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United Technologies Corporation patents


      
Recent patent applications related to United Technologies Corporation. United Technologies Corporation is listed as an Agent/Assignee. Note: United Technologies Corporation may have other listings under different names/spellings. We're not affiliated with United Technologies Corporation, we're just tracking patents.

ARCHIVE: New 2016 2015 2014 2013 2012 2011 2010 2009 | Company Directory "U" | United Technologies Corporation-related inventors




Count Application # Date United Technologies Corporation patents (updated weekly) - BOOKMARK this page
12016003100402/04/16  new patent  Shot tube for die-cast machine
22016003100602/04/16  new patent  Arcuate directionally solidified components and manufacture methods
32016003101002/04/16  new patent  Build platforms for additive manufacturing
42016003101202/04/16  new patent  Powder metallurgy alloy forging
52016003118202/04/16  new patent  Composite flange with three-dimensional weave architecture
62016003241602/04/16  new patent  Gas turbine engine airfoil impingement cooling
72016003272602/04/16  new patent  Gas turbine engine axial compressor rear hub
82016003272702/04/16  new patent  Rotor blade with a conic spline fillet at an intersection between a platform and a neck
92016003272802/04/16  new patent  Gas turbine engine airfoil
102016003272902/04/16  new patent  Composite fan blade
112016003273002/04/16  new patent  Obtuse angle chevron trip strip
122016003273102/04/16  new patent  Thermal barrier coating inside cooling channels
132016003273202/04/16  new patent  Gas turbine engine airfoil geometries and cores for manufacturing process
142016003273502/04/16  new patent  Transient liquid phase bonded tip shroud
152016003273702/04/16  new patent  Turbine blade tip treatment for industrial gas turbines
162016003273802/04/16  new patent  Gas turbine engine blade tip treatment
172016003274202/04/16  new patent  Stator segment
182016003274402/04/16  new patent  Selective coating removal or masking for ground path
192016003274602/04/16  new patent  Assembly for sealing a gap between components of a turbine engine
202016003275002/04/16  new patent  Stationary non-rotating brush seals
212016003275102/04/16  new patent  Reversible blade rotor seal
222016003275302/04/16  new patent  Gas turbine engine with axial compressor having improved air sealing
232016003275402/04/16  new patent  Adjustable blade outer air seal apparatus
242016003275602/04/16  new patent  Low noise turbine for geared turbofan engine
252016003275702/04/16  new patent  Engine inlet total air temperature sensor
262016003275902/04/16  new patent  Machined vane arm of a variable vane actuation system
272016003276302/04/16  new patent  Heatshield discourager seal for a gas turbine engine
282016003276502/04/16  new patent  Bearing compartment sealing system with passive cooling
292016003276702/04/16  new patent  Gas turbine engine with axial compressor with internal cooling pathways
302016003276902/04/16  new patent  Oil transfer passage arrangement for a shaft of a gas turbine engine
312016003277002/04/16  new patent  Geared gas turbine engine with oil deaerator and air removal
322016003277102/04/16  new patent  Fluid-cooled seal arrangement for a gas turbine engine
332016003277202/04/16  new patent  Self cleaning debris filter for fan drive gear system
342016003277302/04/16  new patent  Circulating lubricant through a turbine engine component with parallel pumps
352016003277402/04/16  new patent  Cost effective manufacturing gsac incorporating a stamped preform
362016003277502/04/16  new patent  Engine mid-turbine frame transfer tube for low pressure turbine case cooling
372016003277602/04/16  new patent  Reinforced composite case
382016003277802/04/16  new patent  Rotatable full ring fairing for a turbine engine
392016003277902/04/16  new patent  Castellated latch mechanism for a gas turbine engine
402016003278002/04/16  new patent  Triple flange arrangement for a gas turbine engine
