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Ted Kim

CEO of Insureum

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Edits on 6 Nov, 2022
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CEO of
Smart Block Chain City (SBCC)
Smart Block Chain City (SBCC)
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CEO of
Smart Block Chain City (SBCC)
Smart Block Chain City (SBCC)
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Edits on 11 Aug, 2022
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edited on 11 Aug, 2022
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Company Operating Status
Active
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Dmitrii Iannau
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Twitter
https://twitter.com/fastae
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Dmitrii Iannau
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LinkedIn
http://linkedin.com/in/tedkimzikto
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CEO of
Insureum
Insureum
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Patent primary examiner of
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US Patent 7089728 Single-piece turbine rotor and pinion gear and manufacturing technique for same
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US Patent 7089747 Pressure reduction apparatus and method
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US Patent 7089748 Combustion chamber, in particular of a gas turbine
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US Patent 7093418 Gas turbine engine including a low pressure sump seal buffer source and thermally isolated sump
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US Patent 7093419 Methods and apparatus for operating gas turbine engine combustors
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US Patent 7093421 Spark igniter for gas turbine engine
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US Patent 7093422 Detecting spark in igniter of gas turbine engine by detecting signals in grounded RF shielding
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US Patent 7093424 Thrust reverser system electro-mechanical brake manual release mechanism
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US Patent 7093448 Multi-action on multi-surface seal with turbine scroll retention method in gas turbine engine
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US Patent 7100354 Shut-off system for the avoidance of an overspeed condition in the event of a shaft failure
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US Patent 7104069 Apparatus and method for improving combustion stability
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US Patent 7107756 Turbofan arrangement
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US Patent 7107774 Method and apparatus for combined cycle power plant operation
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US Patent 7111448 Jet nozzle mixer
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US Patent 7111463 Combustion wave ignition for combustors
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US Patent 7114339 Cavity on-board injection for leakage flows
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US Patent 7117680 Cooling scheme for scramjet variable geometry hardware
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US Patent 7121096 Gas turbine engine combustor
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US Patent 7124589 Power cogeneration system and apparatus means for improved high thermal efficiencies and ultra-low emissions
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US Patent 7124591 Method for operating a gas turbine
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US Patent 11175042 Combustion equipment
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US Patent 7137241 Transition duct apparatus having reduced pressure loss
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US Patent 7137244 Reactor for decomposition of ammonium dinitramide-based liquid monopropellants and process for the decomposition
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US Patent 7137245 High area-ratio inter-turbine duct with inlet blowing
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US Patent 7137255 Compact swirl augmented afterburners for gas turbine engines
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US Patent 7137258 Swirler configurations for combustor nozzles and related method
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US Patent 7140186 Method and apparatus for monitoring the performance of a gas turbine system
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US Patent 7143583 Gas turbine combustor, combustion method of the gas turbine combustor, and method of remodeling a gas turbine combustor
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US Patent 7150143 Hybrid fuel cell-pulse detonation power system
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US Patent 7155897 Combustion temperature high speed detection device
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US Patent 7159403 Apparatus for assembling gas turbine engine combustors
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US Patent 7165388 Propulsion device with enclosed plenum
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US Patent 7168236 Compact lightweight ramjet engines incorporating swirl augmented combustion with improved performance
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US Patent 7174703 Ion thrusting system
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US Patent 7174717 Helical channel fuel distributor and method
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US Patent 7178325 Divergent flap for a gas turbine engine
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US Patent 7185496 Synchronizing stationary clutch of compression braking with a two spool gas turbine engine
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US Patent 7185497 Rich quick mix combustion system
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US Patent 7185498 Modular gas turbine
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US Patent 7188466 Passive, high-temperature amplifier for amplifying spark signals detected in igniter in gas turbine engine
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US Patent 7191598 Gas turbine by-pass system
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US Patent 7213392 Rocket engine combustion chamber
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US Patent 7216473 Turbojet engine lubrication system
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US Patent 7216476 Two-axis thrust vectoring nozzle
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US Patent 7225607 Gas turbine braking apparatus and method
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US Patent 7229029 Propulsion system
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US Patent 7231767 Forced air cooling system
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US Patent 7237378 Turbomachine with low noise emissions for aircraft
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US Patent 7237383 Method and device for extracting water in a power plant
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US Patent 7237386 Process for controlling the cooling air mass flow of a gas turbine set
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US Patent 7237389 Attachment system for ceramic combustor liner
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US Patent 7243496 Electric flame control using corona discharge enhancement
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US Patent 7246481 Methods and apparatus for operating gas turbine engines
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US Patent 7246482 Gas turbine engine bleed air power assist system and method
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US Patent 7246483 Energetic detonation propulsion
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US Patent 7246493 Gas turbine
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US Patent 7249463 Aerodynamic fastener shield for turbomachine
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US Patent 7249721 Device and method for injecting a liquid fuel into an air flow for a combustion chamber
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US Patent 7251927 Jet nozzle mixer
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US Patent 7251942 Integrated gearless and nonlubricated auxiliary power unit
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US Patent 7254936 Simple solid propellant rocket engine and super-staged rocket
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US Patent 7254937 Gas turbine heat exchanger assembly and method for fabricating same
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US Patent 7260926 Thermal management system for an aircraft
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US Patent 7263834 Method for cooling a gas turbine system and a gas turbine system for performing this method
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US Patent 7266941 Turbofan case and method of making
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US Patent 7266946 Gas fuel compression by liquification
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US Patent 7269954 Method for operating a gas turbine installation, and gas turbine installation
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US Patent 7269956 Device for utilizing the waste heat of compressors
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US Patent 7269958 Combustor exit duct
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US Patent 7272933 Methods and apparatus for operating gas turbine engines
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US Patent 7275362 Thrust reversers including latching mechanisms and methods for manufacturing such thrust reversers
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US Patent 7278254 Cooling system for a transition bracket of a transition in a turbine engine
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US Patent 7278256 Pulsed combustion engine
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US Patent 7284377 Method and apparatus for operating an intercooler for a gas turbine engine
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US Patent 7287384 Bearing chamber pressurization system
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US Patent 7290394 Fuel injector flexible feed with moveable nozzle tip
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US Patent 7293401 Jet engine noise suppressor
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US Patent 7293402 Injection head for a liquid-propelled rocket engine
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US Patent 7296397 Ventilation system for a convergent divergent exhaust nozzle
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US Patent 7296414 Aircraft engine mounting assembly
‌
US Patent 7299620 Tornado torch igniter
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US Patent 7299621 Three-spool by-pass turbojet with a high by-pass ratio
‌
US Patent 7299634 Combustion chamber
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US Patent 7302792 Pulsed plasma thruster and method of making
‌
US Patent 7302793 Methods and apparatus to reduce turbine engine nozzle basesheet stresses
‌
US Patent 7305816 Rocket augmentation for combined cycle turboaccelerator jet engine
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US Patent 7305832 Work extraction arrangement
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US Patent 7310938 Cooled gas turbine transition duct
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US Patent 7310939 Device for reducing the jet noise of a turbomachine
‌
US Patent 7310950 Inlet airflow cooling control for a power generating system
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US Patent 7313916 Method and apparatus for generating power by combustion of vaporized fuel
