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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 2016 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
12016013785605/19/16  new patent  Nanocellular and nanocellular particle filled polymer composite coating for erosion protection
22016013839905/19/16  new patent  Reinforced gas turbine engine rotor disk
32016013841205/19/16  new patent  Shroud seal and wearliner
42016013841605/19/16  new patent  Variable fan nozzle using shape memory material
52016013842105/19/16  new patent  Nonlinear rolling bearing radial support stiffness
62016013842205/19/16  new patent  Gear carrier flex mount lubrication
72016013842505/19/16  new patent  Turbofan engine front section
82016013847405/19/16  new patent  Low noise compressor rotor for geared turbofan engine
92016013847705/19/16  new patent  Three spool geared turbofan with low pressure compressor drive gear system
102016013852305/19/16  new patent  Optimal thrust control of an aircraft engine
112016012967205/12/16 Underpotential deposition of metal monolayers from ionic liquids
122016013070305/12/16 Cold spray nozzles
132016013094605/12/16 Method to repair variable vanes
142016013094905/12/16 Low noise turbine for geared turbofan engine
152016013095005/12/16 Gas turbine engine component with rib support
162016013095205/12/16 Vibration-damped composite airfoils and manufacture methods
172016013095805/12/16 Gas turbine engine structural guide vanes
182016013096305/12/16 Gas turbine engine and seal assembly therefore
192016013096405/12/16 Gas turbine engine flow control device
202016013096805/12/16 Platforms with leading edge features
212016013097705/12/16 Turbine rotor segmented sideplates with anti-rotation
222016013103605/12/16 Thermal management system for a gas turbine engine
232016013103705/12/16 Supply duct for cooling air
242016013103905/12/16 Gas turbine engine heat exchanger manifold
252016013104305/12/16 Turbine engine gearbox
262016013104405/12/16 Gas turbine engine driving multiple fans
272016013108405/12/16 Geared turbofan arrangement with core split power ratio
282016013115105/12/16 Gas turbine engine airfoil
292016013136305/12/16 Combustor wall aperture body with cooling circuit
302016013136405/12/16 Combustor dilution hole cooling
312016013136505/12/16 Impingement film-cooled floatwall with backside feature
322016013396405/12/16 Flow battery with manifold passage that varies in cross-section
332016013527905/12/16 Instrumented article having compliant layer between conformal electronic device and substrate
342016012138905/05/16 Additively manufactured casting articles for manufacturing gas turbine engine parts
352016012200505/05/16 Embedded engines in hybrid blended wing body
362016012255205/05/16 Abrasive rotor coating with rub force limiting features
372016012255705/05/16 Corrosion resistant hydrophobic coatings and methods of production thereof
382016012316005/05/16 Thermal-sprayed bonding of a ceramic structure to a substrate
392016012316505/05/16 Variable area gas turbine engine component having movable spar and shell
402016012316605/05/16 Turbine vanes with variable fillets
412016012317005/05/16 Sealing systems
422016012317605/05/16 High pressure compressor rotor thermal conditioning using outer diameter gas extraction
432016012317705/05/16 Vane arm with inclined retention slot
442016012318005/05/16 Over speed monitoring using a fan drive gear system
452016012318405/05/16 Combined fan case ice liner and rear liner
462016012318705/05/16 Heatshield assembly with double lap joint for a gas turbine engine
472016012318805/05/16 Stator shroud systems
482016012323005/05/16 Curved plate/fin heater exchanger
492016012323305/05/16 Spline ring for a fan drive gear flexible support
502016012323405/05/16 High pressure compressor rotor thermal conditioning using discharge pressure air
512016012333905/05/16 Radial fastening of tubular synchronizing rings
522016012337305/05/16 Assembly for plugging an aperture in a body
532016012359205/05/16 Gas turbine engine combustor liner panel
542016012359405/05/16 Low lump mass combustor wall with quench aperture(s)
552016012359605/05/16 Combustor with axial staging for a gas turbine engine
562016012657905/05/16 Flow battery with hydrated ion-exchange membrane having maximum water domain cluster sizes
572016011436104/28/16 Wash device
582016011453204/28/16 Continuous fiber-reinforced component fabrication
592016011489404/28/16 Compressor bleed air supply for an aircraft environmental control system
602016011527804/28/16 High performance polymer and process therefor
612016011558404/28/16 Nanoparticle formation mitigation in a deposition process
622016011580004/28/16 Stator assembly with pad interface for a gas turbine engine
632016011580104/28/16 Multi-piece turbine airfoil
642016011580304/28/16 Platform cooling circuit for a gas turbine engine component
652016011580404/28/16 Seal support structure
662016011580604/28/16 Segmented seal
672016011580704/28/16 Multi-piece seal
682016011580804/28/16 Hinged seal
692016011580904/28/16 Bifurcated sliding seal
702016011581004/28/16 Bifurcated sliding seal
712016011581104/28/16 Conformal seal
722016011581204/28/16 Sliding seal
732016011581304/28/16 Dual compliant seal
742016011581404/28/16 Sliding seal
752016011582104/28/16 Bladed rotor disk including anti-vibratory feature
762016011582504/28/16 Seal support structure for a circumferential seal of a gas turbine engine
772016011586504/28/16 Gas turbine engine with high speed low pressure turbine section and bearing support features
782016011586604/28/16 Offset cores for gas turbine engines
792016011587104/28/16 Cooling configuration for a component
802016011616604/28/16 Gas turbine engine combustor liner panel
812016011616904/28/16 Mixer retention
822016010727904/21/16 Airfoil material removal
832016010733104/21/16 Functional inorganics and ceramic additive manufacturing
842016010851304/21/16 Coating system for internally-cooled component and process therefor
852016010873504/21/16 Tandem rotor blades
862016010873804/21/16 Gas turbine component with platform cooling
872016010873904/21/16 Film hole with protruding flow accumulator
882016010874504/21/16 Gas turbine hub
892016010874604/21/16 Vane assembly including two- and three-dimensional arrangements of continuous fibers
902016010874804/21/16 Gas turbine engine with dove-tailed tobi vane
912016010875004/21/16 Circumferential seal with seal dampening elements
922016010875504/21/16 Gas turbine engine component
932016010875804/21/16 Corrugated mid-turbine frame thermal radiation shield
942016010876204/21/16 Falling film evaporator for power generation systems
952016010880704/21/16 Turbofan engine front section
962016010880804/21/16 Turbofan engine bearing and gearbox arrangement
972016010881204/21/16 Conduit for guiding low pressure compressor inner diameter shroud motion
982016010881304/21/16 Additive manufactured ducted heat exchanger
992016010881404/21/16 Additive manufactured ducted heat exchanger system with additively manufactured fairing
1002016010881504/21/16 Heat exchanger assembly
1012016010881904/21/16 Fuel/oil manifold
1022016010882104/21/16 Radially fastened fixed-variable vane system
1032016010885404/21/16 Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
1042016010902504/21/16 Seal ring
1052016010912804/21/16 Gas turbine engine wave geometry combustor liner panel
1062016010241704/14/16 Hierarchically structured duplex anodized aluminum alloy
1072016010255704/14/16 Vibration dampers for turbine blades
1082016010256104/14/16 Gas turbine engine turbine blade tip cooling
1092016010256304/14/16 Gas turbine engine component having trip strips
1102016010257004/14/16 Non-contacting dynamic seal
1112016010257404/14/16 Gas turbine engine convergent/divergent nozzle with unitary synchronization ring for roller track nozzle
1122016010260904/14/16 Pulse detonation combustor
1132016010263404/14/16 Reverse flow single spool core gas turbine engine
1142016010286104/14/16 Gas turbine engine combustor liner panel
1152016009629104/07/16 Metallographic sample preparation method and metallographic sample mold
1162016009728104/07/16 Gas turbine engine airfoil mistuning
1172016009729104/07/16 Stator assembly for a gas turbine engine
1182016009729404/07/16 Brush seal plate
1192016009730404/07/16 Gas turbine engine with low stage count low pressure turbine
1202016009732704/07/16 Synchronized air modulating system
1212016008972203/31/16 Method of manufacturing gas turbine engine component from a molybdenum-rich alloy
1222016009019003/31/16 Aircraft hail screen
1232016009084103/31/16 Gas turbine engine blade slot heat shield
1242016009084403/31/16 Gas turbine engine airfoil cooling passage configuration
1252016009084603/31/16 Gas turbine engine airfoil trailing edge suction side cooling
1262016009084903/31/16 Fan blade with static dissipative coating
1272016009085103/31/16 Airfoil assembly with spacer and tie-spar