412016003282702/04/16  new patent  Turbofan engine bearing and gearbox arrangement
422016003282802/04/16  new patent  Gas turbine engine with low stage count low pressure turbine
432016003283002/04/16  new patent  Gas turbine engine architecture with nested concentric combustor
442016003283102/04/16  new patent  Spinner aft-extended forward return flange
452016003283202/04/16  new patent  Gas turbine engine noise reducing nose cone
462016003283302/04/16  new patent  Thermally conforming acoustic liner cartridge for a gas turbine engine
472016003283502/04/16  new patent  Air-driven particle pulverizer for gas turbine engine cooling fluid system
482016003283802/04/16  new patent  Cartridge style ejector pump
492016003284002/04/16  new patent  Shield for arranging between a bearing and a rotating seal element
502016003293702/04/16  new patent  Gas turbine engine axial drum-style compressor rotor assembly
512016003297602/04/16  new patent  Component configured from martensitic stainless steel
522016003304002/04/16  new patent  Fluid barriers with flexible backing material and methods of repairing and manufacturing the same
532016003312902/04/16  new patent  Additive manufactured gas turbine engine combustor liner panel
542016003313002/04/16  new patent  Fuel nozzle for a gas turbine engine
552016003335802/04/16  new patent  Focused focused optical configuration for nsms probes
562016002327201/28/16 Turbulating cooling structures
572016002327501/28/16 Additive manufacturing baffles, covers, and dies
582016002332001/28/16 Machining tool including a pivoting machining arm and a using the same
592016002342901/28/16 Secondary reinforcement at interface of laminate structure
602016002444401/28/16 Gel solvent and removing diffusion and overlay coatings in gas turbine engines
612016002464201/28/16 Preheat chamber oxidation process
622016002467601/28/16 Bimetallic zincating processing for enhanced adhesion of aluminum on aluminum alloys
632016002492501/28/16 Turbine disk fatigue rejuvenation
642016002492701/28/16 Tie shaft flow trip
652016002492901/28/16 Gas turbine engine airfoil
662016002493401/28/16 Aluminum fan blade construction with welded cover
672016002493501/28/16 Gas turbine engine blade with variable density and wide chord tip
682016002493601/28/16 Low pressure loss cooled blade
692016002493701/28/16 Multi-lobed cooling hole
702016002493801/28/16 Airfoil cooling apparatus
712016002494001/28/16 Fan blade damping device
722016002494201/28/16 Abrasive tipped blades and manufacture methods
732016002494301/28/16 Structural guide vane leading edge
742016002494401/28/16 Transient liquid pahse bonded turbine rotor assembly
752016002494601/28/16 Rotor blade dovetail with round bearing surfaces
762016002494701/28/16 Blade wear pads and manufacture methods
772016002494901/28/16 Mid-turbine frame and gas turbine engine including same
782016002495201/28/16 Assembly for sealing a gap between components of a turbine engine
792016002495501/28/16 Maxmet composites for turbine engine component tips
802016002495601/28/16 Floating blade outer air seal assembly for gas turbine engine
812016002495701/28/16 Gas turbine engine with low stage count low pressure turbine
822016002495801/28/16 Gas turbine engine with low stage count low pressure turbine
832016002495901/28/16 Variable vane drive system
842016002496401/28/16 Gas turbine engine with air-oil cooler oil tank
852016002496501/28/16 Geared architecture turbofan engine thermal management system and method
862016002496801/28/16 Air oil cooler airflow augmentation system
872016002496901/28/16 Composite flange from braided preform
882016002497201/28/16 Nosecone support
892016002500301/28/16 Turbofan engine bearing and gearbox arrangement
902016002500401/28/16 Low noise turbine for geared turbofan engine
912016002500501/28/16 Bifurcated air inlet housing for a miniature gas turbine engine
922016002500601/28/16 Self-cooled orifice structure
932016002501001/28/16 Turbine engine and turbine engine component with cooling pedestals
942016002501301/28/16 Turbine engine face seal arrangement including anti-rotation features
