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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



Fireshield fastener hood

United Technologies

Fireshield fastener hood

Split ring valve

United Technologies

Split ring valve

Search recent Press Releases: United Technologies Corporation-related press releases
Count Application # Date United Technologies Corporation patents (updated weekly) - BOOKMARK this page
12015002710101/29/15 new patent  Geared gas turbine engine architecture for enhanced efficiency
22015002713001/29/15 new patent  Split ring valve
32015002765701/29/15 new patent  Method and casting core for forming a landing for welding a baffle inserted in an airfoil
42015003044001/29/15 new patent  Fireshield fastener hood
52015003044301/29/15 new patent  Split damped outer shroud for gas turbine engine stator arrays
62015002378001/22/15Liner attaching scheme
72015002429601/22/15Method and system for operating a flow battery system based on energy costs
82015001330101/15/15Turbine engine including balanced low pressure stage count
92015001334401/15/15Tube
102015001348001/15/15Plated instrumentation probes and sensors
112015001393401/15/15Article with grouped grain patterns
122015001695401/15/15Blade outer air seal assembly and support
132015001696501/15/15Link arm drag reducing device
142015000826801/08/15Pivot thrust reverser with multi-point actuation
152015000008901/01/15Clamp connector
162015000030301/01/15Wireless power for gas turbine engine instrumentation
172015000030401/01/15Removable nosecone for a gas turbine engine
182015000395601/01/15Variable vane scheduling
192015000396801/01/15Gas turbine engine with attached nosecone
202015000399501/01/15Aircraft engine component with locally tailored materials
212015000399701/01/15Method of forming hybrid metal ceramic components
222014037354912/25/14Cooling hole with curved metering section
232014037355412/25/14Air turbine starter pressure monitor system
242014037361012/25/14Engine inspection apparatus and system
252014037505612/25/14Method of operating a power generation system
262014036654812/18/14Turbine engine gearbox
272014036655412/18/14Cross reference to related applications
282014036655612/18/14Gas turbine engine vane-to-transition duct seal
292014036661312/18/14Probe retention-sealing feature
302014036978312/18/14Self-retaining shear pin for blind mount location
312014036980412/18/14Variable bleed slot in centrifugal impeller
322014036981812/18/14Planetary gear system arrangement with auxiliary oil system
332014036015212/11/14Oil tank mount with yoke
342014036015312/11/14Gas turbine engine thermal management system
352014036330512/11/14Hybrid turbine blade for improved engine performance or architecture
362014035656012/04/14Castings and manufacture methods
372014035839812/04/14Use of ss data trends in fault resolution process
382014035850012/04/14Probalistic high cycle fatigue (hcf) design optimization process
392014034857711/27/14Tie bolt employing differential thread
402014034863011/27/14Noise reducing vane
412014034864011/27/14Thrust efficient turbofan engine
422014033833611/20/14Gas turbine engine combustor with integrated combustor vane
432014033835111/20/14Gas turbine engine combustor with tailored temperature profile
442014033835711/20/14Cavity swirl fuel injector for an augmentor section of a gas turbine engine
452014033836011/20/14Bleed port ribs for turbomachine case
462014033219111/13/14Extreme environment heat exchanger
472014033491611/13/14Borescope inspection port fitting
482014032684211/06/14Oil tank mount with stiffeners
492014031813310/30/14Thrust efficient turbofan engine
502014031814310/30/14Multi-circuit buffer system for a gas turbine engine
512014031814710/30/14Low noise compressor rotor for geared turbofan engine
522014032196110/30/14Mate face cooling holes for gas turbine engine component
532014032302210/30/14Airfoil edge form transfer grinding tool
542014032436310/30/14System reliability analysis and management using physics-based models embedded in a baysian network
552014031112110/23/14Pulse detonation engine having a scroll ejector attenuator
562014031114910/23/14Gas turbine engine fan blade airfoil profile
572014031261110/23/14Locking fluid fittings
582014031454010/23/14Gas turbine engine synchronization ring
592014031454110/23/14Turbomachine thrust balancing system
602014031454210/23/14Gas turbine engine exhaust diffuser with movable struts
612014031454610/23/14Turbine engine gearbox mount with multiple fuse joints
