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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


Ball-end milling cutter tool

United Technologies

Ball-end milling cutter tool

Background radiation measurement system

United Technologies

Background radiation measurement system

Search recent Press Releases: United Technologies Corporation-related press releases
Count Application # Date United Technologies Corporation patents (updated weekly) - BOOKMARK this page
12015008294503/26/15 new patent  Process for producing refractory metal alloy powders
22015008391903/26/15 new patent  Background radiation measurement system
32015008626203/26/15 new patent  Welded assemblies and methods of making welded assemblies
42015008628303/26/15 new patent  Ball-end milling cutter tool
52015007574503/19/15Casting molds, manufacture and use methods
62015007891503/19/15Piloted nut
72015006820903/12/15Method for determining circumferential sensor positioning
82015006821003/12/15Tube fed tangential on-board injector for gas turbine engine
92015006821403/12/15Low thermal mass joint
102015006966803/12/15Multi-dimensional component build system and process
112015007170403/12/15Exhaust duct liner rod hanger
122015006000203/05/15Die casting system and cell
132015006528503/05/15Geared architecture gas turbine engine with oil scavenge
142015005287302/26/15Torque connector lubrication scuppers
152015005290702/26/15Thermal management system for gas turbine engine
162015005378902/26/15Linkage to control and restrain flap movement
172015005012702/19/15Air with integral spring for a gas turbine engine exhaust drive
182015005104002/19/15Oil baffle for gas turbine fan drive gear system
192015004202302/12/15Hybrid part made from monolithic ceramic skin and cmc core
202015004402802/12/15Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
212015004405202/12/15Geared turbofan with fan blades designed to achieve laminar flow
222015004520002/12/15Ceramic component
232015003760202/05/15System and high temperature die casting tooling
242015002710101/29/15Geared gas turbine engine architecture for enhanced efficiency
252015002713001/29/15Split ring valve
262015002765701/29/15Method and casting core for forming a landing for welding a baffle inserted in an airfoil
272015003044001/29/15Fireshield fastener hood
282015003044301/29/15Split damped outer shroud for gas turbine engine stator arrays
292015002378001/22/15Liner attaching scheme
302015002429601/22/15Method and system for operating a flow battery system based on energy costs
312015001330101/15/15Turbine engine including balanced low pressure stage count
322015001334401/15/15Tube
332015001348001/15/15Plated instrumentation probes and sensors
342015001393401/15/15Article with grouped grain patterns
352015001695401/15/15Blade outer air seal assembly and support
362015001696501/15/15Link arm drag reducing device
372015000826801/08/15Pivot thrust reverser with multi-point actuation
382015000008901/01/15Clamp connector
392015000030301/01/15Wireless power for gas turbine engine instrumentation
402015000030401/01/15Removable nosecone for a gas turbine engine
412015000395601/01/15Variable vane scheduling
422015000396801/01/15Gas turbine engine with attached nosecone
432015000399501/01/15Aircraft engine component with locally tailored materials
442015000399701/01/15Method of forming hybrid metal ceramic components
452014037354912/25/14Cooling hole with curved metering section
462014037355412/25/14Air turbine starter pressure monitor system
472014037361012/25/14Engine inspection apparatus and system
482014037505612/25/14Method of operating a power generation system
492014036654812/18/14Turbine engine gearbox
502014036655412/18/14Cross reference to related applications
512014036655612/18/14Gas turbine engine vane-to-transition duct seal
522014036661312/18/14Probe retention-sealing feature
532014036978312/18/14Self-retaining shear pin for blind mount location
542014036980412/18/14Variable bleed slot in centrifugal impeller
552014036981812/18/14Planetary gear system arrangement with auxiliary oil system
562014036015212/11/14Oil tank mount with yoke
572014036015312/11/14Gas turbine engine thermal management system
582014036330512/11/14Hybrid turbine blade for improved engine performance or architecture
592014035656012/04/14Castings and manufacture methods
602014035839812/04/14Use of ss data trends in fault resolution process
612014035850012/04/14Probalistic high cycle fatigue (hcf) design optimization process
