145530 ⎘
Function; Heat transfer, e.g. cooling; Improvement of heat transfer by increasing the heat transfer surface using fins or ribs
Combined acoustic absorber and heat exchanging outlet guide vanes
#602Crossflow turbine airfoil
#603HEAT EXCHANGER TUBE AND AIR-TO-AIR INTERCOOLER
#604Serpentine cooling circuit and method for cooling tip shroud
#605Turbine blade with multiple impingement cooled passages
#606Blade for a gas turbine
#607Blades for gas turbine engines
#608Turbine casing with false flange
#609TURBINE BLADE TIP SHROUD
#610Turbine blade tip shroud
#611Protection device for a turbine stator
#612Cooling structure
#613Turbulated aft-end liner assembly and cooling method
#614Advanced turbulator arrangements for microcircuits
#615Turbine airfoil concave cooling passage using dual-swirl flow mechanism and method
#616Cooling circuit flow path for a turbine section airfoil
#617Multi-pass cooling for turbine airfoils
#618Wavy flow cooling concept for turbine airfoils
#619Nozzles for use with gasifiers and methods of assembling the same
#620Cooled component
#621Angled tripped airfoil peanut cavity
#622TURBINE BLADE WITH INTERNAL COOLING STRUCTURE
#623Cooled turbine blade for a gas turbine and use of such a turbine blade
#624Method and system for cooling fluid in a turbine engine
#625Domed tip cap and related method
#626Near wall cooling for a highly tapered turbine blade
#627Airfoil for a turbine of a gas turbine engine
#628Vane wheel of turbine comprising a vane and at least one cooling channel
#629Damper configured turbine blade
#630Local indented trailing edge heat transfer devices
#631Ceramic matrix composite vane with chordwise stiffener
#632Aerofoil configuration
#633Airfoil, sleeve, and method for assembling a combustor assembly
#634Turbine blade trip strip orientation
#635Method for preventing backflow and forming a cooling layer in an airfoil
#636Airfoil cooling with staggered refractory metal core microcircuits
#637Externally mounted vortex generators for flow duct passage
#638Turbine blade for a gas turbine
#639Turbine airfoil cooling system with spanwise equalizer rib
#640Turbine component with tip flagged pedestal cooling
#641Turbine airfoil cooling system with enhanced tip corner cooling channel
#642Hybrid vapor and film cooled turbine blade
#643High effectiveness cooled turbine blade
#644Turbine blade with split impingement rib
#645Heat transferring cooling features for an airfoil
#646Leading edge cooling using chevron trip strips
#647Leading edge cooling using wrapped staggered-chevron trip strips
#648Turbine airfoil with integral chordal support ribs
#649Gas turbine engine component suction side trailing edge cooling scheme
#650Turbine element
#651Manufacturable and inspectable microcircuits
#652Advanced turbulator arrangements for microcircuits
#653Fanned trailing edge teardrop array
#654Method to augment heat transfer using chamfered cylindrical depressions in cast internal cooling passages
#655Material having internal cooling passage and method for cooling material having internal cooling passage
#656Blade or vane for a turbomachine
#657Turbomachine blade with fluidically cooled shroud
#658Turbine blade with cooling and with improved service life
#659Central cooling circuit for a moving blade of a turbomachine
#660Cooling layout for a turbine blade, turbine blade included therein, turbine and aircraft engine equipped therewith
#661ASSEMBLY FOR CONTROLLING THERMAL STRESSES IN CERAMIC MATRIX COMPOSITE ARTICLES
#662Air deflector for a cooling circuit for a gas turbine blade
#663Manufacturable and inspectable microcircuit cooling for blades
#664Turbine blade including revised trailing edge cooling
#665Turbine bucket tip cap
#666Bipedal damper turbine blade
#667Turbine airfoil with integrated impingement and serpentine cooling circuit
#668Turbine airfoil trailing edge cooling system with segmented impingement ribs
#669Turbulator on the underside of a turbine blade tip turn and related method
#670Device for effecting heat transfer to rotating equipment, in particular gas turbines
#671Member having internal cooling passage
#672Airfoil trailing edge cooling
#673Turbine nozzle with trailing edge convection and film cooling
#674Turbine blade cooling system with bifurcated mid-chord cooling chamber
#675Turbine blade cooling system having multiple serpentine trailing edge cooling channels
#676Article having diffuser holes and method of making same
#677Turbine blade tip cooling system
#678Cooling system including mini channels within a turbine blade of a turbine engine
#679Cooling system with internal flow guide within a turbine blade of a turbine engine
#680Blade outer seal with micro axial flow cooling system
#681Method for providing turbulation on the inner surface of holes in an article, and related articles
#682Internally cooled gas turbine airfoil and method
#683Internally cooled gas turbine airfoil and method
#684Turbine blade turbulator cooling design
#685Methods and apparatus for maintaining rotor assembly tip clearances
#686Aspherical dimples for heat transfer surfaces and method
#687Heat transferring cooling features for an airfoil
#688Airfoil with three-pass serpentine cooling channel and microcircuit
#689Heat transfer augmentation in a compact heat exchanger pedestal array
#690Offset Coriolis turbulator blade
#691Combustor cooling with angled segmented surfaces
#692Impingement cooling system for a turbine blade
#693Drillable super blades
#694Cooled rotor blade
#695Rotor blade with a stick damper
#696Cooled rotor blade
#697Cooled rotor blade and method for cooling a rotor blade
#698Cooled turbine airfoil
#699Turbine nozzle trailing edge cooling configuration
#700Turbulator on the underside of a turbine blade tip turn and related method
#701Fanned trailing edge teardrop array
#702Turbulated hole configurations for turbine blades
#703Tailored turbulation for turbine blades
#704Micro-circuit platform
#705Converging pin cooled airfoil
#706Cooled rotor blade with vibration damping device
#707Cooled rotor blade with vibration damping device
#708Airfoil cooling holes
#709Component and turbine assembly with film cooling
#710Hot gas path component with mesh and impingement cooling
#711Hot gas path component with mesh and dimpled cooling
#712Hot gas path component with mesh and turbulated cooling
#713Gas turbine vane with integral cooling flow control system
#714Split flow turbine nozzle
#715Flow guide component with enhanced cooling
#716Microcircuit cooling for a turbine airfoil
#717Turbine bucket airfoil cooling hole location, style and configuration
#718Microcircuit airfoil mainbody
#719Perimeter-cooled turbine bucket airfoil cooling hole location, style and configuration
#720Turbine blade inner rib profile
#721Gas turbine combustor with enhanced cooling features
#722Airfoil skin passageway cooling enhancement
#723Hydrogen fuel system for a gas turbine engine
#724Ericsson cycle turbine engine
#725Self compensating rocket engine enhancement
#726Cooling arrangement for gas turbine engine components
#727Combined cycle energy recovery method and system
#728Shaped recess flow control