622014031454710/23/14Attachment ceramic matrix composite materials
632014031458110/23/14Method for forming single crystal parts using additive manufacturing and remelt
642014029878810/09/14Gas turbine engine including pneumatic actuator system
652014030142510/09/14Backstrike detection system for laser drilling thin materials
662014030182910/09/14Engine bearing support
672014029021110/02/14Turbine engine including balanced low pressure stage count
682014029021310/02/14Duct blocker seal assembly for a gas turbine engine
692014029026910/02/14Duct blocker seal assembly for a gas turbine engine
702014029455810/02/14Turbomachine fluid delivery manifold and system
712014028350009/25/14Thrust efficient turbofan engine
722014028350109/25/14Elongated geared turbofan with high bypass ratio
732014028674809/25/14Fan containment case with thermally conforming liner
742014028675409/25/14Elongated geared turbofan with high bypass ratio
752014028675509/25/14Ring gear mounting arrangement with oil scavenge scheme
762014028678109/25/14Integral fan blade wear pad and platform seal
772014025966109/18/14Variable area fan nozzle with wall thickness distribution
782014026017609/18/14Lube tube expansion and torque retaining device
792014026018209/18/14Free stream intake for reverse core engine
802014026018309/18/14Variable cycle intake for reverse core engine
812014026032109/18/14Gas turbine engine static structure joint with undercuts
822014026179709/18/14Tube fitting having integrated tee fitting
832014026810009/18/14Multiple laser time of arrival probe
842014026981709/18/14Phosphor thermometry fiber sensor
852014027062509/18/14High temperature uncooled optical probe
862014027110109/18/14Modulated turbine vane cooling
872014027111209/18/14Low noise turbine for geared gas turbine engine
882014027112109/18/14Gas turbine engine architecture with intercooled twin centrifugal compressor
892014027113509/18/14Turbofan engine bearing and gearbox arrangement
902014027117809/18/14Fan blades for gas turbine engines with reduced stress concentration at leading edge
912014027122109/18/14Usage of a witness mark to distinguish support structure from part
922014027245609/18/14Spallation-resistant thermal barrier coating
932014027374709/18/14Removing material from a workpiece with a water jet
942014027375709/18/14Drag finishing system, method and fixture for gas turbine engine airfoils
952014027453109/18/14Fan drive planetary gear system integrated carrier and torque frame
962014025086209/11/14Reverse flow gas turbine engine airflow bypass
972014025086309/11/14Rear mounted reverse core engine thrust reverser
982014025089509/11/14Modulated ejector cooling
992014025138109/11/14Pulse jet liquid gas cleaning system
1002014025179109/11/14Cathodic arc deposition stinger
1012014025180309/11/14Cathodic arc mask assembly lock system
1022014025216009/11/14Reverse flow gas turbine engine removable core
1032014025216109/11/14De-couple geared turbo-fan engine and aircraft
1042014025216209/11/14Uav launching from moving platform
1052014025216709/11/14Reverse core engine thrust reverser for under wing
1062014025218309/11/14Sensor hoop storage and transport apparatus
1072014025276409/11/14Two-piece self-locking mechanism for tube assemblies
1082014025463109/11/14Actively cooled gas turbine sensor probe housing
1092014025511209/11/14Broach tool rake face with a tailored surface topography
1102014025514409/11/14Flanged bushing for variable vane
1112014025515609/11/14Non-contacting seals for geared gas turbine engine bearing compartments
1122014025515809/11/14Coating process for gas turbine engine component with cooling holes
1132014025516209/11/14Adjustable floating oil channel for gas turbine engine gear drive
1142014025516709/11/14Consumable assembly tool for a gas turbine engine
1152014025516809/11/14Inter-module flow discourager
1162014025517209/11/14Low profile push-lock device
1172014025517409/11/14Manufacture of full ring strut vane pack
1182014025518209/11/14Push-lock pin connector
1192014025519609/11/14Double split blade lock ring
1202014025519809/11/14Turbine disk fabrication with in situ material property variation
1212014025520209/11/14Turbine engine nosecone with deformation region
1222014024574909/04/14Nacelle anti-ice valve utilized as compressor stability bleed valve during starting
1232014024575009/04/14Circumferentially retained fairing
1242014024575109/04/14Passages to facilitate a secondary flow between components
