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new Companies with the Most Patent Filings (2010+)

Filing Names

United Technologies Corporation
United Technologies Corporation One Financial Plaza
United Technologies Corporation_20100114
United Technologies Corporation_20100107
United Technologies Corporation_20100121
United Technologies Corporation_20131212
United Technologies Corporation_20100128


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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
12016017593006/23/16  new patent  High temperature fluidized bed for powder treatment
22016017593306/23/16  new patent  Fabrication of articles from nanowires
32016017598806/23/16  new patent  Method to immobilize an entrapped contaminant within a honeycomb structure
42016017599606/23/16  new patent  Repair material preform
52016017600006/23/16  new patent  Methods of roughing and finishing engine hardware
62016017773006/23/16  new patent  Hybrid airfoil for a gas turbine engine
72016017773206/23/16  new patent  Hollow fan blade for a gas turbine engine
82016017773306/23/16  new patent  Method of forming cooling holes
92016017773406/23/16  new patent  Airfoil showerhead pattern apparatus and system
102016017773506/23/16  new patent  Turbine blade having film cooling hole arrangement
112016017773606/23/16  new patent  Cooled airfoil structure
122016017773706/23/16  new patent  Gas turbine engine component with film cooling hole with accumulator
132016017773806/23/16  new patent  Gas turbine engine component with film cooling hole
142016017774006/23/16  new patent  Gas turbine engine component with conformal fillet cooling path
152016017775406/23/16  new patent  Bonded fan platform
162016017775506/23/16  new patent  Hardware geometry for increasing part overlap and maintaining clearance
172016017775606/23/16  new patent  Airfoil fillet
182016017775806/23/16  new patent  Angled rail holes
192016017776306/23/16  new patent  Gas turbine engine sealing arrangement
202016017776406/23/16  new patent  Compliant seal assembly and operating
212016017776506/23/16  new patent  Pinned seal
222016017776606/23/16  new patent  Mini blind stator leakage reduction
232016017776706/23/16  new patent  Trough seal for gas turbine engine
242016017776806/23/16  new patent  Blade tip clearance systems
252016017777206/23/16  new patent  Thermal inspection system
262016017777406/23/16  new patent  Low noise turbine for geared gas turbine engine
272016017778106/23/16  new patent  System and controlling an environmental condition of an engine electronic component
282016017778206/23/16  new patent  Engine component having platform with passageway
292016017778306/23/16  new patent  Housing support nut connection
302016017778806/23/16  new patent  Intergrated seal supports
312016017781906/23/16  new patent  Simplified engine bleed supply with low pressure environmental control system for aircraft
322016017782006/23/16  new patent  Low pressure environmental control system with safe pylon transit
332016017782806/23/16  new patent  Staged heat exchangers for multi-bypass stream gas turbine engines
342016017783006/23/16  new patent  Diffuser case mixing chamber for a turbine engine
352016017784006/23/16  new patent  Auxiliary component mounts
362016017784106/23/16  new patent  Planetary gear system for turbomachine
372016017806306/23/16  new patent  Tiered brush seal
382016017819906/23/16  new patent  Combustor dilution hole active heat transfer control apparatus and system
392016017820106/23/16  new patent  Gas turbine engine components and cooling cavities
402016016711206/16/16 Ceramic core for component casting
412016016712206/16/16 Die casting system and method
422016016718006/16/16 Direct deposition of metallic coating
432016016719006/16/16 Systems and methods for finishing flow elements
442016016719606/16/16 Systems and methods for polishing airfoils
452016016719706/16/16 System and polishing airfoils
462016016779106/16/16 Plated polymer aviation components
472016016779206/16/16 Aircraft anti-icing system
482016016866306/16/16 Aluminum alloys and manufacture methods
492016016871606/16/16 Plated polymer composite molding
502016016872106/16/16 Cold spray nozzle assembly
512016016899606/16/16 Removable riveted balance ring
522016016900006/16/16 Heat transfer pedestals with flow guide features
532016016900106/16/16 Diffused platform cooling holes
542016016900206/16/16 Airfoil trailing edge tip cooling
552016016900406/16/16 Cooling passages for gas turbine engine component
562016016900506/16/16 Gas turbine engine component with increased cooling capacity
572016016900806/16/16 System and blade with protective layer