1282016009085303/31/16 Seal assembly for sealing an axial gap between components
1292016009087103/31/16 Low loss bearing drain
1302016009090903/31/16 Geared gas turbine engine with reduced fan noise
1312016009091403/31/16 Diffuser case strut for a turbine engine
1322016009091503/31/16 Inlet door control for startup of gas turbine engine
1332016009138103/31/16 Method for determining a fault within a flow divider
1342016008310103/24/16 Aircraft engine case shock mount
1352016008330303/24/16 Additive manufacturing of ceramic turbine components by transient liquid phase bonding using metal or ceramic binders
1362016008330403/24/16 Additive manufacturing of ceramic turbine components by partial transient liquid phase bonding using metal binders
1372016008362103/24/16 Composite article having protective coating
1382016008408903/24/16 Internally damped airfoiled component and method
1392016008409003/24/16 Method and assembly for reducing secondary heat in a gas turbine engine
1402016008409403/24/16 Method and fixture for airfoil array assembly
1412016008409603/24/16 Clamped vane arc segment having load-transmitting features
1422016008409903/24/16 Thermally protected seal assembly
1432016008410003/24/16 System and seal retention and protection
1442016008410403/24/16 Fan drive gear system
1452016008410503/24/16 Fan drive gear system
1462016008410603/24/16 Anti-icing core inlet stator assembly for a gas turbine engine
1472016008411303/24/16 Nacelle mounted latching system
1482016008416403/24/16 Plate for metering flow
1492016008416703/24/16 Self-modulated cooling on turbine components
1502016008416803/24/16 Chemistry based methods of manufacture for maxmet composite powders
1512016008450203/24/16 Turbine engine diffuser assembly with airflow mixer
1522016007493303/17/16 Die casting of component having integral seal
1532016007511903/17/16 Precipitation hardened partial transient liquid phase bond
1542016007543803/17/16 Systems for generating auxiliary electrical power for jet aircraft propulsion systems
1552016007613603/17/16 Coated articles and manufacture methods
1562016007637803/17/16 Turbomachine rotors with thermal regulation
1572016007637903/17/16 Turbomachine rotor thermal regulation systems
1582016007638003/17/16 Incidence-tolerant, high-turning fan exit stator
1592016007638103/17/16 Secondary flowpath system for a gas turbine engine
1602016007638203/17/16 Component core with shaped edges
1612016007638303/17/16 Film cooled article
1622016007638403/17/16 Gas turbine engine component having engineered vascular structure
1632016007638603/17/16 Tangential blade root neck conic
1642016007638803/17/16 Fan platform
1652016007639103/17/16 Hinged seal using wire mesh
1662016007639203/17/16 Endwall contouring for airfoil rows with varying airfoil geometries
1672016007639303/17/16 Fan drive gear system with improved misalignment capability
1682016007639503/17/16 Method of manufacturing ice panel segments
1692016007644503/17/16 Geared turbofan engine with high compressor exit temperature
1702016007645103/17/16 Film hole with in-wall accumulator
1712016007645903/17/16 Geared fan with inner counter rotating compressor
1722016007646003/17/16 Nacelle and compressor inlet arrangements
1732016007679903/17/16 Falling film evaporator for mixed refrigerants
1742016006777903/10/16 Local contamination detection in additive manufacturing
1752016006782003/10/16 Selective laser melting system
1762016006828203/10/16 Method for elimination of powder segregation during can filling
1772016006844603/10/16 Systems and methods for ceramic matrix composites
1782016006896803/10/16 Strip process and composition for mcraiy coatings and a using the same
1792016006918703/10/16 Gas turbine engine airfoil
1802016006918803/10/16 Gas turbine engine airfoil structure
1812016006918903/10/16 Splayed tip features for gas turbine engine airfoil
1822016006919003/10/16 Beveled coverplate
1832016006919103/10/16 Gas turbine engine airfoil cooling passage turbulator pedestal
1842016006919303/10/16 Coolant flow redirection component
1852016006919703/10/16 Turbine vane with variable trailing edge inner radius
1862016006919803/10/16 Casting optimized to improve suction side cooling shaped hole performance
1872016006919903/10/16 Stator vane platform with flanges
1882016006920003/10/16 Turbine vane with platform pad
1892016006920103/10/16 Attachment faces for clamped turbine stator of a gas turbine engine
