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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

Component blending tool

United Technologies

Component blending tool

Search recent Press Releases: United Technologies Corporation-related press releases
Count Application # Date United Technologies Corporation patents (updated weekly) - BOOKMARK this page
12015014379405/28/15 new patent  Geared turbofan engine gearbox arrangement
22015014752805/28/15 new patent  Component blending tool
32015013567805/21/15Gas turbine engine with noise attenuating variable area fan nozzle
42015013834205/21/15System and method to determine visible damage
52015014123505/21/15Carbon fiber-reinforced article and method therefor
62015013210605/14/15Gas turbine engine with low fan pressure ratio
72015013211005/14/15High durability turbine exhaust case
82015013213405/14/15Injection molded composite fan platform
92015013214205/14/15Rotor blade with bonded cover
102015012168205/07/15Extraction tool assembly
112015012183805/07/15Conjoined reverse core flow engine arrangement
122015012183905/07/15Tandem thrust reverser with multi-bar linkage
132015012184105/07/15Flow control device for a three stream turbofan engine
142015012184405/07/15Geared turbofan arrangement with core split power ratio
152015012188205/07/15Mixer assembly for a gas turbine engine
162015012188405/07/15Stress relieved rectilinear duct
172015012189305/07/15Adaptive fan reverse core geared turbofan engine with separate cold turbine
182015012189405/07/15Bifurcation fire purge system
192015012189505/07/15Full ring sliding nacelle with thrust reverser
202015012189605/07/15Reverse core flow engine mounting arrangement
212015012203105/07/15Transducer position guide
222015012233905/07/15Variable area bypass nozzle
232015012290505/07/15Passive tangential ejector for an exhaust nozzle of a gas turbine engine
242015012291205/07/15Tandem thrust reverser with multi-point actuation
252015012295205/07/15Gas turbine engine inlet wall design
262015012299805/07/15Method of inspection for cooling holes in turbine airfoil
272015012525905/07/15Gas turbine engine variable pitch fan blade
282015012527005/07/15Atr guide pins for sliding nacelle
292015012528405/07/15Atr full ring sliding nacelle
302015012528505/07/15Integrated nozzle and plug
312015012528605/07/15Atr axial v-groove
322015012529105/07/15Bracket for mounting a stator guide vane arrangement to a strut in a turbine engine
332015012529305/07/15Turbofan engine main bearing arrangement
342015012529505/07/15Wind turbine load mitigation
352015012530405/07/15Mass offset for damping performance
362015012530505/07/15Low profile fan platform attachment
372015012568105/07/15High temperature imaging media for digital image correlation
382015012609605/07/15System and contoured peel grinding
392015011394104/30/15Translating outer cowl flow modulation device and method
402015011394204/30/15Phosphor thermometer with two waveguides
412015011394304/30/15Geared turbofan engine with power density range
422015011394504/30/15Pivoting blocker door
432015011399604/30/15Cascaded multi-variable control system for a turboshaft engine
442015011400204/30/15Geared turbofan engine with a high ratio of thrust to turbine volume
452015011407404/30/15Systems and methods for controlled peening
462015011749304/30/15Phosphor thermometry fiber sensor
472015011780404/30/15Gas turbine engine bushing
482015011806304/30/15Turbine airfoil tip shelf and squealer pocket cooling
492015011806404/30/15Gas turbine engine airfoil trailing edge passage and core for making same
502015010722304/23/15High durability turbine exhaust case
512015011063604/23/15Wear pad to prevent cracking of fan blade
522015011102204/23/15Coating for metal cellular structure and method therefor
532015010193504/16/15Apparatus and ionic liquid electroplating
542015010431504/16/15Fan blade root integrated sealing solution
552015009630304/09/15Gas turbine engine with high speed low pressure turbine section
562015009671304/09/15Rapid tooling insert manufacture
572015009683904/09/15Low loss oil accumulator assembly
582015009883004/09/15Assembly fixture for a stator vane assembly
592015009883504/09/15Castings, casting cores, and methods
602015008991804/02/15Gas turbine lubrication systems
612015008995804/02/15Gas turbine engine with high speed low pressure turbine section