582016016901106/16/16 Turbine airfoil attachment with multi-radial serration profile
592016016901206/16/16 Plated polymer components for a gas turbine engine
602016016901306/16/16 Gas turbine engine component with abrasive surface formed by electrical discharge machining
612016016901606/16/16 Reversible flow blade outer air seal
622016016902006/16/16 Gas turbine engine non-rotating structure wedge seal
632016016902106/16/16 Splined dog-bone seal
642016016902206/16/16 Annular cartridge seal
652016016902906/16/16 Geared turbofan engine with low pressure environmental control system for aircraft
662016016903206/16/16 Borescope plug assembly for gas turbine engine
672016016903406/16/16 Core case heating for gas turbine engines
682016016903606/16/16 Gas turbine engines with heated cases
692016016903906/16/16 Slots for turbomachine structures
702016016904006/16/16 Secondary sealing system
712016016904206/16/16 Temporary post maintenance oil filter for gas-turbine engine
722016016904406/16/16 Liners for turbomachinery cases
732016016904906/16/16 Pre-diffuser strut for gas turbine engine
742016016905006/16/16 Gas turbine engine mid-turbine frame tie rod arrangement
752016016910206/16/16 Reverse core flow gas turbine engine
762016016910806/16/16 Stepped fairing modulated exhaust cooling
772016016911806/16/16 Dual tower shaft gearbox for gas turbine engine
782016016912006/16/16 Fuel schedule for robust gas turbine engine transition between steady states
792016016915706/16/16 Gas turbine engine and thrust reverser assembly therefore
802016016924506/16/16 High compressor exit guide vane assembly to pre-diffuser junction
812016016924606/16/16 Plastic variable inlet guide vane
822016016925606/16/16 Method and assembly for attaching components
832016016926106/16/16 Ceramic bolt for exhaust panel
842016016942606/16/16 Variable cross-section tube profile apparatus and system
852016016951206/16/16 Cooled wall assembly for a combustor and design
862016016951406/16/16 Gas turbine engine diffuser-combustor assembly inner casing
872016016951506/16/16 Edge cooling for combustor panels
882016016951606/16/16 Gas turbine engine combustor bulkhead assembly
892016016952106/16/16 Swirler mount interface for gas turbine engine combustor
902016016952206/16/16 Fuel injector guide(s) for a turbine engine combustor
912016016978306/16/16 Tensile test geometry
922016016993906/16/16 System and coil sensor design, alignment and tuning
932016015883406/09/16 Castings and manufacture methods
942016015883506/09/16 Die casting system and cell
952016015896406/09/16 Ceramic-encapsulated thermopolymer pattern or support with metallic plating
962016015948806/09/16 Plated polymer nosecone
972016016035306/09/16 Interlocked plated polymers
982016016064806/09/16 Rotor disk assembly for a gas turbine engine
992016016065106/09/16 Airfoil including loose damper
1002016016065206/09/16 Cooled pocket in a turbine vane platform
1012016016065406/09/16 Turbine airfoil segment having film cooling hole arrangement
1022016016065606/09/16 Turbine airfoil segment having film cooling hole arrangement
1032016016065706/09/16 Staggered crossovers for airfoils
1042016016065806/09/16 Composite airfoil
1052016016066206/09/16 Turbine airfoil attachment with serration profile
1062016016066506/09/16 Gas turbine engine stator vane asymmetry
1072016016066606/09/16 Pre-diffuser with multiple radii
1082016016066806/09/16 Inner diffuser case cone and skirt
1092016016066906/09/16 Abrasive flow media fixture with end contour
1102016016067006/09/16 Vane assembly of a gas turbine engine
1112016016067306/09/16 Stiffness controlled abradable seal system and methods of making same
1122016016067406/09/16 Gas turbine engine forward bearing compartment architecture
1132016016067606/09/16 Gas turbine engine variable stator vane
1142016016067806/09/16 Ground handling system for a composite fan case and a using the same
1152016016068006/09/16 Compressed chopped fiber composite structural guide vane
1162016016068106/09/16 Plated polymer nacelle
1172016016068506/09/16 Eliminatin of unfavorable outflow margin
1182016016068606/09/16 Lubrication system for a gear system of a gas turbine
1192016016068706/09/16 Outer diffuser case for a gas turbine engine
1202016016071406/09/16 Gas turbine engine with split lubrication system
1212016016075806/09/16 Gas turbine engine nacelle anti-icing system
1222016016076006/09/16 Self-opening cooling passages for a gas turbine engine
1232016016076106/09/16 Gas turbine engine with single turbine driving two compressors
1242016016086306/09/16 Plated polymer fan
1252016016086906/09/16 Plated polymer compressor
