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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



Turbine engine gearbox mount with multiple fuse joints

United Technologies

Turbine engine gearbox mount with multiple fuse joints

Gas turbine engine fan blade airfoil profile

United Technologies

Gas turbine engine fan blade airfoil profile

Search recent Press Releases: United Technologies Corporation-related press releases
Count Application # Date United Technologies Corporation patents (updated weekly) - BOOKMARK this page
12014031112110/23/14 new patent  Pulse detonation engine having a scroll ejector attenuator
22014031114910/23/14 new patent  Gas turbine engine fan blade airfoil profile
32014031261110/23/14 new patent  Locking fluid fittings
42014031454010/23/14 new patent  Gas turbine engine synchronization ring
52014031454110/23/14 new patent  Turbomachine thrust balancing system
62014031454210/23/14 new patent  Gas turbine engine exhaust diffuser with movable struts
72014031454610/23/14 new patent  Turbine engine gearbox mount with multiple fuse joints
82014031454710/23/14 new patent  Attachment apparatus for ceramic matrix composite materials
92014031458110/23/14 new patent  Method for forming single crystal parts using additive manufacturing and remelt
102014029878810/09/14Gas turbine engine including pneumatic actuator system
112014030142510/09/14Backstrike detection system for laser drilling thin materials
122014030182910/09/14Engine bearing support
132014029021110/02/14Turbine engine including balanced low pressure stage count
142014029021310/02/14Duct blocker seal assembly for a gas turbine engine
152014029026910/02/14Duct blocker seal assembly for a gas turbine engine
162014029455810/02/14Turbomachine fluid delivery manifold and system
172014028350009/25/14Thrust efficient turbofan engine
182014028350109/25/14Elongated geared turbofan with high bypass ratio
192014028674809/25/14Fan containment case with thermally conforming liner
202014028675409/25/14Elongated geared turbofan with high bypass ratio
212014028675509/25/14Ring gear mounting arrangement with oil scavenge scheme
222014028678109/25/14Integral fan blade wear pad and platform seal
232014025966109/18/14Variable area fan nozzle with wall thickness distribution
242014026017609/18/14Lube tube expansion and torque retaining device
252014026018209/18/14Free stream intake for reverse core engine
262014026018309/18/14Variable cycle intake for reverse core engine
272014026032109/18/14Gas turbine engine static structure joint with undercuts
282014026179709/18/14Tube fitting having integrated tee fitting
292014026810009/18/14Multiple laser time of arrival probe
302014026981709/18/14Phosphor thermometry fiber sensor
312014027062509/18/14High temperature uncooled optical probe
322014027110109/18/14Modulated turbine vane cooling
332014027111209/18/14Low noise turbine for geared gas turbine engine
342014027112109/18/14Gas turbine engine architecture with intercooled twin centrifugal compressor
352014027113509/18/14Turbofan engine bearing and gearbox arrangement
362014027117809/18/14Fan blades for gas turbine engines with reduced stress concentration at leading edge
372014027122109/18/14Usage of a witness mark to distinguish support structure from part
382014027245609/18/14Spallation-resistant thermal barrier coating
392014027374709/18/14Removing material from a workpiece with a water jet
402014027375709/18/14Drag finishing system, method and fixture for gas turbine engine airfoils
412014027453109/18/14Fan drive planetary gear system integrated carrier and torque frame
422014025086209/11/14Reverse flow gas turbine engine airflow bypass
432014025086309/11/14Rear mounted reverse core engine thrust reverser
442014025089509/11/14Modulated ejector cooling
452014025138109/11/14Pulse jet liquid gas cleaning system
462014025179109/11/14Cathodic arc deposition stinger
472014025180309/11/14Cathodic arc mask assembly lock system
482014025216009/11/14Reverse flow gas turbine engine removable core
492014025216109/11/14De-couple geared turbo-fan engine and aircraft
502014025216209/11/14Uav launching from moving platform
512014025216709/11/14Reverse core engine thrust reverser for under wing
522014025218309/11/14Sensor hoop storage and transport apparatus
532014025276409/11/14Two-piece self-locking mechanism for tube assemblies
542014025463109/11/14Actively cooled gas turbine sensor probe housing
552014025511209/11/14Broach tool rake face with a tailored surface topography
562014025514409/11/14Flanged bushing for variable vane