‌
US Patent 7316547 Reciprocating compressor driven by a linear motor
‌
US Patent 7320222 Burner, method for operating a burner and gas turbine
‌
US Patent 7328571 Semi-axisymmetric scramjet flowpath with conformal nozzle
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US Patent 7334391 Electric power supply equipment
‌
US Patent 7334394 Localized arc filament plasma actuators for noise mitigation and mixing enhancement
‌
US Patent 7334411 Gas turbine heat exchanger assembly and method for fabricating same
‌
US Patent 7337606 Rotary ramjet engine
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US Patent 7340880 Compressed air bypass valve and gas turbine
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US Patent 7347041 Rocket engine combustion chamber
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US Patent 7350360 Annular combustor for a gas turbine
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US Patent 7353647 Methods and apparatus for assembling gas turbine engines
‌
US Patent 7356994 Alignment and positioning system for installing a fuel injector in a gas turbine engine
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US Patent 7363757 Turbine engine with semi-fixed turbine driving a receiver controlled so as to preserve a roughly constant rotation speed
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US Patent 7363763 Combustor
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US Patent 7367191 Device for fixing a burner ring in an afterburner combustion chamber of a turbojet engine
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US Patent 7370466 Extended flashback annulus in a gas turbine combustor
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US Patent 7370467 Turbofan case and method of making
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US Patent 7370469 Rocket chamber heat exchanger
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US Patent 7370478 Method of controlling a gas combustor of a gas turbine
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US Patent 7373772 Turbine combustor transition piece having dilution holes
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US Patent 7373779 Methods and apparatus for cooling gas turbine engines
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US Patent 7373781 Methods and apparatus for injecting cleaning fluids into combustors
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US Patent 7377099 System and method for cooling lateral edge regions of a divergent seal of an axisymmetric nozzle
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US Patent 7377100 Bypass duct fluid cooler
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US Patent 7383686 Secondary flow, high pressure turbine module cooling air system for recuperated gas turbine engines
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US Patent 7386983 Apparatus for driving an accessory gearbox in a gas turbine engine
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US Patent 7389636 Booster rocket engine using gaseous hydrocarbon in catalytically enhanced gas generator cycle
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US Patent 7389643 Inboard radial dump venturi for combustion chamber of a gas turbine
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US Patent 7392651 Turbomachine nozzle cover for reducing jet noise
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US Patent 7395657 Flade gas turbine engine with fixed geometry inlet
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US Patent 7395669 Gas turbine engine combustor
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US Patent 7399169 Compressor
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US Patent 7404286 Orbiting combustion nozzle engine
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US Patent 7406821 Adapter device for a rocket engine nozzle having a movable diverging portion
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US Patent 7406829 Cryogenic liquid oxidizer cooled high energy system
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US Patent 7409819 Gas turbine engine and method of assembling same
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US Patent 7412833 Method of cooling centerbody of premixing burner
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US Patent 7412834 Annular combustion chamber for a turbomachine with an improved inner fastening flange
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US Patent 7421842 Turbine spring clip seal
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US Patent 7424804 Premix burner
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US Patent 7426833 Gas turbine combustor and fuel supply method for same
‌
US Patent 7426834 “Get home” oil supply and scavenge system
‌
US Patent 7428819 Method for the operation of a compressor of a gas turbine with evaporative cooling of the compressor induction air
‌
US Patent 7430868 Method of operating a thermal power plant
‌
US Patent 7430869 System for catalytic combustion
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US Patent 7434383 Bypass duct boss repair technology
‌
US Patent 7434402 System for actively controlling compressor clearances
‌
US Patent 7434403 Method of operating a thermal power plant
‌
US Patent 7434405 Bleed diffuser for gas turbine engine
‌
US Patent 7441409 Combustor liner v-band design
‌
US Patent 7441410 Gas turbine and manufacturing process of gas turbine
‌
US Patent 7448198 Gas turbine braking apparatus and method
‌
US Patent 7448216 Methods and apparatus for operating gas turbine engine combustors
‌
US Patent 7448218 Premix burner and method for burning a low-calorie combustion gas
‌
US Patent 7451600 Gas turbine engine combustor with improved cooling
‌
US Patent 7454894 Supplemental oil cooler airflow for gas turbine engine
‌
US Patent 7454914 Helical channel for distributor and method
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US Patent 7458201 Propulsion device with enclosed plenum