952016002501401/28/16 High temperature disk conditioning system
962016002503801/28/16 Pivot door thrust reverser
972016002504001/28/16 Gas dynamic valve
982016002514001/28/16 Rolling element bearing configured with a channel
992016002514201/28/16 Eccentrically bored sleeve for locating a bearing
1002016002534201/28/16 Active cooling of grommet bosses for a combustor panel of a gas turbine engine
1012016001625301/21/16 Multiple wire electron beam melting
1022016001667301/21/16 Grounding sleeve
1032016001715401/21/16 Lightweight and corrosion resistant abradable coating
1042016001747401/21/16 Thermo-mechanical fatigue resistant aluminum abradable coating
1052016001747501/21/16 Hybrid thermal barrier coating and process of making same
1062016001748101/21/16 Chromium-enriched diffused aluminide
1072016001750101/21/16 Corrosion protection material and protecting aluminum coatings
1082016001751001/21/16 Multifunctional anodized layer
1092016001771201/21/16 Turbine engine repair methods
1102016001771301/21/16 Turbine engine hybrid rotor
1112016001771501/21/16 Fan exit guide vane platform contouring
1122016001771701/21/16 Gas turbine engine airfoil cooling circuit
1132016001771901/21/16 Gas turbine engine blade squealer pockets
1142016001772001/21/16 Airfoil platform impingement cooling holes
1152016001772301/21/16 Co-formed element with low conductivity layer
1162016001772401/21/16 Variable thickness trailing edge cavity and making
1172016001772501/21/16 Blades and manufacture methods
1182016001772601/21/16 Coated articles and manufacture methods
1192016001772701/21/16 Fan blade dovetail and spacer
1202016001772901/21/16 Structural guide vane sonic shape and inspection
1212016001773201/21/16 Off-cambered vanes for gas turbine engines
1222016001773301/21/16 Multiple coating configuration
1232016001773501/21/16 Vane tip machining fixture assembly
1242016001773701/21/16 Gas turbine engine rotor disk-seal arrangement
1252016001773801/21/16 Assembly for sealing a gap between components of a turbine engine
1262016001773901/21/16 Seal assembly for a guide vane assembly
1272016001774201/21/16 Brush seal repair method
1282016001774301/21/16 Actuator for gas turbine engine blade outer air seal
1292016001774501/21/16 Case with vane retention feature
1302016001774601/21/16 Geared architecture to protect critical hardware during fan blade out
1312016001774701/21/16 Oil system debris monitor for a gas turbine engine
1322016001774801/21/16 Gas turbine engine exhaust drain
1332016001775201/21/16 Turbofan engine assembly methods
1342016001775301/21/16 Bolt attachment to composite fan case
1352016001775401/21/16 Mid-turbine frame rod and turbine case flange
1362016001775501/21/16 Common joint for a combustor, diffuser, and tobi of a gas turbine engine
1372016001777501/21/16 Noise attenuating acoustic panel
1382016001779601/21/16 Gas turbine engine having a misturned stage
1392016001780301/21/16 Gas turbine engine de-icing system
1402016001780601/21/16 Gas turbine engine component having shaped pedestals
1412016001780701/21/16 Bench aft sub-assembly for turbine exhaust case fairing
1422016001780901/21/16 Self-purging fuel nozzle system for a gas turbine engine
1432016001781001/21/16 Acoustic liner heat exchanger
1442016001781101/21/16 Gearbox mounting assembly
1452016001781301/21/16 Compact aero-thermo model based degraded mode control
1462016001781401/21/16 Compact aero-thermo model based engine material temperature control
1472016001781501/21/16 Expanding shell flow control device
1482016001784401/21/16 Reverse core engine with thrust reverser
1492016002047701/21/16 Flow battery flow field having volume that is function of power parameter, time parameter and concentration parameter
1502016000884601/14/16 Substrates coated with wear resistant layers and methods of applying wear resistant layers to same
1512016000886701/14/16 Cast components and manufacture and use methods
1522016000888901/14/16 Additive manufacturing the addition of features within cooling holes
