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United Technologies Corporation
United Technologies Corporation One Financial Plaza
United Technologies Corporation_20100114
United Technologies Corporation_20100107
United Technologies Corporation_20100121
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

Count Application # Date United Technologies Corporation patents (updated weekly) - BOOKMARK this page
12015023909508/27/15  new patent  Confined pencil blasting apparatus
22015023956808/27/15  new patent  Pylon shape with geared turbofan for structural stiffness
32015024065808/27/15  new patent  Carbon nanotubes for increasing vibration damping in polymer matrix composite containment cases for aircraft engines
42015024066008/27/15  new patent  Buffer airflow to bearing compartment
52015024066108/27/15  new patent  Repair or remanufacture of liner panels for a gas turbine engine
62015024066208/27/15  new patent  Case assembly for a gas turbine engine
72015024066308/27/15  new patent  Liner lock segment
82015024071208/27/15  new patent  Mid-turbine duct for geared gas turbine engine
92015024072308/27/15  new patent  Bore basket for a gas powered turbine
102015024072408/27/15  new patent  Combustor seal mistake-proofing for a gas turbine engine
112015024072508/27/15  new patent  Gas turbine engine with forward moment arm
122015024074508/27/15  new patent  Angled reverse core gas turbine engine with widened nozzle
132015024086708/27/15  new patent  Turbomachine bearing support structure
142015024106308/27/15  new patent  Combustor with grommet having projecting lip
152015024106708/27/15  new patent  Fastened joint for a tangential on board injector
162015023166508/20/15 Spray masking for rotors
172015023325008/20/15 Gas turbine engine airfoil
182015023325108/20/15 Gas turbine engine airfoil
192015023325208/20/15 Gas turbine engine airfoil
202015023325908/20/15 Fan blade tall dovetail for individually bladed rotors
212015023326408/20/15 Retention of damping media
222015023329308/20/15 Annular spring for a bearing assembly of a gas turbine engine
232015023329508/20/15 Split-zone flow metering t-tube
242015023329708/20/15 Fuel manifold fitting with integral support for a gas turbine engine
252015023329808/20/15 Reduction in jet flap interaction noise with geared turbine engine
262015023330008/20/15 Geared gas turbine engine accessory gearbox
272015023330108/20/15 Method for setting a gear ratio of a fan drive gear system of a gas turbine engine
282015023330208/20/15 Operability geared turbofan engine including compressor section variable guide vanes
292015023330308/20/15 Method for setting a gear ratio of a fan drive gear system of a gas turbine engine
302015023332308/20/15 Gas turbine engine airfoil
312015023358108/20/15 Fuel manifold for a gas turbine engine
322015022606708/13/15 Airfoil array with airfoils that differ in geometry according to geometry classes
332015022607708/13/15 Seal damper with improved retention
342015022608508/13/15 Baffle with flow augmentation feature
352015022611608/13/15 Fan drive gear system module and inlet guide vane coupling mechanism
362015022611708/13/15 Gas turbine engine with distributed fans
372015022612308/13/15 Gas turbine engine buffer cooling system
382015022612508/13/15 Combined high pressure turbine case and turbine intermediate case
392015022613008/13/15 Gas turbine engine including vane structure and seal to control fluid leakage
402015022613108/13/15 Combustor seal system for a gas turbine engine
412015022613208/13/15 Gas turbine engine ring seal
422015022615608/13/15 Non-axisymmetric fixed or variable fan nozzle for boundary layer ingestion propulsion
432015022623108/13/15 Fan blade removal panel
442015022767708/13/15 Gas turbine engine with first turbine vane clocking
452015021738808/06/15 Method of modifying gear profiles
462015021895508/06/15 Compliant cantilevered airfoil
472015021895708/06/15 Guide vane seal
482015021896508/06/15 Variable positioner
492015021896608/06/15 Gas turbine engine fan spacer platform attachments
502015021901108/06/15 Dual oil supply tube
512015021901508/06/15 Seal assembly for a static structure of a gas turbine engine
522015021901708/06/15 Actuator mounted to torque box
532015021924608/06/15 Polymeric or composite interlocking mount assembly for cable harnesses and fluid tubes
542015021933808/06/15 Combustor assembly for a turbine engine
552015020986407/30/15 Method for synthesizing nanowires and nanofoam
