FreshPatents.com Logo


new TOP 200 Companies filing patents this week

new Companies with the Most Patent Filings (2010+)


Similar
Filing Names

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

Popular
Companies


Web
Adobe patents
Amazon patents
Apple patents
Ebay patents
Facebook patents
Google patents
IBM patents
Linkedin patents
Microsoft patents
Oracle patents
Red Hat patents
Yahoo patents

Food/Health
Adidas
Nike patents
Pfizer patents
Monsanto patents
Medtronic patents
Kraft patents

Transportation
Boeing patents
Tesla Motors patents

Telecom
Qualcomm patents
Motorola patents
Nokia patents
RIMM patents

Industrial/Electronics
AMD
Applied Materials
Seagate patents
General Electric
Caterpillar patents
Samsung
Wal-mart patents

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


Systems and methods for dressing grinding wheels

United Technologies

Systems and methods for dressing grinding wheels

Ultra high overall pessure ratio gas turbine engine

United Technologies

Ultra high overall pessure ratio gas turbine engine

Gas turbine engine forward bearing compartment architecture

United Technologies

Gas turbine engine forward bearing compartment architecture

Search recent Press Releases: United Technologies Corporation-related press releases
Count Application # Date United Technologies Corporation patents (updated weekly) - BOOKMARK this page
12015017465306/25/15 new patent  System and methods for removing core elements of cast components
22015017472906/25/15 new patent  Systems and methods for modifying and adding features on grinding wheel surfaces
32015017473106/25/15 new patent  Systems and methods for dressing grinding wheels
42015017648406/25/15 new patent  Geared turbofan with a gearbox aft of a fan drive turbine
52015017649306/25/15 new patent  Gas turbine engine forward bearing compartment architecture
62015017649706/25/15 new patent  Geared turbofan with a gearbox upstream of a fan drive turbine
72015017650206/25/15 new patent  Method of controlling a gas turbine engine using real-time component temperature data
82015017653006/25/15 new patent  Ultra high overall pessure ratio gas turbine engine
92015016550006/18/15Deep rolling tool for blade fatigue life enhancement
102015016551306/18/15Machine for deep rolling tool positioning
112015016551406/18/15Deep rolling tool with force adjustment
122015016551506/18/15Deep rolling tool for processing blade root
132015016557006/18/15Crimping tool
142015016566606/18/15Systems and methods for manufacturing fiber-reinforced polymeric components
152015016712506/18/15Nickel alloy for repairs
162015016714906/18/15Movable evaporation source
172015016754906/18/15Exhaust stream mixer
182015016767606/18/15Gas turbine engine for long range aircraft
192015017256506/18/15Composite image processing for lwir images using geometric features
202015017256606/18/15Natural resolution processing for lwir images
212015015807606/11/15Method of fabricating an investment casting mold and slurry therefor
222015015859706/11/15Emergency power generation via limited variable pitch fan blade
232015015950106/11/15Rigid and rotatable vanes molded within variably shaped flexible airfoils
242015015950806/11/15Core drainage systems for fan case assemblies
252015016009706/11/15Long wave infrared sensing for turbomachine
262015015254406/04/15Coating methods and apparatus
272015015273906/04/15Turbine blade rail damper
282015015274606/04/15Slotted distribution sleeve for a seal plate
292015015278706/04/15Low noise compressor rotor for geared turbofan engine
302015015278906/04/15Multi-bypass stream gas turbine engine with enlarged bypass flow area
312015015372606/04/15Method for inspecting a manufacturing device
322015015678906/04/15Communication of avionic data
332015014379405/28/15Geared turbofan engine gearbox arrangement
342015014752805/28/15Component blending tool
352015013567805/21/15Gas turbine engine with noise attenuating variable area fan nozzle
362015013834205/21/15System and method to determine visible damage
372015014123505/21/15Carbon fiber-reinforced article and method therefor
382015013210605/14/15Gas turbine engine with low fan pressure ratio
392015013211005/14/15High durability turbine exhaust case
402015013213405/14/15Injection molded composite fan platform
412015013214205/14/15Rotor blade with bonded cover
422015012168205/07/15Extraction tool assembly
432015012183805/07/15Conjoined reverse core flow engine arrangement
442015012183905/07/15Tandem thrust reverser with multi-bar linkage
452015012184105/07/15Flow control device for a three stream turbofan engine
462015012184405/07/15Geared turbofan arrangement with core split power ratio
