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United Technologies Corporation
United Technologies Corporation One Financial Plaza
United Technologies Corporation_20100114
United Technologies Corporation_20100107
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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 2015 2014 2013 2012 2011 2010 2009 | Company Directory "U" | United Technologies Corporation-related inventors

Search recent Press Releases: United Technologies Corporation-related press releases
Count Application # Date United Technologies Corporation patents (updated weekly) - BOOKMARK this page
12015010193504/16/15 new patent  Apparatus and ionic liquid electroplating
22015010431504/16/15 new patent  Fan blade root integrated sealing solution
32015009630304/09/15Gas turbine engine with high speed low pressure turbine section
42015009671304/09/15Rapid tooling insert manufacture
52015009683904/09/15Low loss oil accumulator assembly
62015009883004/09/15Assembly fixture for a stator vane assembly
72015009883504/09/15Castings, casting cores, and methods
82015008991804/02/15Gas turbine lubrication systems
92015008995804/02/15Gas turbine engine with high speed low pressure turbine section
102015008995904/02/15Gas turbine engine shaft bearing configuration
112015008294503/26/15Process for producing refractory metal alloy powders
122015008391903/26/15Background radiation measurement system
132015008626203/26/15Welded assemblies and methods of making welded assemblies
142015008628303/26/15Ball-end milling cutter tool
152015007574503/19/15Casting molds, manufacture and use methods
162015007891503/19/15Piloted nut
172015006820903/12/15Method for determining circumferential sensor positioning
182015006821003/12/15Tube fed tangential on-board injector for gas turbine engine
192015006821403/12/15Low thermal mass joint
202015006966803/12/15Multi-dimensional component build system and process
212015007170403/12/15Exhaust duct liner rod hanger
222015006000203/05/15Die casting system and cell
232015006528503/05/15Geared architecture gas turbine engine with oil scavenge
242015005287302/26/15Torque connector lubrication scuppers
252015005290702/26/15Thermal management system for gas turbine engine
262015005378902/26/15Linkage to control and restrain flap movement
272015005012702/19/15Air with integral spring for a gas turbine engine exhaust drive
282015005104002/19/15Oil baffle for gas turbine fan drive gear system
292015004202302/12/15Hybrid part made from monolithic ceramic skin and cmc core
302015004402802/12/15Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
312015004405202/12/15Geared turbofan with fan blades designed to achieve laminar flow
322015004520002/12/15Ceramic component
332015003760202/05/15System and high temperature die casting tooling
342015002710101/29/15Geared gas turbine engine architecture for enhanced efficiency
352015002713001/29/15Split ring valve
362015002765701/29/15Method and casting core for forming a landing for welding a baffle inserted in an airfoil
372015003044001/29/15Fireshield fastener hood
382015003044301/29/15Split damped outer shroud for gas turbine engine stator arrays
392015002378001/22/15Liner attaching scheme
402015002429601/22/15Method and system for operating a flow battery system based on energy costs
412015001330101/15/15Turbine engine including balanced low pressure stage count
432015001348001/15/15Plated instrumentation probes and sensors
442015001393401/15/15Article with grouped grain patterns
452015001695401/15/15Blade outer air seal assembly and support
462015001696501/15/15Link arm drag reducing device
472015000826801/08/15Pivot thrust reverser with multi-point actuation
482015000008901/01/15Clamp connector
492015000030301/01/15Wireless power for gas turbine engine instrumentation
502015000030401/01/15Removable nosecone for a gas turbine engine
512015000395601/01/15Variable vane scheduling
522015000396801/01/15Gas turbine engine with attached nosecone
532015000399501/01/15Aircraft engine component with locally tailored materials
542015000399701/01/15Method of forming hybrid metal ceramic components
552014037354912/25/14Cooling hole with curved metering section
562014037355412/25/14Air turbine starter pressure monitor system
572014037361012/25/14Engine inspection apparatus and system
582014037505612/25/14Method of operating a power generation system
592014036654812/18/14Turbine engine gearbox
602014036655412/18/14Cross reference to related applications
