- Farmington CT, US Lajos H. Horvath - Jupiter FL, US Sami Chukrallah - West Palm Beach FL, US Richard D. Konney - Palm City FL, US
International Classification:
F02M 37/22 B67D 7/02
Abstract:
A method is provided for treating a fuel system of a turbine engine. During this method, a treatment system is connected to the turbine engine. Preservation fluid is drawn out of the fuel system using the treatment system.
Hydraulic Starter Assembly For A Gas Turbine Engine
- Farmington CT, US Sami Chukrallah - West Palm Beach FL, US Richard M. Marshall - Loxahatchee FL, US Ryan W. Hunter - North Palm Beach FL, US
International Classification:
F02C 7/27 F02C 7/32
Abstract:
A starter assembly for a gas turbine engine according to an example of the present disclosure includes, among other things, a fluid-actuated starter coupled to a spool, and a controller operable to cause a reduction in torque output of the starter in response to determining that a first threshold is met. The first threshold relates to an engine operational condition. A method for starting a gas turbine engine is also disclosed.
Hydraulic Starter Assembly For A Gas Turbine Engine
- Farmington CT, US Sami Chukrallah - West Palm Beach FL, US Richard M. Marshall - Loxahatchee FL, US Ryan W. Hunter - North Palm Beach FL, US
International Classification:
F02C 7/27 F02C 7/32
Abstract:
A starter assembly for a gas turbine engine according to an example of the present disclosure includes, among other things, a fluid-actuated starter coupled to a spool, and a controller operable to cause a reduction in torque output of the starter in response to determining that a first predefined threshold is met. The first predefined threshold relates to an engine operational condition. A method for starting a gas turbine engine is also disclosed.
- Farmington CT, US Sami Chukrallah - Palm Beach Gardens FL, US James D. Hunter - Lake Panasoffkee FL, US
International Classification:
F02C 9/28 F02C 7/268 F02C 9/26 F02C 7/232
Abstract:
A fuel assembly for a gas turbine engine according to an example of the present disclosure includes, among other things, a fuel valve that meters flow of fluid between a combustor and a fuel supply, and a controller in communication with the fuel assembly. The controller is programmed to receive data corresponding to a present rotational speed of a gas turbine engine component and data corresponding to at least one present flight condition, and is programmed to cause a flow rate from the fuel valve to change in response to determining that a rate of change in an acceleration rate relating to the present rotational speed meets at least one predetermined threshold. At least one predetermined threshold relates to an engine light-off event of the combustor and is based upon the at least one present flight condition.
- Kohler WI, US Jeffrey L. BRACHT - Cascade WI, US Jennifer J. Van Dalen - Howards Grove WI, US William H. SHARP - Petal MS, US Sami M. CHUKRALLAH - Sheboygan WI, US
International Classification:
F02D 9/02
US Classification:
123403
Abstract:
A governor system assembly and related method for assembling the same. The assembly may include a governor gear, a weight, and a locking pin pivotably coupling the weight to the governor gear along a pivot axis. The locking pin includes a locking segment rotatable into engagement with the gear about the pivot axis for securing the pin to the gear. In one assembly, the locking pin is rotatable between an unlocked position in which the locking pin is axially removable from the gear and a locked position in which a locking pin is not axially removable when the locking segment engages the gear. The locking pin may be L-shaped in some assemblies.
Sikorsky Aircraft Dec 2014 - Apr 2017
Propulsion Integration Engineer
Pratt & Whitney Dec 2014 - Apr 2017
Controls and Diagnostic Systems Senior Engineer
Kohler Co. Jun 2013 - Dec 2014
Development Engineer
Kohler Co. Nov 2011 - Jun 2013
Mechanical Project Engineer
Pratt & Whitney Apr 2011 - Nov 2011
Project Engineer
Education:
Drexel University's Lebow College of Business 2016 - 2018
Master of Business Administration, Masters, Management, Entrepreneurship
Rutgers University 2006 - 2010
Bachelor of Engineering, Bachelors, Aerospace Engineering
Drexel University
Skills:
Product Development Testing Mechanical Product Design Test Development Machining Hands on Approach Manufacturing