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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


Additive manufacturing hybrid core

United Technologies

Additive manufacturing hybrid core

Attachment of structures having different physical characteristics

United Technologies

Attachment of structures having different physical characteristics



Count Application # Date United Technologies Corporation patents (updated weekly) - BOOKMARK this page
12015020270207/23/15  new patent  Gas turbine engine cast structure finishing
22015020270707/23/15  new patent  Attachment of structures having different physical characteristics
32015020341107/23/15  new patent  Additive manufacturing hybrid core
42015020395407/23/15  new patent  Coating system and process
52015020420107/23/15  new patent  Contoured flowpath surface
62015020421207/23/15  new patent  High durability turbine exhaust case
72015020423807/23/15  new patent  Low noise turbine for geared turbofan engine
82015020424407/23/15  new patent  Selectively deoxygenated stored fuel system
92015020434707/23/15  new patent  Fan blades with abrasive tips
102015020444707/23/15  new patent  Radially coacting ring seal
112015020462507/23/15  new patent  High temperature heat transfer interface
122015019784007/16/15 Systems and methods for removing overspray
132015019804507/16/15 High order shaped curve region for an airfoil
142015019804707/16/15 Mistuned airfoil assemblies
152015019805607/16/15 Abradable seal having nanolayer material
162015019809207/16/15 Dual function air diverter and variable area fan nozzle
172015019811607/16/15 Variable area exhaust mixer for a gas turbine engine
182015019817307/16/15 Fan blade with variable thickness composite cover
192015019825307/16/15 Shrouded face seal and components thereof
202015019995207/16/15 Vibration damping material for high temperature use
212015019082407/09/15 Cold spray systems with in-situ powder manufacturing
222015019088907/09/15 Systems and methods for solid state metal repair
232015019089107/09/15 Repair of casting defects
242015019089307/09/15 Systems and methods for airfoil assembly
252015019094907/09/15 Media containment for iso-grid structure forming
262015019202107/09/15 Airfoil cooling arrangement
272015019203407/09/15 Systems and methods for centering bearing compartments
282015019206807/09/15 Auxiliaryy fluid flow system debris filter
292015019207007/09/15 Geared turbofan gas turbine engine architecture
302015019207107/09/15 Geared turbofan gas turbine engine architecture
312015019207207/09/15 Fluid transport system having divided transport tube
322015019209207/09/15 Sliding nozzle flap assembly
332015019214407/09/15 Fan assembly with fan blade under-root spacer
342015019216507/09/15 Systems and methods for centering bearing compartments
352015019229807/09/15 Gas turbine engine with improved fuel efficiency
362015019230007/09/15 Light weight swirler for gas turbine engine combustor and a manufacturing
372015018302607/02/15 Investment mold having metallic donor element
382015018307807/02/15 System and methods for rough grinding
392015018430607/02/15 Electroformed sheath
402015018451307/02/15 Device and repairing a forward frame v-blade in an aircraft engine
412015018485707/02/15 Microcircuit cooling for gas turbine engine combustor
422015018486007/02/15 Spiral pulse detonation tube configuration
432015018510907/02/15 Methods for testing laser shock peening
442015017465306/25/15 System and methods for removing core elements of cast components
452015017472906/25/15 Systems and methods for modifying and adding features on grinding wheel surfaces
462015017473106/25/15 Systems and methods for dressing grinding wheels
472015017648406/25/15 Geared turbofan with a gearbox aft of a fan drive turbine
482015017649306/25/15 Gas turbine engine forward bearing compartment architecture
492015017649706/25/15 Geared turbofan with a gearbox upstream of a fan drive turbine
502015017650206/25/15 Method of controlling a gas turbine engine using real-time component temperature data
512015017653006/25/15 Ultra high overall pessure ratio gas turbine engine
522015016550006/18/15 Deep rolling tool for blade fatigue life enhancement
532015016551306/18/15 Machine for deep rolling tool positioning
542015016551406/18/15 Deep rolling tool with force adjustment
552015016551506/18/15 Deep rolling tool for processing blade root
562015016557006/18/15 Crimping tool
572015016566606/18/15 Systems and methods for manufacturing fiber-reinforced polymeric components
582015016712506/18/15 Nickel alloy for repairs
592015016714906/18/15 Movable evaporation source
602015016754906/18/15 Exhaust stream mixer
612015016767606/18/15 Gas turbine engine for long range aircraft
622015017256506/18/15 Composite image processing for lwir images using geometric features
632015017256606/18/15 Natural resolution processing for lwir images
642015015807606/11/15 Method of fabricating an investment casting mold and slurry therefor
652015015859706/11/15 Emergency power generation via limited variable pitch fan blade
662015015950106/11/15 Rigid and rotatable vanes molded within variably shaped flexible airfoils
672015015950806/11/15 Core drainage systems for fan case assemblies
682015016009706/11/15 Long wave infrared sensing for turbomachine
692015015254406/04/15 Coating methods and apparatus
702015015273906/04/15 Turbine blade rail damper
712015015274606/04/15 Slotted distribution sleeve for a seal plate
722015015278706/04/15 Low noise compressor rotor for geared turbofan engine
732015015278906/04/15 Multi-bypass stream gas turbine engine with enlarged bypass flow area
742015015372606/04/15 Method for inspecting a manufacturing device
752015015678906/04/15 Communication of avionic data
762015014379405/28/15 Geared turbofan engine gearbox arrangement
772015014752805/28/15 Component blending tool
782015013567805/21/15 Gas turbine engine with noise attenuating variable area fan nozzle
792015013834205/21/15 System and method to determine visible damage
802015014123505/21/15 Carbon fiber-reinforced article and method therefor
812015013210605/14/15 Gas turbine engine with low fan pressure ratio
822015013211005/14/15 High durability turbine exhaust case
832015013213405/14/15 Injection molded composite fan platform
842015013214205/14/15 Rotor blade with bonded cover
852015012168205/07/15 Extraction tool assembly
862015012183805/07/15 Conjoined reverse core flow engine arrangement
872015012183905/07/15 Tandem thrust reverser with multi-bar linkage
882015012184105/07/15 Flow control device for a three stream turbofan engine
892015012184405/07/15 Geared turbofan arrangement with core split power ratio
902015012188205/07/15 Mixer assembly for a gas turbine engine
912015012188405/07/15 Stress relieved rectilinear duct
922015012189305/07/15 Adaptive fan reverse core geared turbofan engine with separate cold turbine
932015012189405/07/15 Bifurcation fire purge system
942015012189505/07/15 Full ring sliding nacelle with thrust reverser
952015012189605/07/15 Reverse core flow engine mounting arrangement
962015012203105/07/15 Transducer position guide
972015012233905/07/15 Variable area bypass nozzle
982015012290505/07/15 Passive tangential ejector for an exhaust nozzle of a gas turbine engine
992015012291205/07/15 Tandem thrust reverser with multi-point actuation
1002015012295205/07/15 Gas turbine engine inlet wall design
1012015012299805/07/15 Method of inspection for cooling holes in turbine airfoil
1022015012525905/07/15 Gas turbine engine variable pitch fan blade
1032015012527005/07/15 Atr guide pins for sliding nacelle
1042015012528405/07/15 Atr full ring sliding nacelle
1052015012528505/07/15 Integrated nozzle and plug
1062015012528605/07/15 Atr axial v-groove
1072015012529105/07/15 Bracket for mounting a stator guide vane arrangement to a strut in a turbine engine
1082015012529305/07/15 Turbofan engine main bearing arrangement
1092015012529505/07/15 Wind turbine load mitigation
1102015012530405/07/15 Mass offset for damping performance
1112015012530505/07/15 Low profile fan platform attachment
1122015012568105/07/15 High temperature imaging media for digital image correlation
1132015012609605/07/15 System and contoured peel grinding
1142015011394104/30/15 Translating outer cowl flow modulation device and method
1152015011394204/30/15 Phosphor thermometer with two waveguides
1162015011394304/30/15 Geared turbofan engine with power density range
1172015011394504/30/15 Pivoting blocker door
1182015011399604/30/15 Cascaded multi-variable control system for a turboshaft engine
1192015011400204/30/15 Geared turbofan engine with a high ratio of thrust to turbine volume
1202015011407404/30/15 Systems and methods for controlled peening
1212015011749304/30/15 Phosphor thermometry fiber sensor
1222015011780404/30/15 Gas turbine engine bushing