472015012188205/07/15Mixer assembly for a gas turbine engine
482015012188405/07/15Stress relieved rectilinear duct
492015012189305/07/15Adaptive fan reverse core geared turbofan engine with separate cold turbine
502015012189405/07/15Bifurcation fire purge system
512015012189505/07/15Full ring sliding nacelle with thrust reverser
522015012189605/07/15Reverse core flow engine mounting arrangement
532015012203105/07/15Transducer position guide
542015012233905/07/15Variable area bypass nozzle
552015012290505/07/15Passive tangential ejector for an exhaust nozzle of a gas turbine engine
562015012291205/07/15Tandem thrust reverser with multi-point actuation
572015012295205/07/15Gas turbine engine inlet wall design
582015012299805/07/15Method of inspection for cooling holes in turbine airfoil
592015012525905/07/15Gas turbine engine variable pitch fan blade
602015012527005/07/15Atr guide pins for sliding nacelle
612015012528405/07/15Atr full ring sliding nacelle
622015012528505/07/15Integrated nozzle and plug
632015012528605/07/15Atr axial v-groove
642015012529105/07/15Bracket for mounting a stator guide vane arrangement to a strut in a turbine engine
652015012529305/07/15Turbofan engine main bearing arrangement
662015012529505/07/15Wind turbine load mitigation
672015012530405/07/15Mass offset for damping performance
682015012530505/07/15Low profile fan platform attachment
692015012568105/07/15High temperature imaging media for digital image correlation
702015012609605/07/15System and contoured peel grinding
712015011394104/30/15Translating outer cowl flow modulation device and method
722015011394204/30/15Phosphor thermometer with two waveguides
732015011394304/30/15Geared turbofan engine with power density range
742015011394504/30/15Pivoting blocker door
752015011399604/30/15Cascaded multi-variable control system for a turboshaft engine
762015011400204/30/15Geared turbofan engine with a high ratio of thrust to turbine volume
772015011407404/30/15Systems and methods for controlled peening
782015011749304/30/15Phosphor thermometry fiber sensor
792015011780404/30/15Gas turbine engine bushing
802015011806304/30/15Turbine airfoil tip shelf and squealer pocket cooling
812015011806404/30/15Gas turbine engine airfoil trailing edge passage and core for making same
822015010722304/23/15High durability turbine exhaust case
832015011063604/23/15Wear pad to prevent cracking of fan blade
842015011102204/23/15Coating for metal cellular structure and method therefor
852015010193504/16/15Apparatus and ionic liquid electroplating
862015010431504/16/15Fan blade root integrated sealing solution
872015009630304/09/15Gas turbine engine with high speed low pressure turbine section
882015009671304/09/15Rapid tooling insert manufacture
892015009683904/09/15Low loss oil accumulator assembly
902015009883004/09/15Assembly fixture for a stator vane assembly
912015009883504/09/15Castings, casting cores, and methods
922015008991804/02/15Gas turbine lubrication systems
932015008995804/02/15Gas turbine engine with high speed low pressure turbine section
942015008995904/02/15Gas turbine engine shaft bearing configuration
952015008294503/26/15Process for producing refractory metal alloy powders
962015008391903/26/15Background radiation measurement system
972015008626203/26/15Welded assemblies and methods of making welded assemblies
982015008628303/26/15Ball-end milling cutter tool
992015007574503/19/15Casting molds, manufacture and use methods
1002015007891503/19/15Piloted nut
1012015006820903/12/15Method for determining circumferential sensor positioning
1022015006821003/12/15Tube fed tangential on-board injector for gas turbine engine
1032015006821403/12/15Low thermal mass joint
1042015006966803/12/15Multi-dimensional component build system and process
1052015007170403/12/15Exhaust duct liner rod hanger
1062015006000203/05/15Die casting system and cell
1072015006528503/05/15Geared architecture gas turbine engine with oil scavenge
1082015005287302/26/15Torque connector lubrication scuppers
1092015005290702/26/15Thermal management system for gas turbine engine
1102015005378902/26/15Linkage to control and restrain flap movement
1112015005012702/19/15Air with integral spring for a gas turbine engine exhaust drive
1122015005104002/19/15Oil baffle for gas turbine fan drive gear system
1132015004202302/12/15Hybrid part made from monolithic ceramic skin and cmc core
1142015004402802/12/15Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
1152015004405202/12/15Geared turbofan with fan blades designed to achieve laminar flow
1162015004520002/12/15Ceramic component