572014025515609/11/14Non-contacting seals for geared gas turbine engine bearing compartments
582014025515809/11/14Coating process for gas turbine engine component with cooling holes
592014025516209/11/14Adjustable floating oil channel for gas turbine engine gear drive
602014025516709/11/14Consumable assembly tool for a gas turbine engine
612014025516809/11/14Inter-module flow discourager
622014025517209/11/14Low profile push-lock device
632014025517409/11/14Manufacture of full ring strut vane pack
642014025518209/11/14Push-lock pin connector
652014025519609/11/14Double split blade lock ring
662014025519809/11/14Turbine disk fabrication with in situ material property variation
672014025520209/11/14Turbine engine nosecone with deformation region
682014024574909/04/14Nacelle anti-ice valve utilized as compressor stability bleed valve during starting
692014024575009/04/14Circumferentially retained fairing
702014024575109/04/14Passages to facilitate a secondary flow between components
712014024575309/04/14Gas turbine engine rotor blade
722014024651409/04/14Turbomachine thrust reverser
732014024811509/04/14Active clearance control system with zone controls
742014024811609/04/14Acoustic treatment in an unducted area of a geared turbomachine
752014024812609/04/14Inter-module finger seal
762014024812709/04/14Turbine engine component with dual purpose rib
772014024812809/04/14Seals for a circumferential stop ring in a turbine exhaust case
782014024812909/04/14Lpc flowpath shape with gas turbine engine shaft bearing configuration
792014024813009/04/14Seal hook mount structure with overlapped coating
802014024813609/04/14Multifunction positioning lock washer
812014024815209/04/14Plate for directing flow and film cooling of components
822014024815609/04/14Composite articles and methods
832014023799008/28/14Variable area fan nozzle with wall thickness distribution
842014023802708/28/14Thermally compliant dual wall liner for a gas turbine engine
852014023908308/28/14Pivot thrust reverser surrounding inner surface of bypass duct
862014023908408/28/14Tandem thrust reverser with sliding rails
872014024185108/28/14Axial oil scoop for a gas turbine engine
882014024185608/28/14Gas turbine engine systems involving tip fans
892014024185708/28/14Flow diverter to redirect secondary flow
902014024187408/28/14Wear liner spring seal
912014024189708/28/14Aluminum brazing of hollow titanium fan blades
922014024227808/28/14Split coating mask system for gas turbine engine component
932014023024608/21/14Thermally free hanger with length adjustment feature
942014023040308/21/14Gas turbine engine shaft bearing configuration
952014023045208/21/14Planetary gear system arrangement with auxiliary oil system
962014023094308/21/14Support system bumper for exhaust duct liner hanger
972014023143708/21/14Cap drain plug
982014023407808/21/14Method for setting a gear ratio of a fan drive gear system of a gas turbine engine
992014023407908/21/14Geared architecture for high speed and small volume fan drive turbine
1002014023408508/21/14Bushing arranged between a body and a shaft, and connected to the shaft
1012014023408608/21/14Bushing arranged between a body and a shaft, and connected to the shaft
1022014023408708/21/14Inlet guide vane retention feature
1032014023409808/21/14Turbine case retention hook with insert
1042014022391608/14/14Gas turbine engine with compressor inlet guide vane positioned for starting
1052014022391908/14/14Flexible liner hanger
1062014022392008/14/14Consumable assembly mistake proofing tool for a gas turbine engine
1072014022538808/14/14Latch release mechanism
1082014022693008/14/14Test equipment with housing damping system
1092014022707808/14/14Mid-turbine frame vane assembly support with retention unit
1102014022708408/14/14Compound star gear system with rolling element bearings
1112014022708708/14/14Blade outer air seal surface
1122014022709308/14/14Low profile thermally free blind liner hanger attachment for complex shapes
1132014021599708/07/14Flexible shield for fluid connectors
1142014021600208/07/14Gas turbine engine having slim-line nacelle
1152014021600308/07/14Gas turbine engine with geared turbofan and oil thermal management system
1162014021600508/07/14Gas turbine engine assembly including a thrust reverser
1172014021604208/07/14Combustor component with cooling holes formed by additive manufacturing
1182014021605608/07/14Heat exchange module for a turbine engine
1192014021651308/07/14High zt thermoelectric with reversible junction
1202014021977208/07/14Individual inlet guide vane control for tip turbine engine
1212014021977408/07/14Turbomachine geared architecture support assembly
