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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
12016011436104/28/16  new patent  Wash device
22016011453204/28/16  new patent  Continuous fiber-reinforced component fabrication
32016011489404/28/16  new patent  Compressor bleed air supply for an aircraft environmental control system
42016011527804/28/16  new patent  High performance polymer and process therefor
52016011558404/28/16  new patent  Nanoparticle formation mitigation in a deposition process
62016011580004/28/16  new patent  Stator assembly with pad interface for a gas turbine engine
72016011580104/28/16  new patent  Multi-piece turbine airfoil
82016011580304/28/16  new patent  Platform cooling circuit for a gas turbine engine component
92016011580404/28/16  new patent  Seal support structure
102016011580604/28/16  new patent  Segmented seal
112016011580704/28/16  new patent  Multi-piece seal
122016011580804/28/16  new patent  Hinged seal
132016011580904/28/16  new patent  Bifurcated sliding seal
142016011581004/28/16  new patent  Bifurcated sliding seal
152016011581104/28/16  new patent  Conformal seal
162016011581204/28/16  new patent  Sliding seal
172016011581304/28/16  new patent  Dual compliant seal
182016011581404/28/16  new patent  Sliding seal
192016011582104/28/16  new patent  Bladed rotor disk including anti-vibratory feature
202016011582504/28/16  new patent  Seal support structure for a circumferential seal of a gas turbine engine
212016011586504/28/16  new patent  Gas turbine engine with high speed low pressure turbine section and bearing support features
222016011586604/28/16  new patent  Offset cores for gas turbine engines
232016011587104/28/16  new patent  Cooling configuration for a component
242016011616604/28/16  new patent  Gas turbine engine combustor liner panel
252016011616904/28/16  new patent  Mixer retention
262016010727904/21/16 Airfoil material removal
272016010733104/21/16 Functional inorganics and ceramic additive manufacturing
282016010851304/21/16 Coating system for internally-cooled component and process therefor
292016010873504/21/16 Tandem rotor blades
302016010873804/21/16 Gas turbine component with platform cooling
312016010873904/21/16 Film hole with protruding flow accumulator
322016010874504/21/16 Gas turbine hub
332016010874604/21/16 Vane assembly including two- and three-dimensional arrangements of continuous fibers
342016010874804/21/16 Gas turbine engine with dove-tailed tobi vane
352016010875004/21/16 Circumferential seal with seal dampening elements
362016010875504/21/16 Gas turbine engine component
372016010875804/21/16 Corrugated mid-turbine frame thermal radiation shield
382016010876204/21/16 Falling film evaporator for power generation systems
392016010880704/21/16 Turbofan engine front section
402016010880804/21/16 Turbofan engine bearing and gearbox arrangement
412016010881204/21/16 Conduit for guiding low pressure compressor inner diameter shroud motion
422016010881304/21/16 Additive manufactured ducted heat exchanger
432016010881404/21/16 Additive manufactured ducted heat exchanger system with additively manufactured fairing
442016010881504/21/16 Heat exchanger assembly
452016010881904/21/16 Fuel/oil manifold
462016010882104/21/16 Radially fastened fixed-variable vane system
472016010885404/21/16 Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
482016010902504/21/16 Seal ring
492016010912804/21/16 Gas turbine engine wave geometry combustor liner panel
502016010241704/14/16 Hierarchically structured duplex anodized aluminum alloy
512016010255704/14/16 Vibration dampers for turbine blades
522016010256104/14/16 Gas turbine engine turbine blade tip cooling
532016010256304/14/16 Gas turbine engine component having trip strips
542016010257004/14/16 Non-contacting dynamic seal
552016010257404/14/16 Gas turbine engine convergent/divergent nozzle with unitary synchronization ring for roller track nozzle
562016010260904/14/16 Pulse detonation combustor
572016010263404/14/16 Reverse flow single spool core gas turbine engine
582016010286104/14/16 Gas turbine engine combustor liner panel
592016009629104/07/16 Metallographic sample preparation method and metallographic sample mold
602016009728104/07/16 Gas turbine engine airfoil mistuning
612016009729104/07/16 Stator assembly for a gas turbine engine
622016009729404/07/16 Brush seal plate
632016009730404/07/16 Gas turbine engine with low stage count low pressure turbine
