144080 ⎘
Axial-flow pumps Multi-stage pumps
Sub-classes:HIGH TEMPERATURE GAS COMPRESSOR, SYSTEMS, AND METHODS THEREOF
#2ROTARY MACHINE WITH ROTATABLE HOLLOW SHAFT
#3FORWARD LOAD REDUCTION STRUCTURES FOR AFT-MOST STAGES OF HIGH PRESSURE COMPRESSORS
#4COMPRESSOR SHROUD WITH SWEPT GROOVES
#5BLOWER
#6FLEXIBLE SUPPORT STRUCTURE FOR A GEARED ARCHITECTURE GAS TURBINE ENGINE
#7Forward load reduction structures for aft-most stages of high pressure compressors
#8TANDEM BLADE ROTOR DISK
#9ARRANGEMENT FOR PRESSURIZING OF FLUID
#10Blower
#11DEVICE FOR ACCELERATING REACTION OF SUBSTANCE TO BE STIRRED
#12Inner blade support ring of a turbomachine compressor stator
#13FAN
#14ROTOR AND COMPRESSOR
#15Compressor for an engine
#16Compressor control device, control method for compressor, and control program product for compressor
#17Gas turbine engine with third stream
#18Gas turbine engine with third stream
#19COMPRESSOR SHROUD WITH SWEPT GROOVES
#20Tandem blade rotor disk
#21HIGH AND LOW SPOOL CONFIGURATION FOR A GAS TURBINE ENGINE
#22ROTATING BLADE FOR A TURBOMACHINE
#23EXPANDABLE IMPELLER PUMP
#24Embedded electric machine
#25Thrust efficient gas turbine engine
#26Motor-integrated fluid machine and vertical takeoff and landing aircraft
#27Repeating airfoil tip strong pressure profile
#28Waste heat recovery system
#29Tandem blade rotor disk
#30Turbine section of gas turbine engine
#31Refrigeration system mixed-flow compressor
#32Multi-stage turbomolecular pump
#33Flexible support structure for a geared architecture gas turbine engine
#34Balancing and sealing piston, and associated cooling circuit and method
#35Reverse flow engine architecture
#36FLEXIBLE SUPPORT STRUCTURE FOR A GEARED ARCHITECTURE GAS TURBINE ENGINE
#37Turbine section of high bypass turbofan
#38Turbine section of high bypass turbofan
#39VARIABLE-CYCLE COMPRESSOR WITH A SPLITTERED ROTOR
#40Expandable impeller pump
#41Expandable impeller pump
#42Axi-centrifugal compressor with variable outlet guide vanes
#43Turbine section of high bypass turbofan
#44System and method of reducing post-shutdown engine temperatures
#45Tandem blade rotor disk
#46Variable speed boost compressor for gas turbine engine cooling air supply
#47Gas turbine engine compressors having optimized stall enhancement feature configurations and methods for the production thereof
#48Flexible support structure for a geared architecture gas turbine engine
#49Flexible support structure for a geared architecture gas turbine engine
#50CONCENTRIC TURBINE CONDENSING CYCLE
#51Thrust efficient turbofan engine
#52Tandem rotor blades
#53Downhole blower system with pin bearing
#54Gas turbine engine airfoil
#55Refrigerant compressor
#56Multiphase pump
#57BLEED TUBES
#58Reverse flow engine architecture
#59Signal processing for variable geometry mechanism control
#60Airfoil shape for first stage compressor stator vane
#61Downhole blower system with a passive magnetic radial bearing assembly
#62TURBINE BLADES AND VANES FOR GAS TURBINE ENGINE
#63Fan bypass and shutoff check valve
#64Flexible support structure for a geared architecture gas turbine engine
#65Flexible support structure for a geared architecture gas turbine engine
#66High pressure compressor for an engine
#67Aircraft environmental control system
#68Axial fan blower
#69Gas turbine engine vane end devices
#70Gas turbine engine with ultra high pressure compressor
#71Gas turbine engine compressor
#72Folded heat exchanger for cooled cooling air
#73Embedded electric machine
#74System and method for assembling gas turbine rotor using localized inductive heating
#75MULTISTAGE RADIAL COMPRESSOR AND TURBINE
#76Gas turbine engines and compression systems therefor
#77Expandable impeller pump
#78HIGH PRESSURE COMPRESSOR DIFFUSER FOR AN INDUSTRIAL GAS TURBINE ENGINE
#79Gas turbine engine with high speed low pressure turbine section and bearing support features
#80Fan
#81Multistage axial compressor and gas turbine
#82Compressor system with a gas temperature control at the inlet of the anti-surge line and relevant method
