHT A wind turbine blade with a flow guiding device attached to a profiled contour on a pressure side of the blade is described. The flow guiding device extends... |
| 2011/0243752 |
METHOD FOR MANUFACTURING A RECTIFIER The present invention relates to a method for manufacturing a turbine-engine composite rectifier comprising a ferrule provided with a plurality of stator vanes... |
| 2011/0243751 |
WIND TURBINE BLADES WITH A HARDENED SUBSTRATE CONSTRUCTION A wind turbine blade includes an upper shell member and a lower shell member joined at leading and trailing edges of the blade with a bond material. Portions of... |
| 2011/0243750 |
Wind Turbine Rotor Blade Components and Methods of Making Same Structural preform layers of multiple rigid unidirectional strength elements or rods are constructed and arranged for use in fabricating load-bearing support... |
| 2011/0243749 |
GAS TURBINE ENGINE WITH NON-AXISYMMETRIC SURFACE CONTOURED ROTOR BLADE
PLATFORM A rotor blade for a gas turbine engine includes a platform section between a root section and an airfoil section, the platform section having a non-axisymmetric... |
| 2011/0243748 |
HIGH PRESSURE TURBINE BLADE AIRFOIL PROFILE A two-stage high pressure turbine includes a second stage blade having an airfoil with a profile substantially in accordance with at least an intermediate... |
| 2011/0243747 |
HIGH PRESSURE TURBINE VANE AIRFOIL PROFILE A two-stage high pressure turbine includes a second stage vane having an airfoil with a profile substantially in accordance with at least an intermediate... |
| 2011/0243746 |
COMPOSITE TURBINE BUCKET ASSEMBLY A composite turbine blade assembly includes a ceramic blade including an airfoil portion, a shank portion and an attachment portion; and a transition assembly... |
| 2011/0243745 |
Structure for combining vane frame and vane of hanging fan A structure for combining a vane frame and a vane of a hanging fan includes an elastic plate onto the vane frame, a pressing portion at a front end of the... |
| 2011/0243744 |
SEAL FOR A PLATFORM IN THE ROTOR OF A TURBINE ENGINE A seal for an intermediate platform provided between two adjacent blades in the rotor of a turbine engine, the seal having an elongate shape with an upstream... |
| 2011/0243743 |
ATTACHMENT ASSEMBLIES BETWEEN TURBINE ROTOR DISCS AND METHODS OF ATTACHING
TURBINE ROTOR DISCS A method of attaching two rotor discs in a turbine engine, the method comprising the steps of: forming a first rotor disc that includes a first axial extension... |
| 2011/0243742 |
STATOR STAGE FOR TURBOMACHINE COMPRESSOR A turbomachine stator stage comprising two coaxial shrouds, respectively an inner shroud and an outer shroud with substantially radial vanes extending... |
| 2011/0243741 |
Lubrication System for a Bearing A lubrication system is provided for a bearing with a stationary inner ring and a rotating outer ring. The lubrication system includes a distribution ring... |
| 2011/0243740 |
Planetary Gear A planetary gear including a stationary ring gear, a rotatable planet carrier having an even number of at least four mirror-symmetrically arranged planet... |
| 2011/0243739 |
WINDMILL PITCH DRIVING APPARATUS A windmill pitch driving apparatus is provided, which is capable of achieving improved durability as well as improved output torque and reduced size. The... |
| 2011/0243738 |
WIND TURBINE AND A PITCH BEARING FOR A WIND TURBINE A wind turbine includes a rotor having a rotational axis and a wind turbine blade connected to a hub through a pitch bearing. The pitch bearing includes an... |
| 2011/0243737 |
METHOD AND SYSTEM FOR SECURING LIGHTING PROTECTION CABLES IN A WIND
TURBINE ROTOR BLADE A plurality of lightning receptors are configured along either or both of the suction side and pressure side shell members of a wind turbine blade. At least one... |
| 2011/0243736 |
JOINT SLEEVE FOR A ROTOR BLADE ASSEMBLY OF A WIND TURBINE A joint sleeve for assembling together a first blade section and a second blade section of a rotor blade assembly is disclosed. The joint sleeve may include an... |
