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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
12015027430610/01/15  new patent  Hybrid drive for gas turbine engine
22015027430710/01/15  new patent  Nacelle inner flow structure leading edge latching system
32015027567910/01/15  new patent  Abrasive tip blade manufacture methods
42015027568910/01/15  new patent  Composite fan containment case assembly
52015027569010/01/15  new patent  Vented tangential on-board injector for a gas turbine engine
62015027569210/01/15  new patent  Reduced fan containment threat through liner and blade design
72015027569410/01/15  new patent  Structural guide vane circumferential load bearing shear pin
82015027575710/01/15  new patent  Bleed duct for laminar fan duct flow
92015027576110/01/15  new patent  Seal assembly with cooling feature
102015027576610/01/15  new patent  Geared turbine engine with a d-duct and a thrust reverser
112015027576710/01/15  new patent  Method of defining gas turbine engine control ratings
122015026754109/24/15 Fan blade composite cover with tapered edges
132015026755109/24/15 Auxiliary device for three air flow path gas turbine engine
142015026761009/24/15 Turbine enigne including balanced low pressure stage count
152015026761709/24/15 Integrated thermal system for a gas turbine engine
162015026761809/24/15 Geared turbofan high gearbox power density
172015026773709/24/15 Pitch diameter shank bolt with shear sleeve
182015026780209/24/15 Oil baffle for gas turbine fan drive gear system
192015025860809/17/15 Casting funnel
202015025905909/17/15 Stabilizer sacrificial surfaces
212015026004809/17/15 Component with cooling hole having helical groove
222015026005109/17/15 Geared low fan pressure ratio fan exit guide vane stagger angle
232015026005409/17/15 Low compressor having variable vanes
242015026005709/17/15 Mid-turbine frame with fairing attachment
252015026021509/17/15 High temperature thread locking compound
262015026039909/17/15 Combustor section of a gas turbine engine
272015026040409/17/15 Interface heat shield for a combustor of a gas turbine engine
282015026335809/17/15 Flow battery with mixed flow
292015025124209/10/15 Casting cores and manufacture methods
302015025177409/10/15 Engine installation system
312015025246409/10/15 Equipment for plasma spray with liquid injection
322015025267209/10/15 Ring gear mounting arrangement with oil scavenge scheme
332015025267809/10/15 Fan blade spacer
342015025267909/10/15 Static guide vane with internal hollow channels
352015025268009/10/15 Synchronization ring runner with cradle
362015025268209/10/15 Hybrid blade outer air seal for gas turbine engine
372015025268609/10/15 Rotor blade tip clearance
382015025272309/10/15 Compressor areas for high overall pressure ratio gas turbine engine
392015025272809/10/15 Gas turbine engine having support structure with swept leading edge
402015025272909/10/15 Inner diffuser case struts for a combustor of a gas turbine engine
412015025273009/10/15 Geared turbine engine with relatively lightweight propulsor module
422015025273109/10/15 Gas turbine engine including bleed system coupled to upstream and downstream locations of compressor
432015025273209/10/15 Gas turbine engine with intercooling turbine section and intercooling turbine section bypass
442015025275109/10/15 Geared gas turbine engine integrated with a variable area fan nozzle with reduced noise
452015025275209/10/15 Low weight large fan gas turbine engine
462015025301009/10/15 Dual fuel nozzle with concentric fuel passages for a gas turbine engine
472015025326209/10/15 Systems and methods for x-ray diffraction
482015025579809/10/15 Platinum alloy nano catalyst with a non-platinum core
492015024742409/03/15 Geared turbofan engine with optimized diffuser case flange location
502015024742509/03/15 Non-circular aft nacelle cowling geometry
512015024745409/03/15 Geared turbofan engine with inter-shaft deflection feature
522015024745509/03/15 External core gas turbine engine assembly
532015024745609/03/15 Offset core engine architecture
542015024745809/03/15 Bearing support stiffness control
552015024746009/03/15 Sensor adapter
562015024746109/03/15 Geared turbofan with high fan rotor power intensity
572015024746209/03/15 Gas turbine engine thermal management system for heat exchanger using bypass flow
582015024949909/03/15 Support system for fiber optic components in harsh environment machines