#83Compressor rotor disk for gas turbine
#84Compressor rotor, compressor and gas turbine
#85Axial flow compressor for HVAC chiller systems
#86Turbine section of high bypass turbofan
#87Integrated modular, multi-stage motor-pump/compressor device
#88Supply duct of a compressor of a turbine engine
#89Turbine section of high bypass turbofan
#90Turbine section of high bypass turbofan
#91TANDEM BLADE ROTOR DISK
#92AXI-CENTRIFUGAL COMPRESSOR
#93Gas turbine with a radial-to-axial intake, variable-angle inlet guide vane therefore, and method of operation
#94Pin to reduce relative rotational movement of disk and spacer of turbine engine
#95Intake structure of compressor
#96Gas turbine engine
#97Fan bypass and shutoff check valve
#98Systems and methods for compressor anomaly prediction
#99Compressor arrangement and gas turbine engine
#100Clipped heat shield assembly
#101Twin spool industrial gas turbine engine low pressure compressor with diffuser
#102Turbomachine and method of operating a turbomachine
#103Compressor blade locking mechanism in disk with axial groove
#104TURBINE ENGINE WITH AN EXTENSION INTO A BUFFER CAVITY
#105Vibration damper structure and series fan thereof
#106Gas turbine engine compressors having optimized stall enhancement feature configurations and methods for the production thereof
#107Last turbine rotor disk for a gas turbine, rotor for a gas turbine comprising such last turbine rotor disk and gas turbine comprising such rotor
#108Downhole blower system with bearings and seals
#109Downhole blower system with pin bearing
#110Duct blocker seal assembly for a gas turbine engine
#111High flow low pressure rotary device for gas flow in subatmospheric wells
#112Downhole blower system with passive radial bearings
#113Well optimization using downhole blower system
#114Integrated control of downhole and surface blower systems
#115Reverse flow engine architecture
#116Waste heat recovery system
#117Gas turbine engine vane end devices
#118Multi-stage impeller produced via additive manufacturing
#119Fully integrated hybrid electric jet engine
#120Airfoil shape for twelfth stage compressor stator vane
#121Airfoil shape for sixth stage compressor stator vane
#122Method and apparatus for compressor system pressurization
#123FLEXIBLE SUPPORT STRUCTURE FOR A GEARED ARCHITECTURE GAS TURBINE ENGINE
#124FLEXIBLE SUPPORT STRUCTURE FOR A GEARED ARCHITECTURE GAS TURBINE ENGINE
#125AXIAL FAN BLOWER
#126Embedded electric machine
#127Full-span forward swept airfoils for gas turbine engines
#128Assembly having two compressors, method for retrofitting
#129FLEXIBLE SUPPORT STRUCTURE FOR A GEARED ARCHITECTURE GAS TURBINE ENGINE
#130Repeating airfoil tip strong pressure profile
#131Gas turbine manufacturing method
#132Supplemental cooling air for turbine exhaust components and surfaces
#133Airfoil retention assembly for a gas turbine engine
#134Compressor rotor, compressor, and gas turbine
#135Variable speed boost compressor for gas turbine engine cooling air supply
#136Embedded electric machine
#137Method for improving turbine compressor performance
#138VARIABLE-CYCLE COMPRESSOR WITH A SPLITTERED ROTOR
#139STATIC HUB TRANSITION DUCT
#140Compressor rotor airfoil
#141Intercooling for an axial compressor with radially outer annulus
#142Air injection for an axial compressor with radially outer annulus
#143Method and system for metallic low pressure fan case heating
#144Axial flow compressor assembly
#145Axial compressor with radially outer annulus
#146Multi-stage compressor with multiple bleed plenums
#147Clutch mechanism and method for controlling fan speed
#148Compression system for a turbine engine
#149Refrigerant compressing process with cooled motor
#150FLEXIBLE SUPPORT STRUCTURE FOR A GEARED ARCHITECTURE GAS TURBINE ENGINE
#151Turbine shroud with full hoop ceramic matrix composite blade track and seal system
#152Flexible support structure for a geared architecture gas turbine engine
#153AIRFLOW MANIPULATION DEVICE FOR COMPRESSOR