1532016000939901/14/16 Hybrid compressor bleed air for aircraft use
1542016001019701/14/16 Fixturing for thermal spray coating of gas turbine components
1552016001045801/14/16 Full ring curvic seal
1562016001046001/14/16 Pretrenched rotor for gas turbine engine
1572016001046301/14/16 Gas turbine engine high lift airfoil cooling in stagnation zone
1582016001046501/14/16 Gas turbine engine airfoil leading edge cooling
1592016001046601/14/16 Gas turbine engine component with twisted internal channel
1602016001046701/14/16 Gas turbine engine component cooling channels
1612016001047001/14/16 Frangible sheath for a fan blade of a gas turbine engine
1622016001047301/14/16 Cooling hole for a gas turbine engine component
1632016001047501/14/16 Cantilever stator with vortex initiation feature
1642016001047601/14/16 Shaped rim cavity wing surface
1652016001047701/14/16 Cooled seal assembly for arranging between a stator and a rotor
1662016001047901/14/16 Modular instrumentation egress seal for a gas turbine engine
1672016001048201/14/16 Low leakage multi-directional interface for a gas turbine engine
1682016001048301/14/16 Seal assembly including a notched seal element for arranging between a stator and a rotor
1692016001048401/14/16 Ring-shaped compliant support
1702016001048601/14/16 Aero-actuated vanes
1712016001049001/14/16 Fan drive thrust balance
1722016001050301/14/16 Instrumentation boss for fan containment case
1732016001050701/14/16 Retractable exhaust liner segment for gas turbine engines
1742016001054901/14/16 Oil baffles in carrier for a fan drive gear system
1752016001055001/14/16 Manifold for gas turbine
1762016001055201/14/16 Method and handling pre-diffuser airflow for cooling high pressure turbine components
1772016001055301/14/16 Method and handling pre-diffuser flow for cooling high pressure turbine components
1782016001055401/14/16 Method and handling pre-diffuser airflow for use in adjusting a temperature profile
1792016001055501/14/16 Method and collecting pre-diffuser airflow and routing it to combustor pre-swirlers
1802016001055901/14/16 Finned ignitor grommet for a gas turbine engine
1812016001056101/14/16 Gas turbine engine accessory gearbox
1822016001056201/14/16 Geared turbofan with integral front support and carrier
1832016001056301/14/16 Oil loss protection for a fan drive gear system
1842016001056401/14/16 Bleed valve assembly
1852016001065801/14/16 Composite airfoil bonded to a metallic root
1862016001077301/14/16 Component mount integrated with tube fitting
1872016001079501/14/16 Fan blade lubrication
1882016001086301/14/16 Additive manufactured surface finish
1892016001086601/14/16 Aerating fuel injector system for a gas turbine engine
1902016001350501/14/16 Reactivation of flow battery electrode by exposure to oxidizing solution
1912016001490001/14/16 Apparatus, system, and electronics manufacturing using direct write with fabricated foils
1922016000306201/07/16 Fan blades with protective sheaths and galvanic shields
1932016000135301/07/16 Investment mold with fugitive beads and method related thereto
1942016000135401/07/16 Gas turbine engine component manufacturing method and core for making same
1952016000135601/07/16 Cast component having corner radius to reduce recrystallization
1962016000136401/07/16 Uninteruppted filtering system for selective laser melting powder bed additive manufacturing process
1972016000139001/07/16 System and method low heat weld
1982016000139501/07/16 Sequencing of multi-pass laser shock peening applications
1992016000140401/07/16 Methods and tools for use in repairing gas engine turbine blades
2002016000140701/07/16 Leading edge sheath manufacturing method
2012016000150901/07/16 Additive manufacturing system and additive manufacture utilizing layer-by-layer thermo-mechanical analysis
2022016000187301/07/16 Geared turbofan with improved spinner
2032016000189001/07/16 Apu exhaust system
2042016000189201/07/16 Auxiliary power unit mounting bracket
2052016000253101/07/16 Chemical synthesis of hybrid inorganic-organic nanostructured corrosion inhibitive pigments and methods