592015023909508/27/15 Confined pencil blasting apparatus
602015023956808/27/15 Pylon shape with geared turbofan for structural stiffness
612015024065808/27/15 Carbon nanotubes for increasing vibration damping in polymer matrix composite containment cases for aircraft engines
622015024066008/27/15 Buffer airflow to bearing compartment
632015024066108/27/15 Repair or remanufacture of liner panels for a gas turbine engine
642015024066208/27/15 Case assembly for a gas turbine engine
652015024066308/27/15 Liner lock segment
662015024071208/27/15 Mid-turbine duct for geared gas turbine engine
672015024072308/27/15 Bore basket for a gas powered turbine
682015024072408/27/15 Combustor seal mistake-proofing for a gas turbine engine
692015024072508/27/15 Gas turbine engine with forward moment arm
702015024074508/27/15 Angled reverse core gas turbine engine with widened nozzle
712015024086708/27/15 Turbomachine bearing support structure
722015024106308/27/15 Combustor with grommet having projecting lip
732015024106708/27/15 Fastened joint for a tangential on board injector
742015023166508/20/15 Spray masking for rotors
752015023325008/20/15 Gas turbine engine airfoil
762015023325108/20/15 Gas turbine engine airfoil
772015023325208/20/15 Gas turbine engine airfoil
782015023325908/20/15 Fan blade tall dovetail for individually bladed rotors
792015023326408/20/15 Retention of damping media
802015023329308/20/15 Annular spring for a bearing assembly of a gas turbine engine
812015023329508/20/15 Split-zone flow metering t-tube
822015023329708/20/15 Fuel manifold fitting with integral support for a gas turbine engine
832015023329808/20/15 Reduction in jet flap interaction noise with geared turbine engine
842015023330008/20/15 Geared gas turbine engine accessory gearbox
852015023330108/20/15 Method for setting a gear ratio of a fan drive gear system of a gas turbine engine
862015023330208/20/15 Operability geared turbofan engine including compressor section variable guide vanes
872015023330308/20/15 Method for setting a gear ratio of a fan drive gear system of a gas turbine engine
882015023332308/20/15 Gas turbine engine airfoil
892015023358108/20/15 Fuel manifold for a gas turbine engine
902015022606708/13/15 Airfoil array with airfoils that differ in geometry according to geometry classes
912015022607708/13/15 Seal damper with improved retention
922015022608508/13/15 Baffle with flow augmentation feature
932015022611608/13/15 Fan drive gear system module and inlet guide vane coupling mechanism
942015022611708/13/15 Gas turbine engine with distributed fans
952015022612308/13/15 Gas turbine engine buffer cooling system
962015022612508/13/15 Combined high pressure turbine case and turbine intermediate case
972015022613008/13/15 Gas turbine engine including vane structure and seal to control fluid leakage
982015022613108/13/15 Combustor seal system for a gas turbine engine
992015022613208/13/15 Gas turbine engine ring seal
1002015022615608/13/15 Non-axisymmetric fixed or variable fan nozzle for boundary layer ingestion propulsion
1012015022623108/13/15 Fan blade removal panel
1022015022767708/13/15 Gas turbine engine with first turbine vane clocking
1032015021738808/06/15 Method of modifying gear profiles
1042015021895508/06/15 Compliant cantilevered airfoil
1052015021895708/06/15 Guide vane seal
1062015021896508/06/15 Variable positioner
1072015021896608/06/15 Gas turbine engine fan spacer platform attachments
1082015021901108/06/15 Dual oil supply tube
1092015021901508/06/15 Seal assembly for a static structure of a gas turbine engine
1102015021901708/06/15 Actuator mounted to torque box
1112015021924608/06/15 Polymeric or composite interlocking mount assembly for cable harnesses and fluid tubes
1122015021933808/06/15 Combustor assembly for a turbine engine
1132015020986407/30/15 Method for synthesizing nanowires and nanofoam
1142015021137607/30/15 Turbine vane cooling arrangement
1152015021141607/30/15 Gas turbine engine with twin offset gas generators
1162015021144107/30/15 Variable exhaust mixer and cooler for a three-stream gas turbine engine
1172015021144307/30/15 Divot for blocker doors of thrust reverser system
1182015021144407/30/15 Aft counter-rotating shrouded geared turbofan
1192015021174107/30/15 Method for repairing fuel nozzle guides for gas turbine engine combustors using cold metal transfer weld technology
1202015020270207/23/15 Gas turbine engine cast structure finishing