1172015003760202/05/15System and high temperature die casting tooling
1182015002710101/29/15Geared gas turbine engine architecture for enhanced efficiency
1192015002713001/29/15Split ring valve
1202015002765701/29/15Method and casting core for forming a landing for welding a baffle inserted in an airfoil
1212015003044001/29/15Fireshield fastener hood
1222015003044301/29/15Split damped outer shroud for gas turbine engine stator arrays
1232015002378001/22/15Liner attaching scheme
1242015002429601/22/15Method and system for operating a flow battery system based on energy costs
1252015001330101/15/15Turbine engine including balanced low pressure stage count
1262015001334401/15/15Tube
1272015001348001/15/15Plated instrumentation probes and sensors
1282015001393401/15/15Article with grouped grain patterns
1292015001695401/15/15Blade outer air seal assembly and support
1302015001696501/15/15Link arm drag reducing device
1312015000826801/08/15Pivot thrust reverser with multi-point actuation
1322015000008901/01/15Clamp connector
1332015000030301/01/15Wireless power for gas turbine engine instrumentation
1342015000030401/01/15Removable nosecone for a gas turbine engine
1352015000395601/01/15Variable vane scheduling
1362015000396801/01/15Gas turbine engine with attached nosecone
1372015000399501/01/15Aircraft engine component with locally tailored materials
1382015000399701/01/15Method of forming hybrid metal ceramic components
1392014037354912/25/14Cooling hole with curved metering section
1402014037355412/25/14Air turbine starter pressure monitor system
1412014037361012/25/14Engine inspection apparatus and system
1422014037505612/25/14Method of operating a power generation system
1432014036654812/18/14Turbine engine gearbox
1442014036655412/18/14Cross reference to related applications
1452014036655612/18/14Gas turbine engine vane-to-transition duct seal
1462014036661312/18/14Probe retention-sealing feature
1472014036978312/18/14Self-retaining shear pin for blind mount location
1482014036980412/18/14Variable bleed slot in centrifugal impeller
1492014036981812/18/14Planetary gear system arrangement with auxiliary oil system
1502014036015212/11/14Oil tank mount with yoke
1512014036015312/11/14Gas turbine engine thermal management system
1522014036330512/11/14Hybrid turbine blade for improved engine performance or architecture
1532014035656012/04/14Castings and manufacture methods
1542014035839812/04/14Use of ss data trends in fault resolution process
1552014035850012/04/14Probalistic high cycle fatigue (hcf) design optimization process
1562014034857711/27/14Tie bolt employing differential thread
1572014034863011/27/14Noise reducing vane
1582014034864011/27/14Thrust efficient turbofan engine
1592014033833611/20/14Gas turbine engine combustor with integrated combustor vane
1602014033835111/20/14Gas turbine engine combustor with tailored temperature profile
1612014033835711/20/14Cavity swirl fuel injector for an augmentor section of a gas turbine engine
1622014033836011/20/14Bleed port ribs for turbomachine case
1632014033219111/13/14Extreme environment heat exchanger
1642014033491611/13/14Borescope inspection port fitting
1652014032684211/06/14Oil tank mount with stiffeners
1662014031813310/30/14Thrust efficient turbofan engine
1672014031814310/30/14Multi-circuit buffer system for a gas turbine engine
1682014031814710/30/14Low noise compressor rotor for geared turbofan engine
1692014032196110/30/14Mate face cooling holes for gas turbine engine component
1702014032302210/30/14Airfoil edge form transfer grinding tool
1712014032436310/30/14System reliability analysis and management using physics-based models embedded in a baysian network
1722014031112110/23/14Pulse detonation engine having a scroll ejector attenuator
1732014031114910/23/14Gas turbine engine fan blade airfoil profile
1742014031261110/23/14Locking fluid fittings
1752014031454010/23/14Gas turbine engine synchronization ring
1762014031454110/23/14Turbomachine thrust balancing system
1772014031454210/23/14Gas turbine engine exhaust diffuser with movable struts
1782014031454610/23/14Turbine engine gearbox mount with multiple fuse joints
1792014031454710/23/14Attachment ceramic matrix composite materials
1802014031458110/23/14Method for forming single crystal parts using additive manufacturing and remelt
1812014029878810/09/14Gas turbine engine including pneumatic actuator system
1822014030142510/09/14Backstrike detection system for laser drilling thin materials
1832014030182910/09/14Engine bearing support
1842014029021110/02/14Turbine engine including balanced low pressure stage count
1852014029021310/02/14Duct blocker seal assembly for a gas turbine engine