562015021137607/30/15 Turbine vane cooling arrangement
572015021141607/30/15 Gas turbine engine with twin offset gas generators
582015021144107/30/15 Variable exhaust mixer and cooler for a three-stream gas turbine engine
592015021144307/30/15 Divot for blocker doors of thrust reverser system
602015021144407/30/15 Aft counter-rotating shrouded geared turbofan
612015021174107/30/15 Method for repairing fuel nozzle guides for gas turbine engine combustors using cold metal transfer weld technology
622015020270207/23/15 Gas turbine engine cast structure finishing
632015020270707/23/15 Attachment of structures having different physical characteristics
642015020341107/23/15 Additive manufacturing hybrid core
652015020395407/23/15 Coating system and process
662015020420107/23/15 Contoured flowpath surface
672015020421207/23/15 High durability turbine exhaust case
682015020423807/23/15 Low noise turbine for geared turbofan engine
692015020424407/23/15 Selectively deoxygenated stored fuel system
702015020434707/23/15 Fan blades with abrasive tips
712015020444707/23/15 Radially coacting ring seal
722015020462507/23/15 High temperature heat transfer interface
732015019784007/16/15 Systems and methods for removing overspray
742015019804507/16/15 High order shaped curve region for an airfoil
752015019804707/16/15 Mistuned airfoil assemblies
762015019805607/16/15 Abradable seal having nanolayer material
772015019809207/16/15 Dual function air diverter and variable area fan nozzle
782015019811607/16/15 Variable area exhaust mixer for a gas turbine engine
792015019817307/16/15 Fan blade with variable thickness composite cover
802015019825307/16/15 Shrouded face seal and components thereof
812015019995207/16/15 Vibration damping material for high temperature use
822015019082407/09/15 Cold spray systems with in-situ powder manufacturing
832015019088907/09/15 Systems and methods for solid state metal repair
842015019089107/09/15 Repair of casting defects
852015019089307/09/15 Systems and methods for airfoil assembly
862015019094907/09/15 Media containment for iso-grid structure forming
872015019202107/09/15 Airfoil cooling arrangement
882015019203407/09/15 Systems and methods for centering bearing compartments
892015019206807/09/15 Auxiliaryy fluid flow system debris filter
902015019207007/09/15 Geared turbofan gas turbine engine architecture
912015019207107/09/15 Geared turbofan gas turbine engine architecture
922015019207207/09/15 Fluid transport system having divided transport tube
932015019209207/09/15 Sliding nozzle flap assembly
942015019214407/09/15 Fan assembly with fan blade under-root spacer
952015019216507/09/15 Systems and methods for centering bearing compartments
962015019229807/09/15 Gas turbine engine with improved fuel efficiency
972015019230007/09/15 Light weight swirler for gas turbine engine combustor and a manufacturing
982015018302607/02/15 Investment mold having metallic donor element
992015018307807/02/15 System and methods for rough grinding
1002015018430607/02/15 Electroformed sheath
1012015018451307/02/15 Device and repairing a forward frame v-blade in an aircraft engine
1022015018485707/02/15 Microcircuit cooling for gas turbine engine combustor
1032015018486007/02/15 Spiral pulse detonation tube configuration
1042015018510907/02/15 Methods for testing laser shock peening
1052015017465306/25/15 System and methods for removing core elements of cast components
1062015017472906/25/15 Systems and methods for modifying and adding features on grinding wheel surfaces
1072015017473106/25/15 Systems and methods for dressing grinding wheels
1082015017648406/25/15 Geared turbofan with a gearbox aft of a fan drive turbine
1092015017649306/25/15 Gas turbine engine forward bearing compartment architecture
1102015017649706/25/15 Geared turbofan with a gearbox upstream of a fan drive turbine
1112015017650206/25/15 Method of controlling a gas turbine engine using real-time component temperature data
1122015017653006/25/15 Ultra high overall pessure ratio gas turbine engine
1132015016550006/18/15 Deep rolling tool for blade fatigue life enhancement
1142015016551306/18/15 Machine for deep rolling tool positioning
1152015016551406/18/15 Deep rolling tool with force adjustment
1162015016551506/18/15 Deep rolling tool for processing blade root
1172015016557006/18/15 Crimping tool
1182015016566606/18/15 Systems and methods for manufacturing fiber-reinforced polymeric components
