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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
12015033603711/26/15  new patent  Fuel system with ice and large debris separator filter
22015033623311/26/15  new patent  Conditioning one or more internal surfaces of an object
32015033665511/26/15  new patent  Box wing with angled gas turbine engine cores
42015033685011/26/15  new patent  Thermal barrier coating for cmas resistance and low thermal conductivity
52015033766111/26/15  new patent  T-shaped platform leading edge anti-rotation tabs
62015033766611/26/15  new patent  Platform with curved edges adjacent suction side of airfoil
72015033766711/26/15  new patent  Airfoil cooling device and manufacture
82015033766811/26/15  new patent  Blade rub material
92015033767111/26/15  new patent  Abrasive blade tip treatment
102015033767211/26/15  new patent  Grooved blade outer air seals
112015033767311/26/15  new patent  Segmented clearance control ring
122015033767411/26/15  new patent  Seal assembly for arranging between a stator and a rotor
132015033767511/26/15  new patent  Active clearance control for gas turbine engine
142015033767711/26/15  new patent  Geared turbofan with high speed generator
152015033768111/26/15  new patent  Scupper channelling in gas turbine modules
162015033768211/26/15  new patent  Cooling architecture for turbine exhaust case
172015033768311/26/15  new patent  Angled cut to direct radiative heat load
182015033768411/26/15  new patent  Acoustic treatment to mitigate fan noise
192015033768711/26/15  new patent  Split cast vane fairing
202015033773111/26/15  new patent  Oil pump transfer plate
212015033773211/26/15  new patent  Gas turbine engine mid turbine frame bearing support
222015033773811/26/15  new patent  Two spool gas generator with improved air porting
232015033776211/26/15  new patent  Turbofan thrust reverser system
242015033789111/26/15  new patent  Linkage with spherical or journal bearing assembly
252015033800511/26/15  new patent  Cooling systems for gas turbine engine components
262015033827811/26/15  new patent  Gas turbine engine optical system
272015033836411/26/15  new patent  Multiple-excitation multiple-receiving (memr) capacitance tomography
282015034071011/26/15  new patent  Carbon electrode and method therefor
292015032868111/19/15 Multi-shot casting
302015032871711/19/15 Methods of repairing integrally bladed rotors
312015033022511/19/15 Rotor and gas turbine engine including a rotor
322015033022711/19/15 Blades and blade dampers for gas turbine engines
332015033022811/19/15 Airfoil tip pocket with augmentation features
342015033022911/19/15 Tip leakage flow directionality control
352015033023011/19/15 Tip leakage flow directionality control
362015033023911/19/15 Seal support disk and assembly
372015033024111/19/15 Gas turbine seal assembly and seal support
382015033024411/19/15 Multi-purpose gas turbine seal support and assembly
392015033024511/19/15 Flow diverter element and assembly
402015033024811/19/15 Heat shield for cooling a strut
412015033024911/19/15 Frame strut cooling holes
422015033025011/19/15 Turbine exhaust case architecture
432015033025111/19/15 Gas turbine engine with fluid damper
442015033025411/19/15 Compact nacelle with contoured fan nozzle
452015033025511/19/15 Anti-torsion assembly with wedge-shaped torque block
462015033030011/19/15 Two spool engine core with a starter
472015033030211/19/15 Geared turbofan gas turbine engine architecture
482015033030511/19/15 Anti-icing internal manifold
492015033030611/19/15 Gas generator with mount having air passages
502015033064511/19/15 Comfort estimation and incentive design for energy efficiency
512015033333511/19/15 Flow battery having electrodes with a plurality of different pore sizes and or different layers
522015033335411/19/15 Proton exchange material and method therefor
532015032121711/12/15 Solid state metal powder consolidation for structural components
542015032124911/12/15 Hybrid turbine blade for improved engine performance or architecture
552015032125011/12/15 Method for forming a directionally solidified replacement body for a component using additive manufacturing
562015032125311/12/15 Surface treatment of powers
572015032129611/12/15 Repair material preform
582015032129711/12/15 Systems and methods for repairing a surface of damaged metal components
592015032138211/12/15 Integral ceramic matrix composite fastener with non-polymer rigidization
602015032141711/12/15 Method for producing void-free additively manufactured components