622015008995904/02/15Gas turbine engine shaft bearing configuration
632015008294503/26/15Process for producing refractory metal alloy powders
642015008391903/26/15Background radiation measurement system
652015008626203/26/15Welded assemblies and methods of making welded assemblies
662015008628303/26/15Ball-end milling cutter tool
672015007574503/19/15Casting molds, manufacture and use methods
682015007891503/19/15Piloted nut
692015006820903/12/15Method for determining circumferential sensor positioning
702015006821003/12/15Tube fed tangential on-board injector for gas turbine engine
712015006821403/12/15Low thermal mass joint
722015006966803/12/15Multi-dimensional component build system and process
732015007170403/12/15Exhaust duct liner rod hanger
742015006000203/05/15Die casting system and cell
752015006528503/05/15Geared architecture gas turbine engine with oil scavenge
762015005287302/26/15Torque connector lubrication scuppers
772015005290702/26/15Thermal management system for gas turbine engine
782015005378902/26/15Linkage to control and restrain flap movement
792015005012702/19/15Air with integral spring for a gas turbine engine exhaust drive
802015005104002/19/15Oil baffle for gas turbine fan drive gear system
812015004202302/12/15Hybrid part made from monolithic ceramic skin and cmc core
822015004402802/12/15Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
832015004405202/12/15Geared turbofan with fan blades designed to achieve laminar flow
842015004520002/12/15Ceramic component
852015003760202/05/15System and high temperature die casting tooling
862015002710101/29/15Geared gas turbine engine architecture for enhanced efficiency
872015002713001/29/15Split ring valve
882015002765701/29/15Method and casting core for forming a landing for welding a baffle inserted in an airfoil
892015003044001/29/15Fireshield fastener hood
902015003044301/29/15Split damped outer shroud for gas turbine engine stator arrays
912015002378001/22/15Liner attaching scheme
922015002429601/22/15Method and system for operating a flow battery system based on energy costs
932015001330101/15/15Turbine engine including balanced low pressure stage count
952015001348001/15/15Plated instrumentation probes and sensors
962015001393401/15/15Article with grouped grain patterns
972015001695401/15/15Blade outer air seal assembly and support
982015001696501/15/15Link arm drag reducing device
992015000826801/08/15Pivot thrust reverser with multi-point actuation
1002015000008901/01/15Clamp connector
1012015000030301/01/15Wireless power for gas turbine engine instrumentation
1022015000030401/01/15Removable nosecone for a gas turbine engine
1032015000395601/01/15Variable vane scheduling
1042015000396801/01/15Gas turbine engine with attached nosecone
1052015000399501/01/15Aircraft engine component with locally tailored materials
1062015000399701/01/15Method of forming hybrid metal ceramic components
1072014037354912/25/14Cooling hole with curved metering section
1082014037355412/25/14Air turbine starter pressure monitor system
1092014037361012/25/14Engine inspection apparatus and system
1102014037505612/25/14Method of operating a power generation system
1112014036654812/18/14Turbine engine gearbox
1122014036655412/18/14Cross reference to related applications
1132014036655612/18/14Gas turbine engine vane-to-transition duct seal
1142014036661312/18/14Probe retention-sealing feature
1152014036978312/18/14Self-retaining shear pin for blind mount location
1162014036980412/18/14Variable bleed slot in centrifugal impeller
1172014036981812/18/14Planetary gear system arrangement with auxiliary oil system
1182014036015212/11/14Oil tank mount with yoke
1192014036015312/11/14Gas turbine engine thermal management system
1202014036330512/11/14Hybrid turbine blade for improved engine performance or architecture
1212014035656012/04/14Castings and manufacture methods
1222014035839812/04/14Use of ss data trends in fault resolution process
1232014035850012/04/14Probalistic high cycle fatigue (hcf) design optimization process
1242014034857711/27/14Tie bolt employing differential thread
1252014034863011/27/14Noise reducing vane
1262014034864011/27/14Thrust efficient turbofan engine
1272014033833611/20/14Gas turbine engine combustor with integrated combustor vane
1282014033835111/20/14Gas turbine engine combustor with tailored temperature profile