#154Diffuser of a thermal energy machine and thermal energy machine
#155Thrust efficient turbofan engine
#156TURBINE SECTION OF HIGH BYPASS TURBOFAN
#157Solar chemically recuperated gas turbine system
#158Gas turbine engine with high speed low pressure turbine section and bearing support features
#159Machine train for producing nitric acid
#160Rotor, axial compressor, installation method
#161Method and apparatus for active clearance control
#162Firewall mount hub
#163Axi-centrifugal compressor with variable outlet guide vanes
#164Gas turbine engine with high speed low pressure turbine section and bearing support features
#165Controlled convergence compressor flowpath for a gas turbine engine
#166Turbine rotor blade row, turbine stage, and axial-flow turbine
#167Multi-stage compression system, control device, control method, and program
#168Multi-stage compressor system, control device, malfunction determination method, and program
#169Integrated rotor for an electrical machine and compressor
#170System and method of a fan
#171Low noise compressor rotor for geared turbofan engine
#172System and method of reducing post-shutdown engine temperatures
#173Compressor and method for mounting of a compressor
#174GAS TURBINE ENGINE AIRFOIL
#175GAS TURBINE ENGINE AIRFOIL
#176Gas turbine engine airfoil
#177METHOD AND SYSTEM FOR VARYING TIP CLEARANCE GAP USING AN ACTUATED SHROUD
#178Thrust efficient turbofan engine
#179Thrust efficient turbofan engine
#180AXIAL FLOW DEVICE AND JET ENGINE
#181METHOD AND SYSTEM FOR STALL MARGIN MODULATION AS A FUNCTION OF ENGINE HEALTH
#182FLEXIBLE SUPPORT STRUCTURE FOR A GEARED ARCHITECTURE GAS TURBINE ENGINE
#183VERTICAL TAKE-OFF AND LANDING AIRCRAFT
#184Method for pressure and temperature control of a fluid in a series of cryogenic compressors
#185Multistage turbomachine with embedded electric motors
#186INTERCOOLING SYSTEM AND METHOD FOR A GAS TURBINE ENGINE
#187Method for controlling the speed of cryogenic compressors arranged in series for cooling cryogenic helium
#188Method, compressor and turbomachine
#189Rotor for gas turbine engine
#190Multistage compressor with aerofoil portion profiled in a spanwise direction
#191FLOW GUIDING DEVICE AND TURBO-ENGINE WITH AT LEAST ONE FLOW GUIDING DEVICE
#192Compressor stator vane, axial flow compressor, and gas turbine
#193GEAR SYSTEM ARCHITECTURE FOR GAS TURBINE ENGINE
#194Gear system architecture for gas turbine engine
#195Turbine section of high bypass turbofan
#196Turbine section of high bypass turbofan
#197Folded heat exchanger for cooled cooling air
#198Axial flow compressor, gas turbine including the same, and stator blade of axial flow compressor
#199Patch ring for a compressor
#200Cooling system for a turbine engine
#201Rotor structure for rotating machinery and method of assembly thereof
#202Turbocharger systems with direct turbine interfaces
#203COOLED COMPRESSOR
#204Radial tie-bolt support spring
#205Rotor disk having a centripetal air collection device, compressor comprising said disc and turbomachine with such a compressor
#206Composite splitter lip for axial turbomachine compressor
#207VSV actuation arrangement
#208PUMP, COOLING APPARATUS AND ELECTRONIC DEVICE
#209Article of manufacture for turbomachine
#210Multi coordinate reference system for positioning bladed drum
#211Compression Apparatus
#212Balance piston for multiphase fluid processing
#213Partial-load operation of a gas turbine with an adjustable bypass flow channel
#214Multi-stage co-rotating variable pitch fan
#215Systems and methods for axial compressor with secondary flow
#216Fan module
#217Gas turbine engine compressors having optimized stall enhancement feature configurations and methods for the production thereof
#218Gas turbine axial compressor
#219Thrust efficient turbofan engine
#220COMPRESSOR AREA SPLITS FOR GEARED TURBOFAN
#221Axial compressor rotor incorporating non-axisymmetric hub flowpath and splittered blades
#222Housing device for a compressor stage of a compressor device that is embodied with multiple stages and method for manufacturing a housing device
