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Inventor profile of:

Hany Rizkalla

City:

Stuart, Florida

Country:

United States

Published Applications:

31

Last publication date:

2025-02-06

Top Assignees for applications by Hany Rizkalla

The entities that hold a legal rights for patent applications filed by inventor Rizkalla Hany:

Recent patent applications by Rizkalla Hany

Hany Rizkalla from Stuart, US has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2025-02-06
US20250043735A1
Mechanical engineering

EXHAUST COOLING INJECTION FOR IMPROVED TURNDOWN

 #2 | 2023-12-21
US20230408097A1
Mechanical engineering

MULTITUBE PILOT INJECTOR HAVING A FLAME ANCHOR FOR A GAS TUBINE ENGINE

 #3 | 2023-12-21
US20230408096A1
Mechanical engineering

MULTITUBE PILOT INJECTION INTO TRAPPED VORTICES IN A GAS TURBINE ENGINE

 #4 | 2023-12-21
US20230408095A1
Mechanical engineering

MULTITUBE PILOT INJECTOR HAVING AN INSULATED MANIFOLD FOR A GAS TURBINE COMBUSTOR

 #5 | 2023-12-21
US20230408094A1
Mechanical engineering

Trailing edge fuel injection enhancement for flame holding mitigation

 #6 | 2023-05-04
US20230135396A1
Mechanical engineering

Multitube pilot injector having a split airflow for a gas turbine engine

 #7 | 2016-03-24
US20160084169A1
Mechanical engineering

Method of operating a multi-stage flamesheet combustor

 #8 | 2015-09-24
US20150267620A1
Mechanical engineering

Dynamic and automatic tuning of a gas turbine engine using exhaust temperature and inlet guide vane angle

 #9 | 2015-07-02
US20150184858A1
Mechanical engineering

METHOD OF OPERATING A MULTI-STAGE FLAMESHEET COMBUSTOR

 #10 | 2015-07-02
US20150184856A1
Mechanical engineering

Thermally free liner retention mechanism

 #11 | 2015-03-19
US20150075172A1
Mechanical engineering

Flamesheet combustor contoured liner

 #12 | 2014-09-18
US20140277790A1
Physics

Ensuring non-excessive variation of gradients in auto-tuning a gas turbine engine

 #13 | 2014-09-18
US20140277789A1
Physics

Dynamic tuning of a gas turbine engine to detect and prevent lean blowout

 #14 | 2014-07-17
US20140200721A1
Physics

Stabilizing a gas turbine engine via incremental tuning during transients

 #15 | 2014-07-17
US20140196461A1
Mechanical engineering

Detecting flashback by monitoring engine-dynamic spikes

 #16 | 2014-04-03
US20140090396A1
Mechanical engineering

COMBUSTOR WITH RADIALLY STAGED PREMIXED PILOT FOR IMPROVED

 #17 | 2014-04-03
US20140090390A1
Mechanical engineering

Flamesheet combustor dome

 #18 | 2014-04-03
US20140090389A1
Mechanical engineering

Variable length combustor dome extension for improved operability

 #19 | 2013-10-03
US20130255276A1
Mechanical engineering

Transition Duct Mounting System

 #20 | 2011-11-03
US20110270502A1
Mechanical engineering

Employing fuel properties to auto-tune a gas turbine engine

 #21 | 2011-11-03
US20110265487A1
Mechanical engineering

Dynamically auto-tuning a gas turbine engine

 #22 | 2010-12-02
US20100300108A1
Mechanical engineering

Stabilizing a gas turbine engine via incremental tuning

 #23 | 2009-07-30
US20090188258A1
Mechanical engineering

Altering a natural frequency of a gas turbine transition duct

 #24 | 2009-07-30
US20090188255A1
Mechanical engineering

Combustor end cap assembly

 #25 | 2009-06-11
US20090145983A1
Mechanical engineering

Gas turbine fuel nozzle having improved thermal capability

 #26 | 2009-06-11
US20090145137A1
Mechanical engineering

Transition duct assembly

 #27 | 2005-12-01
US20050262844A1
Mechanical engineering

Combustion liner seal with heat transfer augmentation

 #28 | 2005-08-30
US10424350
-

Flamesheet combustor

 #29 | 2005-07-12
US10465096
-

Dual fuel fin mixer secondary fuel nozzle

 #30 | 2005-05-31
US10452449
-

Gas only fin mixer secondary fuel nozzle

 #31 | 2005-02-24
US20050039460A1
Mechanical engineering

Gas turbine fuel pilot nozzle
InventorID:

460795 ⎘