1252014024575309/04/14Gas turbine engine rotor blade
1262014024651409/04/14Turbomachine thrust reverser
1272014024811509/04/14Active clearance control system with zone controls
1282014024811609/04/14Acoustic treatment in an unducted area of a geared turbomachine
1292014024812609/04/14Inter-module finger seal
1302014024812709/04/14Turbine engine component with dual purpose rib
1312014024812809/04/14Seals for a circumferential stop ring in a turbine exhaust case
1322014024812909/04/14Lpc flowpath shape with gas turbine engine shaft bearing configuration
1332014024813009/04/14Seal hook mount structure with overlapped coating
1342014024813609/04/14Multifunction positioning lock washer
1352014024815209/04/14Plate for directing flow and film cooling of components
1362014024815609/04/14Composite articles and methods
1372014023799008/28/14Variable area fan nozzle with wall thickness distribution
1382014023802708/28/14Thermally compliant dual wall liner for a gas turbine engine
1392014023908308/28/14Pivot thrust reverser surrounding inner surface of bypass duct
1402014023908408/28/14Tandem thrust reverser with sliding rails
1412014024185108/28/14Axial oil scoop for a gas turbine engine
1422014024185608/28/14Gas turbine engine systems involving tip fans
1432014024185708/28/14Flow diverter to redirect secondary flow
1442014024187408/28/14Wear liner spring seal
1452014024189708/28/14Aluminum brazing of hollow titanium fan blades
1462014024227808/28/14Split coating mask system for gas turbine engine component
1472014023024608/21/14Thermally free hanger with length adjustment feature
1482014023040308/21/14Gas turbine engine shaft bearing configuration
1492014023045208/21/14Planetary gear system arrangement with auxiliary oil system
1502014023094308/21/14Support system bumper for exhaust duct liner hanger
1512014023143708/21/14Cap drain plug
1522014023407808/21/14Method for setting a gear ratio of a fan drive gear system of a gas turbine engine
1532014023407908/21/14Geared architecture for high speed and small volume fan drive turbine
1542014023408508/21/14Bushing arranged between a body and a shaft, and connected to the shaft
1552014023408608/21/14Bushing arranged between a body and a shaft, and connected to the shaft
1562014023408708/21/14Inlet guide vane retention feature
1572014023409808/21/14Turbine case retention hook with insert
1582014022391608/14/14Gas turbine engine with compressor inlet guide vane positioned for starting
1592014022391908/14/14Flexible liner hanger
1602014022392008/14/14Consumable assembly mistake proofing tool for a gas turbine engine
1612014022538808/14/14Latch release mechanism
1622014022693008/14/14Test equipment with housing damping system
1632014022707808/14/14Mid-turbine frame vane assembly support with retention unit
1642014022708408/14/14Compound star gear system with rolling element bearings
1652014022708708/14/14Blade outer air seal surface
1662014022709308/14/14Low profile thermally free blind liner hanger attachment for complex shapes
1672014021599708/07/14Flexible shield for fluid connectors
1682014021600208/07/14Gas turbine engine having slim-line nacelle
1692014021600308/07/14Gas turbine engine with geared turbofan and oil thermal management system
1702014021600508/07/14Gas turbine engine assembly including a thrust reverser
1712014021604208/07/14Combustor component with cooling holes formed by additive manufacturing
1722014021605608/07/14Heat exchange module for a turbine engine
1732014021651308/07/14High zt thermoelectric with reversible junction
1742014021977208/07/14Individual inlet guide vane control for tip turbine engine
1752014021977408/07/14Turbomachine geared architecture support assembly
1762014021977808/07/14Gas turbine engine airfoil with vane platform cooling passage
1772014021978308/07/14Gas turbine engine fan drive gear system damper
1782014021978508/07/14Vane arm having a claw
1792014021979108/07/14Lug for preventing rotation of a stator vane arrangement relative to a turbine engine case
1802014021979208/07/14Pylon matched fan exit guide vane for noise reduction in a geared turbofan engine
1812014021979308/07/14Health monitoring for hollow blades
1822014021979408/07/14Bore cavity thermal conditioning system
1832014021980708/07/14Under-root spacer for gas turbine engine fan blade
1842014021980808/07/14Sheath with extended wings
1852014021981508/07/14Multi-lobed cooling hole
1862014022231008/07/14Engine monitor for a multi-engine system
1872014020871407/31/14Thermal management for gas turbine engine