‌
US Patent 7461502 Spacecraft thruster
‌
US Patent 7464532 Apparatus for elimination of transient pressure spikes on stiff fluid systems
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US Patent 7467519 Electricity and synthesis gas generation method
‌
US Patent 7469528 Aircraft braking method and ducted fan jet engine for implementing the method
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US Patent 7472540 Method and device for compensating variations in fuel composition in a gas turbine system
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US Patent 7472543 Jet engine noise suppressor
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US Patent 7475546 Augmentor pilot nozzle
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US Patent 7478525 System and method for controlling the temperature and infrared signature of an engine
‌
US Patent 7481037 Cooling structure of gas turbine tail pipe
‌
US Patent 7484354 Aircraft engine arrangement
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US Patent 7487630 Jet engine with compact arrangement of fan
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US Patent 7493768 Method for increasing the efficiency of a gas turbine system and gas turbine system suitable therefor
‌
US Patent 7500352 Gas turbine engine
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US Patent 7513098 Swirler assembly and combinations of same in gas turbine engine combustors
‌
US Patent 7513101 Synchronized motor thrust reverser actuation system
‌
US Patent 7513117 Method for operating a furnace
‌
US Patent 7520137 Method of controlling the injection of liquid into an inflow duct of a prime mover or driven machine
‌
US Patent 7523614 Combustor
‌
US Patent 7533534 HPT aerodynamic trip to improve acoustic transmission loss and reduce noise level for auxiliary power unit
‌
US Patent 7540152 Combustor
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US Patent 7540153 Combustor
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US Patent 7540154 Gas turbine combustor
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US Patent 7540155 Thermal shield stone for covering the wall of a combustion chamber, combustion chamber and a gas turbine
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US Patent 7546727 Reduced noise jet engine
‌
US Patent 7546734 Homogenous mixture formation by swirled fuel injection
‌
US Patent 7546739 Igniter tube and method of assembling same
‌
US Patent 7549290 Acoustic damper
‌
US Patent 7552590 Tube-type vortex reducer
‌
US Patent 7562532 Method for operating a gas turbine group
‌
US Patent 7565796 Turbofan case and method of making
‌
US Patent 7568335 Gas turbogroup
‌
US Patent 7571609 Gas turbine combustor and fuel supply method for same
‌
US Patent 7571611 Methods and system for reducing pressure losses in gas turbine engines
‌
US Patent 7571612 Gas turbine combustor and fuel supply method for same
‌
US Patent 7581380 Air-breathing electrostatic ion thruster
‌
US Patent 7581384 Turbomachine nozzle cover provided with triangular patterns having a point of inflexion for reducing jet noise
‌
US Patent 7584600 Gas turbine, in particular aircraft engine and method for generating electrical energy in a gas turbine
‌
US Patent 7584620 Support system for transition ducts
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US Patent 7584621 Radially expanding turbine engine exhaust cylinder interface
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US Patent 7587887 Advanced humid air turbine power plant
‌
US Patent 7591136 Antirotation injection system for turbojet
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US Patent 7594388 Counterrotating turbofan engine
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US Patent 7596939 Gas turbine apparatus
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US Patent 7600370 Fluid flow distributor apparatus for gas turbine engine mid-frame section
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US Patent 7600371 Thrust reversers including support members for inhibiting deflection
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US Patent 7600382 Turbine engine with interstage heat transfer
‌
US Patent 7603841 Vortex combustor for low NOx emissions when burning lean premixed high hydrogen content fuel
‌
US Patent 7617684 Impingement cooled can combustor
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US Patent 7617689 Combustor dome assembly including retaining ring
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US Patent 7621117 Apparatus and method for controlling engine windmilling
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US Patent 7621119 Heat exchange injector for use in a rocket engine
‌
US Patent 7624567 Convergent divergent nozzle with interlocking divergent flaps
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US Patent 7631482 Multiple phase power supply for rocket engines
‌
US Patent 7631504 Methods and apparatus for assembling gas turbine engines
‌
US Patent 7634915 Systems and methods for power generation and hydrogen production with carbon dioxide isolation
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US Patent 7637093 Humid air turbine cycle with carbon dioxide recovery
‌
US Patent 7637111 Easily demountable combustion chamber with improved aerodynamic performance
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US Patent 7644587 Method for providing auxiliary power to an electric power plant using fischer-tropsch technology
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US Patent 7647761 System for deicing the nose cone of an aircraft turbojet with oil
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US Patent 7647779 Compliant metal support for ceramic combustor liner in a gas turbine engine
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US Patent 7654092 System for modulating fuel supply to individual fuel nozzles in a can-annular gas turbine
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US Patent 7658077 System for deicing an aircraft turbine engine inlet cone
