Gao; Zhihong

Patent Applications and Registrations

Patent applications and USPTO patent grants for Gao; Zhihong.The latest application filed is for "turbine abradable layer with compound angle, asymmetric surface area ridge and groove pattern".

Company Profile

0.13.10

Gao; Zhihong - Orlando FL
Gao; Zhihong - Shenzhen CN
Gao; Zhihong - Taipei TW
Gao; Zhihong - Taiwan CN

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

Patent Activity

Patent	Date
Turbine abradable layer with compound angle, asymmetric surface area ridge and groove pattern Grant 9,920,646 - Lee , et al. March 20, 2	2018-03-20
Turbine Abradable Layer With Compound Angle, Asymmetric Surface Area Ridge And Groove Pattern App 20170218787 - Lee; Ching-Pang ; et al.	2017-08-03
Turbine abradable layer with asymmetric ridges or grooves Grant 9,249,680 - Lee , et al. February 2, 2	2016-02-02
Turbine Abradable Layer With Asymmetric Ridges Or Grooves App 20150240652 - Lee; Ching-Pang ; et al.	2015-08-27
Method, device, and system for packet transmission on PCIE bus Grant 9,117,033 - Gao , et al. August 25, 2	2015-08-25
Turbine abradable layer with progressive wear zone having a frangible or pixelated nib surface Grant 8,939,706 - Lee , et al. January 27, 2	2015-01-27
Turbine abradable layer with progressive wear zone terraced ridges Grant 8,939,707 - Lee , et al. January 27, 2	2015-01-27
Turbine vane for a gas turbine engine having serpentine cooling channels with internal flow blockers Grant 8,511,968 - Liang , et al. August 20, 2	2013-08-20
Method, Device, and System for Packet Transmission on PCIE Bus App 20130103866 - Gao; Zhihong ; et al.	2013-04-25
Turbine Endwall With Grooved Recess Cavity App 20130064680 - LIANG; GEORGE ; et al.	2013-03-14
Turbine airfoil cooling system with high density section of endwall cooling channels Grant 8,388,304 - Liang , et al. March 5, 2	2013-03-05
Turbine endwall with grooved recess cavity Grant 8,376,705 - Liang , et al. February 19, 2	2013-02-19
Turbine vane for a gas turbine engine having serpentine cooling channels Grant 8,328,518 - Liang , et al. December 11, 2	2012-12-11
Turbine Airfoil Cooling System With High Density Section Of Endwall Cooling Channels App 20120282107 - Liang; George ; et al.	2012-11-08
Inner Shroud Cooling Arrangement In A Gas Turbine Engine App 20120177479 - Azad; Gm Salam ; et al.	2012-07-12
Adjustable water valve of time-controlled type Grant 7,975,980 - Gao , et al. July 12, 2	2011-07-12
Turbine Vane for a Gas Turbine Engine Having Serpentine Cooling Channels with Internal Flow Blockers App 20110038735 - Liang; George ; et al.	2011-02-17
Turbine Vane for a Gas Turbine Engine Having Serpentine Cooling Channels App 20110038709 - Liang; George ; et al.	2011-02-17
Adjustable Water Valve Of Time-controlled Type App 20090242819 - Gao; Youyue ; et al.	2009-10-01

uspto.report is an independent third-party trademark research tool that is not affiliated, endorsed, or sponsored by the United States Patent and Trademark Office (USPTO) or any other governmental organization. The information provided by uspto.report is based on publicly available data at the time of writing and is intended for informational purposes only.

While we strive to provide accurate and up-to-date information, we do not guarantee the accuracy, completeness, reliability, or suitability of the information displayed on this site. The use of this site is at your own risk. Any reliance you place on such information is therefore strictly at your own risk.

All official trademark data, including owner information, should be verified by visiting the official USPTO website at www.uspto.gov. This site is not intended to replace professional legal advice and should not be used as a substitute for consulting with a legal professional who is knowledgeable about trademark law.