642016009732704/07/16 Synchronized air modulating system
652016008972203/31/16 Method of manufacturing gas turbine engine component from a molybdenum-rich alloy
662016009019003/31/16 Aircraft hail screen
672016009084103/31/16 Gas turbine engine blade slot heat shield
682016009084403/31/16 Gas turbine engine airfoil cooling passage configuration
692016009084603/31/16 Gas turbine engine airfoil trailing edge suction side cooling
702016009084903/31/16 Fan blade with static dissipative coating
712016009085103/31/16 Airfoil assembly with spacer and tie-spar
722016009085303/31/16 Seal assembly for sealing an axial gap between components
732016009087103/31/16 Low loss bearing drain
742016009090903/31/16 Geared gas turbine engine with reduced fan noise
752016009091403/31/16 Diffuser case strut for a turbine engine
762016009091503/31/16 Inlet door control for startup of gas turbine engine
772016009138103/31/16 Method for determining a fault within a flow divider
782016008310103/24/16 Aircraft engine case shock mount
792016008330303/24/16 Additive manufacturing of ceramic turbine components by transient liquid phase bonding using metal or ceramic binders
802016008330403/24/16 Additive manufacturing of ceramic turbine components by partial transient liquid phase bonding using metal binders
812016008362103/24/16 Composite article having protective coating
822016008408903/24/16 Internally damped airfoiled component and method
832016008409003/24/16 Method and assembly for reducing secondary heat in a gas turbine engine
842016008409403/24/16 Method and fixture for airfoil array assembly
852016008409603/24/16 Clamped vane arc segment having load-transmitting features
862016008409903/24/16 Thermally protected seal assembly
872016008410003/24/16 System and seal retention and protection
882016008410403/24/16 Fan drive gear system
892016008410503/24/16 Fan drive gear system
902016008410603/24/16 Anti-icing core inlet stator assembly for a gas turbine engine
912016008411303/24/16 Nacelle mounted latching system
922016008416403/24/16 Plate for metering flow
932016008416703/24/16 Self-modulated cooling on turbine components
942016008416803/24/16 Chemistry based methods of manufacture for maxmet composite powders
952016008450203/24/16 Turbine engine diffuser assembly with airflow mixer
962016007493303/17/16 Die casting of component having integral seal
972016007511903/17/16 Precipitation hardened partial transient liquid phase bond
982016007543803/17/16 Systems for generating auxiliary electrical power for jet aircraft propulsion systems
992016007613603/17/16 Coated articles and manufacture methods
1002016007637803/17/16 Turbomachine rotors with thermal regulation
1012016007637903/17/16 Turbomachine rotor thermal regulation systems
1022016007638003/17/16 Incidence-tolerant, high-turning fan exit stator
1032016007638103/17/16 Secondary flowpath system for a gas turbine engine
1042016007638203/17/16 Component core with shaped edges
1052016007638303/17/16 Film cooled article
1062016007638403/17/16 Gas turbine engine component having engineered vascular structure
1072016007638603/17/16 Tangential blade root neck conic
1082016007638803/17/16 Fan platform
1092016007639103/17/16 Hinged seal using wire mesh
1102016007639203/17/16 Endwall contouring for airfoil rows with varying airfoil geometries
1112016007639303/17/16 Fan drive gear system with improved misalignment capability
1122016007639503/17/16 Method of manufacturing ice panel segments
1132016007644503/17/16 Geared turbofan engine with high compressor exit temperature
1142016007645103/17/16 Film hole with in-wall accumulator
1152016007645903/17/16 Geared fan with inner counter rotating compressor
1162016007646003/17/16 Nacelle and compressor inlet arrangements
1172016007679903/17/16 Falling film evaporator for mixed refrigerants
1182016006777903/10/16 Local contamination detection in additive manufacturing
1192016006782003/10/16 Selective laser melting system
1202016006828203/10/16 Method for elimination of powder segregation during can filling
1212016006844603/10/16 Systems and methods for ceramic matrix composites
1222016006896803/10/16 Strip process and composition for mcraiy coatings and a using the same
1232016006918703/10/16 Gas turbine engine airfoil
1242016006918803/10/16 Gas turbine engine airfoil structure
1252016006918903/10/16 Splayed tip features for gas turbine engine airfoil
1262016006919003/10/16 Beveled coverplate