‌
US Patent 7665291 Method and system for heat recovery from dirty gaseous fuel in gasification power plants
‌
US Patent 7665292 Thruster with electro-thermal thrust augmentation
‌
US Patent 7669404 Localized arc filament plasma actuators for noise mitigation and mixing enhancement
‌
US Patent 7669425 Closed loop turbine cooling fluid reuse system for a turbine engine
‌
US Patent 7673455 Gas turbine combustor and fuel supply method for same
‌
US Patent 7673461 Structural turbine engine casing
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US Patent 7677026 Mixer for separate-flow nozzle
‌
US Patent 7685827 Gas turbine cooling systems and methods of assembly
‌
US Patent 7698884 Power transmission arrangement
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US Patent 7703274 Pintle injector
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US Patent 7703288 Fuel nozzle having swirler-integrated radial fuel jet
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US Patent 7703289 Internal fuel manifold having temperature reduction feature
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US Patent 7703290 Air thrust bearing for a gas turbine engine
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US Patent 7707836 Venturi cooling system
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US Patent 7712314 Venturi cooling system
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US Patent 7721553 Method and apparatus for detecting a flashback condition in a gas turbine
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US Patent 7726131 Floatwall dilution hole cooling
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US Patent 7726132 Method for increasing the aerodynamic stability of a working fluid flow of a compressor
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US Patent 7726133 Method for operating a burner of a gas turbine and a power plant
‌
US Patent 7739866 Turbofan case and method of making
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US Patent 7739875 Syngas power systems and method for use thereof
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US Patent 7748208 Compact recirculating lubrication system for a miniature gas turbine engine
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US Patent 7757476 Catalytically activated transient decomposition propulsion system
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US Patent 7757494 Device for feeding fuel to a combustion chamber in a turbomachine
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US Patent 7765787 Turbofan case and method of making
‌
US Patent 7770377 Turbofan arrangement
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US Patent 7770378 Turbofan case and method of making
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US Patent 7770395 Combustor
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US Patent 7779636 Lean direct injection atomizer for gas turbine engines
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US Patent 7784261 Combined cycle power plant
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US Patent 7784264 Slidable spring-loaded transition-to-turbine seal apparatus and heat-shielding system, comprising the seal, at transition/turbine junction of a gas turbine engine
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US Patent 7784268 Partial superheat cycle for operating a pump in a rocket system
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US Patent 7784270 Rotary motion mixer for a converging-stream nozzle of a turbomachine
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US Patent 7788897 Low emissions combustion apparatus and method
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US Patent 7788898 Variable coupling of turbofan engine spools via open differential gear set or simple planetary gear set for improved power extraction and engine operability, with torque coupling for added flexibility
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US Patent 7793488 Turbofan case and method of making
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US Patent 7797921 Control apparatus of extracted air booster system of integrated gasification combined cycle power plant
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US Patent 7797922 Gas turbine engine case and method of making
‌
US Patent 7802431 Combustor liner with reverse flow for gas turbine engine
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US Patent 7805947 Aircraft with disengageable engine and auxiliary power unit components
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US Patent 7805949 Device for supporting and housing auxiliaries in a bypass turbojet
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US Patent 7810309 Fuel system utilizing dual mixing pump
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US Patent 7823374 Heat transfer system and method for turbine engine using heat pipes
‌
US Patent 7827803 Method and apparatus for an aerodynamic stability management system
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US Patent 7828243 SCRAMjet arrangement for hypersonic aircraft
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US Patent 7841165 Gas turbine engine assembly and methods of assembling same
‌
US Patent 7841183 Method and apparatus for delivering a liquid
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US Patent 7841187 Turbomachine comprising a system for cooling the downstream face of an impeller of a centrifugal compressor
‌
US Patent 7845156 Turbofan exhaust system
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US Patent 7854126 Annular combustion chamber with a removable end wall
‌
US Patent 7856827 Structural track support of spraybars/tubing
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US Patent 7856830 Noise reducing combustor
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US Patent 7861512 Turbofan bypass duct air cooled fluid cooler installation