1192015016712506/18/15 Nickel alloy for repairs
1202015016714906/18/15 Movable evaporation source
1212015016754906/18/15 Exhaust stream mixer
1222015016767606/18/15 Gas turbine engine for long range aircraft
1232015017256506/18/15 Composite image processing for lwir images using geometric features
1242015017256606/18/15 Natural resolution processing for lwir images
1252015015807606/11/15 Method of fabricating an investment casting mold and slurry therefor
1262015015859706/11/15 Emergency power generation via limited variable pitch fan blade
1272015015950106/11/15 Rigid and rotatable vanes molded within variably shaped flexible airfoils
1282015015950806/11/15 Core drainage systems for fan case assemblies
1292015016009706/11/15 Long wave infrared sensing for turbomachine
1302015015254406/04/15 Coating methods and apparatus
1312015015273906/04/15 Turbine blade rail damper
1322015015274606/04/15 Slotted distribution sleeve for a seal plate
1332015015278706/04/15 Low noise compressor rotor for geared turbofan engine
1342015015278906/04/15 Multi-bypass stream gas turbine engine with enlarged bypass flow area
1352015015372606/04/15 Method for inspecting a manufacturing device
1362015015678906/04/15 Communication of avionic data
1372015014379405/28/15 Geared turbofan engine gearbox arrangement
1382015014752805/28/15 Component blending tool
1392015013567805/21/15 Gas turbine engine with noise attenuating variable area fan nozzle
1402015013834205/21/15 System and method to determine visible damage
1412015014123505/21/15 Carbon fiber-reinforced article and method therefor
1422015013210605/14/15 Gas turbine engine with low fan pressure ratio
1432015013211005/14/15 High durability turbine exhaust case
1442015013213405/14/15 Injection molded composite fan platform
1452015013214205/14/15 Rotor blade with bonded cover
1462015012168205/07/15 Extraction tool assembly
1472015012183805/07/15 Conjoined reverse core flow engine arrangement
1482015012183905/07/15 Tandem thrust reverser with multi-bar linkage
1492015012184105/07/15 Flow control device for a three stream turbofan engine
1502015012184405/07/15 Geared turbofan arrangement with core split power ratio
1512015012188205/07/15 Mixer assembly for a gas turbine engine
1522015012188405/07/15 Stress relieved rectilinear duct
1532015012189305/07/15 Adaptive fan reverse core geared turbofan engine with separate cold turbine
1542015012189405/07/15 Bifurcation fire purge system
1552015012189505/07/15 Full ring sliding nacelle with thrust reverser
1562015012189605/07/15 Reverse core flow engine mounting arrangement
1572015012203105/07/15 Transducer position guide
1582015012233905/07/15 Variable area bypass nozzle
1592015012290505/07/15 Passive tangential ejector for an exhaust nozzle of a gas turbine engine
1602015012291205/07/15 Tandem thrust reverser with multi-point actuation
1612015012295205/07/15 Gas turbine engine inlet wall design
1622015012299805/07/15 Method of inspection for cooling holes in turbine airfoil
1632015012525905/07/15 Gas turbine engine variable pitch fan blade
1642015012527005/07/15 Atr guide pins for sliding nacelle
1652015012528405/07/15 Atr full ring sliding nacelle
1662015012528505/07/15 Integrated nozzle and plug
1672015012528605/07/15 Atr axial v-groove
1682015012529105/07/15 Bracket for mounting a stator guide vane arrangement to a strut in a turbine engine
1692015012529305/07/15 Turbofan engine main bearing arrangement
1702015012529505/07/15 Wind turbine load mitigation
1712015012530405/07/15 Mass offset for damping performance
1722015012530505/07/15 Low profile fan platform attachment
1732015012568105/07/15 High temperature imaging media for digital image correlation
1742015012609605/07/15 System and contoured peel grinding
1752015011394104/30/15 Translating outer cowl flow modulation device and method
1762015011394204/30/15 Phosphor thermometer with two waveguides
1772015011394304/30/15 Geared turbofan engine with power density range
1782015011394504/30/15 Pivoting blocker door
1792015011399604/30/15 Cascaded multi-variable control system for a turboshaft engine
1802015011400204/30/15 Geared turbofan engine with a high ratio of thrust to turbine volume
1812015011407404/30/15 Systems and methods for controlled peening
1822015011749304/30/15 Phosphor thermometry fiber sensor
1832015011780404/30/15 Gas turbine engine bushing
1842015011806304/30/15 Turbine airfoil tip shelf and squealer pocket cooling