1882014020877107/31/14Gas turbine engine component cooling arrangement
1892014020883707/31/14Gas turbine engine vane embedded beam interrupt optical tip-timing probe system
1902014021099207/31/14Infrared thermography with laser
1912014021226007/31/14Airfoil assembly with paired endwall contouring
1922014021226107/31/14Lightweight shrouded fan
1932014021226207/31/14Variable outer air seal support
1942014021226307/31/14Airfoil with variable profile responsive to thermal conditions
1952014021227007/31/14Gas turbine engine component having suction side cutback opening
1962014021227607/31/14Variable outer air seal fluid control
1972014021228107/31/14Flow feed diffuser
1982014021229207/31/14Airfoil member and composite platform having contoured endwall
1992014021229707/31/14Gas turbine engine serpentine cooling passage with chevrons
2002014021229807/31/14Gas turbine engine turbine blade tip cooling
2012014021278707/31/14Multiple transition flow field and method
2022014021278807/31/14Fuel cell and membrane therefore
2032014020213307/24/14Gas turbine engine mid turbine frame with flow turning features
2042014020217007/24/14Composite articles and methods
2052014020543807/24/14Relationship between fan and primary exhaust stream velocities in a geared gas turbine engine
2062014020545207/24/14Wind turbine blade
2072014020546107/24/14Vacuum degassing laser-blocking material system and procses
2082014020546207/24/14Hvata-hybrid vertical axis turbine assembly operable under omni-directional flow for power generating systems
2092014020549307/24/14High temperature directionally solidified and single crystal die casting
2102014020649607/24/14Method of assembly for gas turbine fan drive gear system
2112014019643307/17/14Gas turbine engine component platform cooling
2122014019643407/17/14Shroud for sealing conduit feed-through
2132014019647007/17/14Gas turbine engine buffer system
2142014019647107/17/14Fan drive gear system flexible support features
2152014019647207/17/14Geared turbofan gas turbine engine architecture
2162014019647307/17/14Geared turbofan gas turbine engine architecture
2172014019917607/17/14Gas turbine engine nose cone attachment configuration
2182014019917707/17/14Airfoil and making
2192014019949007/17/14Deposition substrate temperature and monitoring
2202014019016707/10/14Ceramic combustor can for a gas turbine engine
2212014019017507/10/143d non-axisymmetric combustor liner
2222014019018107/10/14Rotor cover plate
2232014019065407/10/14Cast features for a turbine engine airfoil
2242014019323807/10/14Method for setting a gear ratio of a fan drive gear system of a gas turbine engine
2252014019324607/10/14Cooling hole with crenellation features
2262014019325107/10/14Stator anti-rotation device
2272014019326707/10/14Dmz fracture boundary limit
2282014019424007/10/14Journal pin oil supply for gear system
2292014019427207/10/14Method of treating a preceramic material
2302014018229207/03/14Integral instrumentation in additively manufactured components of gas turbine engines
2312014018229307/03/14Compressor rotor for gas turbine engine with deep blade groove
2322014018230807/03/14Gas turbine engine with v-band clamp connection for collector box
2332014018230907/03/14Geared gas turbine engine exhaust nozzle with chevrons
2342014018280907/03/14Mullite-containing investment casting core
2352014018297207/03/14Case with integral lubricant scavenge passage
2362014018316407/03/14Non-line of sight electro discharge machining system
2372014018329607/03/14Gas turbine engine having fan rotor driven by turbine exhaust and with a bypass
2382014018382507/03/14Finger seal
2392014018609807/03/14Work piece having self-supporting gusset and method related thereto
2402014018615207/03/14Blade outer air seal system for controlled tip clearance
2412014018615807/03/14Gas turbine engine shaft bearing configuration
2422014018616007/03/14Slider seal
2432014018616307/03/14Blade outer air seal having shiplap structure
2442014018616407/03/14Non-line of sight electro discharge machined part
2452014018616507/03/14Adhesive pattern for fan case conformable liner
2462014018616707/03/14Multi-piece fairing for monolithic turbine exhaust case
2472014018616807/03/14Component retention with probe
2482014018619007/03/14Tip leakage flow directionality control
2492014018620007/03/14Fan blade adjustment piezoelectric actuator


ARCHIVE: New 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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