1212015020270707/23/15 Attachment of structures having different physical characteristics
1222015020341107/23/15 Additive manufacturing hybrid core
1232015020395407/23/15 Coating system and process
1242015020420107/23/15 Contoured flowpath surface
1252015020421207/23/15 High durability turbine exhaust case
1262015020423807/23/15 Low noise turbine for geared turbofan engine
1272015020424407/23/15 Selectively deoxygenated stored fuel system
1282015020434707/23/15 Fan blades with abrasive tips
1292015020444707/23/15 Radially coacting ring seal
1302015020462507/23/15 High temperature heat transfer interface
1312015019784007/16/15 Systems and methods for removing overspray
1322015019804507/16/15 High order shaped curve region for an airfoil
1332015019804707/16/15 Mistuned airfoil assemblies
1342015019805607/16/15 Abradable seal having nanolayer material
1352015019809207/16/15 Dual function air diverter and variable area fan nozzle
1362015019811607/16/15 Variable area exhaust mixer for a gas turbine engine
1372015019817307/16/15 Fan blade with variable thickness composite cover
1382015019825307/16/15 Shrouded face seal and components thereof
1392015019995207/16/15 Vibration damping material for high temperature use
1402015019082407/09/15 Cold spray systems with in-situ powder manufacturing
1412015019088907/09/15 Systems and methods for solid state metal repair
1422015019089107/09/15 Repair of casting defects
1432015019089307/09/15 Systems and methods for airfoil assembly
1442015019094907/09/15 Media containment for iso-grid structure forming
1452015019202107/09/15 Airfoil cooling arrangement
1462015019203407/09/15 Systems and methods for centering bearing compartments
1472015019206807/09/15 Auxiliaryy fluid flow system debris filter
1482015019207007/09/15 Geared turbofan gas turbine engine architecture
1492015019207107/09/15 Geared turbofan gas turbine engine architecture
1502015019207207/09/15 Fluid transport system having divided transport tube
1512015019209207/09/15 Sliding nozzle flap assembly
1522015019214407/09/15 Fan assembly with fan blade under-root spacer
1532015019216507/09/15 Systems and methods for centering bearing compartments
1542015019229807/09/15 Gas turbine engine with improved fuel efficiency
1552015019230007/09/15 Light weight swirler for gas turbine engine combustor and a manufacturing
1562015018302607/02/15 Investment mold having metallic donor element
1572015018307807/02/15 System and methods for rough grinding
1582015018430607/02/15 Electroformed sheath
1592015018451307/02/15 Device and repairing a forward frame v-blade in an aircraft engine
1602015018485707/02/15 Microcircuit cooling for gas turbine engine combustor
1612015018486007/02/15 Spiral pulse detonation tube configuration
1622015018510907/02/15 Methods for testing laser shock peening
1632015017465306/25/15 System and methods for removing core elements of cast components
1642015017472906/25/15 Systems and methods for modifying and adding features on grinding wheel surfaces
1652015017473106/25/15 Systems and methods for dressing grinding wheels
1662015017648406/25/15 Geared turbofan with a gearbox aft of a fan drive turbine
1672015017649306/25/15 Gas turbine engine forward bearing compartment architecture
1682015017649706/25/15 Geared turbofan with a gearbox upstream of a fan drive turbine
1692015017650206/25/15 Method of controlling a gas turbine engine using real-time component temperature data
1702015017653006/25/15 Ultra high overall pessure ratio gas turbine engine
1712015016550006/18/15 Deep rolling tool for blade fatigue life enhancement
1722015016551306/18/15 Machine for deep rolling tool positioning
1732015016551406/18/15 Deep rolling tool with force adjustment
1742015016551506/18/15 Deep rolling tool for processing blade root
1752015016557006/18/15 Crimping tool
1762015016566606/18/15 Systems and methods for manufacturing fiber-reinforced polymeric components
1772015016712506/18/15 Nickel alloy for repairs
1782015016714906/18/15 Movable evaporation source
1792015016754906/18/15 Exhaust stream mixer
1802015016767606/18/15 Gas turbine engine for long range aircraft
1812015017256506/18/15 Composite image processing for lwir images using geometric features
1822015017256606/18/15 Natural resolution processing for lwir images
1832015015807606/11/15 Method of fabricating an investment casting mold and slurry therefor
1842015015859706/11/15 Emergency power generation via limited variable pitch fan blade