1222014021977808/07/14Gas turbine engine airfoil with vane platform cooling passage
1232014021978308/07/14Gas turbine engine fan drive gear system damper
1242014021978508/07/14Vane arm having a claw
1252014021979108/07/14Lug for preventing rotation of a stator vane arrangement relative to a turbine engine case
1262014021979208/07/14Pylon matched fan exit guide vane for noise reduction in a geared turbofan engine
1272014021979308/07/14Health monitoring for hollow blades
1282014021979408/07/14Bore cavity thermal conditioning system
1292014021980708/07/14Under-root spacer for gas turbine engine fan blade
1302014021980808/07/14Sheath with extended wings
1312014021981508/07/14Multi-lobed cooling hole
1322014022231008/07/14Engine monitor for a multi-engine system
1332014020871407/31/14Thermal management for gas turbine engine
1342014020877107/31/14Gas turbine engine component cooling arrangement
1352014020883707/31/14Gas turbine engine vane embedded beam interrupt optical tip-timing probe system
1362014021099207/31/14Infrared thermography with laser
1372014021226007/31/14Airfoil assembly with paired endwall contouring
1382014021226107/31/14Lightweight shrouded fan
1392014021226207/31/14Variable outer air seal support
1402014021226307/31/14Airfoil with variable profile responsive to thermal conditions
1412014021227007/31/14Gas turbine engine component having suction side cutback opening
1422014021227607/31/14Variable outer air seal fluid control
1432014021228107/31/14Flow feed diffuser
1442014021229207/31/14Airfoil member and composite platform having contoured endwall
1452014021229707/31/14Gas turbine engine serpentine cooling passage with chevrons
1462014021229807/31/14Gas turbine engine turbine blade tip cooling
1472014021278707/31/14Multiple transition flow field and method
1482014021278807/31/14Fuel cell and membrane therefore
1492014020213307/24/14Gas turbine engine mid turbine frame with flow turning features
1502014020217007/24/14Composite articles and methods
1512014020543807/24/14Relationship between fan and primary exhaust stream velocities in a geared gas turbine engine
1522014020545207/24/14Wind turbine blade
1532014020546107/24/14Vacuum degassing laser-blocking material system and procses
1542014020546207/24/14Hvata-hybrid vertical axis turbine assembly operable under omni-directional flow for power generating systems
1552014020549307/24/14High temperature directionally solidified and single crystal die casting
1562014020649607/24/14Method of assembly for gas turbine fan drive gear system
1572014019643307/17/14Gas turbine engine component platform cooling
1582014019643407/17/14Shroud for sealing conduit feed-through
1592014019647007/17/14Gas turbine engine buffer system
1602014019647107/17/14Fan drive gear system flexible support features
1612014019647207/17/14Geared turbofan gas turbine engine architecture
1622014019647307/17/14Geared turbofan gas turbine engine architecture
1632014019917607/17/14Gas turbine engine nose cone attachment configuration
1642014019917707/17/14Airfoil and method of making
1652014019949007/17/14Deposition substrate temperature and monitoring
1662014019016707/10/14Ceramic combustor can for a gas turbine engine
1672014019017507/10/143d non-axisymmetric combustor liner
1682014019018107/10/14Rotor cover plate
1692014019065407/10/14Cast features for a turbine engine airfoil
1702014019323807/10/14Method for setting a gear ratio of a fan drive gear system of a gas turbine engine
1712014019324607/10/14Cooling hole with crenellation features
1722014019325107/10/14Stator anti-rotation device
1732014019326707/10/14Dmz fracture boundary limit
1742014019424007/10/14Journal pin oil supply for gear system
1752014019427207/10/14Method of treating a preceramic material
1762014018229207/03/14Integral instrumentation in additively manufactured components of gas turbine engines
1772014018229307/03/14Compressor rotor for gas turbine engine with deep blade groove
1782014018230807/03/14Gas turbine engine with v-band clamp connection for collector box
1792014018230907/03/14Geared gas turbine engine exhaust nozzle with chevrons
1802014018280907/03/14Mullite-containing investment casting core
1812014018297207/03/14Case with integral lubricant scavenge passage
1822014018316407/03/14Non-line of sight electro discharge machining system
1832014018329607/03/14Gas turbine engine having fan rotor driven by turbine exhaust and with a bypass
1842014018382507/03/14Finger seal
1852014018609807/03/14Work piece having self-supporting gusset and method related thereto
1862014018615207/03/14Blade outer air seal system for controlled tip clearance