622014034857711/27/14Tie bolt employing differential thread
632014034863011/27/14Noise reducing vane
642014034864011/27/14Thrust efficient turbofan engine
652014033833611/20/14Gas turbine engine combustor with integrated combustor vane
662014033835111/20/14Gas turbine engine combustor with tailored temperature profile
672014033835711/20/14Cavity swirl fuel injector for an augmentor section of a gas turbine engine
682014033836011/20/14Bleed port ribs for turbomachine case
692014033219111/13/14Extreme environment heat exchanger
702014033491611/13/14Borescope inspection port fitting
712014032684211/06/14Oil tank mount with stiffeners
722014031813310/30/14Thrust efficient turbofan engine
732014031814310/30/14Multi-circuit buffer system for a gas turbine engine
742014031814710/30/14Low noise compressor rotor for geared turbofan engine
752014032196110/30/14Mate face cooling holes for gas turbine engine component
762014032302210/30/14Airfoil edge form transfer grinding tool
772014032436310/30/14System reliability analysis and management using physics-based models embedded in a baysian network
782014031112110/23/14Pulse detonation engine having a scroll ejector attenuator
792014031114910/23/14Gas turbine engine fan blade airfoil profile
802014031261110/23/14Locking fluid fittings
812014031454010/23/14Gas turbine engine synchronization ring
822014031454110/23/14Turbomachine thrust balancing system
832014031454210/23/14Gas turbine engine exhaust diffuser with movable struts
842014031454610/23/14Turbine engine gearbox mount with multiple fuse joints
852014031454710/23/14Attachment ceramic matrix composite materials
862014031458110/23/14Method for forming single crystal parts using additive manufacturing and remelt
872014029878810/09/14Gas turbine engine including pneumatic actuator system
882014030142510/09/14Backstrike detection system for laser drilling thin materials
892014030182910/09/14Engine bearing support
902014029021110/02/14Turbine engine including balanced low pressure stage count
912014029021310/02/14Duct blocker seal assembly for a gas turbine engine
922014029026910/02/14Duct blocker seal assembly for a gas turbine engine
932014029455810/02/14Turbomachine fluid delivery manifold and system
942014028350009/25/14Thrust efficient turbofan engine
952014028350109/25/14Elongated geared turbofan with high bypass ratio
962014028674809/25/14Fan containment case with thermally conforming liner
972014028675409/25/14Elongated geared turbofan with high bypass ratio
982014028675509/25/14Ring gear mounting arrangement with oil scavenge scheme
992014028678109/25/14Integral fan blade wear pad and platform seal
1002014025966109/18/14Variable area fan nozzle with wall thickness distribution
1012014026017609/18/14Lube tube expansion and torque retaining device
1022014026018209/18/14Free stream intake for reverse core engine
1032014026018309/18/14Variable cycle intake for reverse core engine
1042014026032109/18/14Gas turbine engine static structure joint with undercuts
1052014026179709/18/14Tube fitting having integrated tee fitting
1062014026810009/18/14Multiple laser time of arrival probe
1072014026981709/18/14Phosphor thermometry fiber sensor
1082014027062509/18/14High temperature uncooled optical probe
1092014027110109/18/14Modulated turbine vane cooling
1102014027111209/18/14Low noise turbine for geared gas turbine engine
1112014027112109/18/14Gas turbine engine architecture with intercooled twin centrifugal compressor
1122014027113509/18/14Turbofan engine bearing and gearbox arrangement
1132014027117809/18/14Fan blades for gas turbine engines with reduced stress concentration at leading edge
1142014027122109/18/14Usage of a witness mark to distinguish support structure from part
1152014027245609/18/14Spallation-resistant thermal barrier coating
1162014027374709/18/14Removing material from a workpiece with a water jet
1172014027375709/18/14Drag finishing system, method and fixture for gas turbine engine airfoils
1182014027453109/18/14Fan drive planetary gear system integrated carrier and torque frame
1192014025086209/11/14Reverse flow gas turbine engine airflow bypass
1202014025086309/11/14Rear mounted reverse core engine thrust reverser
1212014025089509/11/14Modulated ejector cooling
1222014025138109/11/14Pulse jet liquid gas cleaning system
1232014025179109/11/14Cathodic arc deposition stinger
1242014025180309/11/14Cathodic arc mask assembly lock system
1252014025216009/11/14Reverse flow gas turbine engine removable core