612015032142211/12/15 Sensor fusion for powder bed manufacturing process control
622015032176411/12/15 Gas turbine engine inlet wall design
632015032256311/12/15 Fixture for application of coatings and using same
642015032258411/12/15 System and methods for electrochemical grinding with a screen
652015032279711/12/15 Blade element cross-ties
662015032279911/12/15 Method for forming components using additive manufacturing and re-melt
672015032280111/12/15 Airfoil leading edge film array
682015032280511/12/15 Blade underroot spacer with hook removal
692015032280611/12/15 High temperature compliant metallic elements for low contact stress ceramic support
702015032280711/12/15 Multi-ply finger seal
712015032280911/12/15 Blade rub material
722015032281611/12/15 Gas turbine engine and seal assembly therefore
732015032282011/12/15 Shrouded conduit for arranging a fluid flowpath
742015032285411/12/15 Gas turbine engine oil tank
752015032285511/12/15 Reverse flow gas turbine engine core
762015032286011/12/15 Variable vane segment
772015032292211/12/15 Generator with stator supported on rotor
782015032305611/12/15 Fan drive gear system integrated carrier and torque frame
792015032310711/12/15 Fluid couplings and methods for additive manufacturing thereof
802015032318211/12/15 Conjoined grommet assembly for a combustor
812015032318311/12/15 Case with integral heat shielding
822015032318611/12/15 Cooled fuel injector system for a gas turbine engine and operating the same
832015032346711/12/15 Chemiluminescence imaging system and monitoring a combustor flame of a turbine engine
842015031437311/05/15 Additive manufacturing system for minimizing thermal stresses
852015031591611/05/15 Platform with curved edges
862015031591811/05/15 Shrouded turbine blade with cut corner
872015031592211/05/15 Gas turbine engine with reinforced spinner
882015031592411/05/15 Universal seal
892015031592511/05/15 Gas turbine seal assembly and seal support
902015031592911/05/15 Gas turbine engine airfoil cooling passage configuration
912015031593011/05/15 Reducing variation in cooling hole meter length
922015031597411/05/15 Two spool gas generator with improved pressure split
932015031597611/05/15 Gas turbine engine variable area fan nozzle control
942015031597711/05/15 Gas turbine engine with low stage count low pressure turbine
952015031600011/05/15 Gas turbine engine systems and methods involving enhanced fuel dispersion
962015031667711/05/15 Capacitive probe fabricating from spray deposition
972015031855911/05/15 Fuel cell catalyst treatment
982015030671310/29/15 A fabricating a rotor of a turbofan engine
992015030799010/29/15 Method and system for controlling coating in non-line-of-sight locations
1002015030827410/29/15 Engine component with wear surface protection
1012015030828110/29/15 Low permeability high pressure compressor abradable seal for bare ni airfoils having continuous metal matrix
1022015030829210/29/15 Cowl with rate limited lock
1032015030833510/29/15 Method for setting a gear ratio of a fan drive gear system of a gas turbine engine
1042015030833910/29/15 Gas turbine engine with lower bifurcation heat exchanger
1052015030834110/29/15 Compressor injector apparatus and system
1062015030834210/29/15 Gas turbine engine vapor cooled centrifugal impeller
1072015030834310/29/15 Installation mounts for a turbine exhaust case
1082015030834410/29/15 Combination flow divider and bearing support
1092015030834810/29/15 Continuous detonation wave turbine engine
1102015030835110/29/15 Fundamental gear system architecture
1112015030835210/29/15 Gas turbine engine with fan-tied inducer section
1122015030844510/29/15 Gas turbine engine and buffer system therefor
1132015030844910/29/15 Gas turbine engine component with brazed cover
1142015030848510/29/15 Threaded fastener lock
1152015030851010/29/15 Systems and methods for engine bearings
1162015031097110/29/15 Magnetic material and method therefor
1172015029826110/22/15 Mitigating distortion of coated parts during laser drilling
1182015029879410/22/15 Aircraft with forward sweeping t-tail
1192015029881410/22/15 Clocked thrust reversers
1202015029881510/22/15 Redundant mount system
1212015029988410/22/15 Alloying interlayer for electroplated aluminum on aluminum alloys
1222015030017610/22/15 Spinner for electrically grounding fan blades
1232015030018010/22/15 Gas turbine engine turbine blade tip with coated recess
1242015030018610/22/15 Turbine engine variable area vane with feather seal
1252015030018710/22/15 Turbomachine thermal management
1262015030019510/22/15 Blade outer air seal with cored passages
1272015030019710/22/15 Gas turbine engine with geared architecture
1282015030019910/22/15 Turbofan with optical diagnostic capabilities
1292015030020110/22/15 Method of reducing manufacturing variation related to blocked cooling holes
1302015030020510/22/15 Systems and methods for anti-rotational features
1312015030020710/22/15 Gas turbine engine with low stage count low pressure turbine
1322015030025010/22/15 Two spool gas generator to create family of gas turbine engines
1332015030025210/22/15 Accessory gearbox with tower shaft removal capability
1342015030025310/22/15 Reduced length transition ducts
1352015030025610/22/15 Multiple bearing stack retention
1362015030025810/22/15 Cooling hole arrangement for engine component
1372015030026410/22/15 Geared turbofan architecture for regional jet aircraft
1382015030026510/22/15 Gas turbine engine with cooling scheme for drive gear system and pitch control
1392015030026610/22/15 Gas turbine engine buffer system
1402015030029310/22/15 Reverse core turbine engine mounted above aircraft wing
1412015030040110/22/15 Moment relief barrel washer
1422015030047710/22/15 Hardened silver coated journal bearing surfaces and method
1432015030091810/22/15 Combustor flameout detection logic
1442015029070710/15/15 Working additively manufactured parts
1452015029128910/15/15 Asymmetric thrust reversers
1462015029147310/15/15 Energy preparation of ceramic fiber for coating
1472015029233410/15/15 Turbine airfoil tip shelf and squealer pocket cooling
1482015029233610/15/15 Root lightening holes with slot
1492015029233810/15/15 Electrically grounding fan platforms
1502015029234210/15/15 Stator assembly for a gas turbine engine
1512015029234310/15/15 Turbine engine vane arrangement having a plurality of interconnected vane arrangement segments
1522015029234410/15/15 Ingestion blocking endwall feature
1532015029235310/15/15 High pressure compressor thermal shield apparatus and system
1542015029235610/15/15 Heat shield based air dam for a turbine exhaust case
1552015029235810/15/15 Gas turbine engine inner case including non-symmetrical bleed slots
1562015029235910/15/15 Lubricating a rotating component during forward and/or reverse rotation
1572015029240810/15/15 Dual filtration particle separator
1582015029241010/15/15 Gas turbine engine with plural accessory air paths
1592015029241110/15/15 Angled core gas turbine engine mounting
1602015029241510/15/15 Torsion spring internal damper
1612015029243710/15/15 Gas turbine engine convergent/divergent exhaust nozzle divergent seal with dovetail interface
1622015029257510/15/15 Anti-rotational systems and methods
1632015029257710/15/15 Damped anti-rotational systems
1642015029257810/15/15 Systems and methods for shock load reduction
1652015029274110/15/15 Combustor wall assembly for a turbine engine
1662015029393010/15/15 Portable memory device data modeling for effective processing for a gas turbine engine
1672015028360310/08/15 Rib bumper system
1682015028406710/08/15 Stabilizer with structural box and sacrificial surfaces
1692015028407110/08/15 Contra-rotating open rotor distributed propulsion system
1702015028407210/08/15 Drag reduction through ion field flow control
1712015028429510/08/15 Method of forming in-situ boron nitride for ceramic matrix composite environmental protection
1722015028429710/08/15 Formation of voids within components formed from porous substrates
1732015028508110/08/15 Gas turbine engine component with flow separating rib
1742015028508610/08/15 Gas turbine engine turbine vane platform cooling
1752015028509010/08/15 Gas turbine engine forward bearing compartment architecture
1762015028509510/08/15 Air stream mixing inner diameter (id) cavity
1772015028509610/08/15 Enclosed baffle for a turbine engine component
1782015028509710/08/15 Gas turbine engine component with platform cooling circuit
1792015028509910/08/15 Multi-purpose mounting
1802015028514710/08/15 Cooling system with a bearing compartment bypass
1812015028514810/08/15 Carbureted fuel injection system for a gas turbine engine
1822015028515210/08/15 Gas turbine engine and seal assembly therefore
1832015028515410/08/15 Load balanced journal bearing pin
1842015028515510/08/15 Method for setting a gear ratio of a fan drive gear system of a gas turbine engine
1852015028515710/08/15 Variable vane and seal arrangement
1862015028518410/08/15 Metallic-coated polymer thrust reverser cascades
1872015028518610/08/15 Integrated heat exchangers for low fan pressure ratio feared turbofan
