Um, Jae Y

USPTO Trademark & Patent Filings

Trademark applications and grants for Um, Jae Y. Um, Jae Y has 1 trademark applications. The latest application filed is for "GLASS TWO"

Company Profile

Um, Jae Y
y jae um
Um; Jae Y. - Winter Garden FL

State Incorporated	CALIFORNIA
Entity Type	LIMITED LIABILITY COMPANY
Address	1100 s San Pedro Glass Two Los Angeles, CALIFORNIA UNITED STATES 90015

*profile and listings may contain filings by different individuals or companies with the same name. Review application materials to confirm ownership/assignment.
Trademarks Patents

Patent Applications

Patent Application	Date
TURBINE AIRFOIL WITH TRAILING EDGE FEATURES AND CASTING CORE 20210140321 - 16/623824 Lee; Ching-Pang ; et al.	2021-05-13
TURBINE ROTOR AIRFOIL AND CORRESPONDING METHOD FOR REDUCING PRESSURE LOSS IN A CAVITY WITHIN A BLADE 20210025278 - 16/640806 Lee; Ching-Pang ; et al.	2021-01-28
TURBINE BLADE WITH AXIAL TIP COOLING CIRCUIT 20180298763 - 15/525820 Lee; Ching-Pang ; et al.	2018-10-18
INTERNAL COOLING SYSTEM WITH INSERT FORMING NEARWALL COOLING CHANNELS IN AN AFT COOLING CAVITY OF A GAS TURBINE AIRFOIL INCLUDING HEAT DISSIPATING RIBS 20180045059 - 15/504407 Lee; Ching-Pang ; et al.	2018-02-15
GAS TURBINE AIRFOIL INCLUDING INTEGRATED LEADING EDGE AND TIP COOLING FLUID PASSAGE AND CORE STRUCTURE USED FOR FORMING SUCH AN AIRFOIL 20170275998 - 15/508497 Lee; Ching-Pang ; et al.	2017-09-28
Turbine airfoil with trailing edge features and casting core 11,415,000 - 16/623,824 Lee , et al. August 16, 2	2022-08-16
Turbine rotor airfoil and corresponding method for reducing pressure loss in a cavity within a blade 11,111,795 - 16/640,806 Lee , et al. September 7, 2	2021-09-07
Gas turbine airfoil including integrated leading edge and tip cooling fluid passage and core structure used for forming such an airfoil 10,697,306 - 15/508,497 Lee , et al.	2020-06-30
Shroud cooling system for shrouds adjacent to airfoils within gas turbine engines 9,963,996 - 15/327,466 Eng , et al. May 8, 2	2018-05-08
Internal cooling system with insert forming nearwall cooling channels in an aft cooling cavity of an airfoil usable in a gas turbine engine 9,863,256 - 15/505,218 Lee , et al. January 9, 2	2018-01-09

Patent Grants & Applications

Trademark Applications

Mark Image Registration \| Serial	Trademark Application Date
"GLASS TWO" 90316105	GLASS TWO 2020-11-12

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