1262016016087506/09/16 Gas turbine engine with fan clearance control
1272016016092406/09/16 Integral oil damper and jet for lubrication of bearings and seals
1282016016112106/09/16 Gas turbine engine with ceramic panel
1292016016112406/09/16 Single-fitting, dual-circuit fuel nozzle
1302016016124206/09/16 Non-contact strain measurement
1312016015182906/02/16 Additively manufactured core
1322016015185606/02/16 Transient liquid phase bonding of surface coatings metal-covered materials
1332016015197706/02/16 Additive manufacturing system and manufacture
1342016015200506/02/16 Hybrid plated composite stack
1352016015232006/02/16 Gas turbine engine spinner
1362016015284006/02/16 Hydrophobic coating for coated article
1372016015310206/02/16 High temperature additive manufacturing for organic matrix composites
1382016015327906/02/16 Low noise turbine for geared turbofan engine
1392016015328006/02/16 Drill to flow mini core
1402016015328206/02/16 Stress reduction for film cooled gas turbine engine component
1412016015328306/02/16 Gas turbine engine component with converging/diverging cooling passage
1422016015328606/02/16 Turbine clearance control utilizing low alpha material
1432016015328706/02/16 Plated polymer turbine component
1442016015328906/02/16 Gas turbine engine ceramic component assembly attachment
1452016015329106/02/16 Cooling system of a stator assembly for a gas turbine engine having a variable cooling flow mechanism and operation
1462016015329606/02/16 Flow discourager for vane sealing area of a gas turbine engine
1472016015330106/02/16 Non-linearly deflecting brush seal land
1482016015330306/02/16 Snap in platform damper and seal assembly for a gas turbine engine
1492016015330406/02/16 Low loss airfoil platform rim seal assembly
1502016015330506/02/16 Tuned rotor disk
1512016015330606/02/16 Radial position control of case support structure with splined connection
1522016015330706/02/16 Turbine blade tip clearance control
1532016015331006/02/16 Three spool turbofan engine with low noise intermediate turbine rotor
1542016015331106/02/16 Bleed valve resonator drain
1552016015331306/02/16 Flange partial section replacement repair
1562016015331506/02/16 Moment accommodating fastener assembly
1572016015335606/02/16 Geared turbofan engine gearbox arrangement
1582016015335806/02/16 Acoustic panel repair methods and apparatus
1592016015336106/02/16 Bleed valve resonance augmentations
1602016015336206/02/16 Turbomachine bypass flow diverting assembly and method
1612016015336306/02/16 Liquid separating air inlets
1622016015339706/02/16 Gas turbine engine system for modulating flow of fan by-pass air and core engine air
1632016015339906/02/16 Gas turbine engine and thrust reverser assembly therefore
1642016015346306/02/16 Fiber reinforced spacer for a gas turbine engine
1652016015346406/02/16 Aluminum airfoil
1662016015365806/02/16 Combustor wall for a gas turbine engine and acoustic dampening
1672016015365906/02/16 Gas turbine engine ceramic component assembly and bonding material
1682016015366006/02/16 Swirler mount interface for gas turbine engine combustor
1692016015386506/02/16 Gas turbine engine airfoil growth inspection method
1702016014442805/26/16 Build plate and additive manufacturing
1712016014610405/26/16 Angled core engine
1722016014442705/26/16 Fluidized bed for degassing and heat treating powders
1732016014443405/26/16 Method of additively manufacturing articles incorporating a substrate
1742016014446505/26/16 Repair or remanufacture of combustor liner panels with an oxidation resistant braze
1752016014457505/26/16 System and process for evaluating and manufacturing additively manufactured components
1762016014460105/26/16 Reinforced plated polymers
1772016014460205/26/16 Metal-encapsulated polymeric article
1782016014497205/26/16 Blended wing body boundary layer ingesting inlet design integration
1792016014544705/26/16 Plated polymers with intumescent compositions and temperature indicators
1802016014574705/26/16 Brush plating repair plated polymers
1812016014575505/26/16 Lightweight metal parts produced by plating polymers
1822016014575805/26/16 In-situ balancing of plated polymers
1832016014585005/26/16 Plated tubular lattice structure
1842016014602205/26/16 High-modulus coating for local stiffening of airfoil trailing edges
1852016014602305/26/16 Rotor with blades secured by woven fiber attachment system
1862016014603005/26/16 Non-metallic engine case inlet compression seal for a gas turbine engine
1872016014603205/26/16 Pressure seal with non-metallic wear surfaces
1882016014603305/26/16 Gas turbine engine clearance control
1892016014604005/26/16 Alternating vane asymmetry