1292014033835711/20/14Cavity swirl fuel injector for an augmentor section of a gas turbine engine
1302014033836011/20/14Bleed port ribs for turbomachine case
1312014033219111/13/14Extreme environment heat exchanger
1322014033491611/13/14Borescope inspection port fitting
1332014032684211/06/14Oil tank mount with stiffeners
1342014031813310/30/14Thrust efficient turbofan engine
1352014031814310/30/14Multi-circuit buffer system for a gas turbine engine
1362014031814710/30/14Low noise compressor rotor for geared turbofan engine
1372014032196110/30/14Mate face cooling holes for gas turbine engine component
1382014032302210/30/14Airfoil edge form transfer grinding tool
1392014032436310/30/14System reliability analysis and management using physics-based models embedded in a baysian network
1402014031112110/23/14Pulse detonation engine having a scroll ejector attenuator
1412014031114910/23/14Gas turbine engine fan blade airfoil profile
1422014031261110/23/14Locking fluid fittings
1432014031454010/23/14Gas turbine engine synchronization ring
1442014031454110/23/14Turbomachine thrust balancing system
1452014031454210/23/14Gas turbine engine exhaust diffuser with movable struts
1462014031454610/23/14Turbine engine gearbox mount with multiple fuse joints
1472014031454710/23/14Attachment ceramic matrix composite materials
1482014031458110/23/14Method for forming single crystal parts using additive manufacturing and remelt
1492014029878810/09/14Gas turbine engine including pneumatic actuator system
1502014030142510/09/14Backstrike detection system for laser drilling thin materials
1512014030182910/09/14Engine bearing support
1522014029021110/02/14Turbine engine including balanced low pressure stage count
1532014029021310/02/14Duct blocker seal assembly for a gas turbine engine
1542014029026910/02/14Duct blocker seal assembly for a gas turbine engine
1552014029455810/02/14Turbomachine fluid delivery manifold and system
1562014028350009/25/14Thrust efficient turbofan engine
1572014028350109/25/14Elongated geared turbofan with high bypass ratio
1582014028674809/25/14Fan containment case with thermally conforming liner
1592014028675409/25/14Elongated geared turbofan with high bypass ratio
1602014028675509/25/14Ring gear mounting arrangement with oil scavenge scheme
1612014028678109/25/14Integral fan blade wear pad and platform seal
1622014025966109/18/14Variable area fan nozzle with wall thickness distribution
1632014026017609/18/14Lube tube expansion and torque retaining device
1642014026018209/18/14Free stream intake for reverse core engine
1652014026018309/18/14Variable cycle intake for reverse core engine
1662014026032109/18/14Gas turbine engine static structure joint with undercuts
1672014026179709/18/14Tube fitting having integrated tee fitting
1682014026810009/18/14Multiple laser time of arrival probe
1692014026981709/18/14Phosphor thermometry fiber sensor
1702014027062509/18/14High temperature uncooled optical probe
1712014027110109/18/14Modulated turbine vane cooling
1722014027111209/18/14Low noise turbine for geared gas turbine engine
1732014027112109/18/14Gas turbine engine architecture with intercooled twin centrifugal compressor
1742014027113509/18/14Turbofan engine bearing and gearbox arrangement
1752014027117809/18/14Fan blades for gas turbine engines with reduced stress concentration at leading edge
1762014027122109/18/14Usage of a witness mark to distinguish support structure from part
1772014027245609/18/14Spallation-resistant thermal barrier coating
1782014027374709/18/14Removing material from a workpiece with a water jet
1792014027375709/18/14Drag finishing system, method and fixture for gas turbine engine airfoils
1802014027453109/18/14Fan drive planetary gear system integrated carrier and torque frame
1812014025086209/11/14Reverse flow gas turbine engine airflow bypass
1822014025086309/11/14Rear mounted reverse core engine thrust reverser
1832014025089509/11/14Modulated ejector cooling
1842014025138109/11/14Pulse jet liquid gas cleaning system
1852014025179109/11/14Cathodic arc deposition stinger
1862014025180309/11/14Cathodic arc mask assembly lock system
1872014025216009/11/14Reverse flow gas turbine engine removable core
1882014025216109/11/14De-couple geared turbo-fan engine and aircraft
1892014025216209/11/14Uav launching from moving platform
1902014025216709/11/14Reverse core engine thrust reverser for under wing
1912014025218309/11/14Sensor hoop storage and transport apparatus
1922014025276409/11/14Two-piece self-locking mechanism for tube assemblies
1932014025463109/11/14Actively cooled gas turbine sensor probe housing
1942014025511209/11/14Broach tool rake face with a tailored surface topography
1952014025514409/11/14Flanged bushing for variable vane
1962014025515609/11/14Non-contacting seals for geared gas turbine engine bearing compartments
1972014025515809/11/14Coating process for gas turbine engine component with cooling holes
1982014025516209/11/14Adjustable floating oil channel for gas turbine engine gear drive
1992014025516709/11/14Consumable assembly tool for a gas turbine engine
2002014025516809/11/14Inter-module flow discourager
2012014025517209/11/14Low profile push-lock device
2022014025517409/11/14Manufacture of full ring strut vane pack
2032014025518209/11/14Push-lock pin connector
2042014025519609/11/14Double split blade lock ring
2052014025519809/11/14Turbine disk fabrication with in situ material property variation
2062014025520209/11/14Turbine engine nosecone with deformation region
2072014024574909/04/14Nacelle anti-ice valve utilized as compressor stability bleed valve during starting
2082014024575009/04/14Circumferentially retained fairing
2092014024575109/04/14Passages to facilitate a secondary flow between components
2102014024575309/04/14Gas turbine engine rotor blade
2112014024651409/04/14Turbomachine thrust reverser
2122014024811509/04/14Active clearance control system with zone controls
2132014024811609/04/14Acoustic treatment in an unducted area of a geared turbomachine
2142014024812609/04/14Inter-module finger seal
2152014024812709/04/14Turbine engine component with dual purpose rib
2162014024812809/04/14Seals for a circumferential stop ring in a turbine exhaust case
2172014024812909/04/14Lpc flowpath shape with gas turbine engine shaft bearing configuration
2182014024813009/04/14Seal hook mount structure with overlapped coating
2192014024813609/04/14Multifunction positioning lock washer
2202014024815209/04/14Plate for directing flow and film cooling of components
2212014024815609/04/14Composite articles and methods
2222014023799008/28/14Variable area fan nozzle with wall thickness distribution
2232014023802708/28/14Thermally compliant dual wall liner for a gas turbine engine
2242014023908308/28/14Pivot thrust reverser surrounding inner surface of bypass duct
2252014023908408/28/14Tandem thrust reverser with sliding rails
2262014024185108/28/14Axial oil scoop for a gas turbine engine
2272014024185608/28/14Gas turbine engine systems involving tip fans
2282014024185708/28/14Flow diverter to redirect secondary flow
2292014024187408/28/14Wear liner spring seal
2302014024189708/28/14Aluminum brazing of hollow titanium fan blades
2312014024227808/28/14Split coating mask system for gas turbine engine component
2322014023024608/21/14Thermally free hanger with length adjustment feature
2332014023040308/21/14Gas turbine engine shaft bearing configuration
2342014023045208/21/14Planetary gear system arrangement with auxiliary oil system
2352014023094308/21/14Support system bumper for exhaust duct liner hanger
2362014023143708/21/14Cap drain plug
2372014023407808/21/14Method for setting a gear ratio of a fan drive gear system of a gas turbine engine
2382014023407908/21/14Geared architecture for high speed and small volume fan drive turbine
2392014023408508/21/14Bushing arranged between a body and a shaft, and connected to the shaft
2402014023408608/21/14Bushing arranged between a body and a shaft, and connected to the shaft
2412014023408708/21/14Inlet guide vane retention feature
2422014023409808/21/14Turbine case retention hook with insert
2432014022391608/14/14Gas turbine engine with compressor inlet guide vane positioned for starting
2442014022391908/14/14Flexible liner hanger
2452014022392008/14/14Consumable assembly mistake proofing tool for a gas turbine engine
2462014022538808/14/14Latch release mechanism
2472014022693008/14/14Test equipment with housing damping system
2482014022707808/14/14Mid-turbine frame vane assembly support with retention unit
2492014022708408/14/14Compound star gear system with rolling element bearings

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