1272016006919103/10/16 Gas turbine engine airfoil cooling passage turbulator pedestal
1282016006919303/10/16 Coolant flow redirection component
1292016006919703/10/16 Turbine vane with variable trailing edge inner radius
1302016006919803/10/16 Casting optimized to improve suction side cooling shaped hole performance
1312016006919903/10/16 Stator vane platform with flanges
1322016006920003/10/16 Turbine vane with platform pad
1332016006920103/10/16 Attachment faces for clamped turbine stator of a gas turbine engine
1342016006920303/10/16 Integrally bladed rotor
1352016006920403/10/16 Geared annular airflow actuation system for variable cycle gas turbine engines
1362016006921003/10/16 Windback heat shield
1372016006921103/10/16 Bearing compartment with integrated fluid lines
1382016006921203/10/16 Oil transfer bearing
1392016006925903/10/16 Turbine minidisk bumper for gas turbine engine
1402016006926603/10/16 Heat exchanger arrangement for turbine engine
1412016006926703/10/16 Reduced windage fastener assembly for a gas turbine engine
1422016006926903/10/16 Vibration damping hydrostatic seal of gas turbine engine
1432016006927003/10/16 Turbofan engine front section
1442016006927703/10/16 Turboshaft engine control
1452016006929703/10/16 Geared turbine engine with o-duct and thrust reverser
1462016006929803/10/16 Variable orifice jet for a turbine engine
1472016006956703/10/16 Single-walled combustor for a gas turbine engine and manufacture
1482016006956903/10/16 Film cooling circuit for a combustor liner
1492016005930203/03/16 Regenerating an additively manufactured component to cure defects and alter microstructure
1502016005936403/03/16 Wide gap braze
1512016005949703/03/16 In-situ pressure enhanced processing of composite articles
1522016006074803/03/16 Deposition apparatus and methods
1532016006104403/03/16 Regenerating an additively manufactured component
1542016006104503/03/16 Decoupled gas turbine engine
1552016006104603/03/16 Turbine vane with non-uniform wall thickness
1562016006104703/03/16 Gas turbine engine seal
1572016006104803/03/16 Rotor blade with l-shaped feather seal
1582016006105103/03/16 Geared turbofan with three turbines with high speed fan drive turbine
1592016006105203/03/16 Gas turbine engine with high speed low pressure turbine section
1602016006105703/03/16 Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
1612016006111203/03/16 Shielded pass through passage in a gas turbine engine structure
1622016006111303/03/16 Actively cooled blade outer air seal
1632016006120203/03/16 Gear pump on shaft
1642016006133003/03/16 Dual-ended brush seal assembly and manufacture
1652016006158003/03/16 Flexible reference system
1662016005205702/25/16 Gas turbine component manufacturing
1672016005208702/25/16 Method of eliminating sub-surface porosity
1682016005338002/25/16 High temperature and high pressure portable gas heater
1692016005361702/25/16 Rotors with modulus mistuned airfoils
1702016005361902/25/16 Cmc blade with integral 3d woven platform
1712016005362102/25/16 Gas turbine engine airfoil platform edge geometry
1722016005362202/25/16 Stator vane arrangement for a turbine engine
1732016005362302/25/16 Contactless seals for gas turbine engines
1742016005362402/25/16 Radial position control of case supported structure with axial reaction member
1752016005362502/25/16 Airfoils having porous abradable elements
1762016005362602/25/16 Gas turbine engine rapid response clearance control system with air seal segment interface
1772016005362702/25/16 Flexible feather seal for blade outer air seal gas turbine engine rapid response clearance control system
1782016005362802/25/16 Rapid response clearance control system for gas turbine engine
1792016005362902/25/16 Ring seal for blade outer air seal gas turbine engine rapid response clearance control system
1802016005363102/25/16 Gas turbine engine with mount for low pressure turbine section
1812016005363402/25/16 Gas turbine engine with high speed low pressure turbine section and bearing support features
1822016005363502/25/16 Flexible support structure for a geared architecture gas turbine engine
1832016005363602/25/16 Injection molded composite fan platform
1842016005367902/25/16 Gas turbine engine with high speed low pressure turbine section and bearing support features
1852016005368802/25/16 Gas turbine rotors
1862016005369202/25/16 Annular airflow actuation system for variable cycle gas turbine engines
1872016005400102/25/16 Combustor panel t-junction cooling