1882015028549710/08/15 Thermally compliant grommet assembly
1892015028549810/08/15 Grommet assembly and design
1902015028583710/08/15 Apparatus and facilitating transmission of a wireless signal from embedded sensors
1912015028801110/08/15 Electrochemical device and controlling corrosion
1922015027430610/01/15 Hybrid drive for gas turbine engine
1932015027430710/01/15 Nacelle inner flow structure leading edge latching system
1942015027567910/01/15 Abrasive tip blade manufacture methods
1952015027568910/01/15 Composite fan containment case assembly
1962015027569010/01/15 Vented tangential on-board injector for a gas turbine engine
1972015027569210/01/15 Reduced fan containment threat through liner and blade design
1982015027569410/01/15 Structural guide vane circumferential load bearing shear pin
1992015027575710/01/15 Bleed duct for laminar fan duct flow
2002015027576110/01/15 Seal assembly with cooling feature
2012015027576610/01/15 Geared turbine engine with a d-duct and a thrust reverser
2022015027576710/01/15 Method of defining gas turbine engine control ratings
2032015026754109/24/15 Fan blade composite cover with tapered edges
2042015026755109/24/15 Auxiliary device for three air flow path gas turbine engine
2052015026761009/24/15 Turbine enigne including balanced low pressure stage count
2062015026761709/24/15 Integrated thermal system for a gas turbine engine
2072015026761809/24/15 Geared turbofan high gearbox power density
2082015026773709/24/15 Pitch diameter shank bolt with shear sleeve
2092015026780209/24/15 Oil baffle for gas turbine fan drive gear system
2102015025860809/17/15 Casting funnel
2112015025905909/17/15 Stabilizer sacrificial surfaces
2122015026004809/17/15 Component with cooling hole having helical groove
2132015026005109/17/15 Geared low fan pressure ratio fan exit guide vane stagger angle
2142015026005409/17/15 Low compressor having variable vanes
2152015026005709/17/15 Mid-turbine frame with fairing attachment
2162015026021509/17/15 High temperature thread locking compound
2172015026039909/17/15 Combustor section of a gas turbine engine
2182015026040409/17/15 Interface heat shield for a combustor of a gas turbine engine
2192015026335809/17/15 Flow battery with mixed flow
2202015025124209/10/15 Casting cores and manufacture methods
2212015025177409/10/15 Engine installation system
2222015025246409/10/15 Equipment for plasma spray with liquid injection
2232015025267209/10/15 Ring gear mounting arrangement with oil scavenge scheme
2242015025267809/10/15 Fan blade spacer
2252015025267909/10/15 Static guide vane with internal hollow channels
2262015025268009/10/15 Synchronization ring runner with cradle
2272015025268209/10/15 Hybrid blade outer air seal for gas turbine engine
2282015025268609/10/15 Rotor blade tip clearance
2292015025272309/10/15 Compressor areas for high overall pressure ratio gas turbine engine
2302015025272809/10/15 Gas turbine engine having support structure with swept leading edge
2312015025272909/10/15 Inner diffuser case struts for a combustor of a gas turbine engine
2322015025273009/10/15 Geared turbine engine with relatively lightweight propulsor module
2332015025273109/10/15 Gas turbine engine including bleed system coupled to upstream and downstream locations of compressor
2342015025273209/10/15 Gas turbine engine with intercooling turbine section and intercooling turbine section bypass
2352015025275109/10/15 Geared gas turbine engine integrated with a variable area fan nozzle with reduced noise
2362015025275209/10/15 Low weight large fan gas turbine engine
2372015025301009/10/15 Dual fuel nozzle with concentric fuel passages for a gas turbine engine
2382015025326209/10/15 Systems and methods for x-ray diffraction
2392015025579809/10/15 Platinum alloy nano catalyst with a non-platinum core
2402015024742409/03/15 Geared turbofan engine with optimized diffuser case flange location
2412015024742509/03/15 Non-circular aft nacelle cowling geometry
2422015024745409/03/15 Geared turbofan engine with inter-shaft deflection feature
2432015024745509/03/15 External core gas turbine engine assembly
2442015024745609/03/15 Offset core engine architecture
2452015024745809/03/15 Bearing support stiffness control
2462015024746009/03/15 Sensor adapter
2472015024746109/03/15 Geared turbofan with high fan rotor power intensity
2482015024746209/03/15 Gas turbine engine thermal management system for heat exchanger using bypass flow
2492015024949909/03/15 Support system for fiber optic components in harsh environment machines

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