2062016000274701/07/16 Process for treating steel alloys for gears
2072016000280801/07/16 Solution composition and single-bath post treatment of substrate
2082016000304801/07/16 Airfoil with thickened root and fan and engine incorporating same
2092016000304901/07/16 Geared turbofan engine having a reduced number of fan blades and improved acoustics
2102016000305001/07/16 Variable span splitter blade
2112016000305101/07/16 Article with sections having different microstructures and method therefor
2122016000305301/07/16 Gas turbine engine component having transversely angled impingement ribs
2132016000305401/07/16 Gas turbine engine component paired film cooling holes
2142016000305501/07/16 Gas turbine engine component cooling with interleaved facing trip strips
2152016000305601/07/16 Gas turbine engine shaped film cooling hole
2162016000305801/07/16 Rotor and gas turbine engine including same
2172016000306001/07/16 Hybrid fan blades for jet engines
2182016000306101/07/16 Hollow fan blade with extended wing sheath
2192016000306201/07/16 Fan blades with protective sheaths and galvanic shields
2202016000306401/07/16 Abrasive coating and manufacture and use methods
2212016000306501/07/16 Abrasive coating and manufacture and use methods
2222016000306601/07/16 Abrasive preforms and manufacture and use methods
2232016000306701/07/16 Aluminum fan blades with root wear mitigation
2242016000306801/07/16 Method for detecting a compromised component
2252016000307001/07/16 Gas turbine engine stator vane platform reinforcement
2262016000307101/07/16 Gas turbine engine stator vane baffle arrangement
2272016000307201/07/16 Gas turbine engine thin wall composite vane airfoil
2282016000307401/07/16 Gas turbine engine stator vane platform cooling
2292016000307501/07/16 Gas turbine engine stator vane assembly with split shroud
2302016000307601/07/16 Knife edge with increased crack propagation life
2312016000307701/07/16 Gas turbine engine turbine vane rail seal
2322016000307801/07/16 Gasket with thermal and wear protective fabric
2332016000307901/07/16 Gas turbine engine component having variable width feather seal slot
2342016000308001/07/16 Gas turbine engine seal assembly
2352016000308101/07/16 Flexible finger seal for sealing a gap between turbine engine components
2362016000308201/07/16 Contoured blade outer air seal for a gas turbine engine
2372016000308301/07/16 Abradable seal including an abradability characteristic that varies by locality
2382016000308401/07/16 Thermally conformable liner for reducing system level fan blade out loads
2392016000308501/07/16 Turbine engine adaptive low leakage air seal
2402016000308701/07/16 Edge treatment for gas turbine engine component
2412016000309001/07/16 Fan drive gear system spline oil lubrication scheme
2422016000309101/07/16 Nacelle internal and external flow control
2432016000309301/07/16 Fan axial containment system
2442016000309701/07/16 Interlocking rotor assembly with thermal shield
2452016000309801/07/16 Compartment shielding
2462016000310001/07/16 Rolling element bearing configured with a gutter and one or more fluid passages
2472016000310401/07/16 Gas turbine engine attachment structure and method therefor
2482016000310501/07/16 Integrated flex support and front center body
2492016000314201/07/16 Geared turbofan with gearbox seal



ARCHIVE: New 2016 2015 2014 2013 2012 2011 2010 2009



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This listing is an abstract for educational and research purposes is only meant as a recent sample of applications filed, not a comprehensive history. Freshpatents.com is not affiliated or associated with United Technologies Corporation in any way and there may be associated servicemarks. This data is also published to the public by the USPTO and available for free on their website. Note that there may be alternative spellings for United Technologies Corporation with additional patents listed. Browse our Agent directory for other possible listings. Page by FreshPatents.com

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