#223Split axial-centrifugal compressor
#224Multi-stage-type compressor and gas turbine equipped therewith
#225Centrifugal compressor apparatus
#226LOW PRESSURE RATIO FAN ENGINE HAVING A DIMENSIONAL RELATIONSHIP BETWEEN INLET AND FAN SIZE
#227Tandem rotor blades
#228ELECTROMAGNETIC SHAFT-WHEEL COUPLING FOR ARBITRARY DISTRIBUTION OF SHAFT TORQUE IN A TURBINE ENGINE
#229Fluid flow apparatus, fan assembly and associated method
#230System and method for sidestream mixing
#231Compressor airfoil
#232Compressor rotor airfoil
#233AXIAL COMPRESSOR WITH TANDEM BLADES
#234Shaft seal system and a compressor having a corresponding shaft seal system
#235Flexible support structure for a geared architecture gas turbine engine
#236MULTI-STAGE AXIAL COMPRESSOR ARRANGEMENT
#237Methods and systems for antisurge control of turbo compressors with side stream
#238Method and apparatus for controlling a compressor of a gas turbine engine
#239TURBOMACHINE HAVING A TEMPERATURE-CONTROLLED COVER
#240Gas takeoff isolation system
#241Process gas compressor/gas turbine section
#242Method for inspecting a turbine engine rotor with a thru bolt threads inspection apparatus
#243Method of assembling a serial fan
#244Sealing arrangement for fuel cell compressor
#245INTEGRALLY GEARED COMPRESSOR WITH ADJUSTABLE INTERMEDIATE GEARWHEEL
#246Method and system for the rapid inflation of sealed air devices
#247Blade for axial compressor rotor
#248Variable geometry exhaust turbocharger
#249Air pump capable of automatic air supplements
#250Composite Housing with a Metallic Flange for the Compressor of an Axial Turbomachine
#251Air compressor with audible alarm device
#252Expandable impeller pump
#253Exhaust-gas turbocharger
#254Variable geometry lift fan mechanism
#255Bundle guiding device of compressor and bundle guiding method of compressor
#256Gas turbine engine vane end devices
#257METHOD FOR OPERATING A MULTISTAGE COMPRESSOR
#258Duct blocker seal assembly for a gas turbine engine
#259Multi-stage axial compressor with counter-rotation using accessory drive
#260Axial turbine
#261Drainage pump device for washing machine and washing machine therewith
#262High pressure compressor thermal management
#263Compression system
#264Blast shield for high pressure compressor
#265Split intermediate case
#266COMPRESSING SYSTEM
#267Method and guide for removing an inner casing from a turbomachine
#268ARTICLE OF MANUFACTURE FOR TURBOMACHINE
#269Spool for turbo machinery
#270COMPRESSOR CASE OVERHAUL
#271Gas turbine engine compressor stator seal
#272Axial compressor and control method thereof to stabilize fluid
#273Compressor and method of assembling the same
#274Turbomachine rotor with blade roots with adjusting protrusions
#275Axial flow compressor
#276Axial flow compressor
#277Stall detection in fans utilizing frequency converter
#278Vacuum pumping system having an ejector and check valve
#279Compressor arrangement
#280System and method of assembling a supersonic compressor system including a supersonic compressor rotor and a compressor assembly
#281Expandable impeller pump
#282Method for operating a multistage compressor
#283Fan assembly
#284STARTER/GENERATOR INTEGRATED INTO COMPRESSOR OF TURBINE ENGINE
#285High-pressure compression unit for process fluids for industrial plant and a related method of operation
#286Inlet connecting piece for an axial-flow compressor
#287Variable pressure ratio compressor
#288METHOD OF FABRICATING A TURBOMACHINE COMPRESSOR DRUM
#289Casing for a fluid flow machine
#290TURBINE AIRFOIL CLOCKING
#291Rotating unit for an axial-flow compressor
#292Expandable impeller pump
#293Compressor
#294SERIAL FAN MODULE AND FRAME STRUCTURE THEREOF
#295Modular air compression apparatus with separate platform arrangement
#296Method for modifying a multistage compressor
#297Multiple Fans of Cascade Connection
#298Axial flow supercharger and fluid compression machine
#299Expandable impeller pump
#300Aircraft engine with separate auxiliary rotor and fan rotor