612014036655612/18/14Gas turbine engine vane-to-transition duct seal
622014036661312/18/14Probe retention-sealing feature
632014036978312/18/14Self-retaining shear pin for blind mount location
642014036980412/18/14Variable bleed slot in centrifugal impeller
652014036981812/18/14Planetary gear system arrangement with auxiliary oil system
662014036015212/11/14Oil tank mount with yoke
672014036015312/11/14Gas turbine engine thermal management system
682014036330512/11/14Hybrid turbine blade for improved engine performance or architecture
692014035656012/04/14Castings and manufacture methods
702014035839812/04/14Use of ss data trends in fault resolution process
712014035850012/04/14Probalistic high cycle fatigue (hcf) design optimization process
722014034857711/27/14Tie bolt employing differential thread
732014034863011/27/14Noise reducing vane
742014034864011/27/14Thrust efficient turbofan engine
752014033833611/20/14Gas turbine engine combustor with integrated combustor vane
762014033835111/20/14Gas turbine engine combustor with tailored temperature profile
772014033835711/20/14Cavity swirl fuel injector for an augmentor section of a gas turbine engine
782014033836011/20/14Bleed port ribs for turbomachine case
792014033219111/13/14Extreme environment heat exchanger
802014033491611/13/14Borescope inspection port fitting
812014032684211/06/14Oil tank mount with stiffeners
822014031813310/30/14Thrust efficient turbofan engine
832014031814310/30/14Multi-circuit buffer system for a gas turbine engine
842014031814710/30/14Low noise compressor rotor for geared turbofan engine
852014032196110/30/14Mate face cooling holes for gas turbine engine component
862014032302210/30/14Airfoil edge form transfer grinding tool
872014032436310/30/14System reliability analysis and management using physics-based models embedded in a baysian network
882014031112110/23/14Pulse detonation engine having a scroll ejector attenuator
892014031114910/23/14Gas turbine engine fan blade airfoil profile
902014031261110/23/14Locking fluid fittings
912014031454010/23/14Gas turbine engine synchronization ring
922014031454110/23/14Turbomachine thrust balancing system
932014031454210/23/14Gas turbine engine exhaust diffuser with movable struts
942014031454610/23/14Turbine engine gearbox mount with multiple fuse joints
952014031454710/23/14Attachment ceramic matrix composite materials
962014031458110/23/14Method for forming single crystal parts using additive manufacturing and remelt
972014029878810/09/14Gas turbine engine including pneumatic actuator system
982014030142510/09/14Backstrike detection system for laser drilling thin materials
992014030182910/09/14Engine bearing support
1002014029021110/02/14Turbine engine including balanced low pressure stage count
1012014029021310/02/14Duct blocker seal assembly for a gas turbine engine
1022014029026910/02/14Duct blocker seal assembly for a gas turbine engine
1032014029455810/02/14Turbomachine fluid delivery manifold and system
1042014028350009/25/14Thrust efficient turbofan engine
1052014028350109/25/14Elongated geared turbofan with high bypass ratio
1062014028674809/25/14Fan containment case with thermally conforming liner
1072014028675409/25/14Elongated geared turbofan with high bypass ratio
1082014028675509/25/14Ring gear mounting arrangement with oil scavenge scheme
1092014028678109/25/14Integral fan blade wear pad and platform seal
1102014025966109/18/14Variable area fan nozzle with wall thickness distribution
1112014026017609/18/14Lube tube expansion and torque retaining device
1122014026018209/18/14Free stream intake for reverse core engine
1132014026018309/18/14Variable cycle intake for reverse core engine
1142014026032109/18/14Gas turbine engine static structure joint with undercuts
1152014026179709/18/14Tube fitting having integrated tee fitting
1162014026810009/18/14Multiple laser time of arrival probe
1172014026981709/18/14Phosphor thermometry fiber sensor
1182014027062509/18/14High temperature uncooled optical probe
1192014027110109/18/14Modulated turbine vane cooling
1202014027111209/18/14Low noise turbine for geared gas turbine engine
1212014027112109/18/14Gas turbine engine architecture with intercooled twin centrifugal compressor
1222014027113509/18/14Turbofan engine bearing and gearbox arrangement
1232014027117809/18/14Fan blades for gas turbine engines with reduced stress concentration at leading edge
1242014027122109/18/14Usage of a witness mark to distinguish support structure from part