1232015011806304/30/15 Turbine airfoil tip shelf and squealer pocket cooling
1242015011806404/30/15 Gas turbine engine airfoil trailing edge passage and core for making same
1252015010722304/23/15 High durability turbine exhaust case
1262015011063604/23/15 Wear pad to prevent cracking of fan blade
1272015011102204/23/15 Coating for metal cellular structure and method therefor
1282015010193504/16/15 Apparatus and ionic liquid electroplating
1292015010431504/16/15 Fan blade root integrated sealing solution
1302015009630304/09/15 Gas turbine engine with high speed low pressure turbine section
1312015009671304/09/15 Rapid tooling insert manufacture
1322015009683904/09/15 Low loss oil accumulator assembly
1332015009883004/09/15 Assembly fixture for a stator vane assembly
1342015009883504/09/15 Castings, casting cores, and methods
1352015008991804/02/15 Gas turbine lubrication systems
1362015008995804/02/15 Gas turbine engine with high speed low pressure turbine section
1372015008995904/02/15 Gas turbine engine shaft bearing configuration
1382015008294503/26/15 Process for producing refractory metal alloy powders
1392015008391903/26/15 Background radiation measurement system
1402015008626203/26/15 Welded assemblies and methods of making welded assemblies
1412015008628303/26/15 Ball-end milling cutter tool
1422015007574503/19/15 Casting molds, manufacture and use methods
1432015007891503/19/15 Piloted nut
1442015006820903/12/15 Method for determining circumferential sensor positioning
1452015006821003/12/15 Tube fed tangential on-board injector for gas turbine engine
1462015006821403/12/15 Low thermal mass joint
1472015006966803/12/15 Multi-dimensional component build system and process
1482015007170403/12/15 Exhaust duct liner rod hanger
1492015006000203/05/15 Die casting system and cell
1502015006528503/05/15 Geared architecture gas turbine engine with oil scavenge
1512015005287302/26/15 Torque connector lubrication scuppers
1522015005290702/26/15 Thermal management system for gas turbine engine
1532015005378902/26/15 Linkage to control and restrain flap movement
1542015005012702/19/15 Air with integral spring for a gas turbine engine exhaust drive
1552015005104002/19/15 Oil baffle for gas turbine fan drive gear system
1562015004202302/12/15 Hybrid part made from monolithic ceramic skin and cmc core
1572015004402802/12/15 Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
1582015004405202/12/15 Geared turbofan with fan blades designed to achieve laminar flow
1592015004520002/12/15 Ceramic component
1602015003760202/05/15 System and high temperature die casting tooling
1612015002710101/29/15 Geared gas turbine engine architecture for enhanced efficiency
1622015002713001/29/15 Split ring valve
1632015002765701/29/15 Method and casting core for forming a landing for welding a baffle inserted in an airfoil
1642015003044001/29/15 Fireshield fastener hood
1652015003044301/29/15 Split damped outer shroud for gas turbine engine stator arrays
1662015002378001/22/15 Liner attaching scheme
1672015002429601/22/15 Method and system for operating a flow battery system based on energy costs
1682015001330101/15/15 Turbine engine including balanced low pressure stage count
1692015001334401/15/15 Tube
1702015001348001/15/15 Plated instrumentation probes and sensors
1712015001393401/15/15 Article with grouped grain patterns
1722015001695401/15/15 Blade outer air seal assembly and support
1732015001696501/15/15 Link arm drag reducing device
1742015000826801/08/15 Pivot thrust reverser with multi-point actuation
1752015000008901/01/15 Clamp connector
1762015000030301/01/15 Wireless power for gas turbine engine instrumentation
1772015000030401/01/15 Removable nosecone for a gas turbine engine
1782015000395601/01/15 Variable vane scheduling
1792015000396801/01/15 Gas turbine engine with attached nosecone
1802015000399501/01/15 Aircraft engine component with locally tailored materials
1812015000399701/01/15 Method of forming hybrid metal ceramic components
1822014037354912/25/14 Cooling hole with curved metering section
1832014037355412/25/14 Air turbine starter pressure monitor system
1842014037361012/25/14 Engine inspection apparatus and system
1852014037505612/25/14 Method of operating a power generation system
1862014036654812/18/14 Turbine engine gearbox
1872014036655412/18/14 Cross reference to related applications
1882014036655612/18/14 Gas turbine engine vane-to-transition duct seal