1902016014604405/26/16 Internally cooled turbine platform
1912016014604805/26/16 Lubrication of journal bearing during clockwise and counter-clockwise rotation
1922016014604905/26/16 Sealing interface for a case of a gas turbine engine
1932016014605205/26/16 Forged cast forged outer case for a gas turbine engine
1942016014605305/26/16 Blade outer air seal support structure
1952016014605505/26/16 Liner hanger with spherical washers
1962016014610205/26/16 Geared architecture gas turbine engine with oil scavenge
1972016014610305/26/16 Gas turbine engine shaft members and maintenance method
1982016014610905/26/16 Compact aero-thermo model based control system estimator starting algorithm
1992016014646505/26/16 Nozzle guide for a combustor of a gas turbine engine
2002016014660105/26/16 Throat area calculation for a section of a gas turbine engine
2012016013785605/19/16 Nanocellular and nanocellular particle filled polymer composite coating for erosion protection
2022016013839905/19/16 Reinforced gas turbine engine rotor disk
2032016013841205/19/16 Shroud seal and wearliner
2042016013841605/19/16 Variable fan nozzle using shape memory material
2052016013842105/19/16 Nonlinear rolling bearing radial support stiffness
2062016013842205/19/16 Gear carrier flex mount lubrication
2072016013842505/19/16 Turbofan engine front section
2082016013847405/19/16 Low noise compressor rotor for geared turbofan engine
2092016013847705/19/16 Three spool geared turbofan with low pressure compressor drive gear system
2102016013852305/19/16 Optimal thrust control of an aircraft engine
2112016012967205/12/16 Underpotential deposition of metal monolayers from ionic liquids
2122016013070305/12/16 Cold spray nozzles
2132016013094605/12/16 Method to repair variable vanes
2142016013094905/12/16 Low noise turbine for geared turbofan engine
2152016013095005/12/16 Gas turbine engine component with rib support
2162016013095205/12/16 Vibration-damped composite airfoils and manufacture methods
2172016013095805/12/16 Gas turbine engine structural guide vanes
2182016013096305/12/16 Gas turbine engine and seal assembly therefore
2192016013096405/12/16 Gas turbine engine flow control device
2202016013096805/12/16 Platforms with leading edge features
2212016013097705/12/16 Turbine rotor segmented sideplates with anti-rotation
2222016013103605/12/16 Thermal management system for a gas turbine engine
2232016013103705/12/16 Supply duct for cooling air
2242016013103905/12/16 Gas turbine engine heat exchanger manifold
2252016013104305/12/16 Turbine engine gearbox
2262016013104405/12/16 Gas turbine engine driving multiple fans
2272016013108405/12/16 Geared turbofan arrangement with core split power ratio
2282016013115105/12/16 Gas turbine engine airfoil
2292016013136305/12/16 Combustor wall aperture body with cooling circuit
2302016013136405/12/16 Combustor dilution hole cooling
2312016013136505/12/16 Impingement film-cooled floatwall with backside feature
2322016013396405/12/16 Flow battery with manifold passage that varies in cross-section
2332016013527905/12/16 Instrumented article having compliant layer between conformal electronic device and substrate
2342016012138905/05/16 Additively manufactured casting articles for manufacturing gas turbine engine parts
2352016012200505/05/16 Embedded engines in hybrid blended wing body
2362016012255205/05/16 Abrasive rotor coating with rub force limiting features
2372016012255705/05/16 Corrosion resistant hydrophobic coatings and methods of production thereof
2382016012316005/05/16 Thermal-sprayed bonding of a ceramic structure to a substrate
2392016012316505/05/16 Variable area gas turbine engine component having movable spar and shell
2402016012316605/05/16 Turbine vanes with variable fillets
2412016012317005/05/16 Sealing systems
2422016012317605/05/16 High pressure compressor rotor thermal conditioning using outer diameter gas extraction
2432016012317705/05/16 Vane arm with inclined retention slot
2442016012318005/05/16 Over speed monitoring using a fan drive gear system
2452016012318405/05/16 Combined fan case ice liner and rear liner
2462016012318705/05/16 Heatshield assembly with double lap joint for a gas turbine engine
2472016012318805/05/16 Stator shroud systems
2482016012323005/05/16 Curved plate/fin heater exchanger
2492016012323305/05/16 Spline ring for a fan drive gear flexible support

ARCHIVE: New 2016 2015 2014 2013 2012 2011 2010 2009


This listing is an abstract for educational and research purposes is only meant as a recent sample of applications filed, not a comprehensive history. 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