1252014027245609/18/14Spallation-resistant thermal barrier coating
1262014027374709/18/14Removing material from a workpiece with a water jet
1272014027375709/18/14Drag finishing system, method and fixture for gas turbine engine airfoils
1282014027453109/18/14Fan drive planetary gear system integrated carrier and torque frame
1292014025086209/11/14Reverse flow gas turbine engine airflow bypass
1302014025086309/11/14Rear mounted reverse core engine thrust reverser
1312014025089509/11/14Modulated ejector cooling
1322014025138109/11/14Pulse jet liquid gas cleaning system
1332014025179109/11/14Cathodic arc deposition stinger
1342014025180309/11/14Cathodic arc mask assembly lock system
1352014025216009/11/14Reverse flow gas turbine engine removable core
1362014025216109/11/14De-couple geared turbo-fan engine and aircraft
1372014025216209/11/14Uav launching from moving platform
1382014025216709/11/14Reverse core engine thrust reverser for under wing
1392014025218309/11/14Sensor hoop storage and transport apparatus
1402014025276409/11/14Two-piece self-locking mechanism for tube assemblies
1412014025463109/11/14Actively cooled gas turbine sensor probe housing
1422014025511209/11/14Broach tool rake face with a tailored surface topography
1432014025514409/11/14Flanged bushing for variable vane
1442014025515609/11/14Non-contacting seals for geared gas turbine engine bearing compartments
1452014025515809/11/14Coating process for gas turbine engine component with cooling holes
1462014025516209/11/14Adjustable floating oil channel for gas turbine engine gear drive
1472014025516709/11/14Consumable assembly tool for a gas turbine engine
1482014025516809/11/14Inter-module flow discourager
1492014025517209/11/14Low profile push-lock device
1502014025517409/11/14Manufacture of full ring strut vane pack
1512014025518209/11/14Push-lock pin connector
1522014025519609/11/14Double split blade lock ring
1532014025519809/11/14Turbine disk fabrication with in situ material property variation
1542014025520209/11/14Turbine engine nosecone with deformation region
1552014024574909/04/14Nacelle anti-ice valve utilized as compressor stability bleed valve during starting
1562014024575009/04/14Circumferentially retained fairing
1572014024575109/04/14Passages to facilitate a secondary flow between components
1582014024575309/04/14Gas turbine engine rotor blade
1592014024651409/04/14Turbomachine thrust reverser
1602014024811509/04/14Active clearance control system with zone controls
1612014024811609/04/14Acoustic treatment in an unducted area of a geared turbomachine
1622014024812609/04/14Inter-module finger seal
1632014024812709/04/14Turbine engine component with dual purpose rib
1642014024812809/04/14Seals for a circumferential stop ring in a turbine exhaust case
1652014024812909/04/14Lpc flowpath shape with gas turbine engine shaft bearing configuration
1662014024813009/04/14Seal hook mount structure with overlapped coating
1672014024813609/04/14Multifunction positioning lock washer
1682014024815209/04/14Plate for directing flow and film cooling of components
1692014024815609/04/14Composite articles and methods
1702014023799008/28/14Variable area fan nozzle with wall thickness distribution
1712014023802708/28/14Thermally compliant dual wall liner for a gas turbine engine
1722014023908308/28/14Pivot thrust reverser surrounding inner surface of bypass duct
1732014023908408/28/14Tandem thrust reverser with sliding rails
1742014024185108/28/14Axial oil scoop for a gas turbine engine
1752014024185608/28/14Gas turbine engine systems involving tip fans
1762014024185708/28/14Flow diverter to redirect secondary flow
1772014024187408/28/14Wear liner spring seal
1782014024189708/28/14Aluminum brazing of hollow titanium fan blades
1792014024227808/28/14Split coating mask system for gas turbine engine component
1802014023024608/21/14Thermally free hanger with length adjustment feature
1812014023040308/21/14Gas turbine engine shaft bearing configuration
1822014023045208/21/14Planetary gear system arrangement with auxiliary oil system
1832014023094308/21/14Support system bumper for exhaust duct liner hanger
1842014023143708/21/14Cap drain plug
1852014023407808/21/14Method for setting a gear ratio of a fan drive gear system of a gas turbine engine
1862014023407908/21/14Geared architecture for high speed and small volume fan drive turbine
1872014023408508/21/14Bushing arranged between a body and a shaft, and connected to the shaft
