Jinzhang Feng

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Avon, CT, US

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Patents Grantslast 30 patents

Information Patent Grant
Gas turbine engine inlet with noise reduction features
- Patent number 8,286,654
- Issue date Oct 16, 2012
- United Technologies Corporation
- Dilip Prasad
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Gas turbine engine inlet with noise reduction features
- Patent number 7,739,865
- Issue date Jun 22, 2010
- United Technologies Corporation
- Dilip Prasad
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Patents Applicationslast 30 patents

Information Patent Application
GAS TURBINE ENGINE INLET WITH NOISE REDUCTION FEATURES
- Publication number 20100215479
- Publication date Aug 26, 2010
- Dilip Prasad
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Gas turbine engine inlet with noise reduction features
- Publication number 20070163229
- Publication date Jul 19, 2007
- United Technologies Corporation
- Dilip Prasad
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Augmentor liner
- Publication number 20060137352
- Publication date Jun 29, 2006
- United Technologies Corporation
- Dilip Prasad
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
Gas turbine engine inlet with noise reduction features
- Publication number 20050274103
- Publication date Dec 15, 2005
- United Technologies Corporation
- Dilip Prasad
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS