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United Technologies Corporation
United Technologies Corporation One Financial Plaza
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United Technologies Corporation_20100107
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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 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
12014033833611/20/14 new patent  Gas turbine engine combustor with integrated combustor vane
22014033835111/20/14 new patent  Gas turbine engine combustor with tailored temperature profile
32014033835711/20/14 new patent  Cavity swirl fuel injector for an augmentor section of a gas turbine engine
42014033836011/20/14 new patent  Bleed port ribs for turbomachine case
52014033219111/13/14Extreme environment heat exchanger
62014033491611/13/14Borescope inspection port fitting
72014032684211/06/14Oil tank mount with stiffeners
82014031813310/30/14Thrust efficient turbofan engine
92014031814310/30/14Multi-circuit buffer system for a gas turbine engine
102014031814710/30/14Low noise compressor rotor for geared turbofan engine
112014032196110/30/14Mate face cooling holes for gas turbine engine component
122014032302210/30/14Airfoil edge form transfer grinding tool
132014032436310/30/14System reliability analysis and management using physics-based models embedded in a baysian network
142014031112110/23/14Pulse detonation engine having a scroll ejector attenuator
152014031114910/23/14Gas turbine engine fan blade airfoil profile
162014031261110/23/14Locking fluid fittings
172014031454010/23/14Gas turbine engine synchronization ring
182014031454110/23/14Turbomachine thrust balancing system
192014031454210/23/14Gas turbine engine exhaust diffuser with movable struts
202014031454610/23/14Turbine engine gearbox mount with multiple fuse joints
212014031454710/23/14Attachment apparatus for ceramic matrix composite materials
222014031458110/23/14Method for forming single crystal parts using additive manufacturing and remelt
232014029878810/09/14Gas turbine engine including pneumatic actuator system
242014030142510/09/14Backstrike detection system for laser drilling thin materials
252014030182910/09/14Engine bearing support
262014029021110/02/14Turbine engine including balanced low pressure stage count
272014029021310/02/14Duct blocker seal assembly for a gas turbine engine
282014029026910/02/14Duct blocker seal assembly for a gas turbine engine
292014029455810/02/14Turbomachine fluid delivery manifold and system
302014028350009/25/14Thrust efficient turbofan engine
312014028350109/25/14Elongated geared turbofan with high bypass ratio
322014028674809/25/14Fan containment case with thermally conforming liner
332014028675409/25/14Elongated geared turbofan with high bypass ratio
342014028675509/25/14Ring gear mounting arrangement with oil scavenge scheme
352014028678109/25/14Integral fan blade wear pad and platform seal
362014025966109/18/14Variable area fan nozzle with wall thickness distribution
372014026017609/18/14Lube tube expansion and torque retaining device
382014026018209/18/14Free stream intake for reverse core engine
392014026018309/18/14Variable cycle intake for reverse core engine
402014026032109/18/14Gas turbine engine static structure joint with undercuts
412014026179709/18/14Tube fitting having integrated tee fitting
422014026810009/18/14Multiple laser time of arrival probe
432014026981709/18/14Phosphor thermometry fiber sensor
442014027062509/18/14High temperature uncooled optical probe
452014027110109/18/14Modulated turbine vane cooling
462014027111209/18/14Low noise turbine for geared gas turbine engine
472014027112109/18/14Gas turbine engine architecture with intercooled twin centrifugal compressor
482014027113509/18/14Turbofan engine bearing and gearbox arrangement
492014027117809/18/14Fan blades for gas turbine engines with reduced stress concentration at leading edge
502014027122109/18/14Usage of a witness mark to distinguish support structure from part
512014027245609/18/14Spallation-resistant thermal barrier coating
522014027374709/18/14Removing material from a workpiece with a water jet
532014027375709/18/14Drag finishing system, method and fixture for gas turbine engine airfoils
542014027453109/18/14Fan drive planetary gear system integrated carrier and torque frame
552014025086209/11/14Reverse flow gas turbine engine airflow bypass
562014025086309/11/14Rear mounted reverse core engine thrust reverser
572014025089509/11/14Modulated ejector cooling
582014025138109/11/14Pulse jet liquid gas cleaning system
592014025179109/11/14Cathodic arc deposition stinger
602014025180309/11/14Cathodic arc mask assembly lock system
612014025216009/11/14Reverse flow gas turbine engine removable core
622014025216109/11/14De-couple geared turbo-fan engine and aircraft
632014025216209/11/14Uav launching from moving platform
642014025216709/11/14Reverse core engine thrust reverser for under wing
652014025218309/11/14Sensor hoop storage and transport apparatus
662014025276409/11/14Two-piece self-locking mechanism for tube assemblies
672014025463109/11/14Actively cooled gas turbine sensor probe housing
682014025511209/11/14Broach tool rake face with a tailored surface topography
692014025514409/11/14Flanged bushing for variable vane
702014025515609/11/14Non-contacting seals for geared gas turbine engine bearing compartments
712014025515809/11/14Coating process for gas turbine engine component with cooling holes
722014025516209/11/14Adjustable floating oil channel for gas turbine engine gear drive
732014025516709/11/14Consumable assembly tool for a gas turbine engine
742014025516809/11/14Inter-module flow discourager
752014025517209/11/14Low profile push-lock device
762014025517409/11/14Manufacture of full ring strut vane pack
772014025518209/11/14Push-lock pin connector
782014025519609/11/14Double split blade lock ring
792014025519809/11/14Turbine disk fabrication with in situ material property variation
802014025520209/11/14Turbine engine nosecone with deformation region
812014024574909/04/14Nacelle anti-ice valve utilized as compressor stability bleed valve during starting
822014024575009/04/14Circumferentially retained fairing
832014024575109/04/14Passages to facilitate a secondary flow between components
842014024575309/04/14Gas turbine engine rotor blade
852014024651409/04/14Turbomachine thrust reverser
862014024811509/04/14Active clearance control system with zone controls
872014024811609/04/14Acoustic treatment in an unducted area of a geared turbomachine
882014024812609/04/14Inter-module finger seal
892014024812709/04/14Turbine engine component with dual purpose rib
902014024812809/04/14Seals for a circumferential stop ring in a turbine exhaust case
912014024812909/04/14Lpc flowpath shape with gas turbine engine shaft bearing configuration
922014024813009/04/14Seal hook mount structure with overlapped coating
932014024813609/04/14Multifunction positioning lock washer
942014024815209/04/14Plate for directing flow and film cooling of components
952014024815609/04/14Composite articles and methods
962014023799008/28/14Variable area fan nozzle with wall thickness distribution
972014023802708/28/14Thermally compliant dual wall liner for a gas turbine engine
982014023908308/28/14Pivot thrust reverser surrounding inner surface of bypass duct
992014023908408/28/14Tandem thrust reverser with sliding rails
1002014024185108/28/14Axial oil scoop for a gas turbine engine
1012014024185608/28/14Gas turbine engine systems involving tip fans
1022014024185708/28/14Flow diverter to redirect secondary flow
1032014024187408/28/14Wear liner spring seal
1042014024189708/28/14Aluminum brazing of hollow titanium fan blades
1052014024227808/28/14Split coating mask system for gas turbine engine component
1062014023024608/21/14Thermally free hanger with length adjustment feature
1072014023040308/21/14Gas turbine engine shaft bearing configuration
1082014023045208/21/14Planetary gear system arrangement with auxiliary oil system
1092014023094308/21/14Support system bumper for exhaust duct liner hanger
1102014023143708/21/14Cap drain plug
1112014023407808/21/14Method for setting a gear ratio of a fan drive gear system of a gas turbine engine
1122014023407908/21/14Geared architecture for high speed and small volume fan drive turbine
1132014023408508/21/14Bushing arranged between a body and a shaft, and connected to the shaft
1142014023408608/21/14Bushing arranged between a body and a shaft, and connected to the shaft
1152014023408708/21/14Inlet guide vane retention feature
1162014023409808/21/14Turbine case retention hook with insert
1172014022391608/14/14Gas turbine engine with compressor inlet guide vane positioned for starting
1182014022391908/14/14Flexible liner hanger
1192014022392008/14/14Consumable assembly mistake proofing tool for a gas turbine engine
1202014022538808/14/14Latch release mechanism
1212014022693008/14/14Test equipment with housing damping system
1222014022707808/14/14Mid-turbine frame vane assembly support with retention unit
1232014022708408/14/14Compound star gear system with rolling element bearings
1242014022708708/14/14Blade outer air seal surface
1252014022709308/14/14Low profile thermally free blind liner hanger attachment for complex shapes
1262014021599708/07/14Flexible shield for fluid connectors
1272014021600208/07/14Gas turbine engine having slim-line nacelle
1282014021600308/07/14Gas turbine engine with geared turbofan and oil thermal management system
1292014021600508/07/14Gas turbine engine assembly including a thrust reverser
1302014021604208/07/14Combustor component with cooling holes formed by additive manufacturing
1312014021605608/07/14Heat exchange module for a turbine engine
1322014021651308/07/14High zt thermoelectric with reversible junction
1332014021977208/07/14Individual inlet guide vane control for tip turbine engine
1342014021977408/07/14Turbomachine geared architecture support assembly
1352014021977808/07/14Gas turbine engine airfoil with vane platform cooling passage
1362014021978308/07/14Gas turbine engine fan drive gear system damper
1372014021978508/07/14Vane arm having a claw
1382014021979108/07/14Lug for preventing rotation of a stator vane arrangement relative to a turbine engine case
1392014021979208/07/14Pylon matched fan exit guide vane for noise reduction in a geared turbofan engine
1402014021979308/07/14Health monitoring for hollow blades
1412014021979408/07/14Bore cavity thermal conditioning system
1422014021980708/07/14Under-root spacer for gas turbine engine fan blade
1432014021980808/07/14Sheath with extended wings
1442014021981508/07/14Multi-lobed cooling hole
1452014022231008/07/14Engine monitor for a multi-engine system
1462014020871407/31/14Thermal management for gas turbine engine
1472014020877107/31/14Gas turbine engine component cooling arrangement
1482014020883707/31/14Gas turbine engine vane embedded beam interrupt optical tip-timing probe system
1492014021099207/31/14Infrared thermography with laser
1502014021226007/31/14Airfoil assembly with paired endwall contouring
1512014021226107/31/14Lightweight shrouded fan
1522014021226207/31/14Variable outer air seal support
1532014021226307/31/14Airfoil with variable profile responsive to thermal conditions
1542014021227007/31/14Gas turbine engine component having suction side cutback opening
1552014021227607/31/14Variable outer air seal fluid control
1562014021228107/31/14Flow feed diffuser
1572014021229207/31/14Airfoil member and composite platform having contoured endwall
1582014021229707/31/14Gas turbine engine serpentine cooling passage with chevrons
1592014021229807/31/14Gas turbine engine turbine blade tip cooling
1602014021278707/31/14Multiple transition flow field and method
1612014021278807/31/14Fuel cell and membrane therefore
1622014020213307/24/14Gas turbine engine mid turbine frame with flow turning features
1632014020217007/24/14Composite articles and methods
1642014020543807/24/14Relationship between fan and primary exhaust stream velocities in a geared gas turbine engine
1652014020545207/24/14Wind turbine blade
1662014020546107/24/14Vacuum degassing laser-blocking material system and procses
1672014020546207/24/14Hvata-hybrid vertical axis turbine assembly operable under omni-directional flow for power generating systems
1682014020549307/24/14High temperature directionally solidified and single crystal die casting
1692014020649607/24/14Method of assembly for gas turbine fan drive gear system
1702014019643307/17/14Gas turbine engine component platform cooling
1712014019643407/17/14Shroud for sealing conduit feed-through
1722014019647007/17/14Gas turbine engine buffer system
1732014019647107/17/14Fan drive gear system flexible support features
1742014019647207/17/14Geared turbofan gas turbine engine architecture
1752014019647307/17/14Geared turbofan gas turbine engine architecture
1762014019917607/17/14Gas turbine engine nose cone attachment configuration
1772014019917707/17/14Airfoil and method of making
1782014019949007/17/14Deposition substrate temperature and monitoring
1792014019016707/10/14Ceramic combustor can for a gas turbine engine
1802014019017507/10/143d non-axisymmetric combustor liner
1812014019018107/10/14Rotor cover plate
1822014019065407/10/14Cast features for a turbine engine airfoil
1832014019323807/10/14Method for setting a gear ratio of a fan drive gear system of a gas turbine engine
1842014019324607/10/14Cooling hole with crenellation features
1852014019325107/10/14Stator anti-rotation device
1862014019326707/10/14Dmz fracture boundary limit
1872014019424007/10/14Journal pin oil supply for gear system
1882014019427207/10/14Method of treating a preceramic material
1892014018229207/03/14Integral instrumentation in additively manufactured components of gas turbine engines
1902014018229307/03/14Compressor rotor for gas turbine engine with deep blade groove
1912014018230807/03/14Gas turbine engine with v-band clamp connection for collector box
1922014018230907/03/14Geared gas turbine engine exhaust nozzle with chevrons
1932014018280907/03/14Mullite-containing investment casting core
1942014018297207/03/14Case with integral lubricant scavenge passage
1952014018316407/03/14Non-line of sight electro discharge machining system
1962014018329607/03/14Gas turbine engine having fan rotor driven by turbine exhaust and with a bypass
1972014018382507/03/14Finger seal
1982014018609807/03/14Work piece having self-supporting gusset and method related thereto
1992014018615207/03/14Blade outer air seal system for controlled tip clearance
2002014018615807/03/14Gas turbine engine shaft bearing configuration
2012014018616007/03/14Slider seal
2022014018616307/03/14Blade outer air seal having shiplap structure
2032014018616407/03/14Non-line of sight electro discharge machined part
2042014018616507/03/14Adhesive pattern for fan case conformable liner
2052014018616707/03/14Multi-piece fairing for monolithic turbine exhaust case
2062014018616807/03/14Component retention with probe
2072014018619007/03/14Tip leakage flow directionality control
2082014018620007/03/14Fan blade adjustment piezoelectric actuator
2092014018620507/03/14Reconditioning oxidized powder
2102014018665607/03/14Spallation-resistant thermal barrier coating
2112014017388106/26/14Blind installation pin for a gas turbine engine mount
2122014017389606/26/14Holding a combustor panel during coating process
2132014017389706/26/14Anti-torsion assembly
2142014017405506/26/14Turbine section of high bypass turbofan
2152014017405606/26/14Gas turbine engine with low stage count low pressure turbine
2162014017408806/26/14Alignment system and methodology to account for variation in a gas turbine engine
2172014017409106/26/14Repair procedure for a gas turbine engine via variable polarity welding
2182014017409206/26/14Closure of cooling holes with a filling agent
2192014017409406/26/14Apu exhaust housing perforated ring
2202014017409806/26/14Turbine disc with reduced neck stress concentration
2212014017416206/26/14Ignitor plug isolation chamber (ipic) for a gas turbine engine
2222014017425206/26/14Mount with an axial upstream linkage for conneting a gearbox to a turbine engine case
2232014017485506/26/14Pressurized reserve lubrication system for a gas turbine engine
2242014017502706/26/14Fuel system with electrically heated filter screen
2252014017817406/26/14Gas turbine engine including a pre-diffuser heat exchanger
2262014017817506/26/14Air turbine starter monitor system
2272014017818506/26/14Egress seal assembly
2282014017819606/26/14Turbomachine with clamp coupling shaft and rotor hub together
2292014017824106/26/14Absorbed impurities reduction in additive manufacturing systems
2302014017824406/26/14Gaseous based desulfurization of alloys
2312014017824506/26/14Low sulfur nickel base substrate alloy and overlay coating system
2322014017871006/26/14Alloying interlayer for electroplated aluminum on aluminum alloys
2332014016537606/19/14Cat arc process and part holding apparatus
2342014016553006/19/14Bi-directional auxiliary lubrication system
2352014016553406/19/14Gas turbine engine compressor arrangement
2362014016557006/19/14Oscillating heat pipe for thermal management of gas turbine engines
2372014016557506/19/14Nozzle section for a gas turbine engine
2382014016557806/19/14Ovate swirler assembly for combustors
2392014016557906/19/14High pressure turbine speed calculation from fuel system hydraulic pressures
2402014016558206/19/14Cross-flow turbine engine
2412014016558506/19/14Oblong swirler assembly for combustors
2422014016558606/19/14Turbine start method
2432014016558806/19/14Turbo compressor for bleed air
2442014016558906/19/14Gas turbine engine with accessory gear box
2452014016559106/19/14Turbine under platform air seal strip
2462014016559306/19/14Gas turbine engine turbine blade leading edge tip trench cooling
2472014016573606/19/14Traversing time of arrival probe
2482014016576206/19/14Fan drive gear system assembly guide
2492014016614406/19/14Composite ducts and methods

ARCHIVE: New 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



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