1902016006920303/10/16 Integrally bladed rotor
1912016006920403/10/16 Geared annular airflow actuation system for variable cycle gas turbine engines
1922016006921003/10/16 Windback heat shield
1932016006921103/10/16 Bearing compartment with integrated fluid lines
1942016006921203/10/16 Oil transfer bearing
1952016006925903/10/16 Turbine minidisk bumper for gas turbine engine
1962016006926603/10/16 Heat exchanger arrangement for turbine engine
1972016006926703/10/16 Reduced windage fastener assembly for a gas turbine engine
1982016006926903/10/16 Vibration damping hydrostatic seal of gas turbine engine
1992016006927003/10/16 Turbofan engine front section
2002016006927703/10/16 Turboshaft engine control
2012016006929703/10/16 Geared turbine engine with o-duct and thrust reverser
2022016006929803/10/16 Variable orifice jet for a turbine engine
2032016006956703/10/16 Single-walled combustor for a gas turbine engine and manufacture
2042016006956903/10/16 Film cooling circuit for a combustor liner
2052016005930203/03/16 Regenerating an additively manufactured component to cure defects and alter microstructure
2062016005936403/03/16 Wide gap braze
2072016005949703/03/16 In-situ pressure enhanced processing of composite articles
2082016006074803/03/16 Deposition apparatus and methods
2092016006104403/03/16 Regenerating an additively manufactured component
2102016006104503/03/16 Decoupled gas turbine engine
2112016006104603/03/16 Turbine vane with non-uniform wall thickness
2122016006104703/03/16 Gas turbine engine seal
2132016006104803/03/16 Rotor blade with l-shaped feather seal
2142016006105103/03/16 Geared turbofan with three turbines with high speed fan drive turbine
2152016006105203/03/16 Gas turbine engine with high speed low pressure turbine section
2162016006105703/03/16 Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
2172016006111203/03/16 Shielded pass through passage in a gas turbine engine structure
2182016006111303/03/16 Actively cooled blade outer air seal
2192016006120203/03/16 Gear pump on shaft
2202016006133003/03/16 Dual-ended brush seal assembly and manufacture
2212016006158003/03/16 Flexible reference system
2222016005205702/25/16 Gas turbine component manufacturing
2232016005208702/25/16 Method of eliminating sub-surface porosity
2242016005338002/25/16 High temperature and high pressure portable gas heater
2252016005361702/25/16 Rotors with modulus mistuned airfoils
2262016005361902/25/16 Cmc blade with integral 3d woven platform
2272016005362102/25/16 Gas turbine engine airfoil platform edge geometry
2282016005362202/25/16 Stator vane arrangement for a turbine engine
2292016005362302/25/16 Contactless seals for gas turbine engines
2302016005362402/25/16 Radial position control of case supported structure with axial reaction member
2312016005362502/25/16 Airfoils having porous abradable elements
2322016005362602/25/16 Gas turbine engine rapid response clearance control system with air seal segment interface
2332016005362702/25/16 Flexible feather seal for blade outer air seal gas turbine engine rapid response clearance control system
2342016005362802/25/16 Rapid response clearance control system for gas turbine engine
2352016005362902/25/16 Ring seal for blade outer air seal gas turbine engine rapid response clearance control system
2362016005363102/25/16 Gas turbine engine with mount for low pressure turbine section
2372016005363402/25/16 Gas turbine engine with high speed low pressure turbine section and bearing support features
2382016005363502/25/16 Flexible support structure for a geared architecture gas turbine engine
2392016005363602/25/16 Injection molded composite fan platform
2402016005367902/25/16 Gas turbine engine with high speed low pressure turbine section and bearing support features
2412016005368802/25/16 Gas turbine rotors
2422016005369202/25/16 Annular airflow actuation system for variable cycle gas turbine engines
2432016005400102/25/16 Combustor panel t-junction cooling
2442016005420502/25/16 Dynamic obtaining a sample of materials
2452016005648702/25/16 Method of maintaining health of a flow battery
2462016004726602/18/16 Movable air seal for gas turbine engine
2472016004724702/18/16 Fan blade grounding tab
2482016004725002/18/16 Showerhead hole scheme apparatus and system
2492016004725102/18/16 Cooling hole having unique meter portion



ARCHIVE: New 2016 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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