1882016005420502/25/16 Dynamic obtaining a sample of materials
1892016005648702/25/16 Method of maintaining health of a flow battery
1902016004726602/18/16 Movable air seal for gas turbine engine
1912016004724702/18/16 Fan blade grounding tab
1922016004725002/18/16 Showerhead hole scheme apparatus and system
1932016004725102/18/16 Cooling hole having unique meter portion
1942016004725502/18/16 Gas turbine engine blade containment system
1952016004725802/18/16 Inner stage turbine seal for gas turbine engine
1962016004725902/18/16 Gas turbine engine stress isolation scallop
1972016004726002/18/16 Turbomachine blade assemblies
1982016004726402/18/16 Blade outer air seal having partial coating
1992016004726802/18/16 Gas turbine engine with low stage count low pressure turbine
2002016004726902/18/16 Smart active clearance control between a rotor blade and a shroud
2012016004727002/18/16 Split ring spring dampers for gas turbine rotor assemblies
2022016004727102/18/16 Ducting platform cover plate
2032016004727302/18/16 Turbofan engine main bearing arrangement
2042016004727502/18/16 Composite attachment structure with 3d weave
2052016004728102/18/16 Emergency oil system
2062016004730402/18/16 Ultra high overall pressure ratio gas turbine engine
2072016004730602/18/16 Gas turbine engine with high speed low pressure turbine section and bearing support features
2082016004731102/18/16 Gas turbine engine cooling fluid metering system
2092016004742202/18/16 Bearing assembly with lubricant/coolant passages
2102016003899902/11/16 Isothermal shot tube assembly
2112016003972002/11/16 Method of treating a preceramic material
2122016004027202/11/16 Die-castable nickel based superalloy composition
2132016004028102/11/16 Spallation-resistant thermal barrier coating
2142016004028402/11/16 Pressure modulated coating
2152016004031202/11/16 Sacrificial coating and procedure for electroplating aluminum on aluminum alloys
2162016004053402/11/16 Disk lug impingement for gas turbine engine airfoil
2172016004053802/11/16 Aluminum fan blade tip with thermal barrier
2182016004053902/11/16 Engine component having support with intermediate layer
2192016004054102/11/16 Lightweight blade for gas turbine engine
2202016004054202/11/16 Cover plate for a rotor assembly of a gas turbine engine
2212016004054702/11/16 Blade outer air seal with secondary air sealing
2222016004054802/11/16 Ceramic coating system and method
2232016004055002/11/16 Variable vane control system
2242016004055102/11/16 Geometrically segmented coating on contoured surfaces
2252016004055402/11/16 Rear bearing sleeve for gas turbine auxiliary power unit
2262016004055502/11/16 Compressor case snap assembly
2272016004059402/11/16 Counter-rotating low pressure turbine without turbine exhaust case
2282016004059802/11/16 Low noise compressor for geared gas turbine engine
2292016004060002/11/16 Multi-axial brush seal
2302016004060402/11/16 Pressure sensor noise filter prior to surge detection for a gas turbine engine
2312016004062602/11/16 Twin target thrust reverser module
2322016004062702/11/16 Aerodynamic track fairing for a gas turbine engine fan nacelle
2332016004087902/11/16 Combustor panel with increased durability
2342016004088102/11/16 Gas turbine engine combustor
2352016004088602/11/16 Joint for sealing a gap between casing segments of an industrial gas turbine engine combustor
2362016003100402/04/16 Shot tube for die-cast machine
2372016003100602/04/16 Arcuate directionally solidified components and manufacture methods
2382016003101002/04/16 Build platforms for additive manufacturing
2392016003101202/04/16 Powder metallurgy alloy forging
2402016003118202/04/16 Composite flange with three-dimensional weave architecture
2412016003241602/04/16 Gas turbine engine airfoil impingement cooling
2422016003272602/04/16 Gas turbine engine axial compressor rear hub
2432016003272702/04/16 Rotor blade with a conic spline fillet at an intersection between a platform and a neck
2442016003272802/04/16 Gas turbine engine airfoil
2452016003272902/04/16 Composite fan blade
2462016003273002/04/16 Obtuse angle chevron trip strip
2472016003273102/04/16 Thermal barrier coating inside cooling channels
2482016003273202/04/16 Gas turbine engine airfoil geometries and cores for manufacturing process
2492016003273502/04/16 Transient liquid phase bonded tip shroud



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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