1852015015950106/11/15 Rigid and rotatable vanes molded within variably shaped flexible airfoils
1862015015950806/11/15 Core drainage systems for fan case assemblies
1872015016009706/11/15 Long wave infrared sensing for turbomachine
1882015015254406/04/15 Coating methods and apparatus
1892015015273906/04/15 Turbine blade rail damper
1902015015274606/04/15 Slotted distribution sleeve for a seal plate
1912015015278706/04/15 Low noise compressor rotor for geared turbofan engine
1922015015278906/04/15 Multi-bypass stream gas turbine engine with enlarged bypass flow area
1932015015372606/04/15 Method for inspecting a manufacturing device
1942015015678906/04/15 Communication of avionic data
1952015014379405/28/15 Geared turbofan engine gearbox arrangement
1962015014752805/28/15 Component blending tool
1972015013567805/21/15 Gas turbine engine with noise attenuating variable area fan nozzle
1982015013834205/21/15 System and method to determine visible damage
1992015014123505/21/15 Carbon fiber-reinforced article and method therefor
2002015013210605/14/15 Gas turbine engine with low fan pressure ratio
2012015013211005/14/15 High durability turbine exhaust case
2022015013213405/14/15 Injection molded composite fan platform
2032015013214205/14/15 Rotor blade with bonded cover
2042015012168205/07/15 Extraction tool assembly
2052015012183805/07/15 Conjoined reverse core flow engine arrangement
2062015012183905/07/15 Tandem thrust reverser with multi-bar linkage
2072015012184105/07/15 Flow control device for a three stream turbofan engine
2082015012184405/07/15 Geared turbofan arrangement with core split power ratio
2092015012188205/07/15 Mixer assembly for a gas turbine engine
2102015012188405/07/15 Stress relieved rectilinear duct
2112015012189305/07/15 Adaptive fan reverse core geared turbofan engine with separate cold turbine
2122015012189405/07/15 Bifurcation fire purge system
2132015012189505/07/15 Full ring sliding nacelle with thrust reverser
2142015012189605/07/15 Reverse core flow engine mounting arrangement
2152015012203105/07/15 Transducer position guide
2162015012233905/07/15 Variable area bypass nozzle
2172015012290505/07/15 Passive tangential ejector for an exhaust nozzle of a gas turbine engine
2182015012291205/07/15 Tandem thrust reverser with multi-point actuation
2192015012295205/07/15 Gas turbine engine inlet wall design
2202015012299805/07/15 Method of inspection for cooling holes in turbine airfoil
2212015012525905/07/15 Gas turbine engine variable pitch fan blade
2222015012527005/07/15 Atr guide pins for sliding nacelle
2232015012528405/07/15 Atr full ring sliding nacelle
2242015012528505/07/15 Integrated nozzle and plug
2252015012528605/07/15 Atr axial v-groove
2262015012529105/07/15 Bracket for mounting a stator guide vane arrangement to a strut in a turbine engine
2272015012529305/07/15 Turbofan engine main bearing arrangement
2282015012529505/07/15 Wind turbine load mitigation
2292015012530405/07/15 Mass offset for damping performance
2302015012530505/07/15 Low profile fan platform attachment
2312015012568105/07/15 High temperature imaging media for digital image correlation
2322015012609605/07/15 System and contoured peel grinding
2332015011394104/30/15 Translating outer cowl flow modulation device and method
2342015011394204/30/15 Phosphor thermometer with two waveguides
2352015011394304/30/15 Geared turbofan engine with power density range
2362015011394504/30/15 Pivoting blocker door
2372015011399604/30/15 Cascaded multi-variable control system for a turboshaft engine
2382015011400204/30/15 Geared turbofan engine with a high ratio of thrust to turbine volume
2392015011407404/30/15 Systems and methods for controlled peening
2402015011749304/30/15 Phosphor thermometry fiber sensor
2412015011780404/30/15 Gas turbine engine bushing
2422015011806304/30/15 Turbine airfoil tip shelf and squealer pocket cooling
2432015011806404/30/15 Gas turbine engine airfoil trailing edge passage and core for making same
2442015010722304/23/15 High durability turbine exhaust case
2452015011063604/23/15 Wear pad to prevent cracking of fan blade
2462015011102204/23/15 Coating for metal cellular structure and method therefor
2472015010193504/16/15 Apparatus and ionic liquid electroplating
2482015010431504/16/15 Fan blade root integrated sealing solution
2492015009630304/09/15 Gas turbine engine with high speed low pressure turbine section

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