1262014025216109/11/14De-couple geared turbo-fan engine and aircraft
1272014025216209/11/14Uav launching from moving platform
1282014025216709/11/14Reverse core engine thrust reverser for under wing
1292014025218309/11/14Sensor hoop storage and transport apparatus
1302014025276409/11/14Two-piece self-locking mechanism for tube assemblies
1312014025463109/11/14Actively cooled gas turbine sensor probe housing
1322014025511209/11/14Broach tool rake face with a tailored surface topography
1332014025514409/11/14Flanged bushing for variable vane
1342014025515609/11/14Non-contacting seals for geared gas turbine engine bearing compartments
1352014025515809/11/14Coating process for gas turbine engine component with cooling holes
1362014025516209/11/14Adjustable floating oil channel for gas turbine engine gear drive
1372014025516709/11/14Consumable assembly tool for a gas turbine engine
1382014025516809/11/14Inter-module flow discourager
1392014025517209/11/14Low profile push-lock device
1402014025517409/11/14Manufacture of full ring strut vane pack
1412014025518209/11/14Push-lock pin connector
1422014025519609/11/14Double split blade lock ring
1432014025519809/11/14Turbine disk fabrication with in situ material property variation
1442014025520209/11/14Turbine engine nosecone with deformation region
1452014024574909/04/14Nacelle anti-ice valve utilized as compressor stability bleed valve during starting
1462014024575009/04/14Circumferentially retained fairing
1472014024575109/04/14Passages to facilitate a secondary flow between components
1482014024575309/04/14Gas turbine engine rotor blade
1492014024651409/04/14Turbomachine thrust reverser
1502014024811509/04/14Active clearance control system with zone controls
1512014024811609/04/14Acoustic treatment in an unducted area of a geared turbomachine
1522014024812609/04/14Inter-module finger seal
1532014024812709/04/14Turbine engine component with dual purpose rib
1542014024812809/04/14Seals for a circumferential stop ring in a turbine exhaust case
1552014024812909/04/14Lpc flowpath shape with gas turbine engine shaft bearing configuration
1562014024813009/04/14Seal hook mount structure with overlapped coating
1572014024813609/04/14Multifunction positioning lock washer
1582014024815209/04/14Plate for directing flow and film cooling of components
1592014024815609/04/14Composite articles and methods
1602014023799008/28/14Variable area fan nozzle with wall thickness distribution
1612014023802708/28/14Thermally compliant dual wall liner for a gas turbine engine
1622014023908308/28/14Pivot thrust reverser surrounding inner surface of bypass duct
1632014023908408/28/14Tandem thrust reverser with sliding rails
1642014024185108/28/14Axial oil scoop for a gas turbine engine
1652014024185608/28/14Gas turbine engine systems involving tip fans
1662014024185708/28/14Flow diverter to redirect secondary flow
1672014024187408/28/14Wear liner spring seal
1682014024189708/28/14Aluminum brazing of hollow titanium fan blades
1692014024227808/28/14Split coating mask system for gas turbine engine component
1702014023024608/21/14Thermally free hanger with length adjustment feature
1712014023040308/21/14Gas turbine engine shaft bearing configuration
1722014023045208/21/14Planetary gear system arrangement with auxiliary oil system
1732014023094308/21/14Support system bumper for exhaust duct liner hanger
1742014023143708/21/14Cap drain plug
1752014023407808/21/14Method for setting a gear ratio of a fan drive gear system of a gas turbine engine
1762014023407908/21/14Geared architecture for high speed and small volume fan drive turbine
1772014023408508/21/14Bushing arranged between a body and a shaft, and connected to the shaft
1782014023408608/21/14Bushing arranged between a body and a shaft, and connected to the shaft
1792014023408708/21/14Inlet guide vane retention feature
1802014023409808/21/14Turbine case retention hook with insert
1812014022391608/14/14Gas turbine engine with compressor inlet guide vane positioned for starting
1822014022391908/14/14Flexible liner hanger
1832014022392008/14/14Consumable assembly mistake proofing tool for a gas turbine engine
1842014022538808/14/14Latch release mechanism
1852014022693008/14/14Test equipment with housing damping system
1862014022707808/14/14Mid-turbine frame vane assembly support with retention unit
1872014022708408/14/14Compound star gear system with rolling element bearings
1882014022708708/14/14Blade outer air seal surface