1862014029026910/02/14Duct blocker seal assembly for a gas turbine engine
1872014029455810/02/14Turbomachine fluid delivery manifold and system
1882014028350009/25/14Thrust efficient turbofan engine
1892014028350109/25/14Elongated geared turbofan with high bypass ratio
1902014028674809/25/14Fan containment case with thermally conforming liner
1912014028675409/25/14Elongated geared turbofan with high bypass ratio
1922014028675509/25/14Ring gear mounting arrangement with oil scavenge scheme
1932014028678109/25/14Integral fan blade wear pad and platform seal
1942014025966109/18/14Variable area fan nozzle with wall thickness distribution
1952014026017609/18/14Lube tube expansion and torque retaining device
1962014026018209/18/14Free stream intake for reverse core engine
1972014026018309/18/14Variable cycle intake for reverse core engine
1982014026032109/18/14Gas turbine engine static structure joint with undercuts
1992014026179709/18/14Tube fitting having integrated tee fitting
2002014026810009/18/14Multiple laser time of arrival probe
2012014026981709/18/14Phosphor thermometry fiber sensor
2022014027062509/18/14High temperature uncooled optical probe
2032014027110109/18/14Modulated turbine vane cooling
2042014027111209/18/14Low noise turbine for geared gas turbine engine
2052014027112109/18/14Gas turbine engine architecture with intercooled twin centrifugal compressor
2062014027113509/18/14Turbofan engine bearing and gearbox arrangement
2072014027117809/18/14Fan blades for gas turbine engines with reduced stress concentration at leading edge
2082014027122109/18/14Usage of a witness mark to distinguish support structure from part
2092014027245609/18/14Spallation-resistant thermal barrier coating
2102014027374709/18/14Removing material from a workpiece with a water jet
2112014027375709/18/14Drag finishing system, method and fixture for gas turbine engine airfoils
2122014027453109/18/14Fan drive planetary gear system integrated carrier and torque frame
2132014025086209/11/14Reverse flow gas turbine engine airflow bypass
2142014025086309/11/14Rear mounted reverse core engine thrust reverser
2152014025089509/11/14Modulated ejector cooling
2162014025138109/11/14Pulse jet liquid gas cleaning system
2172014025179109/11/14Cathodic arc deposition stinger
2182014025180309/11/14Cathodic arc mask assembly lock system
2192014025216009/11/14Reverse flow gas turbine engine removable core
2202014025216109/11/14De-couple geared turbo-fan engine and aircraft
2212014025216209/11/14Uav launching from moving platform
2222014025216709/11/14Reverse core engine thrust reverser for under wing
2232014025218309/11/14Sensor hoop storage and transport apparatus
2242014025276409/11/14Two-piece self-locking mechanism for tube assemblies
2252014025463109/11/14Actively cooled gas turbine sensor probe housing
2262014025511209/11/14Broach tool rake face with a tailored surface topography
2272014025514409/11/14Flanged bushing for variable vane
2282014025515609/11/14Non-contacting seals for geared gas turbine engine bearing compartments
2292014025515809/11/14Coating process for gas turbine engine component with cooling holes
2302014025516209/11/14Adjustable floating oil channel for gas turbine engine gear drive
2312014025516709/11/14Consumable assembly tool for a gas turbine engine
2322014025516809/11/14Inter-module flow discourager
2332014025517209/11/14Low profile push-lock device
2342014025517409/11/14Manufacture of full ring strut vane pack
2352014025518209/11/14Push-lock pin connector
2362014025519609/11/14Double split blade lock ring
2372014025519809/11/14Turbine disk fabrication with in situ material property variation
2382014025520209/11/14Turbine engine nosecone with deformation region
2392014024574909/04/14Nacelle anti-ice valve utilized as compressor stability bleed valve during starting
2402014024575009/04/14Circumferentially retained fairing
2412014024575109/04/14Passages to facilitate a secondary flow between components
2422014024575309/04/14Gas turbine engine rotor blade
2432014024651409/04/14Turbomachine thrust reverser
2442014024811509/04/14Active clearance control system with zone controls
2452014024811609/04/14Acoustic treatment in an unducted area of a geared turbomachine
2462014024812609/04/14Inter-module finger seal
2472014024812709/04/14Turbine engine component with dual purpose rib
2482014024812809/04/14Seals for a circumferential stop ring in a turbine exhaust case
2492014024812909/04/14Lpc flowpath shape with gas turbine engine shaft bearing configuration



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. 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

###

     SHARE