1852015011806404/30/15 Gas turbine engine airfoil trailing edge passage and core for making same
1862015010722304/23/15 High durability turbine exhaust case
1872015011063604/23/15 Wear pad to prevent cracking of fan blade
1882015011102204/23/15 Coating for metal cellular structure and method therefor
1892015010193504/16/15 Apparatus and ionic liquid electroplating
1902015010431504/16/15 Fan blade root integrated sealing solution
1912015009630304/09/15 Gas turbine engine with high speed low pressure turbine section
1922015009671304/09/15 Rapid tooling insert manufacture
1932015009683904/09/15 Low loss oil accumulator assembly
1942015009883004/09/15 Assembly fixture for a stator vane assembly
1952015009883504/09/15 Castings, casting cores, and methods
1962015008991804/02/15 Gas turbine lubrication systems
1972015008995804/02/15 Gas turbine engine with high speed low pressure turbine section
1982015008995904/02/15 Gas turbine engine shaft bearing configuration
1992015008294503/26/15 Process for producing refractory metal alloy powders
2002015008391903/26/15 Background radiation measurement system
2012015008626203/26/15 Welded assemblies and methods of making welded assemblies
2022015008628303/26/15 Ball-end milling cutter tool
2032015007574503/19/15 Casting molds, manufacture and use methods
2042015007891503/19/15 Piloted nut
2052015006820903/12/15 Method for determining circumferential sensor positioning
2062015006821003/12/15 Tube fed tangential on-board injector for gas turbine engine
2072015006821403/12/15 Low thermal mass joint
2082015006966803/12/15 Multi-dimensional component build system and process
2092015007170403/12/15 Exhaust duct liner rod hanger
2102015006000203/05/15 Die casting system and cell
2112015006528503/05/15 Geared architecture gas turbine engine with oil scavenge
2122015005287302/26/15 Torque connector lubrication scuppers
2132015005290702/26/15 Thermal management system for gas turbine engine
2142015005378902/26/15 Linkage to control and restrain flap movement
2152015005012702/19/15 Air with integral spring for a gas turbine engine exhaust drive
2162015005104002/19/15 Oil baffle for gas turbine fan drive gear system
2172015004202302/12/15 Hybrid part made from monolithic ceramic skin and cmc core
2182015004402802/12/15 Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
2192015004405202/12/15 Geared turbofan with fan blades designed to achieve laminar flow
2202015004520002/12/15 Ceramic component
2212015003760202/05/15 System and high temperature die casting tooling
2222015002710101/29/15 Geared gas turbine engine architecture for enhanced efficiency
2232015002713001/29/15 Split ring valve
2242015002765701/29/15 Method and casting core for forming a landing for welding a baffle inserted in an airfoil
2252015003044001/29/15 Fireshield fastener hood
2262015003044301/29/15 Split damped outer shroud for gas turbine engine stator arrays
2272015002378001/22/15 Liner attaching scheme
2282015002429601/22/15 Method and system for operating a flow battery system based on energy costs
2292015001330101/15/15 Turbine engine including balanced low pressure stage count
2302015001334401/15/15 Tube
2312015001348001/15/15 Plated instrumentation probes and sensors
2322015001393401/15/15 Article with grouped grain patterns
2332015001695401/15/15 Blade outer air seal assembly and support
2342015001696501/15/15 Link arm drag reducing device
2352015000826801/08/15 Pivot thrust reverser with multi-point actuation
2362015000008901/01/15 Clamp connector
2372015000030301/01/15 Wireless power for gas turbine engine instrumentation
2382015000030401/01/15 Removable nosecone for a gas turbine engine
2392015000395601/01/15 Variable vane scheduling
2402015000396801/01/15 Gas turbine engine with attached nosecone
2412015000399501/01/15 Aircraft engine component with locally tailored materials
2422015000399701/01/15 Method of forming hybrid metal ceramic components
2432014037354912/25/14 Cooling hole with curved metering section
2442014037355412/25/14 Air turbine starter pressure monitor system
2452014037361012/25/14 Engine inspection apparatus and system
2462014037505612/25/14 Method of operating a power generation system
2472014036654812/18/14 Turbine engine gearbox
2482014036655412/18/14 Cross reference to related applications
2492014036655612/18/14 Gas turbine engine vane-to-transition duct seal

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