1892014022709308/14/14Low profile thermally free blind liner hanger attachment for complex shapes
1902014021599708/07/14Flexible shield for fluid connectors
1912014021600208/07/14Gas turbine engine having slim-line nacelle
1922014021600308/07/14Gas turbine engine with geared turbofan and oil thermal management system
1932014021600508/07/14Gas turbine engine assembly including a thrust reverser
1942014021604208/07/14Combustor component with cooling holes formed by additive manufacturing
1952014021605608/07/14Heat exchange module for a turbine engine
1962014021651308/07/14High zt thermoelectric with reversible junction
1972014021977208/07/14Individual inlet guide vane control for tip turbine engine
1982014021977408/07/14Turbomachine geared architecture support assembly
1992014021977808/07/14Gas turbine engine airfoil with vane platform cooling passage
2002014021978308/07/14Gas turbine engine fan drive gear system damper
2012014021978508/07/14Vane arm having a claw
2022014021979108/07/14Lug for preventing rotation of a stator vane arrangement relative to a turbine engine case
2032014021979208/07/14Pylon matched fan exit guide vane for noise reduction in a geared turbofan engine
2042014021979308/07/14Health monitoring for hollow blades
2052014021979408/07/14Bore cavity thermal conditioning system
2062014021980708/07/14Under-root spacer for gas turbine engine fan blade
2072014021980808/07/14Sheath with extended wings
2082014021981508/07/14Multi-lobed cooling hole
2092014022231008/07/14Engine monitor for a multi-engine system
2102014020871407/31/14Thermal management for gas turbine engine
2112014020877107/31/14Gas turbine engine component cooling arrangement
2122014020883707/31/14Gas turbine engine vane embedded beam interrupt optical tip-timing probe system
2132014021099207/31/14Infrared thermography with laser
2142014021226007/31/14Airfoil assembly with paired endwall contouring
2152014021226107/31/14Lightweight shrouded fan
2162014021226207/31/14Variable outer air seal support
2172014021226307/31/14Airfoil with variable profile responsive to thermal conditions
2182014021227007/31/14Gas turbine engine component having suction side cutback opening
2192014021227607/31/14Variable outer air seal fluid control
2202014021228107/31/14Flow feed diffuser
2212014021229207/31/14Airfoil member and composite platform having contoured endwall
2222014021229707/31/14Gas turbine engine serpentine cooling passage with chevrons
2232014021229807/31/14Gas turbine engine turbine blade tip cooling
2242014021278707/31/14Multiple transition flow field and method
2252014021278807/31/14Fuel cell and membrane therefore
2262014020213307/24/14Gas turbine engine mid turbine frame with flow turning features
2272014020217007/24/14Composite articles and methods
2282014020543807/24/14Relationship between fan and primary exhaust stream velocities in a geared gas turbine engine
2292014020545207/24/14Wind turbine blade
2302014020546107/24/14Vacuum degassing laser-blocking material system and procses
2312014020546207/24/14Hvata-hybrid vertical axis turbine assembly operable under omni-directional flow for power generating systems
2322014020549307/24/14High temperature directionally solidified and single crystal die casting
2332014020649607/24/14Method of assembly for gas turbine fan drive gear system
2342014019643307/17/14Gas turbine engine component platform cooling
2352014019643407/17/14Shroud for sealing conduit feed-through
2362014019647007/17/14Gas turbine engine buffer system
2372014019647107/17/14Fan drive gear system flexible support features
2382014019647207/17/14Geared turbofan gas turbine engine architecture
2392014019647307/17/14Geared turbofan gas turbine engine architecture
2402014019917607/17/14Gas turbine engine nose cone attachment configuration
2412014019917707/17/14Airfoil and making
2422014019949007/17/14Deposition substrate temperature and monitoring
2432014019016707/10/14Ceramic combustor can for a gas turbine engine
2442014019017507/10/143d non-axisymmetric combustor liner
2452014019018107/10/14Rotor cover plate
2462014019065407/10/14Cast features for a turbine engine airfoil
2472014019323807/10/14Method for setting a gear ratio of a fan drive gear system of a gas turbine engine
2482014019324607/10/14Cooling hole with crenellation features
2492014019325107/10/14Stator anti-rotation device



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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