1892014036661312/18/14 Probe retention-sealing feature
1902014036978312/18/14 Self-retaining shear pin for blind mount location
1912014036980412/18/14 Variable bleed slot in centrifugal impeller
1922014036981812/18/14 Planetary gear system arrangement with auxiliary oil system
1932014036015212/11/14 Oil tank mount with yoke
1942014036015312/11/14 Gas turbine engine thermal management system
1952014036330512/11/14 Hybrid turbine blade for improved engine performance or architecture
1962014035656012/04/14 Castings and manufacture methods
1972014035839812/04/14 Use of ss data trends in fault resolution process
1982014035850012/04/14 Probalistic high cycle fatigue (hcf) design optimization process
1992014034857711/27/14 Tie bolt employing differential thread
2002014034863011/27/14 Noise reducing vane
2012014034864011/27/14 Thrust efficient turbofan engine
2022014033833611/20/14 Gas turbine engine combustor with integrated combustor vane
2032014033835111/20/14 Gas turbine engine combustor with tailored temperature profile
2042014033835711/20/14 Cavity swirl fuel injector for an augmentor section of a gas turbine engine
2052014033836011/20/14 Bleed port ribs for turbomachine case
2062014033219111/13/14 Extreme environment heat exchanger
2072014033491611/13/14 Borescope inspection port fitting
2082014032684211/06/14 Oil tank mount with stiffeners
2092014031813310/30/14 Thrust efficient turbofan engine
2102014031814310/30/14 Multi-circuit buffer system for a gas turbine engine
2112014031814710/30/14 Low noise compressor rotor for geared turbofan engine
2122014032196110/30/14 Mate face cooling holes for gas turbine engine component
2132014032302210/30/14 Airfoil edge form transfer grinding tool
2142014032436310/30/14 System reliability analysis and management using physics-based models embedded in a baysian network
2152014031112110/23/14 Pulse detonation engine having a scroll ejector attenuator
2162014031114910/23/14 Gas turbine engine fan blade airfoil profile
2172014031261110/23/14 Locking fluid fittings
2182014031454010/23/14 Gas turbine engine synchronization ring
2192014031454110/23/14 Turbomachine thrust balancing system
2202014031454210/23/14 Gas turbine engine exhaust diffuser with movable struts
2212014031454610/23/14 Turbine engine gearbox mount with multiple fuse joints
2222014031454710/23/14 Attachment ceramic matrix composite materials
2232014031458110/23/14 Method for forming single crystal parts using additive manufacturing and remelt
2242014029878810/09/14 Gas turbine engine including pneumatic actuator system
2252014030142510/09/14 Backstrike detection system for laser drilling thin materials
2262014030182910/09/14 Engine bearing support
2272014029021110/02/14 Turbine engine including balanced low pressure stage count
2282014029021310/02/14 Duct blocker seal assembly for a gas turbine engine
2292014029026910/02/14 Duct blocker seal assembly for a gas turbine engine
2302014029455810/02/14 Turbomachine fluid delivery manifold and system
2312014028350009/25/14 Thrust efficient turbofan engine
2322014028350109/25/14 Elongated geared turbofan with high bypass ratio
2332014028674809/25/14 Fan containment case with thermally conforming liner
2342014028675409/25/14 Elongated geared turbofan with high bypass ratio
2352014028675509/25/14 Ring gear mounting arrangement with oil scavenge scheme
2362014028678109/25/14 Integral fan blade wear pad and platform seal
2372014025966109/18/14 Variable area fan nozzle with wall thickness distribution
2382014026017609/18/14 Lube tube expansion and torque retaining device
2392014026018209/18/14 Free stream intake for reverse core engine
2402014026018309/18/14 Variable cycle intake for reverse core engine
2412014026032109/18/14 Gas turbine engine static structure joint with undercuts
2422014026179709/18/14 Tube fitting having integrated tee fitting
2432014026810009/18/14 Multiple laser time of arrival probe
2442014026981709/18/14 Phosphor thermometry fiber sensor
2452014027062509/18/14 High temperature uncooled optical probe
2462014027110109/18/14 Modulated turbine vane cooling
2472014027111209/18/14 Low noise turbine for geared gas turbine engine
2482014027112109/18/14 Gas turbine engine architecture with intercooled twin centrifugal compressor
2492014027113509/18/14 Turbofan engine bearing and gearbox arrangement



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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