| 2011/0243735 |
SYSTEM OF CONTRA-ROTATING PROPELLERS DRIVEN BY A PLANETARY GEAR TRAIN
PROVIDING A BALANCED DISTRIBUTION OF... A system of contra-rotating propellers for an aircraft turbomachine, including: a free power turbine including a first rotor; first and second propellers; and a... |
| 2011/0243734 |
LEAD STOP FOR ROTOR SYSTEM WITH FLUID-ELASTOMERIC LEAD/LAG DAMPER A rotor system includes a lead stop mounted to a spindle and a lead stop plate mounted to a rotor hub arm, the lead stop operable to contact the lead stop plate... |
| 2011/0243733 |
SUSPENSION TYPE SWING MECHANISM The present invention provides a suspension type swing mechanism, which comprises: a fastening base, the circumference thereof is radially pivoted with a... |
| 2011/0243732 |
PUMP IMPELLER A pump impeller has two impeller bodies attached to each other. Each impeller body has an annular base wall and multiple partition protrusions separately formed... |
| 2011/0243731 |
ELASTOMERIC BEARING SYSTEM MOTION LIMITER The invention relates to a backing plate used for an elastomeric bearing system, the backing plate comprising a plate which defines an at least partial annulus... |
| 2011/0243730 |
SYSTEMS AND METHODS FOR DETERMINING DEFLECTION OF A WIND TURBINE SHAFT A system and a method for measuring deflection of a shaft in a wind turbine and adjusting a pitch angle of a rotor blade in the wind turbine based on the... |
| 2011/0243729 |
DEVICE FOR ADJUSTMENT OF A ROTOR BLADE, WIND ENERGY CONVERTER, AND METHOD
FOR ADJUSTING A ROTOR BLADE Some general aspects of the invention provide a device (151, 152, 114) for adjustment of a pivotally mounted rotor blade (101) of a wind energy converter. The... |
| 2011/0243728 |
Blower designed for fitting particularly in a chamber furnace The blower designed particularly for fitting in a chamber furnace has the hub of the rotor wheel in the shape of a solid of revolution with its slant height... |
| 2011/0243727 |
STEAM TURBINE HALF SHELL JOINT ASSEMBLY A joint assembly for a steam turbine includes a threaded stud extending through mating openings in a first flange of the first half shell and in a second flange... |
| 2011/0243726 |
Canopy for a Wind Turbine Nacelle A canopy for a wind turbine nacelle is provided. The canopy includes a frame made of bars and covering plates. The frame is self supporting, the bars are made... |
| 2011/0243725 |
TURBINE SHROUD MOUNTING APPARATUS WITH ANTI-ROTATION FEATURE A turbine shroud mounting apparatus includes: (a) a shroud hanger having an arcuate body and including an arcuate first hook which protrudes radially inward and... |
| 2011/0243724 |
TURBINE AIRFOIL TO SHROUND ATTACHMENT A turbine airfoil (31) with an end portion (42) that tapers (44) toward the end (43) of the airfoil. A ridge (46) extends around the end portion. It has... |
| 2011/0243723 |
FAN GUARD A fan guard includes a bracket, a guide sheet and at least two guide ribs. The bracket defines a vent in the center of the bracket. The guide sheet is located... |
| 2011/0243722 |
ANTI-ROTATION SLOT FOR TURBINE VANE A fixed vane section for a gas turbine engine includes an anti-rotation slot that receives a pin for maintaining a desired position while providing for movement... |
| 2011/0243721 |
SIMPLIFIED VARIABLE GEOMETRY TURBOCHARGER WITH VANE RINGS The flow path of exhaust gas to the turbine wheel (70) of a turbocharger is influenced by relative motion between two rings of vanes, at least one of which... |
| 2011/0243720 |
High Efficiency Blower Housing with Unequal Size Inlet Openings An air handler blower assembly includes a blower housing containing a centrifugal fan and a motor mounted on the blower housing and connected to the fan. The... |
| 2011/0243719 |
NON-CIRCULAR AFT NACELLE COWLING GEOMETRY A nacelle for a turbofan propulsion system that extends along a centerline includes a forward cowling and an aft cowling. To improve the fit of a turbofan... |
Copyright 2008−2013 Patents.com