1882014023408608/21/14Bushing arranged between a body and a shaft, and connected to the shaft
1892014023408708/21/14Inlet guide vane retention feature
1902014023409808/21/14Turbine case retention hook with insert
1912014022391608/14/14Gas turbine engine with compressor inlet guide vane positioned for starting
1922014022391908/14/14Flexible liner hanger
1932014022392008/14/14Consumable assembly mistake proofing tool for a gas turbine engine
1942014022538808/14/14Latch release mechanism
1952014022693008/14/14Test equipment with housing damping system
1962014022707808/14/14Mid-turbine frame vane assembly support with retention unit
1972014022708408/14/14Compound star gear system with rolling element bearings
1982014022708708/14/14Blade outer air seal surface
1992014022709308/14/14Low profile thermally free blind liner hanger attachment for complex shapes
2002014021599708/07/14Flexible shield for fluid connectors
2012014021600208/07/14Gas turbine engine having slim-line nacelle
2022014021600308/07/14Gas turbine engine with geared turbofan and oil thermal management system
2032014021600508/07/14Gas turbine engine assembly including a thrust reverser
2042014021604208/07/14Combustor component with cooling holes formed by additive manufacturing
2052014021605608/07/14Heat exchange module for a turbine engine
2062014021651308/07/14High zt thermoelectric with reversible junction
2072014021977208/07/14Individual inlet guide vane control for tip turbine engine
2082014021977408/07/14Turbomachine geared architecture support assembly
2092014021977808/07/14Gas turbine engine airfoil with vane platform cooling passage
2102014021978308/07/14Gas turbine engine fan drive gear system damper
2112014021978508/07/14Vane arm having a claw
2122014021979108/07/14Lug for preventing rotation of a stator vane arrangement relative to a turbine engine case
2132014021979208/07/14Pylon matched fan exit guide vane for noise reduction in a geared turbofan engine
2142014021979308/07/14Health monitoring for hollow blades
2152014021979408/07/14Bore cavity thermal conditioning system
2162014021980708/07/14Under-root spacer for gas turbine engine fan blade
2172014021980808/07/14Sheath with extended wings
2182014021981508/07/14Multi-lobed cooling hole
2192014022231008/07/14Engine monitor for a multi-engine system
2202014020871407/31/14Thermal management for gas turbine engine
2212014020877107/31/14Gas turbine engine component cooling arrangement
2222014020883707/31/14Gas turbine engine vane embedded beam interrupt optical tip-timing probe system
2232014021099207/31/14Infrared thermography with laser
2242014021226007/31/14Airfoil assembly with paired endwall contouring
2252014021226107/31/14Lightweight shrouded fan
2262014021226207/31/14Variable outer air seal support
2272014021226307/31/14Airfoil with variable profile responsive to thermal conditions
2282014021227007/31/14Gas turbine engine component having suction side cutback opening
2292014021227607/31/14Variable outer air seal fluid control
2302014021228107/31/14Flow feed diffuser
2312014021229207/31/14Airfoil member and composite platform having contoured endwall
2322014021229707/31/14Gas turbine engine serpentine cooling passage with chevrons
2332014021229807/31/14Gas turbine engine turbine blade tip cooling
2342014021278707/31/14Multiple transition flow field and method
2352014021278807/31/14Fuel cell and membrane therefore
2362014020213307/24/14Gas turbine engine mid turbine frame with flow turning features
2372014020217007/24/14Composite articles and methods
2382014020543807/24/14Relationship between fan and primary exhaust stream velocities in a geared gas turbine engine
2392014020545207/24/14Wind turbine blade
2402014020546107/24/14Vacuum degassing laser-blocking material system and procses
2412014020546207/24/14Hvata-hybrid vertical axis turbine assembly operable under omni-directional flow for power generating systems
2422014020549307/24/14High temperature directionally solidified and single crystal die casting
2432014020649607/24/14Method of assembly for gas turbine fan drive gear system
2442014019643307/17/14Gas turbine engine component platform cooling
2452014019643407/17/14Shroud for sealing conduit feed-through
2462014019647007/17/14Gas turbine engine buffer system
2472014019647107/17/14Fan drive gear system flexible support features
2482014019647207/17/14Geared turbofan gas turbine engine architecture
2492014019647307/17/14Geared turbofan gas turbine engine architecture

ARCHIVE: New 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