1872014018615807/03/14Gas turbine engine shaft bearing configuration
1882014018616007/03/14Slider seal
1892014018616307/03/14Blade outer air seal having shiplap structure
1902014018616407/03/14Non-line of sight electro discharge machined part
1912014018616507/03/14Adhesive pattern for fan case conformable liner
1922014018616707/03/14Multi-piece fairing for monolithic turbine exhaust case
1932014018616807/03/14Component retention with probe
1942014018619007/03/14Tip leakage flow directionality control
1952014018620007/03/14Fan blade adjustment piezoelectric actuator
1962014018620507/03/14Method and apparatus for reconditioning oxidized powder
1972014018665607/03/14Spallation-resistant thermal barrier coating
1982014017388106/26/14Blind installation pin for a gas turbine engine mount
1992014017389606/26/14Method and system for holding a combustor panel during coating process
2002014017389706/26/14Anti-torsion assembly
2012014017405506/26/14Turbine section of high bypass turbofan
2022014017405606/26/14Gas turbine engine with low stage count low pressure turbine
2032014017408806/26/14Alignment system and methodology to account for variation in a gas turbine engine
2042014017409106/26/14Repair procedure for a gas turbine engine via variable polarity welding
2052014017409206/26/14Closure of cooling holes with a filling agent
2062014017409406/26/14Apu exhaust housing perforated ring
2072014017409806/26/14Turbine disc with reduced neck stress concentration
2082014017416206/26/14Ignitor plug isolation chamber (ipic) for a gas turbine engine
2092014017425206/26/14Mount with an axial upstream linkage for conneting a gearbox to a turbine engine case
2102014017485506/26/14Pressurized reserve lubrication system for a gas turbine engine
2112014017502706/26/14Fuel system with electrically heated filter screen
2122014017817406/26/14Gas turbine engine including a pre-diffuser heat exchanger
2132014017817506/26/14Air turbine starter monitor system
2142014017818506/26/14Egress seal assembly
2152014017819606/26/14Turbomachine with clamp coupling shaft and rotor hub together
2162014017824106/26/14Absorbed impurities reduction in additive manufacturing systems
2172014017824406/26/14Gaseous based desulfurization of alloys
2182014017824506/26/14Low sulfur nickel base substrate alloy and overlay coating system
2192014017871006/26/14Alloying interlayer for electroplated aluminum on aluminum alloys
2202014016537606/19/14Cat arc process and part holding apparatus
2212014016553006/19/14Bi-directional auxiliary lubrication system
2222014016553406/19/14Gas turbine engine compressor arrangement
2232014016557006/19/14Oscillating heat pipe for thermal management of gas turbine engines
2242014016557506/19/14Nozzle section for a gas turbine engine
2252014016557806/19/14Ovate swirler assembly for combustors
2262014016557906/19/14High pressure turbine speed calculation from fuel system hydraulic pressures
2272014016558206/19/14Cross-flow turbine engine
2282014016558506/19/14Oblong swirler assembly for combustors
2292014016558606/19/14Turbine start method
2302014016558806/19/14Turbo compressor for bleed air
2312014016558906/19/14Gas turbine engine with accessory gear box
2322014016559106/19/14Turbine under platform air seal strip
2332014016559306/19/14Gas turbine engine turbine blade leading edge tip trench cooling
2342014016573606/19/14Traversing time of arrival probe
2352014016576206/19/14Fan drive gear system assembly guide
2362014016614406/19/14Composite ducts and methods
2372014016622906/19/14Minimization of re-crystallization in single crystal castings
2382014016625506/19/14Closure of cooling holes with a filing agent
2392014016683506/19/14Multi-dimensional extending protective arm
2402014016990806/19/14Nut plate fastener with elongated fastener aperture
2412014016993406/19/14Anti-ice supply system for inlet guide vanes
2422014016993506/19/14Lightweight shrouded fan blade
2432014016994106/19/14Forward compartment baffle arrangement for a geared turbofan engine
2442014016995006/19/14Variable vane having body formed of first material and trunnion formed of second material
2452014016995606/19/14Overmolded vane platform
2462014016997206/19/14Fan with integral shroud
2472014016997506/19/14Rotor blade root spacer with a fracture feature
2482014016997606/19/14Rotor blade root spacer for arranging between a rotor disk and a root of a rotor blade
2492014016997906/19/14Gas turbine engine fan blade platform seal


ARCHIVE: New 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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