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US Patent 7866141 Cooling device for the primary nozzle of a dual-flow turbojet engine
‌
US Patent 7870717 Advanced hydrogen auxiliary power unit
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US Patent 7874162 Supercritical steam combined cycle and method
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US Patent 7882693 Turbofan engine assembly and method of assembling same
‌
US Patent 7886517 Impingement jets coupled to cooling channels for transition cooling
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US Patent 7886518 Turbofan engine cowl assembly and method of operating the same
‌
US Patent 7891166 Water rocket engine with a two-phase nozzle
‌
US Patent 7891193 Cooling of a multimode fuel injector for combustion chambers, in particular of a jet engine
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US Patent 7900433 Fan exhaust nozzle for turbofan engine
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US Patent 7905083 Turbofan engine assembly and method of assembling same
‌
US Patent 7908865 Device for injecting a mixture of air and fuel, and combustion chamber and turbomachine provided with such a device
‌
US Patent 7908868 Device for mounting an air-flow dividing wall in a turbojet engine afterburner
‌
US Patent 7908869 Thermal and external load isolating impeller shroud
‌
US Patent 7913495 Gas turbine and manufacturing process of gas turbine
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US Patent 7921634 Turbofan engine assembly and method of assembling same
‌
US Patent 7921653 Internal manifold air extraction system for IGCC combustor and method
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US Patent 7926259 Turbofan engine assembly and method of assembling same
‌
US Patent 7926286 Heat shield for a fuel manifold
‌
US Patent 7937947 Gas turbine and manufacturing process of gas turbine
‌
US Patent 7946104 Bleed air relief system for engines
‌
US Patent 7950239 Method for operating a gas turbine plant
‌
US Patent 7954324 Gas turbine engine
‌
US Patent 7963094 Fragmentor for bird ingestible gas turbine engine
‌
US Patent 7963100 Cooling system for high-speed vehicles and method of cooling high-speed vehicles
‌
US Patent 7966806 Turbofan engine assembly and method of assembling same
‌
US Patent 7966809 Single-piece hybrid rocket motor
‌
US Patent 7966832 Combustor
‌
US Patent 7971423 Gas turbine engine comprising a starter in the auxiliary gear box
‌
US Patent 7971439 Annular turbomachine combustion chamber
‌
US Patent 7980058 Air compression type engine for aviation
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US Patent 7997061 Turbojet engine for aircraft, propulsion unit comprising such a turbojet engine and aircraft comprising such a propulsion unit
‌
US Patent 8001790 Gas turbine
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US Patent 8001793 Gas turbine engine reverse-flow combustor
‌
US Patent 8006500 Swirl combustor with counter swirl fuel slinger
Edits on 8 Dec, 2021
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edited on 8 Dec, 2021
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Patent primary examiner of
‌
US Patent 8006500 Swirl combustor with counter swirl fuel slinger
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Golden AI
edited on 8 Dec, 2021
Edits made to:
Infobox (+1 properties)
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Patent primary examiner of
‌
US Patent 8001793 Gas turbine engine reverse-flow combustor
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Golden AI
edited on 8 Dec, 2021
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Infobox (+1 properties)
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Patent primary examiner of
‌
US Patent 8001790 Gas turbine
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Golden AI
edited on 8 Dec, 2021
Edits on 8 Dec, 2021
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Golden AI
edited on 8 Dec, 2021
Edits made to:
Infobox (+1 properties)
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Patent primary examiner of
‌
US Patent 7980058 Air compression type engine for aviation
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Golden AI
edited on 8 Dec, 2021
Edits made to:
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Patent primary examiner of
‌
US Patent 7971439 Annular turbomachine combustion chamber
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Golden AI
edited on 8 Dec, 2021
Edits made to:
Infobox (+1 properties)
Infobox
Patent primary examiner of
‌
US Patent 7971423 Gas turbine engine comprising a starter in the auxiliary gear box
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Golden AI
edited on 8 Dec, 2021
Edits made to:
Infobox (+1 properties)
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Patent primary examiner of
‌
US Patent 7966832 Combustor
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Golden AI
edited on 8 Dec, 2021
Edits made to:
Infobox (+1 properties)
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Patent primary examiner of
‌
US Patent 7966809 Single-piece hybrid rocket motor
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Golden AI
edited on 8 Dec, 2021
Edits made to:
Infobox (+1 properties)
Infobox
Patent primary examiner of
‌
US Patent 7966806 Turbofan engine assembly and method of assembling same
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Golden AI
edited on 8 Dec, 2021
Edits made to:
Infobox (+1 properties)
Infobox
Patent primary examiner of
‌
US Patent 7963100 Cooling system for high-speed vehicles and method of cooling high-speed vehicles
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Golden AI
edited on 8 Dec, 2021
Edits made to:
Infobox (+1 properties)
Infobox
Patent primary examiner of
‌
US Patent 7963094 Fragmentor for bird ingestible gas turbine engine
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Golden AI
edited on 7 Dec, 2021
Edits made to:
Infobox (+1 properties)
Infobox
Patent primary examiner of
‌
US Patent 7954324 Gas turbine engine

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